CN102275631A - Jet propulsion device - Google Patents

Jet propulsion device Download PDF

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Publication number
CN102275631A
CN102275631A CN2010101957322A CN201010195732A CN102275631A CN 102275631 A CN102275631 A CN 102275631A CN 2010101957322 A CN2010101957322 A CN 2010101957322A CN 201010195732 A CN201010195732 A CN 201010195732A CN 102275631 A CN102275631 A CN 102275631A
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CN
China
Prior art keywords
jet
fluid
propulsion plant
vortex
cylinder
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CN2010101957322A
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Chinese (zh)
Inventor
王舜清
吕銮昌
王化婷
王化舆
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Zhidian Science & Technology Co Ltd
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Zhidian Science & Technology Co Ltd
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Priority to CN2010101957322A priority Critical patent/CN102275631A/en
Publication of CN102275631A publication Critical patent/CN102275631A/en
Pending legal-status Critical Current

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Abstract

The invention provides a jet propulsion device which is provided with a pressure pump, wherein as pressure in a pipe is greater than pressure outside the pipe, the gas is sprayed outside in a jet flow manner so as to generate counteractive thrust or for aeration. Through the invention, a power system of a propeller is kept above the waterline so as to reduce the requirement for water tightness, reduce the fault rate and lower the high cost resulting from the requirement for the sealing height. Meanwhile, as a roller with a spiral lug inside is used for replacing a propeller blade, environmental protection and safety effects can be achieved without hurting human bodies, submarines or rocks.

Description

Jet-propulsion plant
Technical field
The invention provides a kind of jet-propulsion plant, this jet-propulsion plant forms a force lift, and greater than the outer pressure of pipe, gas outwards sprays in the mode of jet flow by the force value in managing, and produces reaction thrust, or is used for the usefulness of inflation.Simultaneously, technology of the present invention remains on the waterline angle of rake power system, to reduce the requirement of watertight, reduces rate of breakdown, and reduce because of the leak free requirement for height produce expensive.And the cylinder that has spiralled fins with inside replaces propeller blade, can reach the environmental protection and the safe effect that do not injure human body, epibiota or reef.
Background technology
The prior art that applicant of the present invention applied for, the jet fluid propelling unit (US Patent number US7497657B2) that is TaiWan, China patent of invention I296599 number has been introduced a kind of spiral or straight line water conservancy diversion lug or diversion groove by inside pipe wall, to increase the friction of fluid, make and be the pory fluid that scatters originally, when being subjected to pressurization/rotation/extruding, can twisting together into the boundling shape, and form the pipe internal pressure, this boundling shape fluid can produce propulsive force, makes carrier be advanced.
Because most angle of rake power system all is underwater, therefore, makes angle of rake power system behind et out of order, keep in repair and be difficult for often because the watertight technology is bad.The technology of the present invention remains on the waterline angle of rake power system, to reduce the requirement of watertight, reduces rate of breakdown, and reduce because of the leak free requirement for height produce expensive.
Summary of the invention
It all is underwater that the present invention will solve most angle of rake power system exactly, therefore often because the watertight technology is bad, makes angle of rake power system keep in repair the technical matters that is difficult for behind et out of order.
The present invention solves above-mentioned technical matters by the following technical programs.
The invention provides a kind of plug-in vertical jet-propulsion plant, comprise:
One carrier;
One engine installation has motor and power supply device;
One jet-propulsion plant, this jet-propulsion plant stands on the water surface, and its front end is provided with admission port, its tail end is connected with connection tube towards water surface part, in order to the linking jet apparatus, and this jet-propulsion plant is to be used for to jet apparatus ejection gas, to produce reaction thrust;
One carrier and power connecting device are in order to connect this carrier and this jet-propulsion plant.
Above-mentioned plug-in vertical jet-propulsion plant, wherein this jet-propulsion plant comprises:
One fluid boundling vortex standpipe device, this fluid boundling vortex standpipe jet apparatus has front wide and rear narrow hollow tube cylinder, and its inwall is connected with the spiral stream guidance lug;
One jet apparatus, this jet apparatus is connected with aforesaid fluid boundling vortex standpipe device by a connection tube, and Xiang Shuizhong ejection gas, to produce reaction thrust.
Above-mentioned plug-in vertical jet-propulsion plant, wherein this fluid boundling vortex standpipe device further comprises:
One engine installation~transmission shaft, one fixed support, all flow device, one fluid pressurization guide vane means, make the preceding of cylinder can form a fluid pressor areas, this the pressurization after fluid can allow cut stream device cut stream easily, one water conservancy diversion bending is located at the forward edge of pressurized with fluid guide vane means, be used for side and cut stream to reduce the generation of crosswind or flow-disturbing, also allow down the easier gathering of hydraulic fluid pressurize, all stream device projectioies are at the leading edge place of cylinder, in the pressure fluid importing cylinder with drum front end, one fluid inlet, one vortex standpipe, one cylinder transmission shaft, one Hooke's coupling.
Above-mentioned plug-in vertical jet-propulsion plant, wherein this jet apparatus comprises:
One front and back jet control device, its upper end is connected with latching connector or with aforementioned jet pipe, has the flow jeting port of advancing, reach a reversing flow jeting port, be used for controlling fluid or the motion of jet flow backward forward, make carrier be able to smoothly to moving ahead or retreating backward, a latching connector, be used for connecting the jet pipe of front end and interconnect with the front and back jet control device of lower end, be convenient to assemble tail end, a fan jet plate that maintenance update jet apparatus, a jet pipe, a connection tube, a jet flow outlet device are positioned at jet apparatus, in order to enlarge the area of thrust.
Above-mentioned plug-in vertical jet-propulsion plant further comprises:
One control direction device, direction of passage control stalk and control such as reversing control stalk etc. are advanced, are retreated or travel direction such as turning in order to the operation carrier; One device safe in utilization, this device safe in utilization have a plunger and are connected with aforementioned jet-propulsion plant, in case when plunger was not connected with this jet-propulsion plant, the engine installation of this jet-propulsion plant will shut down automatically.
The invention provides a kind of fixed type jet-propulsion plant, comprise:
One carrier;
One engine installation has motor and power supply device;
One jet-propulsion plant, this jet-propulsion plant stands on the water surface, and its front end is provided with admission port, its tail end is connected with connection tube towards water surface part, in order to the linking jet apparatus, and this jet-propulsion plant is used for to jet apparatus ejection gas, to produce reaction thrust.
Above-mentioned fixed type jet-propulsion plant, wherein this jet-propulsion plant comprises:
One fluid boundling vortex standpipe device, this fluid boundling vortex standpipe jet apparatus has front wide and rear narrow hollow tube cylinder, and its inwall then is connected with the spiral stream guidance lug;
One jet apparatus, this jet apparatus is connected with aforesaid fluid boundling vortex standpipe device by a connection tube, and Xiang Shuizhong ejection gas, to produce reaction thrust.
Above-mentioned fixed type jet-propulsion plant, wherein this fluid boundling vortex standpipe device further comprises:
One engine installation~transmission shaft, one fixed support, all flow device, one fluid pressurization guide vane means, make the preceding of cylinder can form a fluid pressor areas, this the pressurization after fluid can allow cut stream device cut stream easily, one water conservancy diversion bending is located at the forward edge of pressurized with fluid guide vane means, be used for side and cut stream to reduce the generation of crosswind flow-disturbing, allow simultaneously and press down the fluid collection pressurization, all stream device projectioies are at the leading edge place of cylinder, in the pressure fluid importing cylinder with drum front end, one fluid inlet, one vortex standpipe, one cylinder transmission shaft, one Hooke's coupling.
Above-mentioned fixed type jet-propulsion plant, wherein this jet apparatus comprises:
One front and back jet control device, its upper end is connected with latching connector or with aforementioned jet pipe, has the flow jeting port of advancing, reach a reversing flow jeting port, be used for controlling fluid or the motion of jet flow backward forward, make carrier be able to smoothly to moving ahead or retreating backward, a latching connector, be used for connecting the jet pipe of front end and interconnect with the front and back jet control device of lower end, be convenient to assemble tail end, a fan jet plate that maintenance update jet apparatus, a jet pipe, a connection tube, a jet flow outlet device are positioned at jet apparatus, in order to enlarge the area of thrust.
Above-mentioned fixed type jet-propulsion plant further comprises:
One control direction device, direction of passage control stalk and control such as reversing control stalk etc., advancing, retreating or travel direction such as turning in order to the operation carrier; One device safe in utilization, this device safe in utilization have a plunger and are connected with aforementioned jet-propulsion plant, in case when plunger was not connected with this jet-propulsion plant, the engine installation of this jet-propulsion plant will shut down automatically.
The invention provides a kind of jet-propulsion plant, comprise:
One engine installation has motor and power supply device;
One fluid boundling vortex standpipe device, this fluid boundling vortex standpipe jet apparatus has front wide and rear narrow hollow tube cylinder, and its inwall is connected with the spiral stream guidance lug;
One jet apparatus, this jet apparatus is connected with aforesaid fluid boundling vortex standpipe device by a connection tube, and Xiang Shuizhong ejection gas, to produce reaction thrust.
Above-mentioned jet-propulsion plant, wherein this fluid boundling vortex standpipe device further comprises:
One engine installation~transmission shaft, one fixed support, all flow device, one fluid pressurization guide vane means, make the preceding of cylinder can form a fluid pressor areas, this the pressurization after fluid can allow cut stream device cut stream easily, one water conservancy diversion bending is located at the forward edge of pressurized with fluid guide vane means, be used for side and cut stream to reduce the generation of crosswind flow-disturbing, also allow and press down the fluid collection pressurization, all stream device projectioies are at the leading edge place of cylinder, in the pressure fluid importing cylinder with drum front end, one fluid inlet, one vortex standpipe, one cylinder transmission shaft, one Hooke's coupling.
Above-mentioned jet-propulsion plant, wherein this jet apparatus comprises:
One front and back jet control device, its upper end is connected with latching connector or with aforementioned jet pipe, has the flow jeting port of advancing, reach a reversing flow jeting port, be used for controlling fluid or the motion of jet flow backward forward, make carrier be able to smoothly to moving ahead or retreating backward, a latching connector, be used for connecting the jet pipe of front end and interconnect with the front and back jet control device of lower end, be convenient to assemble tail end, a fan jet plate that maintenance update jet apparatus, a jet pipe, a connection tube, a jet flow outlet device are positioned at jet apparatus, in order to enlarge the area of thrust.
Above-mentioned jet-propulsion plant further comprises:
One control direction device, the control of direction of passage control stalk and reversing control stalk etc., advancing, retreating or travel direction such as turning in order to the operation carrier; One device safe in utilization, this device safe in utilization have a plunger and are connected with aforementioned jet-propulsion plant, in case when plunger was not connected with this jet-propulsion plant, the engine installation of this jet-propulsion plant will shut down automatically.
Above-mentioned each technical scheme of the present invention can realize following technique effect:
One) allow jet-propulsion plant of the present invention become a force lift, greater than the outer pressure of pipe, gas can outwards spray in the mode of jet flow by the force value in managing, and produces reaction thrust, or is used for the usefulness of inflation.
Two) angle of rake power system is remained on the waterline,, reduces rate of breakdown to reduce the requirement of watertight, and reduce because of the leak free requirement for height produce expensive.
Three) cylinder that has a spiralled fins with inside replaces propeller blade, can reach the environmental protection and the safe effect that do not injure human body, epibiota or reef.
Description of drawings
Fig. 1 has shown plug-in vertical jet-propulsion plant of the present invention and carrier waterborne.
Fig. 2 has shown fluid boundling vortex standpipe device of the present invention.
Fig. 3 has shown plug-in vertical jet-propulsion plant of the present invention.
Fig. 4 has shown front and back of the present invention jet control device.
Fig. 5 has shown jet flow outlet device of the present invention.
Fig. 6 has shown fixed type jet-propulsion plant of the present invention.
[primary clustering nomenclature]
Plug-in vertical jet-propulsion plant of 100---and carrier waterborne
110---inflatable carrier device
The 120---rudder
125---hydrofoil plate
130---direction control stalk
132---controls direction device
The 134---speed controller
The 136---control stalk of moveing backward
The 138---pulley
The 140---control line
150---device safe in utilization
The 152---safety control
154---safety stick placing device
The 156---wrist ring
The 158---connecting band
160---safety plunger seat
The 162---plunger
170---carrier adaptation arrangement
The 172---supporting plate
174---carrier and power connecting device
The 176---connecting device that swings
178---U type draw-in groove plate
180---lifts connecting device up and down
182---trip bar
The 184---device that is locked
The 186---rotating plate
The 188---screw
The 190---chuck
The 200---jet-propulsion plant
The jet fluid bundled device of 210---drum-type
215---engine installation~transmission shaft
The 216---filter screen
The 217---dividing plate
The 218---shell
The 220---cylinder
222---spiral stream guidance lug
The 225---fixed support
The 226---bearing
The 228---direction of flow
The 230---fluid intake
232---pressurized with fluid guide vane means
233---water conservancy diversion bending
234---pressurized with fluid district
235---cuts the stream device
The 236---rotation direction
240---cylinder transmission shaft
The 245---hollow tube
246---vortex standpipe
248---fluid volume clustered column body (eddy water notes)
250---produces spiral boundling fluid thrust
265---fluid boundling vortex standpipe device
270---connection tube device
The 272---connection tube
280---specific function ejecting device
The plug-in vertical jet-propulsion plant of 300---
The 305---carrier
The 310---engine installation
The 315---controller
The 320---actuator
The 325---motor
The 330---Hooke's coupling
335---water shutoff bearing
The 340---battery module
The 345---electric wire
The 350---charger
The 355---plug
Jet control device before and after the 400---
The 405---jet apparatus
The 415---latching connector
The 420---jet pipe
The 422---flow jeting port
The 425---flow jeting port that advances
The 430---flow jeting port of moveing backward
435---jet flow rotating disk
440---main spring device
The 445---forward streams to
The 450---flow direction of moveing backward
500---jet flow outlet device
510---fan jet plate
The 515---flow deflector
The 520---reaction thrust
605---fixed type jet-propulsion plant
The 610---driver
The mini Wave Race car body of 620---
The two buoyancy aids of 622---
Buoyancy aid in the middle of the 624---
The 625---storage box
The 630---seat cushion
The 635---back cushion
The 640---protection pad
645---direction control handle
The 650---handgrip
The 655---latch closure
The 660---adjustable foot controls
665---adjustable foot controls seat
The 670---deflecting plate
The 675---flow guide bar
The specific embodiment
Please refer to Fig. 1, for showing plug-in vertical jet-propulsion plant of the present invention and carrier waterborne.In this embodiment, plug-in vertical jet-propulsion plant of the present invention and carrier waterborne 100 comprise the direction control stalk 130 of the direct of travel of an inflatable carrier device 110, may command inflatable carrier device 110, plug-in vertical jet-propulsion plant 300 at least.
The carrier waterborne of indication in the present invention also is applicable to the carrier 305 of other on-inflatable formula.
In this embodiment, inflatable carrier device 110 of the present invention is to produce thrust by a plug-in vertical jet-propulsion plant 300 (please refer to Fig. 3), the present invention uses electro-motor 325, if but carrier waterborne 305 is when needing bigger power, also can use internal combustion engine, turbine engine of various different styles etc. instead, with the kinetic energy in the realistic use, thrust requirement.
In this embodiment, fluid boundling vortex standpipe device 265 (please refer to Fig. 2), its power resources are engine installation 310 of the present invention (please refer to Fig. 3), adopt front wide and rear narrow hollow tube cylinder design, and install fluid pressurization guide vane means 232 additional at the front end place of cylinder 220, allow the preceding of cylinder 220 can form a fluid pressor areas 234, the fluid after this pressurization can allow cuts the stream device 235 easier streams of cutting; There is cutting of a projection to flow device 235 at the leading edge place of cylinder 220, Ben Qie stream device 235 can be with the pressure fluid of cylinder 220 front ends, along the rotation direction of cylinder 220 with pressure fluid with rotate, dig spoon, strong mode of irritating etc. imports pressure fluid in the cylinder 220; At least one spiral stream guidance lug 222 is arranged in cylinder 220.When cylinder 220 is rolling, will utilize the spacing of cutting stream and decreasing worm-pitch of the spiral stream guidance lug 222 in the cylinder 220 can produce a pressure fluid (air or water) mode of motion, add the front wide and rear narrow design of cylinder 220, cylinder 220 is after continuous and continuous rotation, spiral stream guidance lug 222 in cylinder 220 can overturn the fluid in the tube, when cutting stream, also can produce pressure fluid simultaneously constantly by the extruding of the generation behind forward direction phenomenon, so hollow tube 245 places (centre and tail end) in cylinder 220 pipes begin to produce pressure, thereby form a vortex standpipe 246 gradually.So, will produce the outwards ejection of fluid volume clustered column body 248 (promptly producing spiral fashion boundling fluid thrust 250) at the tail end of cylinder 220, thereby produce a reaction thrust 520 when the fluid pressure value in the cylinder during gradually greater than cylinder 220 exterior pressure.This kind thrust is enough to promote inflatable carrier device 110 of the present invention or on-inflatable formula carrier device.When producing spiral fashion boundling fluid thrust 250, because it presents spurting or column penetrates, therefore also can form the jet or water column of a brute force, reaction thrust 520 producing methods of this kind can come from fluid boundling vortex standpipe device 265 of the present invention, or the product non-of the present invention with this function all can.
In this embodiment, plug-in vertical jet-propulsion plant of the present invention and carrier waterborne 100 its operations, use with connection mode as follows: on the appropriate location of inflatable carrier device 110, establish a plug-in vertical jet-propulsion plant 300, allow inflatable carrier device 110 be able to advance forward or backward to produce certain kinetic energy and thrust, direction control stalk 130 then is to interconnect with plug-in vertical jet-propulsion plant 300, its main purpose is exactly can be by the control of this direction control stalk 130, allow the swing of rotating plug-in vertical jet-propulsion plant about 300 natures, so reach can optional turning purpose.
In addition, relevant its relevant assembly and function, operation, connection etc. are please in detail referring to figs. 2 to Fig. 8.
Please refer to Fig. 2, it has shown fluid boundling vortex standpipe device of the present invention.In this embodiment, before the fluid boundling vortex standpipe device 265 of the present invention a fluid pressor areas 234 is arranged, the main purpose of this device is when the cylinder on the cylinder transmission shaft 240 220 is rotating, can allow fluid intake 230 places before the cylinder 220, because of rotation that the pressurized with fluid guide vane means 232 in the place ahead and a water conservancy diversion bending 233 etc. are arranged and the relation of cutting the stream motion, and produce hydraulic fluid.So when cylinder transmission shaft 240 is constantly rotating, simultaneously also can constantly produce new following hydraulic fluid, the side of water conservancy diversion bending 233 of adding the forward edge of pressurized with fluid guide vane means 232 is cut to flow and is done, can reduce the generation of crosswind, flow-disturbing, also can allow down hydraulic fluid form a pressurization phenomenon of inwardly assembling gradually, and produce a powerful column pressure fluid pattern.The column pressure fluid that this district is produced mainly is that the stream device 235 of cutting before the feed roller 220 uses, when the cylinder on the cylinder transmission shaft 240 220 when low, middling speed is rotated, it can allow cuts the spoon shape body that flows device 235, exterior down hydraulic fluid is cut in the cylinder 220 very easily, allow and cut stream device 235 and fluid constantly can be irritated by force in tube, thereby the fluid in the Yi Rangguan is kept the flow regime of advancing from front to back at any time, and unlikely meeting becomes the idle running phenomenon that no fluid flows in the pipe, and then the situation of no thrust power (stall) takes place.So when cylinder transmission shaft 240 when low, middling speed is rotated, it has complementary pressurized with fluid effect, allows fluid is easier to enter cutting in the stream device 235 on the cylinder 220.If when cylinder transmission shaft 240 when middle and high speed turns round, if the design in no pressurized with fluid district 234, then on the cylinder 220 cut stream device 235 spoon shape body, can cut fluid vaporization before the stream device 235 because of the relation of high speed rotating easily allow, so be easy to generate the cavitation corrosion phenomenon, and then cause can't allowing fluid enter in the cylinder 220, just can't produce thrust certainly.Therefore when cylinder transmission shaft 240 when middle and high speed turns round, it more needs the design in pressurized with fluid district 234, because the pressure fluid that it produced, can prevent to allow and cut fluid vaporization before the stream device 235, allow fluid enter cutting in the stream device 235 on the cylinder 220 easily, so just can not produce the cavitation corrosion phenomenon, be not afraid of in the cylinder 220 yet and can't allow fluid enter, will possess certain thrust certainly.
In this embodiment, has fluid pressurization guide vane means 232 in the pressurized with fluid district 234 before the fluid boundling vortex standpipe device 265 of the present invention at least, it is connected with cylinder transmission shaft 240, with cylinder 220 all be on same axle center, the setting of one fixed support 225 is arranged at its front end place, in fixed support 225, then there is a bearing 226 to be connected with cylinder transmission shaft 240, just cylinder transmission shaft 240 is fixed on one by this connection, and cylinder transmission shaft 240 can not be shaken when rotating or displacement, biased phenomenon.The position of this pressurized with fluid guide vane means 232 is the place aheads of cutting stream device 235 at cylinder 220, therefore when cylinder transmission shaft 240 rotates, it also can rotate along same direction simultaneously, and along with the curved width of cloth of stream curved surface of cutting of pressurization flow deflector designs, fluid can be bent width of cloth direction along the stream curved surface of cutting of pressurization flow deflector, fluid is pressed to the place ahead place of cutting stream device 235, allow the fluid after pressing down can be correct well, and the concentrated area enters into and cuts in the stream device 235; One water conservancy diversion bending 233, its position is on the forward edge of pressurized with fluid guide vane means 232, the outer rim of the forward edge of pressurized with fluid flow deflector is the curved curved design of an ecto-entad, this design is except that having stable cutting the effect of stream, also have with the pressurized with fluid flow deflector when rotating at effluent that its side produced, stream looses, the effect that the phenomenon of flow-disturbing etc. is eliminated, when cutting stream, side also the fluid that presses down inwardly can be imported, and then form a pressurization phenomenon of inwardly assembling, and the powerful column pressure fluid pattern that produces enters and cuts in the stream device 235; One direction of flow 228, its main purpose be exactly can be very clear and definite on figure the flow direction that demonstrates fluid.
In this embodiment, motor 325 on the engine installation 310, engine installation~transmission shaft 215 and cylinder transmission shaft 240, fluid boundling vortex standpipe device 265 etc., all utilize at least one fixed support 225, be fixed in the plug-in vertical jet-propulsion plant 300.
When fluid through one rotate fluid boundling vortex standpipe device 265 time, fluid is the formed powerful column pressure fluid when rotating through pressurized with fluid guide vane means 232 in the pressurized with fluid district 234 of front end and water conservancy diversion bending 233 earlier, and then cutting of process fluid intake 230 places flowed device 235, with the column pressure fluid with continuous rotation and dig spoon, the mode of strong filling etc., pressure fluid is cut in the pipe of cylinder 220, then pressure fluid in pipe along with the water conservancy diversion direction of spiral stream guidance lug 255, the rotation of flowing after beginning produces by forward direction in the pipe of cylinder 220 and cut the stream motion, because the pitch of spiral stream guidance lug 255 is to adopt front wide and rear narrow design, when so fluid rotates in fluid boundling vortex standpipe device 265, the effect that fluid in hollow tube 245 is pushed after being subjected to constantly by forward direction, therefore fluid can produce certain pressure gradually in pipe, and form a vortex standpipe 246, so the fluid behind the pressurized will form fluid volume clustered column body 248, its meeting is moved towards the opening part of the tail end of vortex standpipe 246, when the force value of greatly too cylinder 220 outsides gradually of the force value in its pipe, will the spin tail end of vortical pressure pipe 246 of pressure fluid in this moment pipe outwards sprays, and produce spiral fashion boundling fluid thrust 250, and then form a reflex thrust 520.The tail end of its fluid boundling vortex standpipe device 265, also can be connected with connection tube device 270, jet pipe 420 or specific function ejecting device 280 etc. use (as inflation, fluid extract out, draw water, jet or water column).
In this embodiment, the structure of fluid boundling vortex standpipe device 265 of the present invention comprises one engine installation~transmission shaft 215, a cylinder 220, a spiral stream guidance lug 222, a fixed support 225, a bearing 226, a direction of flow 228, fluid inlet 230, one fluid pressurization guide vane means 232, a water conservancy diversion bending 233, a fluid pressor areas 234, all stream devices 235, a rotation direction 236, a cylinder transmission shaft 240, a hollow tube 245, a vortex standpipe 246, fluid volume clustered column body 248, a generation spiral boundling fluid thrust 250 at least.
In this embodiment, engine installation~the transmission shaft 215 of the assembly of fluid boundling vortex standpipe device 265 of the present invention, its main purposes is the kinetic energy that is produced on the engine installation 310, by this device its kinetic energy commentaries on classics is reached on the cylinder transmission shaft 240, and the rotation of drive pressurized with fluid guide vane means 232 and fluid boundling vortex standpipe device 265, and then produce spiral boundling fluid thrust 250; One cylinder 220, it is the circular housing of fluid boundling vortex standpipe device 265, it is a front wide and rear narrow rounded cylindrical shell design, its inwall then is to be connected with spiral stream guidance lug 222, effect with protection spiral stream guidance lug 222 also has the effect that fluids in the cylinder 220 produce pressure within it of flowing through that allows in addition; One spiral stream guidance lug 222, its peripheral edge portion is connected with the inwall of cylinder 220, its inner ring fore-end then is connected with the outer rim of cylinder transmission shaft 240, and its interlude and afterbody all are to be hollow form, to form a boundling pressure space, an i.e. vortex standpipe 246, its main purpose is to allow fluid through after the motion of this assembly, will change former flow rate of fluid, the path, pressure, and in a vortex standpipe 246, produce a force value greater than external pressure, and outwards spray, and then produce the reaction thrust 520 of fluid volume clustered column body 248 by tail pipe; One fixed support 225, in a bearing 226 device is arranged, motion by bearing 226, allow rotations such as engine installation~transmission shaft 215 on the engine installation 310 and cylinder transmission shaft 240, fluid boundling vortex standpipe device 265, and engine installation~transmission shaft 215 is fixed on the engine installation 310, and cylinder transmission shaft 240, fluid boundling vortex standpipe device 265 etc. are fixed in the plug-in vertical jet-propulsion plant 300; One bearing 226, its main purpose is for being used for rotational power plant~transmission shaft 215 and cylinder transmission shaft 240, fluid boundling vortex standpipe device 265; One fluid inlet 230, it is positioned at pressurized with fluid district 234, and the front end place of cutting stream device 235 of cylinder 220 is inlet ports of fluid (water or gas); All flow device 235, be spiral stream guidance lug 222 and expose to cylinder 220 part foremost, when cylinder 220 is rotating, it can form the spoon shape body of all streams, exterior fluid is cut in the cylinder 220 easily, allow the fluid of cylinder 220 front ends constantly in tube, irritate by force, and pass through the rotation of the spiral stream guidance lug 222 in the cylinder 220, and easily form the phenomenon of fluid pressurization; One rotation direction 236, its main purpose is the rotation direction that demonstrates engine installation~transmission shaft 215, cylinder transmission shaft 240, pressurized with fluid guide vane means 232, cylinder 220, fluid boundling vortex standpipe device 265 etc. that can be clear and definite on figure; One cylinder transmission shaft 240, its main purpose are for to be connected the one end with engine installation~transmission shaft 215, the part of the other end in tube then is connected with the front end of spiral stream guidance lug 222, and then drive the rotation of cylinder 220; One hollow tube 245, be the interlude of spiral stream guidance lug 222 inner rings and the part of tail end, its main purpose be allow enter in the cylinder 220 (front wide and rear narrow) fluid have one to flow, kink, boundling, the space of pressurization, when the centre of this assembly and end section after the rotation of cylinder 220, the stream of cutting of the spiral stream guidance lug 222 of projection moves on inside pipe wall again, to form a revolving vortex standpipe 246, the fluid of Gun Donging will form the shape of fluid volume clustered column body 248 within it, because its bore of fluid discharge outlet of tail end is narrower, so the pars intermedia in pipe is to the tail end place, to can produce a cooresponding force value gradually, when the force value in its pipe during gradually greater than the pressure outside managing, fluid pressure in its pipe will spray outside tail pipe, and then produce spiral boundling fluid thrust 250, also be and produce the reaction thrust 520 that sprays; One vortex standpipe 246, its position is exactly hollow tube 245 positions in cylinder 220, the tail end of front end next-door neighbour cylinder transmission shaft 240, front end broad tail end is then narrower, the spiral stream guidance lug 222 that projection is arranged on tube wall, be used for the fluid in the pipe produced along with the rotation of spiral stream guidance lug 222 and cut stream motion,, further produce spiral boundling fluid thrust 250 outside tail pipe, to discharge to cause fluid volume clustered column body 248; One fluid volume clustered column body 248 promptly is the charging fluid of the spiral vortex type boundling body shape that produced in vortex standpipe 246; One produces spiral boundling fluid thrust 250, it promptly is the vortex standpipe 246 in cylinder 220, the fluid volume clustered column body 248 of the columnar fluid that is produced after kink that tail end sprayed, boundling, pressurization, it has the effect (as Water Jet) of the reaction thrust 520 of an injecting type.
This figure only is the explanation of an embodiment, but its purposes is not placed restrictions on the usefulness of carrier in waterborne or water, also can be used for other place, as fluid power plant, fluid engine etc.
Please refer to Fig. 3, for showing plug-in vertical jet-propulsion plant 300 of the present invention.In this embodiment, on the plug-in vertical jet-propulsion plant 300 of the present invention, many relate to fluid boundling vortex standpipe device 265 or other relevant component Name, connection, function, uses are arranged, and these all described in detail in Fig. 1 and Fig. 2, so do not repeat them here.If any not clear part, please refer to Fig. 1, Fig. 2.
In this embodiment, the keystone configuration assembly of plug-in vertical jet-propulsion plant 300 of the present invention comprises a jet-propulsion plant 200 at least, this jet-propulsion plant 200 is on the water surface and stand on the water surface, end towards the water surface has a connection tube 272, in order to be connected jet apparatus 405, and this jet-propulsion plant 200 is used to spray gas, to produce reaction thrust 520, one front and back jet control device 400, one control direction device 132, one device 150 safe in utilization, one carrier 305, one carrier and power connecting device 174 are in order to be connected this carrier and this jet-propulsion plant 200.
In this embodiment, jet-propulsion plant 200 of the present invention comprises: an engine installation 310 has the power supply device of motor 325 and battery module 340; One fluid boundling vortex standpipe device 265, the jet apparatus 405 of this fluid boundling vortex standpipe 265 has front wide and rear narrow hollow tube cylinder, and its inwall is connected with spiral stream guidance lug 222; One jet apparatus 405, this jet apparatus is connected with aforesaid fluid boundling vortex standpipe device 265 by a connection tube 272, and Xiang Shuizhong ejection gas, to produce reaction thrust 520.
In this embodiment, with regard to the effect of the keystone configuration assembly of plug-in vertical jet-propulsion plant 300 of the present invention, connect and do one and explain orally easily: jet-propulsion plant 200, its main purpose is to convert kinetic energy (being produced by engine installation 310) to thrust (by fluid boundling vortex standpipe device 265), and the control speed on the speed controller 134, it is waterborne that carrier 305 can at random be travelled on; Front and back jet control device 400, its main purpose is with the thrust of jet-propulsion plant 200 final gained, utilizes the control of this assembly, can allow carrier 305 be able to smoothly to moving ahead or retreating backward; Control direction device 132, its main purpose are the control of direction of passage control stalk 130, reversing control stalk 136 etc., advancing, retreating or the travel direction of turning etc. in order to operation carrier 305; Device 150 safe in utilization, its main purpose is the protection driver 610 a kind of security consideration reached when falling into water (typically refer to driver 610 situation) of being expert at, when in case driver 610 breaks away from certain distance range with carrier 305, engine installation 310 on the carrier 305 will shut down automatically, too far away to prevent that carrier 305 breaks away from driver 610, cause accident; Carrier and power connecting device 174 are used for interconnecting between jet-propulsion plant 200 and the carrier 305.
In this embodiment, jet-propulsion plant 200 its keystone configuration assemblies of the present invention comprise an engine installation 310 at least, this device is meant the motor 325 of battery module 340 electric power of supplying, be the power resources of jet-propulsion plant 200, but during if any the demand of other kinetic energy, also can change and adopt other various power system, to satisfy the demand on the actual or special kinetic energy of carrier 305, as internal combustion engine, injection engine, turbine engine, green motility engine, give birth to that the matter power traction is held up, fuel engine etc. replaces; One speed controller 134, its main purposes is the power capacity of control engine installation 310 outputs, and then the kinetic energy speed of control fluid boundling vortex standpipe device 265; One fluid boundling vortex standpipe device, 265 (please refer to Fig. 2); One connection tube 272, its position is at the tail end place of fluid boundling vortex standpipe device 265, significant feature is exactly that its front end can allow the cylinder 220 of fluid boundling vortex standpipe device 265 be connected with this assembly, its other end then links together with jet pipe 420, form a sleeve pipe that is connected the different assemblies in two ends, allow fluids volume clustered column bodies 248 in the fluid boundling vortex standpipe device 265 flow to smoothly in the jet pipe 420 well and outwards ejection.This assembly also can be connected use with specific function ejecting device 280, for other special purpose, as inflation, fluid extract out, draw water, jet or water column etc.; One jet pipe 420, its position interconnects with it below connection tube 272, its main purposes is that the fluid volume clustered column body 248 that fluid boundling vortex standpipe device 265 is sprayed is directed in the jet control device 400 of front and back, with the kinetic energy that advances or retreat as carrier 305; One filter screen 216, place between the ventilation foremost of fluid boundling vortex standpipe device 265 and locate, its main purpose is exactly the foreign material between filtered air, and outside it is blocked in, only allowed the fluid that filters enter in the fluid boundling vortex standpipe device 265, to avoid damaging fluid boundling vortex standpipe device 265.If also can install filter material additional whenever necessary, make the fluid that enters clean more in suitable part; One dividing plate 217, its main purposes is the assembly that separates different device on the one hand, is convenient to fixation kit, leakproof, reaches operations such as renewal, maintenance, maintenance, then is intensity and the impact resistance power that can strengthen shell 218 on the other hand; One shell 218; can be used for protecting all component and the device of jet-propulsion plant 200 in it; then can be designed to meet hydromechanical streamline moulding outside it, can reduce the fluid resistance when advancing on the one hand, rudder 120 uses then can be worked as in the place under waterline on the other hand.
In this embodiment, jet apparatus 405 of the present invention comprises a jet pipe 420, a front and back jet control device 400, a fan jet plate 510, a connection tube 272, a jet flow outlet device 500, a rudder 120, a hydrofoil plate 125 at least.
In this embodiment, front and back of the present invention jet control device 400 (its detail drawing please refer to Fig. 4), its keystone configuration assembly comprises a latching connector 415 at least, its upper end then is connected with the jet pipe 420 of connection tube 272 belows, its main purpose is exactly to be used for being connected with the front end of front and back jet control device 400, so that be used for the whole front and back jet control device of organizing 400 of dismounting, renewal or maintenance; One jet pipe 420; One flow jeting port 422, its fluid that will be sprayed in top jet pipe 420 volume clustered column body 248 fluids import in the jet flow rotating disk 435; One flow jeting port 425 that advances, its position is at the rear of jet flow rotating disk 435, can allow fluid roll up clustered column body 248 fluids, jet pipe 420 by jet flow rotating disk 435 rears, jet flow is directed on the jet flow outlet device 500, and then produce the reaction thrust 520 of a jet flow, therefore can allow carrier 305 be advanced; One reversing flow jeting port 430, its position is in the place ahead of jet flow rotating disk 435, can allow fluid roll up clustered column body 248 fluids, by the directly outwards ejection of opening part in jet flow rotating disk 435 its place aheads, and then produce the reaction thrust 520 of a jet flow, therefore can allow carrier 305 be retreated; One jet flow rotating disk 435, the inlet of its fluid are the flow jeting ports 422 of top, have the outlet of two places, and a place is the flow jeting port 425 (advancing) that advances at its rear, and another place is the reversing flow jeting port 430 (retreating) in its place ahead.Its main function is exactly to be used for controlling fluid or jet flow backward motion forward, use in the design normal, the flow jeting port 425 that advances at its rear is to be the unlatching shape, the reversing flow jeting port 430 in its place ahead then is to be to close shape, so fluid volume clustered column body 248 fluids in this assembly just can outwards spray from the rear, and allow carrier 305 be advanced.In case driver 610 starts after the reversing control stalk 136, will wait by pulley 138, control line 140 and rotate this assembly, simultaneously the flow jeting port 425 that advances at rear is closed, and allow the reversing flow jeting port 430 in the place ahead open, therefore fluid volume clustered column body 248 fluids will spray from the place ahead, and allow carrier 305 be retreated; Single-revolution spring installation 440, its main purpose are exactly to allow be the jet flow rotating disk 435 that retreats, after driver 610 loosens reversing control stalk 136 gradually, by the main spring in this assembly, allow jet flow rotating disk 435 rotate back into again again and are the pattern of advancing; One forward streams is meant fluid is presented the flow direction (advancing) of ejection backward to 445; One reversing flows to 450, is meant fluid is presented the flow direction (retreating) of ejection forward; One jet flow outlet device 500 is positioned at the tail end (its detail drawing please refer to Fig. 5) of jet apparatus 405, this device can be by the styling design of special various ejiction openings, shape, volume size, bubbles volume, speed or the direction of ejecting fluid be can change, thereby different thrust, resistance, sound produced; This jet flow outlet device 500 comprises a fan jet plate 510, and its main purpose is fluid to be rolled up the fluid of clustered column body 248, by the water conservancy diversion pattern of this assembly, increases or enlarge the area of thrust, to increase reaction thrust 520 effects of thrust; Flow deflector 515 mainly is after the fluid that fan jet plate 510 is sprayed is passed through the guiding of this assembly, can avoid producing too many flow-disturbing phenomenon on the one hand, then is the place that can smoothly the thrust direct fluid be desired to reach on the other hand; One reaction thrust 520, it meets the known law of motion; One rudder 120, its main application also can keep the vertical degree of stability of carrier 305 simultaneously for allowing carrier 305 have the function of turning to; One hydrofoil plate 125 can allow carrier 305 keep certain horizontal stable degree in motion.
In this embodiment, control direction device 132 of the present invention, its keystone configuration assembly comprises a direction control stalk 130 at least, it is grip foremost, and the utensil that available hand or use are convenient to grasp this assembly is controlled, and is equipped with a safe plunger seat 160 in the appropriate position of its grip, plunger 162 for device 150 safe in utilization uses, in case after plunger 162 broke away from safe plunger seat 160, jet-propulsion plant 200 shut down immediately, with the safety of guaranteeing that driver 610 is expert at and reaches.Another purposes is, at the tail end place of its control stalk, is connected with jet-propulsion plant 200, and as long as driver 610 is this assembly of swing, with regard to the direct of travel of may command carrier 305; One reversing control stalk 136, its main purpose are exactly the pattern that will originally advance and travel, and the operation by this assembly and pulley 138, control line 140, front and back jet control device 400 etc. retreats the purpose of travelling and allow carrier 305 reach; One pulley 138, be connected with control line 140 at its outer rim place, main purpose be exactly by its can be arbitrarily to the principle of front or rear rolling, control line 140 can be moved forward and backward, reduce friction on the one hand, can allow driver 610 more laborsaving, easy to operate when control reversing control stalk 136 on the other hand; One control line 140, the one end is connected with reversing control stalk 136, utilize with at least one pulley 138 more therebetween and change this assembly in the operational pattern that turns to, then be connected at its other end with front and back jet control device 400, its main purpose is the control by this assembly, and allows carrier 305 reach to advance or retreat the purpose of travelling.
In this embodiment, device safe in utilization 150 of the present invention, its keystone configuration assembly comprises a safety control 152 at least, this assembly is arranged in the engine installation 310, its topmost purposes is to be used for responding to plunger 162 whether in safety plunger seat 160, if, then can start or continue operation jet-propulsion plant 200, if it is opposite, then it stops the operation of jet-propulsion plant 200 immediately, its main purpose be exactly can direct control jet-propulsion plant 200 the effect that starts or stops operation; One safe stick placing device 154; normally place on driver 610 the body; locate as wrist, arm or foot, ankle, shank etc.; easily tighten is difficult for the place of overslaugh control again; as long as plunger 162 1 leaves safe plunger seat 160, jet-propulsion plant 200 is out of service immediately, otherwise; jet-propulsion plant 200 still can continue operation, and its topmost purpose is exactly the safety on protection driver 610 travels.
In this embodiment, safe stick placing device 154 of the present invention, its keystone configuration assembly comprises a wrist ring 156 at least, mainly be to be used for being convenient to driver 610 to carry plunger 162 or be fixed on driver 610 the body, the general common snare that all is used for is being located as wrist, arm or foot, ankle, shank etc., and easily tighten is difficult for the place of overslaugh control again; One connecting band 158, the one end is connected with wrist ring 156, the other end then is connected with plunger 162, this assembly length in the use, then be to decide with general driver's 610 action radius, the oversize or too short safe effect that all can directly have influence on the operation of jet-propulsion plant 200 or use; One safe plunger seat 160 places the appropriate position of direction control stalk 130 grip foremost, uses for plunger 162; One plunger 162 is used for inserting in the safe plunger seat 160, is in the scope of may command jet-propulsion plant 200 to guarantee driver 610.
In this embodiment, device safe in utilization 150 of the present invention also can adopt the pattern of controlled in wireless to monitor.As safe plunger seat 160 and plunger 162 grades are all adopted the wire-less inductive devices of non-touch-type instead, can break away from or reduce driver 610 and be connected puzzlement problem with 158 length distance.The scope of its wireless induction is set, and also can adopt distributed fixed-point apparatus, makes the action radius of driver 610 on carrier 305 broad, convenient more, but can therefore not have influence on the safety on travelling.
In this embodiment, carrier of the present invention and power connecting device 174, its keystone configuration assembly comprises a carrier adaptation arrangement 170 at least, its main purpose is the equipment mechanism by this assembly, with plug-in vertical jet- propulsion plant 300 and 305 mutual linking together of carrier, and then allow driver 610 be convenient to dismounting, renewal, maintenance and dexterous manipulating; One plug-in vertical jet-propulsion plant 300 (please refer to the detailed description of leading portion); One carrier 305 (please refer to the detailed description of leading portion).
In this embodiment, carrier adaptation arrangement 170 of the present invention, its keystone configuration assembly comprises a supporting plate 172 at least, its position then is the suitable place that places on the carrier 305, and can be provided with and control plug-in vertical jet-propulsion plant 300, and can utilize this assembly to fix or support plug-in vertical jet-propulsion plant 300; One connecting device 176 that swings, its main purposes is for being the movable sheet moulding joining place with the preceding end housing 218 of plug-in vertical jet-propulsion plant 300 on the one hand, can interconnect with the movable sheet moulding joining place of U type draw-in groove plate 178 rear ends by this assembly, and utilize trip bar 182 to fix or separate.Then be to allow connect and be fixed on plug-in vertical jet-propulsion plant 300 on the carrier 305 on the other hand, but the mode that swings of driver's 610 direction of passage control stalks 130, to reach the purpose that turns to about control; One U type draw-in groove plate 178, its moulding is the U font shape of the formula of couching, main function will be locked device 184 exactly by assemblies such as a rotating plate 186, a screw 188, chucks 190, with its clamping and be fixed on the splint holder 172 of carrier 305, and realize interconnective relation, so just can allow the normal use that plug-in vertical jet-propulsion plant 300 can be firm.On the other hand, be provided with one in the appropriate position of this assembly and lift connecting device 180 up and down,, can allow plug-in vertical jet-propulsion plant 300 make the action of lifting or putting down by the control of a trip bar 182; One lifts connecting device 180 up and down, its position is arranged on the appropriate position of U type draw-in groove plate 178, its main function is exactly when carrier 305 runs into the shoal water zone and is unfavorable for that comparatively carrier 305 travels, or when having foreign matter to bump in the water, or carrier 305 desires are debarked when stopping, can push trip bar 182 earlier aside, and then plug-in vertical jet-propulsion plant 300 is pressed down forward, so just plug-in vertical jet-propulsion plant 300 can be raised and fixed.If will be when continue using plug-in vertical jet-propulsion plant 300, allow it return to spendable appropriate location as long as press down plug-in vertical jet-propulsion plant 300, again with 182 fastenings of trip bar and fix, can recover the function of this assembly, 300 of plug-in vertical jet-propulsion plants can begin to continue to use; One trip bar 182 mainly is be used for getting loose or fixedly swing connecting device 176, U type draw-in groove plate 178; One device 184 that is locked, its main purposes are that U type draw-in groove plate 178 is connected with supporting plate 172 on the carrier 305 by this assembly; One rotating plate 186, its lower end is connected with spiral shell 188, is used for the usefulness of rotation lock fixer 184; One spiral shell 188, its upper end is a rotating plate 186, its lower end is a chuck 190, utilizes the effect of its helical rotation, gets loose or is locked on the supporting plate on the carrier 305 172 with the mode of rotating; One chuck 190, its upper end is connected with spiral shell 188, mainly is the rotation that utilizes assemblies such as rotating plate 186, screw 188, and then allows this assembly reach to get loose or be locked on the supporting plate on the carrier 305 172.
In this embodiment, engine installation 310 of the present invention, its keystone configuration assembly are at least one controller 315, actuator 320, safety control 152, motor 325, engine installation~transmission shaft 215, Hooke's coupling 330, water shutoff bearing 335, battery module 340, electric wire 345, charger 350, plug 355.
In this embodiment, the assembly in the engine installation 310 of the present invention is done an explanation with regard to its use, purposes, a battery module 340, and its main purpose is for providing the power source of this engine installation 310 abundances; One electric wire 345 is delivered to electric power on other relevant device that needs electric energy; One controller 315, its function are burning voltage, current delivery control; One actuator 320 is the drg of CD-ROM drive motor 325 rotations; One safety control 152 is a control assembly of device 150 safe in utilization; One motor 325 is one electric energy to be changed into the device of kinetic energy, can allow transmission shaft in this assembly according to its different electric energy power, electric current, and produce different rotating speeds; One Hooke's coupling 330, its main purposes for will be not the transmission shaft on same bobbin, after the two ends by this assembly are connected, when rotating, its kinetic energy changeed reaching on another transmission shaft; One water shutoff bearing 335, its main purpose is the sealing effectiveness by this bearing, can allow extraneous fluid be difficult for flowing in the body, and then have influence on the operation of normal parts; One charger 350 can be led into this assembly by plug 355 with it with the electric power (direct current (DC) or alternating current) in the external world, then through changing or directly being stored in the battery module 340, so that the electric power that will consume replenishes, makes things convenient for electric power to continue to use; One plug 355 is that this assembly is inserted on the socket of extraneous power supply, and the electric power in the external world is introduced in the charger 350.
In this embodiment, when the user will use this plug-in vertical jet-propulsion plant 300, at first plug-in vertical jet-propulsion plant 300 to be ready for, and hang over outward on the supporting plate 172 of carrier 305, subsequently and check the connecting device 176 that swings, U type draw-in groove plate 178, lift connecting device 180 etc. up and down, whether place appropriate reaching and fix, and then carrier 305 is shifted onto on the water surface, wait for starting and sails.
In this embodiment, when the user will use this plug-in vertical jet-propulsion plant 300, whether the electric power that must inspect the battery module 340 in the engine installation 310 earlier is sufficient, if when finding power shortage, plug 355 can be inserted on the power supply base, it is interior till abundance that exterior electric power is entered battery module 340 by electric wire 345, charger 350.After close examination electric power abundance, driver 610 essential elder generations are with the plunger 162 of device 150 safe in utilization, in the safe plunger seat 160 of the front end of direction of insertion control stalk 130, then could the turns on power switch, by controller 315, allow motor 325 rotate after the startup of actuator 320, transmission shaft on the motor 325 can be connected with the front end of engine installation~transmission shaft 215 by Hooke's coupling 330 then, and water shutoff bearing 335 is exactly to pass engine installation~transmission shaft 215, its purposes is exactly outside the moist fluid outside the dividing plate 217 is blocked in, do not allow electronic accessory parts in the engine installation 310, equipment or motor 325 etc. are because of easily getting wet or moisture is too much damaged; The other end of engine installation~transmission shaft 215 then is connected with cylinder transmission shaft 240 on the fluid boundling vortex standpipe device 265, so when motor 325 begins to rotate, the same time just allows fluid boundling vortex standpipe device 265 also begin to rotate, regulation and control along with controller 315, the variation that will allow the rotating speed of fluid boundling vortex standpipe device 265 produce speed, when quickening, the fluid that enters in the tube can produce jet thrust because of excessive extruding, thereby driving carrier 305 advances; Gradually slow or when stopping when motor 325 rotating speeds, then fluid boundling vortex standpipe device 265 can become at a slow speed or halts because of the thrust decay that is sprayed.
In addition, in cylinder transmission shaft 240, its front end place is provided with a fixed support 225, in fixed support 225, there is a bearing 226 closely to be connected with cylinder transmission shaft 240, mainly be in order to resting barrel transmission shaft 240, it can be remained on the same axle center at any time rotates, be right after thereafter be exactly pressurized with fluid guide vane means 232, it after rotating because of cutting the motion of stream, will form a fluid pressor areas 234, allow pressurization fluid later can import cutting in the stream device 235 of fluid boundling vortex standpipe device 265 front ends smoothly well, and with strong filling and the mode of digging spoon along with the curved surface of the spiral stream guidance lug 222 in the cylinder 220 is cut stream mode, allow the outer pressure fluid of pipe enter in the interior vortex standpipe 246 of pipe, after constantly rotating, will make the continuous pressurization campaign before the fluid that is trapped in the pipe is subjected to managing gradually, the outlet of adding cylinder 220 tail ends is narrower, so strength of the generation mutual extrusion that the fluid in the pipe will be gradually, in case when the fluid pressure value in the pipe when managing external pressure, extruded fluid will externally spray fast in the pipe, and then produce a reaction thrust 520,305 of carriers can be travelled therefrom (advance or retreat).
Please refer to Fig. 4, for showing front and back of the present invention jet control device.In this embodiment, all assemblies in the front and back of the present invention jet control device 400 and function, operation, connection etc. will repeat no more at this all in Fig. 3 detailed explanation mistake, please be with reference to figure 2, Fig. 3.
In this embodiment, front and back of the present invention jet control device 400 just presents the constructional drawing of side at this figure, and the position of assembly and mutual annexation, and at length is presented in the figure.
Please refer to Fig. 5, for showing jet flow outlet device of the present invention.In this embodiment, all assemblies in the jet flow outlet device 500 of the present invention and function, operation, connection etc. will repeat no more at this all in Fig. 3 detailed explanation mistake, please be with reference to figure 2, Fig. 3, Fig. 4.
In this embodiment, jet flow outlet device 500 of the present invention just presents the constructional drawing of overlooking at this figure, and the position of assembly and mutual annexation, and at length is presented in the figure.
Please refer to Fig. 6, it has shown fixed type jet-propulsion plant 605 of the present invention, comprise a carrier 305, a jet-propulsion plant 200, this jet-propulsion plant 200 is on the water surface and be fixed in mini Wave Race car body 620 (carrier 305), end towards the water surface has a connection tube 272, in order to being connected jet apparatus 405, and this jet-propulsion plant 605 is used for Xiang Shuizhong ejection gas, to produce reaction thrust 520.
Fixed type jet-propulsion plant 605 of the present invention is to adopt non-plug-in mode, it is to be fixed on the mini Wave Race car body 620 (carrier 305), remaining component and structure all with plug-in vertical jet-propulsion plant 300 identical (please refer to Fig. 3), so do not repeat them here.
After describing preferred embodiment of the present invention in detail, those of ordinary skill in the field can be well understood to, under the prerequisite of scope that does not break away from claims and spirit, can carry out various variations and change, this is not limited to the embodiment of the embodiment of specification sheets.

Claims (14)

1. a plug-in vertical jet-propulsion plant is characterized in that, comprises:
One carrier;
One engine installation has motor and power supply device;
One jet-propulsion plant, this jet-propulsion plant are to stand on the water surface, and its front end is provided with admission port, its tail end is connected with connection tube towards water surface part, in order to the linking jet apparatus, and this jet-propulsion plant is to be used for to jet apparatus ejection gas, to produce reaction thrust;
One carrier and power connecting device are in order to connect this carrier and this jet-propulsion plant.
2. plug-in vertical jet-propulsion plant according to claim 1 is characterized in that this jet-propulsion plant comprises:
One fluid boundling vortex standpipe device, this fluid boundling vortex standpipe jet apparatus has front wide and rear narrow hollow tube cylinder, and its inwall is connected with the spiral stream guidance lug;
One jet apparatus, this jet apparatus is connected with aforesaid fluid boundling vortex standpipe device by a connection tube, and Xiang Shuizhong ejection gas, to produce reaction thrust.
3. plug-in vertical jet-propulsion plant according to claim 2 is characterized in that, this fluid boundling vortex standpipe device further comprises:
One engine installation~transmission shaft, one fixed support, all flow device, one fluid pressurization guide vane means, make the preceding of cylinder can form a fluid pressor areas, this the pressurization after fluid can allow cut stream device cut stream easily, one water conservancy diversion bending is located at the forward edge of pressurized with fluid guide vane means, be used for side and cut stream to reduce the generation of crosswind or flow-disturbing, also allow down hydraulic fluid be easier to assemble pressurization, all stream device projectioies are at the leading edge place of cylinder, in the pressure fluid importing cylinder with drum front end, one fluid inlet, one vortex standpipe, one cylinder transmission shaft, one Hooke's coupling.
4. plug-in vertical jet-propulsion plant according to claim 1 and 2 is characterized in that this jet apparatus comprises:
One front and back jet control device, its upper end is connected with latching connector or with aforementioned jet pipe, has the flow jeting port of advancing, reach a reversing flow jeting port, be used for controlling fluid or the motion of jet flow backward forward, make carrier be able to smoothly to moving ahead or retreating backward, one latching connector, be used for connecting the jet pipe of front end and interconnect with the front and back jet control device of lower end, be convenient to assemble the maintenance update jet apparatus, one jet pipe, one connection tube, one jet flow outlet device is positioned at the tail end of jet apparatus, one fan jet plate, in order to enlarge the area of thrust, the ejecting device of one specific function is for inflation, fluid is extracted out, draw water, jet or water column uses.
5. plug-in vertical jet-propulsion plant according to claim 1 is characterized in that, further comprises:
One control direction device, the control of direction of passage control stalk and reversing control stalk is advanced, is retreated or the turning driving direction in order to the operation carrier; One device safe in utilization, this device safe in utilization have a plunger and are connected with aforementioned jet-propulsion plant, in case when plunger was not connected with this jet-propulsion plant, the engine installation of this jet-propulsion plant will shut down automatically.
6. a fixed type jet-propulsion plant is characterized in that, comprises:
One carrier;
One engine installation has motor and power supply device;
One jet-propulsion plant, this jet-propulsion plant stands on the water surface, and its front end is the admission port place, its tail end is connected with connection tube towards water surface part, in order to the linking jet apparatus, and this jet-propulsion plant is used for to jet apparatus ejection gas, to produce reaction thrust.
7. fixed type jet-propulsion plant according to claim 6 is characterized in that, this jet-propulsion plant comprises:
One fluid boundling vortex standpipe device, this fluid boundling vortex standpipe jet apparatus has front wide and rear narrow hollow tube cylinder, and its inwall is connected with the spiral stream guidance lug;
One jet apparatus, this jet apparatus is connected with aforesaid fluid boundling vortex standpipe device by a connection tube, and Xiang Shuizhong ejection gas, to produce reaction thrust.
8. fixed type jet-propulsion plant according to claim 7 is characterized in that, this fluid boundling vortex standpipe device further comprises:
One engine installation~transmission shaft, one fixed support, all flow device, one fluid pressurization guide vane means, make the preceding of cylinder can form a fluid pressor areas, this the pressurization after fluid can allow cut stream device cut stream easily, one water conservancy diversion bending is located at the forward edge of pressurized with fluid guide vane means, be used for side and cut stream to reduce the generation of crosswind flow-disturbing, also allow and press down the fluid collection pressurization, all stream device projectioies are at the leading edge place of cylinder, in the pressure fluid importing cylinder with drum front end, one fluid inlet, one vortex standpipe, one cylinder transmission shaft, one Hooke's coupling.
9. according to claim 6 and 7 described fixed type jet-propulsion plants, it is characterized in that this jet apparatus comprises:
One front and back jet control device, its upper end is connected with latching connector or with aforementioned jet pipe, has the flow jeting port of advancing, reach a reversing flow jeting port, be used for controlling fluid or the motion of jet flow backward forward, make carrier be able to smoothly to moving ahead or retreating backward, one latching connector, be used for connecting the jet pipe of front end and interconnect with the front and back jet control device of lower end, be convenient to assemble the maintenance update jet apparatus, one jet pipe, one connection tube, one jet flow outlet device is positioned at the tail end of jet apparatus, one fan jet plate, in order to enlarge the area of thrust, one specific function ejecting device is for inflation, fluid is extracted out, draw water, jet or water column uses.
10. fixed type jet-propulsion plant according to claim 6 is characterized in that, further comprises:
One control direction device, direction of passage control stalk and the control of reversing control stalk are in order to the travel direction that advances, retreats or turn of operation carrier; One device safe in utilization, this device safe in utilization have a plunger and are connected with aforementioned jet-propulsion plant, in case when plunger was not connected with this jet-propulsion plant, the engine installation of this jet-propulsion plant will shut down automatically.
11. a jet-propulsion plant is characterized in that, comprises:
One engine installation has motor and power supply device;
One fluid boundling vortex standpipe device, this fluid boundling vortex standpipe jet apparatus has front wide and rear narrow hollow tube cylinder, and its inwall is connected with the spiral stream guidance lug;
One jet apparatus, this jet apparatus is connected with aforesaid fluid boundling vortex standpipe device by a connection tube, and Xiang Shuizhong ejection gas, to produce reaction thrust.
12. jet-propulsion plant according to claim 11 is characterized in that, this fluid boundling vortex standpipe device further comprises:
One engine installation~transmission shaft, one fixed support, all flow device, one fluid pressurization guide vane means, make the preceding of cylinder can form a fluid pressor areas, this the pressurization after fluid can allow cut stream device cut stream easily, one water conservancy diversion bending is located at the forward edge of pressurized with fluid guide vane means, be used for side and cut stream to reduce the generation of crosswind flow-disturbing, allow simultaneously and press down the fluid collection pressurization, all stream device projectioies are at the leading edge place of cylinder, in the pressure fluid importing cylinder with drum front end, one fluid inlet, one vortex standpipe, one cylinder transmission shaft, one Hooke's coupling.
13. jet-propulsion plant according to claim 11 is characterized in that, this jet apparatus comprises:
One front and back jet control device, its upper end is connected with latching connector or with aforementioned jet pipe, has the flow jeting port of advancing, reach a reversing flow jeting port, be used for controlling fluid or the motion of jet flow backward forward, make carrier be able to smoothly to moving ahead or retreating backward, one latching connector, be used for connecting the jet pipe of front end and interconnect with the front and back jet control device of lower end, be convenient to assemble the maintenance update jet apparatus, one jet pipe, one connection tube, one jet flow outlet device is positioned at the tail end of jet apparatus, one fan jet plate, in order to enlarge the area of thrust, one specific function ejecting device is for inflation, fluid is extracted out, draw water, jet or water column uses.
14. jet-propulsion plant according to claim 11 is characterized in that, further comprises:
One control direction device, the control of direction of passage control stalk and reversing control stalk is in order to the travel direction that advances, retreats or turn of operation carrier; One device safe in utilization, this device safe in utilization have a plunger and are connected with aforementioned jet-propulsion plant, in case when plunger was not connected with this jet-propulsion plant, the engine installation of this jet-propulsion plant will shut down automatically.
CN2010101957322A 2010-06-09 2010-06-09 Jet propulsion device Pending CN102275631A (en)

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CN104477360A (en) * 2014-11-12 2015-04-01 中国船舶重工集团公司第七○二研究所 Gas ejecting ring-rotating component combined gas ejecting device
CN105775084A (en) * 2016-04-05 2016-07-20 周瑞 Externally-hung axial-flow power pump spray propeller special for ships

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104477360A (en) * 2014-11-12 2015-04-01 中国船舶重工集团公司第七○二研究所 Gas ejecting ring-rotating component combined gas ejecting device
CN105775084A (en) * 2016-04-05 2016-07-20 周瑞 Externally-hung axial-flow power pump spray propeller special for ships

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