CN110761937A - Oscillating blade motor - Google Patents
Oscillating blade motor Download PDFInfo
- Publication number
- CN110761937A CN110761937A CN201911132124.4A CN201911132124A CN110761937A CN 110761937 A CN110761937 A CN 110761937A CN 201911132124 A CN201911132124 A CN 201911132124A CN 110761937 A CN110761937 A CN 110761937A
- Authority
- CN
- China
- Prior art keywords
- blade
- rotor
- guide rail
- outer edge
- motor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03C—POSITIVE-DISPLACEMENT ENGINES DRIVEN BY LIQUIDS
- F03C2/00—Rotary-piston engines
- F03C2/30—Rotary-piston engines having the characteristics covered by two or more of groups F03C2/02, F03C2/08, F03C2/22, F03C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F03C2/308—Rotary-piston engines having the characteristics covered by two or more of groups F03C2/02, F03C2/08, F03C2/22, F03C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in F03C2/08 and having a hinged member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/40—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member
- F01C1/44—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member with vanes hinged to the inner member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/04—Lubrication
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/08—Rotary pistons
- F01C21/0809—Construction of vanes or vane holders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/08—Rotary pistons
- F01C21/0809—Construction of vanes or vane holders
- F01C21/0818—Vane tracking; control therefor
- F01C21/0827—Vane tracking; control therefor by mechanical means
- F01C21/0836—Vane tracking; control therefor by mechanical means comprising guiding means, e.g. cams, rollers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/10—Outer members for co-operation with rotary pistons; Casings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/18—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Hydraulic Motors (AREA)
Abstract
The invention discloses a swing blade motor which comprises a cylinder body (1), a cylinder cover (2), a rotor (3) and blades (4), wherein the rotor (3) is movably connected with the inner edges of the blades (4), and the blades (4) can rotate and swing relative to the rotor (3); a blade guide rail (5) is arranged on the cylinder cover (2), and the outer edge of the blade (4) is tightly attached to the inner wall of the cylinder body (1) under the action of the blade guide rail (5); the problem of prior art structure itself cause the not enough of motor working property is solved, adopt swing blade and blade guide rail technical structure for the motion of blade is more smooth the reliability higher, and the leakproofness is better, has reduced the frictional force of cylinder body inner wall, more does not have the reverse resistance of machinery itself, has improved the work efficiency of motor greatly.
Description
Technical Field
The invention relates to the technical field of hydraulic and pneumatic power conversion and the like, in particular to a swing blade motor.
Background
The vane motor consists of main parts including cylinder, rotor, cylinder cover, vanes, etc. the vane motor has inner wall of the cylinder and outer wall of the rotor in different radial distances and forms different stressed lengths and areas under the action of pressurized liquid or gas to produce torque to drive the rotor to rotate.
In the existing vane type hydraulic (pneumatic) motor, a rotor is provided with a vane chute, vanes of the vane type hydraulic (pneumatic) motor do reciprocating motion in the radial direction of the rotor relative to the rotor, the overall motion distance of the vanes is the maximum gap between the rotor and a cylinder body, and the movement of the vanes has large kinetic energy loss; the outward movement of the blades needs to be realized by means of external forces such as springs or hydraulic pressure, air pressure and the like in the rotor, and the rotor has a relatively complex structure and large weight; the existing vane type hydraulic (pneumatic) motor has relatively simple vane design, the radial movement of the vane is powered by a spring or hydraulic (pneumatic) pressure outwards, and when the motor works, the movement of the vane may have hysteresis phenomena, which causes hydraulic (pneumatic) leakage and reduces the motor efficiency; the blades move inwards to provide reverse force by the inner wall of the cylinder body, certain friction force can be generated, the direction of the reverse force is not radial but forms a certain angle, and the reverse force provides the radial force for the blades and resistance force for the movement of the blades and the rotor at the same time, so that the motor efficiency is reduced; the blades are installed in the rotor through the sliding grooves, the length of the blades is limited, the maximum gap between the rotor and the cylinder body is relatively small, and the capacity ratio, the flow ratio and the working efficiency of the motor are affected.
In short, the conventional vane-type hydraulic (pneumatic) motor is greatly limited in flow rate, power ratio and energy conversion efficiency due to the restriction of the vane structure, connection and movement mode.
Disclosure of Invention
The invention aims to design a vane motor with a novel structure, which overcomes the defects of motor performance caused by the structure of the prior art, adopts the technical structure of the swing vanes and the vane guide rails, ensures that the movement of the vanes is smoother, the reliability is higher, the sealing performance is better, reduces the friction force of the inner wall of a cylinder body, has no reverse resistance of the machine, and greatly improves the energy conversion efficiency of the motor; meanwhile, the novel technical structure realizes higher liquid (gas) capacity ratio of the vane motor, improves the liquid (gas) flow ratio of the vane motor and further improves the power ratio of the motor.
The invention is realized by the following technical scheme: a swing blade motor comprises a cylinder body, a cylinder cover, a rotor and blades, wherein the rotor is movably connected with the inner edge of the blades, and the blades can rotate and swing relative to the rotor; the cylinder cover is provided with a blade guide rail, and the outer edge of the blade is tightly attached to the inner wall of the cylinder body under the action of the blade guide rail.
In order to better implement the invention, the following structure is adopted in particular: the radial section of the outer wall of the rotor is of a regular polygon structure (a circular structure can be used, but the structure is not limited to the circular structure), the corners of the outer wall of the rotor are provided with hinges connected with the inner edges of the blades, the outer wall of the rotor is connected with the inner edges of the blades through the hinges, the blades can rotate and swing relative to the rotor and around the hinge shafts, reciprocating sliding of the blades in blade grooves of the rotor is avoided, and friction resistance and kinetic energy loss of the blades are reduced.
In order to better implement the invention, the following structure is adopted in particular: the blade adopts an A structure: the outer edge of the blade is embedded with a blade roller (a built-in high-speed bearing), the outer edge of the blade axially penetrates through the outer edge of the blade and the blade roller and is also provided with a blade round shaft, the blade round shaft extends out of two ends of the blade, two ends of the blade round shaft are provided with guide rail matching parts capable of doing track motion in the blade guide rail, the guide rail matching parts adopt guide rail bearings or sliders, the outer wall of the blade roller is contacted with the inner wall of the cylinder body, the blade passes through the guide rail matching parts and the blade roller, under the action of the inner wall of the cylinder body and the blade guide rail, the outer edge part of the blade is tightly attached to the inner wall of the cylinder body, and the; the reliability of the movement of the blade is improved, and the aims of improving the sealing performance of the blade and reducing the leakage of liquid (gas) are fulfilled.
In order to better implement the invention, the following structure is adopted in particular: the blade adopts a structure B: the two ends of the outer edge of each blade are provided with circular shafts for installing a guide rail fitting piece adopting a guide rail bearing or a sliding block, and the motion trail of the outer edge of each blade is controlled under the matching of the guide rails of the blades, so that the outer edge of each blade is tightly attached to the inner wall of the cylinder body.
In order to better implement the invention, the following structure is adopted in particular: the blade adopts a C structure: the blade is equipped with the circle axle along both ends outward for the installation adopts the guide rail fitting piece of guide rail bearing or slider, is equipped with the roller bearing caulking groove at the blade outer edge, is equipped with the blade roller bearing in the roller bearing caulking groove, and this structure can reduce the frictional resistance between blade and the cylinder body.
In order to better implement the invention, the following structure is adopted in particular: the cylinder body is also provided with a discharge port and an inlet, and when the space of a bin chamber formed by the cylinder body, a cylinder cover, a rotor and blades between the two blades reaches the minimum capacity, the outer edge position of the front blade in the rotation direction of the rotor is the initial position of the liquid (gas) inlet, and the outer edge position of the rear blade is the end position of the liquid (gas) discharge port; when the chamber space reaches the maximum capacity, the outer edge position of the latter blade is the end position of the liquid (gas) inlet, the outer edge position of the former blade is the initial position of the liquid (gas) outlet, and during the setting, the inlet and outlet (outlet and inlet) of the liquid (gas) can be arranged on the cylinder body or the cylinder cover. In practical application, the opening position of the inlet and outlet can be properly adjusted according to the rotation speed of the motor and the liquid (gas) pressure because the liquid (gas) can generate hysteresis phenomenon during movement.
In order to better implement the invention, the following structure is adopted in particular: the rotor is also provided with a lubricating oil storage bin and a lubricating oil channel, the lubricating oil channel is communicated with the lubricating oil storage bin and the hinge, and the movable part of the hinge is lubricated by using the centrifugal force generated when the rotor rotates; the blade is also provided with a blade lubricating oil channel (or a blade lubricating oil storage bin is arranged on the blade), the lubricating oil storage bin is communicated with the lubricating oil channel through a hinge to lubricate the movable part of the outer edge of the blade, the lubricating oil storage bin (or the blade lubricating oil storage bin) is communicated with a blade round shaft (or a round shaft) of the outer edge of the blade, a blade roller, a blade rolling shaft, a guide rail matching piece and the like through the hinge and the lubricating oil channel, and when the rotor and the blade rotate, the lubricating oil is sent to the hinge connected with the rotor and the blade, the outer edge of the blade, the round shaft (or the blade round shaft) connected with the blade, the blade roller or the blade rolling shaft, the guide rail matching piece and the like by using; the lubricating oil storage bin can be used for supplementing lubricating oil in the working clearance of the motor through an opening of a cylinder cover; according to the rotating speed of the motor, the lubricating oil supply amount, the maintenance period and the like, the flow limiting part is arranged in the lubricating oil channel, so that effective lubrication and safe operation of equipment are realized.
In order to better implement the invention, the following structure is adopted in particular: the back edge (relative to the moving direction of the blade) of the auxiliary blade is hinged with the outer edge of the main blade by adopting an auxiliary blade hinge, the two ends of the front edge of the auxiliary blade are provided with auxiliary blade round shafts, and the auxiliary blade round shafts are matched with guide rail bearing parts or sliding block parts which can control the front edge of the auxiliary blade to closely cling to the inner wall of the cylinder head to move in a track under the action of a blade guide rail; the guide rail bearing piece or the sliding block piece controls the front edge movement track of the auxiliary blade under the action of the blade guide rail, so that the auxiliary blade is tightly attached to the inner wall of the cylinder body, and the liquid (gas) leakage is prevented at the corresponding section from the discharge port to the inlet at the outer edge of the blade (when the blade is in a back pressure state), thereby playing a good sealing role; when the structure is particularly applied to a vane motor serving as an air pressure motor, the function of sealing the inlet (air) of the vane motor in advance can be achieved, the expansion pressure of the air is fully utilized to do work, and the purpose of improving the energy conversion efficiency of the vane motor is achieved.
In order to better implement the invention, the following structure is adopted in particular: the inner side of the blade guide rail on the cylinder cover and the corresponding section of the outer edge of the blade from the discharge port to the inlet are provided with back pressure supporting springs, so that the gap between the blade and the inner wall of the cylinder body is reduced, and the sealing property between the outer edge of the blade and the inner wall of the cylinder body is improved.
In order to better implement the invention, the following structure is adopted in particular: the blade guide rail of the cylinder cover is a groove, and the blade guide rail is positioned between the inner wall of the cylinder body and the outer wall of the rotor and close to one side of the inner wall of the cylinder body; the guide rail inner wall of the blade guide rail of the cylinder cover is matched with the guide rail bearing, when the guide rail inner wall is arranged, the inner wall of the cylinder body can replace the outer wall of the guide rail, and the width of the guide rail groove is slightly larger than the diameter of the guide rail bearing, so that the guide rail bearing is prevented from generating high-speed friction when the positive pressure section and the negative pressure section of the blade rotate in opposite directions; the outer groove wall mainly plays a role in sealing.
In order to better implement the invention, the following structure is adopted in particular: the cylinder body adopts a structure that the middle part of the radial section is a straight line section, and the two ends of the radial section are curved sections, so that the moving track of the blade is more reasonable, the liquid (gas) flow rate ratio of the blade motor is improved to the maximum extent, and the power ratio of the blade motor is improved.
Compared with the prior art, the invention has the following advantages and beneficial effects:
the present invention relates to a hydraulic and pneumatic vane motor, and is characterized by that in the radial direction of rotor, relative to the rotor, its vane can implement reciprocating motion, and the moving distance of whole vane is the maximum gap between rotor and cylinder body.
In the existing hydraulic and pneumatic vane motor, a rotor is provided with vane grooves, a spring needs to be installed or hydraulic and pneumatic channels need to be designed, and the rotor is relatively complex in structure and heavy; the rotor of the invention has the advantages of relatively simple structure, simple manufacturing process, relatively low cost, easy maintenance and light weight.
The existing hydraulic and pneumatic vane motor has relatively simple vane design, the radial movement of the vane is powered by a spring or liquid (gas) pressure, and when the motor works, the vane movement may generate hysteresis, which causes liquid (gas) leakage and reduces the motor efficiency; the vanes provide a reverse force inwards from the inner wall of the cylinder body, a certain friction force can be generated, the direction of the reverse force is not radial, but forms a certain angle with the vanes, and the reverse force provides a radial force for the vanes, and simultaneously provides resistance for the movement of the vanes and the rotor, so that the motor efficiency is reduced; the invention designs the blade guide rail, the guide rail fitting piece, the blade roller or the blade rolling shaft which are matched, so that the motion of the blade is smoother, the reliability is higher, the sealing performance is better, the friction force of the inner wall of the cylinder body is reduced, the reverse resistance of the machine is avoided, and the working efficiency of the motor is greatly improved; although the blade of the invention has relatively complex design, compared with the complexity and the difficulty of the manufacturing process of the traditional blade motor rotor, the blade is still simple and easy, and the manufacturing cost is also reduced to a certain extent.
The conventional vane type hydraulic (pneumatic) motor has a small capacity of a hydraulic (pneumatic) chamber formed between vanes due to the restriction of a vane structure, and the flow rate ratio and the power ratio of the motor are greatly limited. According to the vane motor, the capacity of the liquid (gas) chamber formed between the vanes is large, and the power of the motor can be greatly improved under the condition that the volumes of the motors are similar.
Compared with the traditional vane motor, the vane motor optimizes the liquid (gas) inlet and outlet, and makes qualitative design on the opening position and the ending position of the inlet and outlet, thereby being beneficial to fully utilizing the liquid (gas) to generate torque and power and improving the efficiency of the vane motor.
The invention comprises a plurality of chambers for working, more than two chambers are always in a liquid (gas) inlet working state, and a blocking state does not exist; the blade works reliably under the action of the blade guide rail; the blades are paired and arranged in an axisymmetric manner, and the whole motor is basically in a shaft balance state, so that the vibration and the noise of the blade motor can be well controlled.
The invention can directly generate rotary power by utilizing pressurized liquid (water and oil) or gas (including high-pressure fuel gas and high-pressure steam generated by fuel oil and fuel gas), and has higher energy conversion efficiency. The device can be widely used for generating electricity or driving other mechanical devices, and can also be used as a liquid and air pump base structure.
Compared with the hydraulic and pneumatic motors which are widely applied at present, the invention has the advantages of simple structure, reliable work, convenient maintenance, simple manufacturing and mounting process and low manufacturing cost, and has the obvious characteristics of high power ratio and high energy conversion efficiency.
Drawings
Fig. 1 is a schematic view of the structure of the present invention (first operating state).
Fig. 2 is a schematic view of the structure of the present invention (second operation state).
Fig. 3 is a schematic structural view (third operating state) of the present invention.
Fig. 4 is a schematic structural view (fourth operation state) of the present invention.
Fig. 5 is a schematic view of a rotor according to the present invention.
Fig. 6 is a schematic structural view of the cylinder head according to the present invention.
Fig. 7 is a schematic view of the structure of the blade (adopting a roller) of the invention.
Fig. 8 is a schematic view of the structure of the blade (using a roller) according to the present invention.
Fig. 9 is a schematic structural view of a blade (third blade) according to the invention.
Fig. 10 is a schematic view of the structure of the sub-vane (back pressure seal vane).
Figure 11 is a schematic view of the arrangement of the back pressure support springs of the present invention.
FIG. 12 is a front view of the liquid (gas) inlet and outlet (A is the outlet and B is the inlet) according to the present invention.
Fig. 13 is a schematic view of the structure of the present invention (including the secondary blade structure).
Fig. 14 is a schematic diagram of a modified structure of the present invention (rotor section of a is pentagonal, cylinder section of B is elliptical).
FIG. 15 is a schematic view of a vane motor having a cylindrical cylinder, a cylindrical rotor, and arcuate vanes, with the cylinder and rotor in an eccentric position.
The device comprises a cylinder body 1, a cylinder cover 2, a rotor 3, blades 4, blade guide rails 5, a lubricating oil storage bin 6, a lubricating oil channel 7, a hinge 8, a hinge 9, a hinge rotating shaft 10, a blade round shaft 11, a guide rail matching piece 12, a blade roller 13, a blade lubricating oil channel 14, auxiliary blades 15, auxiliary blade hinges 16, auxiliary blade round shafts 17, back pressure supporting springs 18, a discharge port 19, an inlet 20, a fixing hole 21 and a round shaft 22.
Detailed Description
The present invention will be described in further detail with reference to examples, but the embodiments of the present invention are not limited thereto.
In order to make the objects, technical solutions and advantages of the embodiments of the present invention more apparent, the technical solutions of the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings of the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all embodiments of the present invention. All other embodiments, which can be obtained by a person skilled in the art without any inventive step based on the embodiments of the present invention, are within the scope of the present invention. Thus, the following detailed description of the embodiments of the present invention, presented in the figures, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention.
In the description of the present invention, it is to be understood that the terms etc. indicate orientations or positional relationships based on those shown in the drawings only for the convenience of describing the present invention and simplifying the description, but do not indicate or imply that the referred devices or elements must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
In the present invention, unless otherwise expressly stated or limited, "above" or "below" a first feature means that the first and second features are in direct contact, or that the first and second features are not in direct contact but are in contact with each other via another feature therebetween. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
It is worth noting that: in the present application, when it is necessary to apply the known technology or the conventional technology in the field, the applicant may have the case that the known technology or/and the conventional technology is not specifically described in the text, but the technical means is not specifically disclosed in the text, and the present application is considered to be not in compliance with the twenty-sixth clause of the patent law.
Example 1:
as shown in fig. 1, 5, 6, and 7, a vane motor is mainly composed of a cylinder 1 (stator ring), two cylinder heads 2, a rotor 3, six vanes 4, six pairs of guide bearings, six vane rollers 12, and the like.
As shown in fig. 1, a cylinder body 1 is cylindrical, is an external structural member of the motor, and can be fixed to a cylinder cover 2 through a flange; the section of the cylinder body 1 is shaped like an annular runway (the invention is not limited to be similar to the annular runway, and can also be round, oval and the like); the cylinder body 1 is provided with a liquid (gas) inlet and outlet (a discharge port 19 and an inlet 20), when the space of a bin chamber formed by the cylinder body 1, the rotor 3, the cylinder cover 2 and the blades 4 reaches the minimum capacity between the two blades 4, the outer edge position of the previous blade 4 in the rotation direction of the rotor 3 is the initial position of the inlet 20, and the outer edge position of the next blade 4 is the end position of the discharge port 19; when the chamber space reaches the maximum capacity, the trailing vane 4 outer edge position is the end position of the inlet 20 and the leading vane outer edge or vane roller 12 position is the start position of the discharge 19.
As shown in fig. 6, the cylinder cover 2 is a plate with a straight line and a circular arc shape, and is an outer structural member of the vane motor to fix the vane motor; a fixing hole 21 of the rotor rotating shaft is arranged in the cylinder cover 2, and the rotor 3 is fixed in the cylinder body 1 through the rotor rotating shaft; the cylinder cover is provided with a blade guide rail 5, the blade guide rail 5 is an annular groove and is used for inserting a guide rail bearing of the blade, and the guide rail bearing is matched with the inner wall of the cylinder body 1 to control the motion track of the outer edge of the blade 4.
As shown in fig. 1 and 5, the rotor 3 is in a diamond column shape (but not limited thereto, it may also be in a circular shape), the cross section of the outer wall is in a regular hexagon shape (but not limited thereto, it may also be in a regular hexagon shape, it may also be in any polygon shape), the two ends of the rotor 3 are cylindrical rotor rotating shafts, which pass through the fixing holes 21 in the cylinder cover 2, the rotor 3 is placed at the central position in the cylinder body 1, so that the rotor 3 and the cylinder body 1 are axially kept the same, and the rotor 3 is limited to make a rotational movement relative to the cylinder body; one end of the rotor rotating shaft extends out of the cylinder cover 2 and is a torque and power output part; on the cross section, the different rotor radial directions form the distance difference between the inner wall of the cylinder body 1 and the outer wall of the rotor 3; hinge 8 is established to 3 outer wall edges and corners of rotor, and all hinges 8 equidistance distribute on the rotor outer wall, and hinge 8 cooperation hinge pivot 9 is used for linking with blade 4 and makes blade 4 swing on rotor 3.
As shown in fig. 7, the blade 4 is rectangular plate-shaped (not limited to plate-shaped), the inner edge of the blade is provided with a hinge 8, and the outer edge of the blade 4 adopts a blade with a structure a: the blades 4 are positioned between the cylinder body 1 and the rotor 3 and between the two cylinder covers 2, the inner edges of the blades 4 are connected to the rotor 3 in a hinge mode through hinges 8, and the blades can rotate and swing between the cylinder body 1 and the rotor 3; a blade round shaft 10 is arranged at the outer edge of the blade 4, a blade roller 12 (a built-in high-speed bearing) is embedded at the outer edge of the blade 4, and the blade round shaft 10 axially penetrates through the outer edge of the blade 4 and the blade roller 12 and extends out of the two ends of the blade 4; part of fixed guide rail fitting parts (guide rail bearings are adopted here) 11 extending from both ends of the blade circular shaft 10 control the motion track of the outer edge of the blade 4 under the matching of the blade guide rail 5; the vanes 4 make the outer edges of the vanes 4 tightly attached to the inner wall of the cylinder body 1 under the action of the inner wall of the cylinder body 1 and the vane guide rail 5 through the guide rail bearing and the vane roller 12. The diameter of the guide rail bearing is set slightly smaller than the groove width of the blade guide 5.
The working principle of the embodiment is as follows:
as shown in figure 1, a space formed by the cylinder body 1, the rotor 3, the cylinder cover 2 and the blades 4 is a motor liquid (gas) chamber between the two blades 4, when the chamber is in a liquid (gas) pressing-in stage, in the rotating direction of the rotor 3, under the action of the liquid (gas) pressure of the chamber, the circumferential force of the previous blade 4 conducted to the hinge 8 is greater than the reverse force of the next blade 4, so that a pressure difference of the rotor 3 in the rotating direction is formed, a torque is formed to push the rotor 3 to rotate, the chamber is in an acting state at the stage, when the chamber is in a liquid (gas) discharging stage, due to the release of the liquid (gas) pressure of the chamber, the chamber pressure is smaller, the reverse pressure formed by the previous blade 4 and the next blade 4 of the chambers ③ and ⑥ is smaller, and the resistance formed by the rotation of the rotor 3 is smaller.
The working process of the embodiment is as follows:
as shown in fig. 1, capacities of the chambers ① and ④ are at a minimum state, liquid (gas) in the chambers is at a critical point state of discharging to pressing, the chambers ② and ⑤ are at a working state of continuously pressing liquid (gas), and the chambers ③ and ⑥ are at a continuous discharging state of liquid (gas).
As shown in fig. 2, when the rotor 3 rotates a certain angle, the chambers ①, ④ are continuously in the working state of pressing in liquid (gas) from the previous working state, the capacities of the chambers ②, ⑤ reach the maximum, the liquid (gas) in the chambers is at the critical point of pressing in, transferring out, the working state of the chambers is finished, and the liquid (gas) in the chambers ③, ⑥ are continuously out.
As shown in fig. 3, when the rotor continues to rotate by a certain angle, chambers ① and ④ are in a state of continuously pressing in and doing work, chambers ② and ⑤ are in a state of continuously discharging liquid (gas) from the previous working state, and chambers ③ and ⑥ are in a state of continuously discharging liquid (gas).
As shown in fig. 4, when the rotor rotates a certain angle, the chambers ①, ④ are in the state of continuously pressing in and applying work, and enter the initial (shown in fig. 1) states of chambers ②, ⑤, the chambers ②, ⑤ are in the state of continuously discharging liquid (gas), and enter the initial states of chambers ③, ⑥, the capacities of the chambers ③, ⑥ reach the minimum, and the chambers are at the critical point of liquid (gas) discharging and pressing in, and enter the initial states of chambers ④ 0, ④ 1.
The working state of the vane motor is the working process that the rotor 3 rotates by 60 degrees; when the rotor 3 rotates 180 degrees, each bin can complete the complete process from liquid (gas) entering to discharge or from discharge to entering, namely each bin can complete a complete working process; the rotor 3 rotates 360 degrees, and each chamber can complete two complete working processes.
When the bin is in a working state, the front blade 4 of the bin is in a positive pressure state, and the front blade 4 is tightly attached to the inner wall of the cylinder body 1 due to the liquid (gas) pressure because the blade 4 and the inner wall of the cylinder body 1 form a certain angle, so that a good sealing effect is achieved.
As the preferred embodiment, the defect that the energy conversion efficiency of the motor is low due to the structure of the prior art of the vane motor is overcome, the novel structure is adopted, the movement of the vanes is smoother, the reliability is higher, the sealing performance is better, and the energy conversion efficiency and the power of the motor can be greatly improved.
The vane motor is suitable for power plant powered by pressurized liquid.
Example 2:
the present embodiment is further optimized based on embodiment 1, and the same parts as those in the foregoing technical solutions will not be described herein again, as shown in fig. 11, in order to better implement the present invention, the following structure is particularly adopted: and a back pressure supporting spring 18 is arranged at the corresponding section (the blade 4 is in a back pressure state) from the discharge port 19 to the inlet 20 at the inner side of the blade guide rail 5 of the cylinder cover 2 and the outer edge of the blade 4, so that the gap between the blade 4 and the inner wall of the cylinder body 1 is reduced, and the sealing property of the blade motor is improved.
When the vane 4 is in a back pressure state, the gap caused by mechanical wear and the action of the liquid (gas) pressure may cause liquid (gas) leakage, and the scheme is an optimized scheme aiming at the problem.
As a preferred embodiment, the present solution aims to further improve the sealing performance and motor efficiency of the motor.
Example 3:
the present embodiment is further optimized on the basis of embodiment 1, and the same parts as those in the foregoing technical solutions will not be described herein again, as shown in fig. 10 and 13, in order to better implement the present invention, the following structure is particularly adopted: an auxiliary blade 15 (back pressure sealing blade) is connected with the outer edge of the blade 4 and the movement front of the blade 4, the rear edge (relative to the movement direction of the blade) of the auxiliary blade 15 is connected with the outer edge of the blade 4 by an auxiliary blade hinge 16, auxiliary blade circular shafts 17 arranged at two ends of the front edge of the auxiliary blade 15 are matched with a guide rail bearing piece or a sliding block piece, the movement track of the front edge of the auxiliary blade 15 is controlled under the action of a blade guide rail 5 to be tightly attached to the inner wall of the cylinder body 1, and when the auxiliary blade 15 runs on the corresponding section of the outer edge of the blade 4, which is positioned from a discharge port 19 to an inlet 20 (the blade 4 is in a back pressure state), liquid (gas) leakage is prevented; when the structure is particularly applied to a vane motor serving as a pneumatic motor, the function of sealing the air inlet (inlet 20) of the motor in advance can be achieved, the air expansion pressure is fully utilized to do work, and the purpose of improving the efficiency of the pneumatic motor is achieved.
The gas is different from the liquid, the compressed and expanded states exist, the compressed gas has certain energy, the scheme seals the inlet 20 in advance through the auxiliary blade, and the opening positions of the inlet and the outlet are adjusted according to the gas pressure and the expansion rate, so that the energy released by the expansion of the gas can be effectively utilized.
The scheme has a state that an air compression inlet is completely closed, and can be solved by designing a special starting air pressure channel, for example, the starting air pressure channel is designed between the inlet 20 and the outlet 19 of the rotor 3 in the rotating direction, and can be closed after the motor is started.
When the vane 4 is in a back pressure state, the gap caused by mechanical wear and the action of the liquid (gas) pressure can cause liquid (gas) leakage, and the scheme is another optimized scheme aiming at the problem.
As a preferred embodiment, the motor has better sealing performance, can fully utilize gas expansion pressure to do work, has higher energy conversion efficiency, and is suitable for the field with higher requirement on energy conversion efficiency or applied to gas with pressure.
Example 4:
the present embodiment is further optimized on the basis of the above embodiments, and the same parts as those in the foregoing technical solutions will not be described again here, as shown in fig. 5 and 7, in order to better implement the present invention, the following structures are particularly adopted: the lubricating oil lubrication device is characterized in that a lubricating oil storage bin 6 and a lubricating oil channel 7 are arranged on the rotor 3, a vane lubricating oil channel 14 is arranged on the vane 4, the lubricating oil storage bin 6, the hinge 8, the guide rail bearing and the vane roller 12 are communicated through the lubricating oil channel 7 and the vane lubricating oil channel 14, and when the rotor 3 and the vane 4 rotate, lubricating oil is delivered to the hinge 8 connected with the rotor 3 and the vane 4, the vane roller 12 connected with the vane 4, the guide rail bearing and the like by utilizing centrifugal force, so that lubrication of movable parts is realized.
As a preferred embodiment, the scheme aims to improve the convenience of equipment maintenance, reduce equipment abrasion and prolong the service life of the equipment.
In the attached drawings 1-4, the arrow of the square frame is the flowing direction of liquid (gas), and the arrow direction on the rotor 3 is the rotating direction of the rotor.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in any way, and all simple modifications and equivalent variations of the above embodiments according to the technical spirit of the present invention are within the scope of the present invention.
Claims (9)
1. The utility model provides a swing blade motor, includes cylinder body (1), cylinder cap (2), rotor (3) and blade (4), its characterized in that: the rotor (3) is movably connected with the inner edge of the blade (4), and the blade (4) can rotate and swing relative to the rotor (3); the cylinder cover (2) is provided with a blade guide rail (5), and the outer edge of the blade (4) is tightly attached to the inner wall of the cylinder body (1) under the action of the blade guide rail (5).
2. A swing blade motor as claimed in claim 1, wherein: the radial section of the outer wall of the rotor (3) is of a regular polygon structure, and a hinge (8) connected with the inner edge of the blade (4) is arranged at the corner of the outer wall of the rotor (3).
3. A swing blade motor as claimed in claim 1, wherein: the blade guide rail (5) of the cylinder cover (2) is a groove, and the blade guide rail (5) is located between the inner wall of the cylinder body (1) and the outer wall of the rotor (3) and close to one side of the inner wall of the cylinder body (1).
4. A swing blade motor as claimed in claim 2, wherein: the rotor (2) is provided with a lubricating oil storage bin (6) and a lubricating oil channel (7), the lubricating oil channel (7) is communicated with the lubricating oil storage bin (6) and the hinge (8), and the movable part is lubricated by centrifugal force generated when the rotor (3) rotates.
5. An oscillating vane motor as defined in claim 4 wherein: the blade (4) is provided with a blade lubricating oil channel (14) which is communicated with the lubricating oil channel (7) through a hinge (8) to lubricate the movable part of the outer edge of the blade (4).
6. A swing blade motor according to any one of claims 1 to 3, wherein: the outer edge of blade (4) is inlayed and is equipped with blade cylinder (12), the outer edge of blade (4) is gone up the axial and is run through blade (4) outer edge and blade cylinder (12) and still be provided with blade circle axle (10) outside blade (4), and blade circle axle (10) extend the both ends of blade (4), be provided with on the both ends of blade circle axle (10) and be the guide rail fitting piece (11) of orbit motion in blade guide rail (5), the outer wall of blade cylinder (12) contacts with the inner wall of cylinder body (1).
7. A swing blade motor according to any one of claims 1 to 3, wherein: the outer edge and the motion front of the blade (4) are also connected with an auxiliary blade (15), the rear edge of the motion direction of the auxiliary blade (15) is connected with the outer edge of the blade (4) by an auxiliary blade hinge (16), the two ends of the front edge of the auxiliary blade (15) are provided with auxiliary blade round shafts (17), and the auxiliary blade round shafts (17) are matched with guide rail bearing parts or sliding block parts which can control the front edge of the auxiliary blade (15) to be tightly attached to the inner wall of the cylinder body (1) to move along a track under the action of the blade guide rail (5).
8. A swing blade motor according to any one of claims 1 to 3, wherein: the cylinder body (1) is further provided with a discharge port (19) and an inlet (20), and when the space of a bin formed by the cylinder body (1), a cylinder cover (2), a rotor (3) and blades (4) between the two blades (4) reaches the minimum capacity, the outer edge position of the previous blade (4) in the rotation direction of the rotor (3) is the starting position of the inlet (20), and the outer edge position of the next blade (4) is the ending position of the discharge port (19); when the chamber space reaches the maximum capacity, the outer edge position of the next blade (4) is the end position of the inlet (20), and the outer edge position of the previous blade (4) is the starting position of the discharge opening (19).
9. A swing blade motor as claimed in claims 1 to 3, wherein: and a back pressure supporting spring (18) is arranged on the inner side of the blade guide rail (5) on the cylinder cover (2) and on the corresponding section of the outer edge of the blade (4) from the discharge port (19) to the inlet (20).
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201911132124.4A CN110761937A (en) | 2019-11-19 | 2019-11-19 | Oscillating blade motor |
CN202010645345.8A CN111608851A (en) | 2019-11-19 | 2020-07-07 | Hydraulic power device with swinging blades |
PCT/CN2020/127509 WO2021098542A1 (en) | 2019-11-19 | 2020-11-09 | Swing blade-type hydraulic power device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201911132124.4A CN110761937A (en) | 2019-11-19 | 2019-11-19 | Oscillating blade motor |
Publications (1)
Publication Number | Publication Date |
---|---|
CN110761937A true CN110761937A (en) | 2020-02-07 |
Family
ID=69338466
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201911132124.4A Pending CN110761937A (en) | 2019-11-19 | 2019-11-19 | Oscillating blade motor |
CN202010645345.8A Pending CN111608851A (en) | 2019-11-19 | 2020-07-07 | Hydraulic power device with swinging blades |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202010645345.8A Pending CN111608851A (en) | 2019-11-19 | 2020-07-07 | Hydraulic power device with swinging blades |
Country Status (2)
Country | Link |
---|---|
CN (2) | CN110761937A (en) |
WO (1) | WO2021098542A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021098542A1 (en) * | 2019-11-19 | 2021-05-27 | 李光惠 | Swing blade-type hydraulic power device |
CN115324889A (en) * | 2022-08-31 | 2022-11-11 | 安徽理工大学 | Novel displacement pump |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116357407B (en) * | 2023-05-31 | 2023-08-18 | 日照职业技术学院 | Centrifugal constant speed device for steam turbine |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8404335D0 (en) * | 1984-02-18 | 1984-03-21 | Collier P | Fluid machines |
EP0601218B1 (en) * | 1992-11-27 | 1997-01-22 | Andro Caric | Rotary piston machine |
CN1163651A (en) * | 1994-08-23 | 1997-10-29 | 丹提卡特国际有限公司 | Fluid reaction device |
CN1138136A (en) * | 1995-06-12 | 1996-12-18 | 吕文杰 | Rear-front vane rotor engine |
US6082324A (en) * | 1998-09-05 | 2000-07-04 | Liu; Nien-Tzu | Rotary internal combustion engine |
NO20043203D0 (en) * | 2004-07-28 | 2004-07-28 | Reidar Sorby | Rotating machine |
GB0518573D0 (en) * | 2005-09-12 | 2005-10-19 | Phoenix Product Dev Ltd | Self-aligning rotary piston machine |
CN200964870Y (en) * | 2006-10-31 | 2007-10-24 | 黄庆培 | Rotary vane piston |
CN101397914A (en) * | 2007-09-24 | 2009-04-01 | 陈军 | Novel mass flow blade mechanism |
CA2677006A1 (en) * | 2009-08-28 | 2011-02-28 | Jean Pierre Hofman | Hydraulic generator (liquid flow generator) |
CN102094727B (en) * | 2010-12-02 | 2014-08-27 | 无锡中阳新能源科技有限公司 | Compressed air engine and optimization integrated system |
RU2538148C2 (en) * | 2012-11-07 | 2015-01-10 | Рустем Наилевич Тимерзянов | Rotary-vane device |
CN103912489B (en) * | 2014-03-10 | 2016-05-25 | 汤斌 | Eccentric moving vane pump |
CN104100300B (en) * | 2014-07-08 | 2017-01-18 | 黄石巨丰机械制造有限公司 | Power transmission device and pneumatic motor |
CN104454018A (en) * | 2014-11-29 | 2015-03-25 | 白明 | Rotary power machine |
CN105201557A (en) * | 2015-09-21 | 2015-12-30 | 重庆大学 | Rotary blade machine |
CN107218082B (en) * | 2017-06-16 | 2019-05-03 | 盐城市东荣石油机械有限公司 | A kind of pneumatic vane motor with lubricant passage way |
CN107939450A (en) * | 2017-11-24 | 2018-04-20 | 李四屯 | Multipurpose vane Mechanical-power-producing mechanism |
CN110761937A (en) * | 2019-11-19 | 2020-02-07 | 李光惠 | Oscillating blade motor |
CN212671984U (en) * | 2019-11-19 | 2021-03-09 | 李光惠 | Hydraulic power device with swinging blades |
-
2019
- 2019-11-19 CN CN201911132124.4A patent/CN110761937A/en active Pending
-
2020
- 2020-07-07 CN CN202010645345.8A patent/CN111608851A/en active Pending
- 2020-11-09 WO PCT/CN2020/127509 patent/WO2021098542A1/en active Application Filing
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021098542A1 (en) * | 2019-11-19 | 2021-05-27 | 李光惠 | Swing blade-type hydraulic power device |
CN115324889A (en) * | 2022-08-31 | 2022-11-11 | 安徽理工大学 | Novel displacement pump |
CN115324889B (en) * | 2022-08-31 | 2024-03-29 | 安徽理工大学 | Displacement pump |
Also Published As
Publication number | Publication date |
---|---|
WO2021098542A1 (en) | 2021-05-27 |
CN111608851A (en) | 2020-09-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN110761937A (en) | Oscillating blade motor | |
US9322272B2 (en) | Planetary rotary type fluid motor or engine and compressor or pump | |
EP2205831B1 (en) | A rotary fluid-displacement assembly | |
CN201568303U (en) | Symmetrical balance type synchronous rotating compression machine | |
EA013630B1 (en) | Vane machine with stationary and rotating cylinder parts | |
CN112211831A (en) | Air suspension high-speed centrifugal compressor | |
CN101498306B (en) | Rotary compressor | |
CN212671984U (en) | Hydraulic power device with swinging blades | |
CN105697366A (en) | Blade type sea water pump | |
CN103423150A (en) | Rotor fluid mechanical transfiguration mechanism | |
CN201144808Y (en) | Water cooled oil-free lubrication sliding blade compressor | |
CN112610438A (en) | Piston pump | |
CN103492720B (en) | The compressor cooled down is carried out by the liquid jet | |
CN201155460Y (en) | Rotary compressor | |
CN102278305A (en) | Scroll type automobile air-conditioner compressor | |
WO2011015122A1 (en) | Conversion device of mechanical motion and fluid motion | |
CN219472332U (en) | Flexible sealing structure of vacuum pump | |
CN111997748A (en) | Rolling sealed rotor engine | |
WO2016004384A1 (en) | Rotary compressor having a discharge valve assembly | |
CN220081667U (en) | Pump head of needle roller type vortex compressor | |
CN218030609U (en) | Torsional spring return rolling friction scraper fan | |
CN115163200B (en) | Rotary piston steam engine | |
RU2804163C1 (en) | Multifunctional ellipsoidal three-blade rotor machine | |
CN204126893U (en) | Air condition compressor | |
CN109488622A (en) | A kind of big flow air intake structure of magnetic suspension air blower |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20200207 |
|
WD01 | Invention patent application deemed withdrawn after publication |