CN104276280A - Design scheme of framework structure - Google Patents
Design scheme of framework structure Download PDFInfo
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- CN104276280A CN104276280A CN201310436296.7A CN201310436296A CN104276280A CN 104276280 A CN104276280 A CN 104276280A CN 201310436296 A CN201310436296 A CN 201310436296A CN 104276280 A CN104276280 A CN 104276280A
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Abstract
The invention discloses a design scheme of a framework structure. The design scheme can be applied to an aircraft, and the aircraft can take off and land vertically and can move front and back as well as left and right like a cross; the operability of the aircraft is improved. The aircraft can take a flying saucer shape, a cuboid shape, a streamline shape, a cone shape, a shuttle shape, a pipe shape and the like and is good in pneumatic arrangement; by the adoption of full-motor operation, the aircraft can fly in the air and sail and sink in the sea; furthermore, emission of waste gas to an atmosphere and an ocean environment is reduced, so that the framework structure has environment-friendly and pollution-free effects and can be applied to civil use and military use.
Description
Art:
The present invention relates to framework design technology.
Background technology:
At present, mostly number adopts solid rotor aircraft of the prior art is the fuselage design of bird form, its taking off vertically, the aspect of performance that lands is difficult to integrate, although some aircraft can take off vertically, vertical landing manipulation operations, its aerodynamic arrangement needs to be improved further.
Summary of the invention:
The present invention want technical solution problem to be provide a kind of structural strength, pneumatic more reasonably framework design scheme for above-mentioned existing vehicle technology present situation.
The present invention solves the technical scheme that said frame structure technology problem adopts, a kind of shell/body, inside is folded row by pipe and is linked together, and comprises floor, separation wallboard, it is characterized in that, described shell/body is inner, with center-point/line for base, be provided with the longitudinal tube connected perpendicular to one another, horizontal pipe, its pipeline opening communicates with body space outerpace, the described longitudinal tube connected perpendicular to one another, the two ends of horizontal pipe are connected to form a body (pipe for the body be connected to form by pipe by pipe, be called for short body pipe), on described body pipe, with body inside center for point, be provided with the vertical pipe of symmetrical Boulez, its two ends mouth of pipe of vertical pipe communicates with body space outerpace, described body is inner, be a little with center, be provided with the vertical pipe of symmetrical Boulez, the lower end mouth of pipe of vertical pipe communicates with body space outerpace, it is obstructed that the upper end of pipeline is provided with pipe close, described shell/body is provided with various cabin as required, port/cabin door and valve.
As preferably, described in be provided with the body pipe of vertical pipe, its pipeline with longitudinally, horizontal pipeline connects.
As preferably, the vertical pipe on described body pipe, the wall body of vertical pipe is provided with the port communicated with each other with body pipe, and is provided with a breach, breach is provided with sealable gear chamber, gear is provided with electrical motor.
Being provided with one in vertical pipe on described body pipe can the sliding sleeve of left-right rotation, the wall body of described sliding sleeve is provided with port, the outer wall of described sliding sleeve and the inwall of vertical pipe are provided with circumferential recess, groove is embedded with piston ring seals, piston ring seals simultaneously can locate for sliding sleeve provides to install again in sealing, the outer wall of described sliding sleeve one end is provided with the circumferential gear teeth.
As preferably, described with enclosure interior center for point, the vertical pipe of symmetrical Boulez, its upper and lower two ends wall body is provided with hole, duct plug is provided with in the upper end of pipeline, be provided with the piston element of landing gear moving up and down in described pipeline, piston element and pipeline are provided with sealing member each other and seal, and the lower end of pipeline is provided with end cap and fixes, seals.
As preferably, the described two ends install pipeline that is longitudinal, horizontal pipeline connected perpendicular to one another has the pipeline (or being collapsed shape from two ends pipeline to the mouth of pipe) that one section of radial direction is less, described longitudinal, the horizontal pipeline connected perpendicular to one another is provided with breach to the top pipe wall body at radial less pipeline place, required electric propeller machine/motor fan and turbine/wind power generating set are hung in from here and is arranged in radial less pipeline, described breach is provided with breach lid.
The pipe end of described portraitlandscape is provided with rudder blade or air grid blade.
Described shell/body is inner, outside, and all ports are provided with cabin door.
Framed structure technology of the present invention can be applicable to aircraft, compared with existing aircraft technology, the invention has the advantages that; Eliminate the wing design structure of conventional aircraft, wing and body is made to be fused to entirety, adopt framed structure technology of the present invention can adopt full motor operation, make aircraft can do vertical takeoff, landing, and all around can move and right-angle steering manipulation operations as cross, substantially increase the manipulative capability energy of aircraft.Aircraft can adopt UFO-shape, streamline contour, taper, shuttle shape, pipe bar shaped etc., can have better aerodynamic arrangement, and owing to adopting full motor operation, aircraft can not have tail to spray infrared signature.
Accompanying drawing explanation;
Fig. 1 is birds-eye view of the present invention.
Fig. 2 is vertical cross-sectional of the present invention.
Fig. 3 is upward view of the present invention.
Fig. 4 is analysis chart of the present invention.
Detailed description of the invention;
Below in conjunction with accompanying drawing embodiment, the present invention is described in further detail.
Example one: as shown in Figure 1, Figure 2, Figure 3, Figure 4, a kind of shell/body 1, is characterized in that, described shell/body 1 is inner, with center-point/line for base, be provided with the longitudinal tube 2 connected perpendicular to one another, horizontal pipe 3, its pipeline opening communicates with body 1 space outerpace, the described longitudinal direction 2 connected perpendicular to one another, laterally the pipe two ends of 3 are connected to form a body by body pipe 4, on described body pipe 4, with body 1 inside center for point, be provided with the vertical pipe 5 of symmetrical Boulez, the two ends mouth of pipe of vertical pipe 5 communicates with body 1 space outerpace, described body 1 is inner, be a little with center, be provided with the vertical pipe 6 of symmetrical Boulez, the lower end mouth of pipe of vertical pipe 6 communicates with body 1 space outerpace, the upper end of pipeline 6 is provided with pipe close 61, described shell/body 1 is provided with various port 7 as required, floor, separation wallboard 8.
As preferably, described in be provided with the body pipe 4 of vertical pipe 5, its pipeline with longitudinally 2, laterally 3 pipeline connect.
Described vertical pipe 5, the wall body of vertical pipe 5 is provided with the port 51 communicated with each other with body pipe 4, and is provided with a breach 52, and breach 52 place is provided with sealable gear chamber, and gear is provided with electrical motor.
5 li, described vertical pipe is provided with one can the sliding sleeve 53 of left-right rotation, the wall body of described sliding sleeve 53 is provided with port 531, the outer wall of described sliding sleeve 53 and the inwall of vertical pipe 5 are provided with circumferential recess, groove is embedded with piston ring seals 532, piston ring can provide location and installation for sliding sleeve again while sealing, and the outer wall of described sliding sleeve 53 one end is provided with the circumferential gear teeth 533.
Described vertical pipe 6, its upper and lower two ends wall body is provided with hole 62, is provided with duct plug 61 in pipeline upper end, in its pipeline, is provided with piston element moving up and down, piston element and pipeline are provided with sealing member each other and seal, and the lower end of pipeline is provided with end cap and fixes, seals.
As preferably, the described longitudinal direction 2 connected perpendicular to one another, laterally the pipeline pipe end of 3 is provided with the less pipeline 21 of one section of radial direction, 31, the pipeline that described radial direction is less is arranged electric propeller/fan machine and turbine/wind power generating set are installed, vertical duct 5 on described body pipe 4 is arranged electric propeller/fan machine is installed, the described longitudinal direction 2 connected perpendicular to one another, laterally the top pipe wall body at the pipeline place that the pipeline of 3 is extremely radial less is provided with breach, breach is provided with breach lid 22, 32, electric propeller/motor fan and turbine/wind power generating set hang in thus and are arranged on radial less pipeline 21, 31 li.
Described longitudinal, horizontal pipe end is provided with rudder blade, grid leaf 9.
Described shell/body is inner, outside, and all ports 7 are provided with hatch door.
Example two: this example is the manipulation of aircraft is the sense of direction of all around by pipe tunnel 2, the horizontal pipeline 3 0/field shape pipeline connected perpendicular to one another.The operating table surface of operator's compartment, procedure operation; Start; Electric propeller on all pipe tunnels 2, horizontal pipeline 3, vertical duct 5/fan machine starts and enters low-speed running, and self-checking system shows that all are normal.Procedure operation enters unsettled stop program; Message handler processes the spline of the electronic oar/fan machine making all vertical duct 5 lower ends automatically, and aircraft is unsettled balances the rotating speed stopped automatically to regulate the electric screw of vertical duct 5 upper end fan machine to keep, and operation is packed up in the piston element/vertical drop frame retraction body 1 of vertical duct 6 li.After aircraft is unsettled, can be optionally different, can select to take off also can optional m igration, flight, also can flying on the other hand takes off on the other hand handles simultaneously.
Take off, table top operation makes total rpm governor (bar) of the electronic oar/fan machine on vertical duct 5 upwards, make the acceleration of the electronic oar/fan machine of all vertical duct 5 upper ends, screw propeller/flabellum cutting air produces lift, gas simultaneously in pipeline 5 produces pressure Jet with downward flow direction and produces vertical lift, make the liftoff vertical lift-off of aircraft, when hand one unclamps rpm governor (bar), rpm governor (bar) can automatically reset in centre, message handler regulates the electric propeller of vertical duct 5 upper end/fan machine to keep the rotating speed of the unsettled balance stop of aircraft automatically.
Mobile, table top operation pipe tunnel 2, the overhead control bar (switch) of the electronic oar/fan machine at horizontal pipeline 3 two ends, when overhead control bar forward time, the electronic oar in the rear end/fan machine spline of pipe tunnel 2, front end screw propeller/flabellum cutting air produces tractive force makes aircraft move forward, when control stalk backward time, the electronic oar in the front end/fan machine spline of pipe tunnel 2, rear end screw propeller/flabellum cutting air produces tractive force makes aircraft move backward, when control stalk left time, the electronic oar of the right-hand member/fan machine spline of horizontal pipeline 3, left end screw propeller/flabellum cutting air produces tractive force makes aircraft be moved to the left, when control stalk to the right time, the electronic oar of the left end/fan machine spline of horizontal pipeline 3, right-hand member screw propeller/flabellum cutting air produces tractive force makes aircraft move right, when total rotating speed control stalk (switch) is at midway location, due to longitudinal tube 2, the two ends electronic oar/fan machine of horizontal pipe 3 operates with identical rotating speed simultaneously, therefore aircraft can be made to keep front and back, the state appearance of left-right balance.
Flight; Accelerate, electronic oar/total the rpm governor of fan machine of operation pipe tunnel 2, horizontal pipeline 3 makes motor speed raise, air pressure in ten shape piping chambers is raised, thus make mobile, flying speed acceleration, [its mechanics principle one is the tractive force that the oar/flabellum cutting air of head end screw propeller/fan machine produces, one be left and right end screw propeller (fan) machine in air inlet duct road, produce the antagonistic force of high pressure gas from mouth of pipe ejection high pressure gas generation after tail in pipeline].When aircraft and air speed of relative movement reach certain value (generation towing force), respond to first device and award execution machine constitutive element device quantity of information, actuating unit can start the electronic oar/flabellum running of vertical duct 5 lower end automatically, make motor gear through 52 simultaneously, the gear teeth 533 drive sliding sleeve 53 to deflect an angle, breach 51 on pipeline 5 is overlapped with breach 531, and the pressed gas that the electronic oar on pipeline 5/fan machine is produced imports ten/field shape pipeline through body pipe 4.
Prepare landing, reduction of speed, table top operation makes pipe tunnel 2, electronic oar/fan machine the rotating speed of horizontal pipeline 3 and vertical duct 5 lowers, gaseous tension in the shape pressure pipeline of ten/field is lowered, motor gear is through 52 simultaneously, the gear teeth 533 drive sliding sleeve 53 to deflect an angle, make pipe tunnel 2 and horizontal pipeline 3 and body pipe 4 obstructed with the pipeline of vertical duct 5, when aircraft and air speed of relative movement arrive certain value slowly, respond to first device and award execution machine constitutive element device quantity of information, actuating unit process can make the electronic oar/fan machine spline of vertical duct 5 lower end automatically, and automatically regulate the electric screw fan machine of vertical duct 5 upper end to keep the rotating speed of the unsettled balance of aircraft.
Landing; Total rpm governor (bar) of the electronic oar/fan machine of table top operation vertical duct 5 is downward, the rotating speed of the electronic oar/fan machine of all vertical duct 5 upper ends is declined, thus aircraft declines, when hand one unclamps total rpm governor (bar), rpm governor (bar) can automatically reset at intermediary information processor, makes the upper end of vertical duct 5 screw propeller/fan machine keep the rotating speed of the unsettled balance stop of aircraft.
During flight, wind power generating set energy automatic operation is powered to main power source, aloft aircraft its fly control and can be manipulated by the rudder blade 9 on pipe end or also can adopt that the mouth of pipe of the longitudinal pipe 2 on body pipe 4, transverse pipe 3, vertical duct 5 is jet manipulates flight attitude.
Landing mode can land on land, also can land at mother ship carrier.The ground that vertical drop damping balancing device can make aircraft drop to injustice keeps balance.
Lower rice root nematode; The aircraft landing water surface, starts dive program, and start water pump to the water filling of setting-out cabin, its directional control operate the same with airflight, be electric propeller/fan machine is at this moment that employing low speed operates.
Its control cabin can be arranged on centre.Compared with bird form wing aircraft of the prior art, aircraft frame structure of the present invention eliminates traditional wing design, make wing and body be fused to entirety and have better aerodynamic arrangement, owing to adopting full motor operation technology, make aircraft can fly also can do maritime navigation and dive as sky, and reduce the exhaust emission to air, marine environment.
Claims (13)
1. a framework design scheme, a kind of shell/body 1, includes floor, partition wall, it is characterized in that, described body 1 is inner, be provided with at least one longitudinal tube 2 connected perpendicular to one another, horizontal pipe 3, its pipeline opening communicates with body 1 space outerpace, the described longitudinal direction 2 connected perpendicular to one another, laterally the pipe two ends of 3 are connected to form a body by body pipe 4, on described body pipe 4, with body 1 inside center for base, be provided with the vertical pipe 5 of symmetrical Boulez, the two ends mouth of pipe of vertical pipe 5 communicates with body 1 space outerpace, described body 1 is inner, take center as base, be provided with the vertical pipe 6 of symmetrical Boulez, the lower end mouth of pipe of vertical pipe 6 communicates with body 1 space outerpace, the upper end of pipeline 6 is provided with pipe close 61, described shell/body 1 is provided with various port 7 as required, floor, partition wall 8.
2. a kind of shell/body according to claim 1, is characterized in that; The described body pipe 4 being provided with vertical pipe 5, its pipeline communicates with pipe tunnel 2, horizontal pipeline 3.
3. a kind of shell/body according to claim 1,2, is characterized in that; Described vertical pipe 5, its wall body is provided with the port 51 communicated with each other with body pipe 4, and is provided with a breach 52, breach is provided with sealable gear chamber, gear is provided with electrical motor.
4. a kind of shell/body according to claim 3, is characterized in that; 5 li, described vertical pipe is provided with one can the sliding sleeve 53 of left-right rotation, the wall body of described sliding sleeve 53 is provided with port 531, the outer wall of described sliding sleeve 53 and the inwall of vertical pipe 5 are provided with circumferential recess, groove is embedded with piston ring seals 532, the outer wall of described sliding sleeve 53 one end is provided with the gear teeth 533.
5. a kind of shell/body according to claim 1, is characterized in that; Described vertical pipe 6, its upper and lower two ends wall body is provided with hole 62, is provided with duct plug 61 in pipeline upper end, 6 li, described pipeline is provided with piston element moving up and down, piston element and pipeline are provided with sealing member each other and seal, and the lower end of pipeline is provided with end cap and fixes, seals.
6. a kind of shell/body according to claim 1, is characterized in that; The described longitudinal pipeline of 2, laterally 3 connected perpendicular to one another, its pipe ends is provided with the less pipeline 21,31 of one section of radial direction, the described longitudinal pipeline of 2, laterally 3 connected perpendicular to one another is provided with breach 22,32 and breach lid to the top pipe wall body at radial less pipeline place, the pipeline 21,31 that described radial direction is less is arranged electric propeller/motor fan and wind (water) power generator group are installed, the vertical duct 5 on described body pipe 4 is arranged electric propeller/motor fan is installed.
7. a kind of shell/body according to claim 1, is characterized in that; Described longitudinal, horizontal pipe end is provided with rudder blade or air grid blade 9.
8. a kind of shell/body according to claim 1, is characterized in that; The shape of described shell/body is the flying saucer bodily form.
9. a kind of shell/body according to claim 1, is characterized in that; The shape of described shell/body is cone-shaped.
10. a kind of shell/body according to claim 1, is characterized in that; The shape of described shell/body is the shuttle bar bodily form.
11. a kind of shell/bodies according to claim 1, is characterized in that; The shape of described shell/body is the streamline bodily form.
12. a kind of shell/bodies according to claim 1, is characterized in that; The shape of described shell/body is the pipe bar bodily form.
13. a kind of shell/bodies according to claim 1, is characterized in that; The shape side of the being bodily form of described shell/body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310436296.7A CN104276280A (en) | 2013-07-11 | 2013-09-14 | Design scheme of framework structure |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320423972 | 2013-07-11 | ||
| CN201320423972.2 | 2013-07-11 | ||
| CN201310436296.7A CN104276280A (en) | 2013-07-11 | 2013-09-14 | Design scheme of framework structure |
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| Publication Number | Publication Date |
|---|---|
| CN104276280A true CN104276280A (en) | 2015-01-14 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310436296.7A Pending CN104276280A (en) | 2013-07-11 | 2013-09-14 | Design scheme of framework structure |
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| CN (1) | CN104276280A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945515A (en) * | 2018-07-18 | 2018-12-07 | 中国人民解放军总参谋部第六十研究所 | A kind of helicopter fuselage frame and its application method with monitoring device |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0439014A2 (en) * | 1990-01-08 | 1991-07-31 | Harald Teinzer | Fan-in-wingedge aircraft |
| CN201334115Y (en) * | 2008-12-24 | 2009-10-28 | 王洪涛 | Ascensional force bay-type aircraft |
| RO127094A2 (en) * | 2010-08-18 | 2012-02-28 | Marius Brebenel | Lenticular aircraft with blades |
| CN202529147U (en) * | 2012-03-12 | 2012-11-14 | 罗才德 | Worm disk-shaped aircraft |
-
2013
- 2013-09-14 CN CN201310436296.7A patent/CN104276280A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0439014A2 (en) * | 1990-01-08 | 1991-07-31 | Harald Teinzer | Fan-in-wingedge aircraft |
| CN201334115Y (en) * | 2008-12-24 | 2009-10-28 | 王洪涛 | Ascensional force bay-type aircraft |
| RO127094A2 (en) * | 2010-08-18 | 2012-02-28 | Marius Brebenel | Lenticular aircraft with blades |
| CN202529147U (en) * | 2012-03-12 | 2012-11-14 | 罗才德 | Worm disk-shaped aircraft |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945515A (en) * | 2018-07-18 | 2018-12-07 | 中国人民解放军总参谋部第六十研究所 | A kind of helicopter fuselage frame and its application method with monitoring device |
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Application publication date: 20150114 |
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