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CN101865089A - Planet hoisting linkage device - Google Patents

Planet hoisting linkage device Download PDF

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Publication number
CN101865089A
CN101865089A CN200910106630A CN200910106630A CN101865089A CN 101865089 A CN101865089 A CN 101865089A CN 200910106630 A CN200910106630 A CN 200910106630A CN 200910106630 A CN200910106630 A CN 200910106630A CN 101865089 A CN101865089 A CN 101865089A
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CN
China
Prior art keywords
fin
shaft
axle
hoisting
sprocket wheel
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Pending
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CN200910106630A
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Chinese (zh)
Inventor
周跃平
周红球
周星果
尹雄鹰
周文珺
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周文珺
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Priority to CN200910106630A priority Critical patent/CN101865089A/en
Publication of CN101865089A publication Critical patent/CN101865089A/en
Pending legal-status Critical Current

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    • Y02E10/722

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Abstract

The invention relates to a planet hoisting linkage device, which can be used in rotary reducing flapping wing motive power equipment equipped by tools for electricity generation, transportation and the like. The planet hoisting linkage device comprises a gear set 1, a shaft 2, a bearing 3, a center shaft 4, a belt pulley 5, a rotating wheel 6, a belt 7, a belt 8 and a belt pulley 9, wherein the shaft 2 and the bearing 3 form a hoisting shaft mechanism, the belt pulley 5, the belt 7, the belt pulley 9 and the gear set 1 form a set of linkage mechanism, and the movement of a pair of hoisting shaft mechanisms are mutually controlled through the linkage mechanism. When the shaft of one set of the hoisting shaft mechanism does autorotation, the shaft of the other relevant hoisting shaft mechanism is driven through the linkage mechanism to do the autorotation in the opposite direction. The rotating wheel 6 and the center shaft 4 can rotate around the center axial line of the center shaft 4, and four sets of hoisting shaft mechanisms and two sets of linkage mechanisms also simultaneously rotate around the center axial line of the center shaft 4. The invention can be used for electricity generation and traffic transportation tools, and has the effects of high reliability, light weight, high efficiency and the like.

Description

Planet hoisting linkage device
The present invention relates to can be used for a kind of planet hoisting linkage device in the revolution reducing flapping wing power equipment of tool configuration such as generating electricity and transport.
The scheme that I provide a kind of revolving flapping wings reducing machine on December 14th, 2008, application number is 2008101884409, this scheme provides and can be used for wind-power electricity generation, a kind of new power technology such as hydroelectric power and communications and transportation, adopt flexible material such as parachute fabric etc. to rotatablely move in this scheme around same central axis reducing, realize power generating equipment or required power-assisted of facilities for transport and communication or transmission of power, adopt winding plant to control the motion of flexible material in this scheme, but the winding plant in this scheme has following deficiency: winding plant in this scheme adopts the spring technology or the linkage technique be made up of motor and generator or linked by hydraulic pump motor and to control the folding and unfolding of fin, and the elevator control technique of this scheme has following deficiency:
Under bigger wind-force and hydraulic action, spring is difficult to the folding and unfolding of control fin, and fin may occur and other part tied up in knots, breaks down easily;
In this scheme, fin adopts hydraulic pump motor to control the folding and unfolding of fin, and fin revolves and turns around, and the positive and negative conversion of hydraulic pump motor palpus once, the rotating speed of hydraulic pump motor is the several times of fin rotational speed even tens times, like this, hydraulic pump motor forward and reverse two states hockets, like this, this scheme is very high to the hydraulic pump motor quality requirement under fast state, hydraulic pump motor is easy to generate fault under fast state, and therefore, this scheme is not suitable under the high-speed motion state.
In this scheme, fin also adopts the electronic control technology of being made up of motor and generator, because stretching out, fin drives generator rotation generating under waterpower and wind-force effect, regain under the ordering about of motor, the rotating speed of motor and generator is the several times of fin rotational speed even tens times, under fast state, generator and motor also must stop and the alternately conversion of high speed rotating state moment, therefore, this scheme is very high to the quality requirement of motor, generator, is not suitable for high-speed motion state.
Existing winding plant is generally reel and rotates the purpose that reaches the remote folding and unfolding of control object around the reel axle center, the axle or the axle bed of reel generally are fixed on the bearing, therefore, general hoisting mechanism has only a reel, the axle or the axle bed of reel also are fixed on the bearing basically, bearing can move, and generally can not rotate; Even have the hoisting mechanism of a plurality of reels, the axle or the axle bed of each reel also are fixed on the bearing basically, bearing can move, generally can not rotate, also not interlock control rotation between the reel, therefore, existing hoisting mechanism is difficult in generating or automobile or boats and ships or aircraft power equipment or the power assistive device.
The present invention seeks to provides a kind of planet hoisting linkage device for the planet hoisting device of fin rotary variable-diameter motion.
Planet hoisting linkage device involved in the present invention be this realize, it is characterized in that having runner; It is characterized in that having and comprise 2 covers or comprise the elevator axis mechanism of forming by axle more than 2 covers that the elevator axis mechanism links to each other with runner; It is characterized in that having 1 cover or the above linking mechanism of 1 cover, every cover linking mechanism overlaps above elevator axis mechanism with 2 covers or 2 and links to each other.
Its working principle is as follows: runner can rotate around its central axis, the elevator axis mechanism is distributed on the runner, the elevator axis mechanism also can rotate around its central axis with runner, the axle of elevator axis mechanism can rotate around the central axis of oneself, be called rotation herein, the axle of elevator axis mechanism is similar to the same central axis rotation that also centers on self when rotating with runner of planetary motion.
It is to be mutually related that 2 covers or the above elevator axis mechanism of 2 covers are arranged in the elevator axis mechanism, realizes that by linking mechanism linking mechanism has following three kinds of schemes:
One of reel linkage control device scheme: comprise the chain type linking mechanism of forming by sprocket wheel and chain;
Two of reel linkage control device scheme: by the gear type linking mechanism that comprises that gear is formed;
Three of reel linkage control device scheme: comprise the belt type linking mechanism of forming by belt pulley and belt.
The axle of elevator axis mechanism generally is exactly the reel of hoisting mechanism or the transmission shaft that links to each other with the hoisting mechanism reel.
The rotation of other one or more reel is controlled in the rotation of one or more reels in the planet hoisting mechanism by linking mechanism like this.
The invention will be further described below in conjunction with embodiment and embodiment's application examples and accompanying drawing.
Shown in the accompanying drawing 1 is one of embodiments of the invention.
Shown in the accompanying drawing 2 is two of embodiments of the invention.
Shown in the accompanying drawing 3 is three of embodiments of the invention.
Shown in the accompanying drawing 4 is one of application example of embodiments of the invention two.
Shown in the accompanying drawing 5 is one of application example of embodiments of the invention three.
Shown in the accompanying drawing 6 is one of application example of embodiments of the invention one.
Shown in the accompanying drawing 7 is four of embodiments of the invention.
Accompanying drawing 1:1, gear train; 2, axle; 3, bearing; 4, central shaft; 5, belt pulley; 6, runner; 7, belt; 8, belt; 9, belt pulley.
Accompanying drawing 2:10, runner; 11, sun gear; 12, central shaft; 13, small gear; 14, hydraulic pump motor; 15, support; 16, planetary pinion; 17, clutch mechanism; 18, axle; 19, clutch mechanism; 20, planetary pinion; 21, hydraulic pump motor; 22, sun gear; 23, runner.
Accompanying drawing 3:24, bearing; 25, axle; 26, sprocket wheel; 27, central shaft; 28, chain; 29, gear train; 30, sprocket wheel; 31, runner; 32, sprocket wheel; 33, gear train; 34, axle; 35, runner.
Accompanying drawing 4:36, support; 37, back shaft; 38, servomotor; 39, runner; 40, linking mechanism and hydraulic pump motor; 41, generator; 42, central shaft; 43, chain; 44, drag-line; 45, wing chain bar; 46, axle; 47, upper bracket; 48, linking mechanism and hydraulic pump motor; 49, sprocket wheel; 50, wind transducer; 51, fin; 52, sprocket wheel.
Accompanying drawing 5:53, support; 54, hydraulic drive motor; 55, elevator axis mechanism; 56, sprocket wheel; 57, linking mechanism; 58, runner; 59, fin; 60, wing chain lever arrangement; 61, fin; 62, sprocket wheel; 63, oil hydraulic cylinder; 64, sprocket wheel; 65, support; 66, oil hydraulic pump; 67, planet hoisting linkage device; 68, fin; 69, sprocket wheel; 70, hydraulic jack; 71, wheel; 72, oil pump; 73, chain; 74, driver seat; 75, foot treadle and sprocket wheel; 76, manual control box; 77, frame.
Accompanying drawing 6:78, support; 79, fin; 80, power plant; 81, communication apparatus; 82, airscrew; 83, planet hoisting linkage device; 84, wing chain lever arrangement; 85, sprocket wheel; 86, expansion tightening wheel.
In the accompanying drawing 7: 87, axle; 88, gear; 89, gear; 90, axle; 91, gear; 92, axle; 93, bearing; 94, runner; 95, gear; 96, rotor endcap.
Embodiment two shown in the accompanying drawing 2 is by comprising one of gear type linking mechanism scheme implementation example that gear is formed, this embodiment two includes 2 covers by the gear type linking mechanism that comprises that gear is formed, and forms a cover elevator axis mechanism by planetary pinion 16 and clutch mechanism 17, axle 18 etc.; Axle 18 is exactly the reel of fin, 8 cover elevator axis mechanisms are arranged in the present embodiment, the two ends of 8 cover elevator axis mechanisms are distributed on respectively on runner 10 and the runner 23, sun gear 11 is respectively the linking mechanism of two cover planet hoisting linkage devices with sun gear 22, the direction that they rotate is opposite, a clockwise rotates, another then inverse clock rotation, sun gear 11 and 8 planetary pinion 16 gear motions, sun gear 22 and 8 planetary pinion 20 gear motions, planetary pinion 16 is opposite with the direction of planetary pinion 20 rotations.
Runner 10, runner 23, central shaft 12 rotate together around the central axis of central shaft 12 is equidirectional, in the time of planetary pinion 16 and planetary pinion 20, axle 18 rotations, also rotate with runner 10 and runner 23.
Sun gear 11 links to each other with hydraulic pump motor 14 by small gear 13, and sun gear 22 links to each other with hydraulic pump motor 21 by small gear.Hydraulic pump motor 14 is opposite with the direction that hydraulic pump motor 21 rotates, and one of them hydraulic pump motor pumps pressure oil and enters another hydraulic pump motor, promotes the rightabout rotation of this hydraulic pump motor.
By clutch mechanism 17 Control Shafts 18 and sun gear 11 transmitting movements, by clutch mechanism 19 Control Shafts 18 and sun gear 22 transmitting movements, the state of clutch mechanism 17 is relevant with the position that runner 10 rotates, the state of clutch mechanism 19 is relevant with the position that runner 23 rotates, and the state of clutch mechanism 17 and clutch mechanism 19 can be controlled by comprising the electric power mechanism that is made up of brush or comprising that the hydraulic mechanism of being made up of the hydraulic pressure thrust plate waits.
The rotation of 8 axles 18 is to be mutually related, interrelated by central gear 11 and central gear 22, the autorotation of every axle 18 is relevant with clutch mechanism 19 pivotal positions with the clutch mechanism 17 that links to each other separately, when clutch mechanism 17 is in bonding state with 19 1 of clutch mechanismes, another then is in separated state, every axle 18 rotates at certain regional inverse clock, every axle 18 rotates at certain regional clockwise, the axle 18 of inverse clock rotation is interrelated, the axle 18 of clockwise rotation is interrelated, and the axle 18 of inverse clock rotation is interrelated by hydraulic pump motor 14 and hydraulic pump motor 21 with the axle 18 of clockwise rotation.
This paper is described further by the use of the application examples shown in the accompanying drawing 4 to embodiment two in the accompanying drawing 2.
Shown in the accompanying drawing 4 is a kind of wind-driven generator, in should use-case, axle 46 is exactly the axle in the elevator axis mechanism in the planet hoisting linkage device among the embodiment two in the accompanying drawing 2, the reel of fin just, the two ends of axle 46 are distributed on respectively on the pair of turning wheels 39, runner 39 is exactly the runner in the planet hoisting linkage device among the embodiment two shown in the accompanying drawing 2, and wing chain bar 45 can be around sprocket wheel 49 and sprocket wheel 52, central shaft 42 cycle rotations by chain 43.
8 fins are arranged in this wind-driven generator, fin 51 is to be made by the flexible material of rectangular shape, fin 51 is fixed on the wing chain bar 45 on one side, fin 51 another sides are fixed on the axle 46, the overwhelming majority of every fin 51 can twist on the axle 46 that links to each other separately, and around 8 fin distribution center axles 42, the fin 51 that the clockwise and anticlockwise correspondence of every axle 46 is attached thereto is in axle 46 folding and unfoldings, wing chain bar 45 and axle 46 are when rotating around central shaft 42, and fin 51 is also around central shaft 42 rotations.
Sprocket wheel 52 stretches out under the wind-force effect with sprocket wheel 49 central point lines the right fin 51, drive runner 39, wing chain bar 45, chain 43, axle 46, sprocket wheel 52 rotatablely moves around central shaft 42, fin 51 also rotates around central shaft 42 simultaneously, the fin 51 that stretches out drives the rotation of linking mechanism and hydraulic pump motor 40, and pump pressure oil, pressure oil drives linking mechanism and hydraulic pump motor 48 rotates, the fin that drives the sprocket wheel 52 and the sprocket wheel 49 central point line left sides reclaims, when the fin on the sprocket wheel 52 and the sprocket wheel 49 central point line left sides is recovered to a certain degree, this fin then rotates into sprocket wheel 52 and enters with sprocket wheel 49 central point lines the right and stretch out stroke, when the fin of sprocket wheel 52 on the right of sprocket wheel 49 central point lines reached to a certain degree, this fin then rotated into sprocket wheel 52 and enters the recovery stroke with the sprocket wheel 49 central point line left sides.
Fin drives central shaft 42 and rotates under the wind-force effect, central shaft 42 drives generator 41 and rotates generating.
In should use-case, generator can be strengthened fixing by many drag-lines 44, can be by the rotation of wind transducer 50 control servomotors 38, and the control wind-driven generator rotates, and makes the wind-power electricity generation machine face in the face of wind-force, improves wind energy power efficient; In should use-case, can include torque spring and axle in wing chain bar 45 inner chambers, wing chain bar 45 also can rotate around its axle, the small part of fin 51 can twist in by the effect of this torque spring on the wing chain bar 45, be that wing chain bar 45 also has certain elevator effect, because the rotating speed of sun gear is certain, each planetary rotating speed too, every fin 51 is the same by the time receiving speed of axle 46 like this, speed when putting too, and the variable in distance speed between different fin two ends (promptly be fixed on an end of wing chain bar 45 with fixedly an end of planet hoisting linkage device axle) is different, the fin tension force that has can be excessive, the meeting that has is very little, and the same position difference that fin rotates can be very big at the position tension force that has, very little at the position tension force that has, can effectively regulate the tension force of each fin like this by this torque spring and wing chain bar 45, a spot of fin twists on the wing chain bar 45, fin can not take place and other position is tangled in running; In should use-case, sprocket wheel and chain can adopt many rows formula sprocket wheel and chain, strengthen the intensity of chain.
Since the generator set of the wind-driven generator shown in should use-case below, wind energy is an electric energy by the movement conversion of fin mainly, fin adopts flexible material to make, greatly alleviated the load of support 36, upper bracket 47 and back shaft 37, the advantage that present embodiment has is in light weight, cost is low, efficient is high.
Wind-driven generator in the embodiment of the invention is combined with sea farming equipment, just can make the sea farming wind power plant; Wind-driven generator in the embodiment of the invention is combined with sea water desalting equipment, just can make seawater wind-force desalting plant; Wind-driven generator in the embodiment of the invention is combined with hydrogen producer, just can make seawater wind-force hydrogen producer; The equipment that power supply, burning things which may cause a fire disaster, grain source, water source have been arranged, the following people life of can on the ocean, settling down for a long time.
The fin that wind-driven generator can adopt bulk in the embodiment of the invention is as the wind energy crossover tool, when being used to generate electricity, can also be used for anti-dust storm in the embodiment of the invention.
Wind energy is not only very abundant on the earth, and also exist on other many celestial bodies in the universe, because wind-driven generator is in light weight in the embodiment of the invention, be convenient to be transported on other celestial body from the earth, especially from sun celestial body far away, a little less than the luminous energy, wind energy just can provide the energy for human development has the celestial body of air on these celestial bodies.
Embodiment one shown in the accompanying drawing 1 is one of embodiment who comprises the belt type linking mechanism scheme of being made up of belt pulley and belt, axle 2 constitutes a cover elevator axis mechanism with bearing 3, have 4 cover elevator axis mechanisms in the present embodiment, and be distributed on the runner 6 around, by belt pulley 5, belt 7, belt pulley 9, gear train 1 grade is formed a cover linking mechanism, gear train 1 is a pair of intermeshed gear, a gear links to each other with the axle of elevator axis mechanism, another gear links to each other with the axle of belt pulley 9, control the motion of embodiment's one pairing left and right elevator axis mechanism mutually by linking mechanism, the effect of linking mechanism is in the present embodiment: when the axle time rotational of a cover elevator axis mechanism wherein, will drive the axle opposite direction rotation of relevant another set of elevator axis mechanism by linking mechanism; Another is controlled by another set of linking mechanism mutually to the elevator axis mechanism, and belt 7 needs to isolate certain distance with 8 of belts just can not interfere mutually; Runner 6 rotates with the central axis that central shaft 4 can enclose central shaft 4, and the central axis that 4 cover elevator axis mechanisms and 2 cover linking mechanisms also together enclose central shaft 4 rotates.
This paper is described further by the use of the application examples shown in the accompanying drawing 6 to embodiment one in the accompanying drawing 1 again.
Shown in the accompanying drawing 6 is exactly one of the actual application scheme of embodiment one in the accompanying drawing 1, shown in the accompanying drawing 6 be a kind of can vertical lift and fly able aircraft, planet hoisting linkage device 83 is exactly to comprise by belt pulley among the embodiment one, belt, axle, the planet hoisting linkage device that runner etc. are formed, sprocket wheel 85 includes 3 pairs of sprocket wheels totally 6 sprocket wheels, wherein a pair of is drive sprocket, drive chain is near planet hoisting linkage device 83, two pairs is driven sprocket in addition, one end of fin 79 links to each other with wing chain lever arrangement 84, cover elevator axis mechanism in the other end and the planet hoisting linkage device 83 links to each other, by 85 rotations of power plant 80 driving sprocket wheels, drive wing chain lever arrangement 84 around cycle rotation between 85 3 pairs of sprocket wheels of sprocket wheel, when sprocket wheel 85 rotates at inverse clock, wing chain bar also inverse clock rotates, drive also inverse clock rotation of fin 79, fin 79 is when rotating, the fin of top is pulled out by wing chain bar 84, and the reel that drives the elevator axis mechanism that is attached thereto rotates, it is belt pulley that the reel of elevator axis mechanism rotates by linking mechanism, belt, the reel counter-rotation of the another set of elevator axis mechanism that gear set drive is relevant, and the fin that the below is attached thereto is regained, when the fin of former below rotates to the top, when the fin of former top rotates to the below, equally, the fin that constantly stretches out that is in the top is regained the fin of below by planet hoisting linkage device 83.Fin is in the process of rotation, produce downward flapping wing effect, the drive air moves downward, the air pressure of top will be lower than the air pressure of below, pressure reduction will promote aircraft and move upward up and down, generation is similar to the tension of existing helicopter propeller cavitation, in addition, when fin drive air moves downward, the air that moves downward also produces a kind of impulse force that makes progress, also promote aircraft and move upward, produce the momentum effect when being similar to air breathing engine jet, sprocket wheel 85 inverse clocks on the left side rotate and just produce thrust upwards in the accompanying drawing 6, the runner on the right then needs clockwise to rotate in the accompanying drawing 6, just can produce thrust upwards, when the thrust that makes progress during greater than the weight of aircraft, aircraft just can move upward.Motion by airscrew 82 just can produce forward thrust, and aircraft just can fly forward, and communication apparatus 81 is responsible for providing the flight information of aircraft and the transport information in territorial sky.
Expansion tightening wheel 86 can prevent effectively that chain 43 from getting loose.
This aircraft because adopt flexible material such as parachute fabric as fin, have in light weight, the advantage that efficient is high.
Embodiment three shown in the accompanying drawing 3 is one of embodiments that comprise the chain type linking mechanism scheme of being made up of sprocket wheel and chain, axle 34 is formed the elevator axis mechanism with bearing 24, have 6 cover elevator axis mechanisms in the present embodiment, 6 axle two ends of 6 cover elevator axis mechanisms are distributed on runner 31 and the runner 35, the part of axle is exactly a reel between runner 31 and the runner 35, sprocket wheel 26, chain 28, sprocket wheel 30, gear train 33 are formed linking mechanism, in the present embodiment, have 3 cover linking mechanisms, every cover linking mechanism a pair of elevator axis mechanism of ining succession respectively.
Runner 31, runner 35, central shaft 27, linking mechanism, elevator axis mechanism can rotate around the central axis of central shaft 27, central shaft 27 is hollow shafts, the axle of elevator axis mechanism can be around the axis rotation of oneself, opposite with the axle sense of rotation of the 2 cover elevator axis mechanisms that link to each other of same linking mechanism, wherein the axle of a cover elevator axis mechanism rotates the axle that drives another set of elevator axis mechanism by linking mechanism and reverses.
This paper is described further by the use of the application examples shown in the accompanying drawing 5 to the embodiment three shown in this accompanying drawing 3.Accompanying drawing 5 has been showed the two kinds of difference in functionalitys of the embodiment shown in the accompanying drawing 3, and is a kind of as the power-assisted instrument, another kind of as power tool.
Shown in the accompanying drawing 5 is a kind of manpower aircraft voluntarily.
The driver drives oil pumps 72 and rotates by foot treadle and sprocket wheel 75, chain 73, oil pump 72 pumps pressure oil, the driver ejects oil hydraulic cylinder 63 piston rods with oil hydraulic cylinder 70 piston rods by manual control box 76 and regains, support 53 is that the axle center upwards turns to several angle with the central shaft of sprocket wheel 56, and support 65 is that the axle center rotates several angle with the central shaft of sprocket wheel 64.
The driver enters hydraulic drive motor 54 by manual control box 76 with the pressure oil conversion, hydraulic drive motor 54 clockwise rotating band movable sprockets 56 rotate, drive wing chain lever arrangement 60 cycle rotation between sprocket wheel 56 and sprocket wheel 62, drive fin 59, fin 61, elevator axis mechanism 55, linking mechanism 57 rotate with sprocket wheel 56 clockwises, the fin 61 of sprocket wheel 56 and sprocket wheel 62 central point lines top is pulled out in the rotation of wing chain lever arrangement 60 simultaneously, the fin 61 of top stretch out the withdrawal that drives relevant fin below sprocket wheel 56 and sprocket wheel 6 lines of centres by linking mechanism.Fin stretches out in the process of regaining and rotating, produce the effect of flapping wing, because support 53 is that the axle center upwards turns to several angle with the central shaft of sprocket wheel 56, flapping wing produces certain thrust upwards and backwards, thrust backward reach a certain size will promote manpower voluntarily aircraft on the ground to overtake, sprocket wheel 56 and relevant 6 revolution reducing fins thereof are in the present embodiment as a kind of power tool.
Aircraft is on the ground to overtake voluntarily for manpower, will there be air and fin 68 to produce motion mutually, because support 65 is that the axle center rotates several angle with the central shaft of sprocket wheel 64, if fin 68 is under the situation that braking state do not rotate, fin 68 then only produces resistance and the wing lift that makes progress with the effect of wind-force, fin 68 is under the free rotary state, wind-force will promote fin 68 inverse clocks and rotate, the rotation of the inverse clock rotating band hydrodynamic press pump 66 of fin 68, fin 68 is when producing wing lift upwards, and wind-force is transformed into the hydraulic pressure energy, the pressure oil that oil hydraulic pump 66 pumps enters hydraulic drive motor 54, quicken hydraulic drive motor 54 rotation, accelerated the rotating speed of sprocket wheel 56, increased the flapping wing power of sprocket wheel 56 with the fin of sprocket wheel 6 lines of centres top.
Sprocket wheel 64 and relevant 6 revolution reducing fins thereof are in the present embodiment as a kind of power-assisted instrument.
Flapping wing power and wing lift are big more, and the manpower frictional force on aircraft and ground voluntarily is more little, and flapping wing power is big more, and thrust backward is also big more, and aircraft speed to overtake is fast more voluntarily for manpower.
Aircraft speed to overtake is fast more voluntarily for manpower, and the speed that air and fin 68 move mutually is fast more, and the wing lift that fin 68 produces is bigger, and the rotating speed of oil hydraulic pump 66 will be faster, and the power of oil hydraulic pump 66 outputs is just more.The wing power-assisted of front fin 61 wing power and back fin 68 forms a kind of feedback, and like this, the flapping wing power and the wing lift that make progress will be bigger.
When flapping wing power that makes progress and the wing lift that makes progress continue to increase constantly, the flapping wing power that makes progress and the wing lift sum that makes progress be greater than manpower voluntarily during aircraft and driver's weight, and manpower aircraft voluntarily will break away from ground and aloft flies.The people is because the relation of body weight and physical efficiency, past is difficult to as the bird free flight by other unpowered equipment always, existing unpowered glider can only fly in the short distance of specific place, can not rely on manpower to take off and finish airflight, because the wing power-assisted of front wing power and back forms a kind of feedback in the present embodiment, people need not much strength and consumption, and people just can carry out free flight aloft by means of present embodiment of the present invention.
When the present invention combines with the automobile means of transportation on ground, just can become air-assisted energy-saving automobile or wind-force automobile voluntarily.
When the present invention combines with the ship instrument of the water surface, just can become air-assisted energy-conservation boats and ships or wind-force boats and ships voluntarily.
Embodiment four shown in the accompanying drawing 7 is by comprising two of gear type linking mechanism scheme implementation example that gear is formed, include 4 cover elevator axis mechanisms, a cover linking mechanism, this linking mechanism is made up of gear 88, gear 89, gear 91, gear 95 etc., axle 87 links by this linking mechanism mutually with axle 92, axle 87 is opposite with the direction of axle 92 rotations, and axle 90 can be by other linking mechanism and relevant axle interlock.
As from the foregoing, the present invention has great exploitation value.

Claims (3)

1. the present invention relates to can be used for a kind of planet hoisting linkage device in the revolution reducing flapping wing power equipment of tool configuration such as generating electricity and transport, it is characterized in that having runner;
2. planet hoisting linkage device according to claim 1, it is characterized in that having comprise 2 the cover or 2 the cover more than comprise the elevator axis mechanism of forming by axle, the elevator axis mechanism links to each other with runner;
3. according to claim 1 and the described planet hoisting linkage device of claim 2, it is characterized in that having a cover or the above linking mechanism of a cover, every cover linking mechanism links to each other with 2 covers or the above elevator axis mechanism of 2 covers.
CN200910106630A 2009-04-14 2009-04-14 Planet hoisting linkage device Pending CN101865089A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN200910106630A CN101865089A (en) 2009-04-14 2009-04-14 Planet hoisting linkage device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN200910106630A CN101865089A (en) 2009-04-14 2009-04-14 Planet hoisting linkage device

Publications (1)

Publication Number Publication Date
CN101865089A true CN101865089A (en) 2010-10-20

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CN200910106630A Pending CN101865089A (en) 2009-04-14 2009-04-14 Planet hoisting linkage device

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102180263A (en) * 2011-04-02 2011-09-14 王志成 External gear engaged flapping wing raising force generation device
CN102180264A (en) * 2011-04-02 2011-09-14 王志成 Internal-toothed flapping wing lifting force generation device
WO2012113287A1 (en) * 2011-02-21 2012-08-30 Zhou Yueping Reciprocal flapping wing fluid energy transformation device

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012113287A1 (en) * 2011-02-21 2012-08-30 Zhou Yueping Reciprocal flapping wing fluid energy transformation device
CN102180263A (en) * 2011-04-02 2011-09-14 王志成 External gear engaged flapping wing raising force generation device
CN102180264A (en) * 2011-04-02 2011-09-14 王志成 Internal-toothed flapping wing lifting force generation device
CN102180263B (en) * 2011-04-02 2012-12-12 王志成 External gear engaged flapping wing raising force generation device
CN102180264B (en) * 2011-04-02 2012-12-12 王志成 Internal-toothed flapping wing lifting force generation device

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