WO2010066156A1 - Dispositif à diamètre variable de pale tournante - Google Patents

Dispositif à diamètre variable de pale tournante Download PDF

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Publication number
WO2010066156A1
WO2010066156A1 PCT/CN2009/074910 CN2009074910W WO2010066156A1 WO 2010066156 A1 WO2010066156 A1 WO 2010066156A1 CN 2009074910 W CN2009074910 W CN 2009074910W WO 2010066156 A1 WO2010066156 A1 WO 2010066156A1
Authority
WO
WIPO (PCT)
Prior art keywords
bracket
wing
transmission
mounting member
rotor
Prior art date
Application number
PCT/CN2009/074910
Other languages
English (en)
Chinese (zh)
Inventor
周跃平
周文珺
Original Assignee
Zhou Yueping
Zhou Wenjun
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Zhou Yueping, Zhou Wenjun filed Critical Zhou Yueping
Publication of WO2010066156A1 publication Critical patent/WO2010066156A1/fr

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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
    • F03B—MACHINES OR ENGINES FOR LIQUIDS
    • F03B17/00—Other machines or engines
    • F03B17/06—Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head"
    • F03B17/062—Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head" with rotation axis substantially at right angle to flow direction
    • F03B17/063—Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head" with rotation axis substantially at right angle to flow direction the flow engaging parts having no movement relative to the rotor during its rotation
    • F03B17/064—Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head" with rotation axis substantially at right angle to flow direction the flow engaging parts having no movement relative to the rotor during its rotation and a rotor of the endless-chain type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2210/00—Working fluid
    • F05B2210/16—Air or water being indistinctly used as working fluid, i.e. the machine can work equally with air or water without any modification
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/30—Energy from the sea, e.g. using wave energy or salinity gradient

Definitions

  • the present invention relates to a power plant, and more particularly to a swing flapping reducer.
  • the existing wind energy and water energy utilization devices are similar in principle. They use wind or water flow to drive the motion of the fixed or basic fixed structure of the airfoil to generate kinetic energy, and then convert the kinetic energy into the required form energy through energy conversion device or directly apply The kinetic energy produced by the fins.
  • the existing wind energy utilization device and the water utilization device airfoil cannot be expanded and contracted in a large size, so that the wind energy utilization device and the water energy utilization device are not universal, and the utilized wind energy and water energy efficiency are low.
  • Aircraft, cars, flying boats and other transportation equipment can generate wing power through wings and relatively moving air or water.
  • Wing power is primarily used to assist in the movement of transportation equipment.
  • the wings on these transportation equipment are basically fixed or small angle swings. Therefore, such wings are generally used as boosting devices and cannot be used as propulsion devices.
  • This kind of wing as a power-assisting device can generate certain wing power while interacting with air in motion, but it also generates certain resistance. This kind of assisting wing needs to consume a lot of energy in motion.
  • the technical problem to be solved by the present invention is to provide a flap size and position that can be flexibly changed in view of the drawback that the size and position of the wind power utilization or water power utilization power device of the prior art cannot be flexibly changed.
  • the rotary flapping reducer is to provide a flap size and position that can be flexibly changed in view of the drawback that the size and position of the wind power utilization or water power utilization power device of the prior art cannot be flexibly changed.
  • the technical solution adopted by the present invention to solve the technical problem is: constructing a rotary flapping wing reducing device, package A transmission device mounted on the wing bracket device, the transmission device including a transmission member and a rotating member; the transmission member including a mounting member, the rotating member including a mounting member.
  • the wing bracket device includes a mounting member; the mounting member is a connecting portion of the transmission member or the rotating member or the wing bracket device or is fixedly mounted on the transmission member or A separate component on the rotating member or wing bracket assembly.
  • the wing bracket device includes a bracket and a slide provided on the bracket to form a raft; the slide is welded to the bracket or fixed by a mounting member. Mounted on the bracket.
  • the transmission member includes a pulley disposed on the slide rail, and a fin fixing device fixedly mounted on the pulley by the mounting member.
  • the wing bracket device comprises a bracket, at least one pulley disposed on the bracket or at least one sprocket disposed on the bracket; the pulley or The sprocket is mounted on the bracket by a first shaft.
  • the transmission member includes a chain, and a fin fixing device fixedly mounted on the chain by the mounting member; at least one of the chain is provided a mounting member; the chain is meshed with the sprocket.
  • the transmission member includes a belt, and a fin fixing device fixedly mounted on the belt by a mounting member, and the belt is provided with at least one Mount
  • the belt has teeth or holes
  • the fin fixing device is mounted on the belt through the mounting member and the teeth or holes of the belt;
  • the belt of the teeth or holes engages with the pulleys on the wing bracket assembly; or the belt with teeth or holes engages with the sprocket on the wing bracket assembly.
  • the rotating member includes a rotor, a fin fixing device fixedly mounted on the rotor by a mounting member, and the rotor is mounted on the bracket through the second shaft;
  • the rotor is mounted on the first shaft by means of a mounting or the rotor is mounted on the pulley by means of a mounting or the rotor is mounted on the sprocket by means of a mounting.
  • the transmission device includes a flap, and the flap is an elastic material such as a rubber sheet or a flexible cloth such as a parachute cloth, a canvas, or the like; [15] One end of the flap is mounted on the transmission member by a fin fixing device, and the other end of the fin is mounted on the rotating member by a fin fixing device.
  • the rotary flapping wing reducing device embodying the present invention has the following advantageous effects:
  • the present invention mounts the transmission device on the wing bracket device, and mounts the mounting member on the transmission member and the rotating member of the transmission device, Both ends are respectively mounted on the transmission member and the rotating member through the fin fixing means.
  • the fin fixing device on the rotating member rotates around the rotor, the rotor is also rotatable, and the fin fixing device on the transmission member also rotates around the rotor.
  • the invention can be used for wind power generation, and can also be used in transportation tools, and has the functions of low energy consumption and power assist.
  • Figure la is a schematic view showing the installation of the first embodiment of the rotary flapping device of the present invention.
  • FIG. 2a is a schematic view showing the installation of the second embodiment of the rotary flapping wing reducing device of the present invention
  • FIG. 2b is a schematic structural view of a second embodiment of the rotary flapping wing reducing device of the present invention.
  • FIG. 3 is a schematic view showing the installation of the third embodiment of the rotary flapping wing reducing device of the present invention.
  • FIG. 4 is a schematic structural view of a fourth embodiment of the rotary flapping wing reducing device of the present invention.
  • FIG. 5 is a schematic structural view of a fifth embodiment of the rotary flapping wing reducing device of the present invention.
  • Figure 6a is a schematic structural view of a sixth embodiment of the rotary flapping device of the present invention.
  • Figure 6b is a schematic structural view of a sixth embodiment of the rotary flapping device of the present invention.
  • FIG. 7 is a schematic diagram of a wing hoisting of a sixth embodiment of the rotary flapping wing reducing device of the present invention.
  • Figure 8 is a diagram showing a sixth embodiment of the slewing flapping machine of the present invention.
  • Example 1 The specific structure of the rotary flapping wing reducing device provided by the present invention is as shown in FIG. 1.
  • the rotating flapping wing reducing device comprises at least two oppositely disposed wing bracket devices 1, and a transmission device 2 mounted on the wing bracket device 1.
  • the transmission device 2 includes a transmission member 200 and a rotating member 210;
  • the wing bracket device 1 includes a mounting member 220;
  • the transmission member 200 includes a mounting member 220, and the rotating member 210 includes a mounting member 220.
  • the mounting member 220 is a sub-portion of the transmission member 200 or the rotating member 210 or the wing bracket device 1 or a separate component fixedly mounted on the transmission member 200 or the rotating member 210 or the wing bracket device 1.
  • the wing bracket device 1 includes a bracket 101 and a slide 201 disposed on the bracket 101.
  • the slide 201 is welded to the bracket 101 or fixedly mounted on the bracket 101 by a mounting member 220.
  • the rotating member 210 is a rotor 213, and the rotor 213 includes at least one mounting member 220, and a fin fixing device 4 fixedly mounted on the rotor 213 by a mounting member 220. Each of the two ends of the fin fixing device 4 is respectively mounted. Pie. 220.
  • the rotor 213 is mounted on the bracket 101 via the second shaft 211, and the rotor 213 and the fin fixing device 4 are rotated about their second shafts 211.
  • the transmission member 200 includes at least one pulley 202 disposed on the slide 201.
  • the fin fixing device 4 is mounted on the pulley 202 through the mounting member 220, and each of the two ends of the fin fixing device 4 respectively corresponds to one mounting member 220. .
  • the pulleys 202 are mounted on the chute 201 of the bracket 101; the adjacent fin fixing devices 4 are connected by a chain 204 or a belt 203, and the fin fixing devices 4 are connected in a ring shape by a chain 204 or a belt 203, the chain 204 It may be a commonly used chain, or the outer panel of the chain 204 may be made of a steel cord or a cord or a belt; the rotating member 210 is mounted in a region surrounded by the transmission member 200 and the slide 201.
  • the fins 3 are elastic material products, one end of each fin 3 is mounted on the fin fixing device 4 of the rotating member 210, and the other end of the fin 3 is mounted on the fin of the rotating member transmission member 200.
  • the annular transmission member 200 is rotatable about the rotating member 210 along the track of the slide 201, and the rotating member 210 is also rotatable about its central axis.
  • the flap 3 also rotates around the central axis of the rotating member 210 due to the slide.
  • the distances from the points on the track of 201 to the central axis of the transmission member 200 are different, and the distance between the fin fixing devices 4 at both ends of the fins 3 is also different, thereby generating the same rotation of the fins around the central axis of the rotating member 210, the fins 3
  • the size is also different.
  • the swing flapping device comprises at least two oppositely disposed wing bracket devices 1, a transmission 2 mounted on the wing bracket device 1, said transmission 2 comprising a transmission member 200 and rotating member 210; the wing bracket device 1 includes a mounting member 220; the transmission member 200 includes a mounting member 220, and the rotating member 210 includes a mounting member 220.
  • the mounting member 220 is a sub-portion of the transmission member 200 or the rotating member 210 or the wing bracket device 1 or a separate member fixedly mounted to the transmission member 200 or the rotating member 210 or the wing bracket device 1.
  • the wing bracket device 1 includes at least two pulleys 212 of different sizes mounted on the bracket 101, and the pulley 212 is fixedly mounted on the bracket 101 by a first shaft 207 and a bearing 209. The pulley 212 rotates about a first axis 207.
  • the rotating member 210 includes a rotor 213 and a fin fixing device 4 mounted on a pulley 212, the fin fixing device 4 being mounted on the rotor 213 by a mounting member 220; the rotor 213 passing through the mounting member
  • the 220 is mounted on the first shaft 207 or mounted to the pulley 212 by a mounting member 220.
  • the fin fixing device 4 on the 213 is rotated about the first shaft 207.
  • the transmission member 200 includes a belt 203 having teeth or holes and a fin fixing device 4, and the belt 203 is meshed with the pulley 212; the two ends of the associated fin fixing device 4 are respectively mounted on the belt through the mounting member 220. 203.
  • the distance from the fin fixing device 4 of the transmission member 200 to the first shaft 207 differs depending on the rotation angle, so that the fin fixing device 4 of the transmission member 200 generates a variable-diameter movement.
  • the rotary flapping wing reducing device comprises at least two oppositely disposed wing bracket devices 1, a transmission device 2 mounted on the wing bracket device 1, the transmission device 2 including the transmission member 200 and the rotation
  • the wing bracket device 1 includes a mounting member 220;
  • the transmission member 200 includes a mounting member 220, and
  • the rotating member 210 includes a mounting member 220.
  • the mounting member 220 is an attachment portion of the transmission member 200 or the rotating member 210 or a separate member fixedly mounted to the transmission member 200 or the rotating member 210.
  • the wing bracket device 1 includes at least two sprocket wheels 214 of different sizes mounted on the bracket 101, and the sprocket 214 is fixedly mounted on the bracket 101 by a first shaft 207 and a bearing 209.
  • the sprocket 214 rotates about a first axis 207.
  • the rotating member 210 is a rotor 213 and a fin fixing device 4 mounted on the first shaft 207, and the fin fixing device 4 is mounted on the rotor 213 through a mounting member 220;
  • the member 220 is mounted on the first shaft 207 or mounted on the sprocket 214 by a mounting member 220.
  • the rotor fixing device 4 on the rotor 213 and the rotor 213 is rotated about the first shaft 207.
  • the transmission member 200 includes a chain 204 and a fin fixing device 4, and the chain 204 is engaged with the sprocket 214; the two ends of the fin fixing device 4 are respectively mounted on the chain 204 by the mounting member 220.
  • the chain 204 may be a commonly used chain, or the outer panel of the chain 204 may be made of a steel cord or a cord or a belt.
  • the distance from the fin fixing device 4 of the transmission member 200 to the first shaft 207 differs depending on the rotation angle, so that the fin fixing device 4 of the transmission member 200 produces a variable-diameter rotational motion.
  • the application of the invention can be either kinetic energy generated by the external wind or water pushing the flap motion, and then converted into energy of the desired form by the energy conversion device or directly using the motion generated by the flap motion.
  • the moving fins can generate electricity by driving the generator to work.
  • wind or water flows on the fins 3, since the area of the fins 3 at the upper end of the central axis of the rotating member 210 is smaller than the area of the lower end fins 3 of the rotating member 210, the wings of the lower end fins 3 of the rotating member 210 The power is much greater than the wing power at the upper end of the axis of the rotating member 210.
  • the flap 3 and the transmission member 200 are rotatable about the rotating member 210, and are extended and contracted.
  • the flap 3 rotates through the flap fixing device 4 to rotate the rotating member 210, and the rotating member 210 drives the power generating device 5 to generate electricity.
  • multiple sets of variable-diameter rotary-wing generators can be used to build a power station for hydroelectric or wind power generation in rivers and oceans.
  • the variable-turn rotary-wing generator is suitable for small-scale power generation. Also suitable for large-scale power stations.
  • the present invention can also be applied to vehicles: ships, vehicles, airplanes, etc., by means of a power unit that drives the motion of the airfoil to generate power, to propel the vehicle forward, or to generate wing lift by wind or water to move the airfoil or
  • the wing is reduced in force, and the wing lift or wing resistance is converted into the forward power of the vehicle through the energy conversion mechanism to achieve the purpose of energy saving, and the braking force of the vehicle is increased by the wing drop force, or the vehicle is realized by the wing lift or the wing drop force. The turn.
  • the rotary flapping reducer is mounted on the vehicle, and the slide 201 is fixed to the wing bracket device 1.
  • the transmission member 200 is rotatable on the slide 201 by the pulley 202, and the rotor 213 is also rotatable. Since the angle at which the fin fixing device 4 and the rotor 213 rotate is different, the distance between the fin fixing devices 4 of the fin is different. It has the function of a rotary flapping reducer.
  • the fin fixing device 4 is connected to the hoisting device 6, and the flap 3 adjusts the size of the flap 3 by the hoisting device 6.
  • the telescopic cylinder 7 can adjust the angle of the rotary flap reducer.
  • the power unit drives the vehicle forward, and when the vehicle is traveling forward, the rotary flapper is rotated downward through the telescopic cylinder 7, and the relatively moving air acts on the airfoil 3, and the same direction is generated upward.
  • the wing lift and the backward resistance, the wing lift and the resistance generate torque to drive the rotor 213 to move, the rotor 213 drives the rotation of the kinetic energy conversion device 8, and the kinetic energy conversion device 8 accelerates the vehicle forward by the aerodynamic propulsion device 9, the resistance of the airfoil 3 Both the wing and the lift are transformed into the driving force of progress.
  • the rotary flapper reducer and its fins do not excessively consume the energy of the vehicle at the same time as the wing lift or resistance is generated.
  • the wing lift produced by the rotary flap reducer is greater than the weight of the vehicle, the vehicle can even fly in the air. Therefore, the vehicle needs to be smaller.
  • the power input can maintain the energy consumption inside the vehicle operating mechanism, and the high speed can be achieved. Direct use of wind energy to achieve energy savings.
  • the power supply can be decelerated by cutting off the power supply or cutting off the supply of kinetic energy of the wing kinetic energy conversion device.
  • a brake cymbal is required to rotate the rotary flapping damper upward through the telescopic cylinder and to limit the rotation of the fin fixing device, and the angle of the upward rotation reaches a certain angle, and the downward wing lowering force and the backward resistance are generated.
  • the downward wing drop force increases the braking friction of the vehicle and the ground.
  • the steering of the vehicle can be achieved by adjusting the wing drop force on the side of the vehicle and the lift of the wing through the telescopic cylinder.
  • Figure 6a and Figure 6b show a schematic view of the structure of a swing flapper reducer mounted on a ship.
  • Figure 6b shows the schematic diagram of the structure of the rotary flapping reducer mounted on the ship.
  • the principle of action is the same as that of the vehicle shown in Figure 5, which is adjusted by adjusting the angle of the variable-turning flapping wing.
  • the slewing flapping sailboat can sail quickly under the headwind, because it transforms the energy of the headwind into the power of sailing, and reduces the draught of the sailboat.
  • Figure 6a is a schematic view showing the structure of the rotary flapping reducer as a propulsion device mounted on the ship.
  • the power unit 10 drives the transmission device 2 to rotate, and drives the fins 3 to rotate, and the fins 3 are reversed. Rotating the cymbal pushes the boat 37 forward, and the flap 3 rotates to push the boat 37 backwards.
  • the flap hoisting mechanism can be mounted on the fin fixing device to adjust the flap size according to actual needs.
  • the flap hoisting mechanism can be controlled by a spring or hydraulic pump motor or motor.
  • One of the schematics of the flap hoisting mechanism through the spring controlled flap hoisting mechanism is shown in Fig. 7: the fin fixing device 4 can be driven by the torsion spring 66, and Rotatable, the flap 3 is extended by air or hydraulic force to drive the flap fixing device 4 to rotate, and the twisting spring 66 is also driven to move.
  • the torsion spring 66 drives the wing.
  • the sheet fixing device 4 is rotated, and the same flap 3 is retracted.
  • FIG. 8 One of the schematic diagrams of the airfoil hoisting mechanism controlled by the hydraulic pump motor is shown in Fig. 8:
  • the airfoil 3 is extended by air or hydraulic force, and the stroke reversing valve 71 is connected to the right position.
  • the motor 70 is rotated by the fin fixing device 4, and a certain pressure oil is pumped into the high-pressure oil circuit chain 72; when the flap 3 is brought into the retracted position by the flap fixing device 4, the stroke reversing valve 71 is turned on.
  • the pressure oil in the high pressure oil circuit chain 72 drives the motor 70 to reverse, and the motor 70 drives the airfoil fixing device 4 to rotate, and the airfoil 3 is retracted.
  • the present invention mounts a transmission on a wing bracket device and a mounting member on the transmission member and the rotating member of the transmission.
  • the transmission member rotates around the rotating member, and the rotating member is also rotatable.
  • the fin mounted between the transmission member and the rotating member also rotates, and the rotating member and the wing on the transmission member are different according to the angle at which the fin fixing device rotates with the rotor.
  • the distance between the fixtures is different, and the size of the fins is different, resulting in a variable diameter rotation.
  • the invention can be used for wind power generation, and can also be used in transportation tools, and has the functions of low energy consumption and power assist.

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Wind Motors (AREA)

Abstract

La présente invention concerne un dispositif à diamètre variable de pale tournante comprenant un dispositif de transmission (2) qui est fixé sur un dispositif de support de pale (1), le dispositif de transmission (2) comprenant une partie de transmission (200) et une partie tournante (210). La partie de transmission (200) comprend des éléments de fixation (220) et la partie tournante (210) comprend des éléments de fixation (220). Les éléments de fixation (220) sont des éléments supplémentaires de la partie de transmission (200) ou de la partie tournante (210), ou des éléments individuels qui sont montés fixement sur la partie de transmission (200) ou la partie tournante (210). Deux extrémités des pales (3) tournent avec la rotation de la partie de transmission (200) et de la partie tournante (210) à travers les dispositifs de fixation de pale (4) qui sont fixés sur la partie de transmission (200) et la partie tournante (210). Lorsque les pales (3) tournent autour de la partie tournante (210), les angles de rotation sont différents et les distances entre les dispositifs de fixation de pale (4) des deux extrémités des pales (3) sont différentes.
PCT/CN2009/074910 2008-12-14 2009-11-12 Dispositif à diamètre variable de pale tournante WO2010066156A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CNA2008101884409A CN101457745A (zh) 2008-12-14 2008-12-14 回转扑翼变径器
CN200810188440.9 2008-12-14

Publications (1)

Publication Number Publication Date
WO2010066156A1 true WO2010066156A1 (fr) 2010-06-17

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Application Number Title Priority Date Filing Date
PCT/CN2009/074910 WO2010066156A1 (fr) 2008-12-14 2009-11-12 Dispositif à diamètre variable de pale tournante

Country Status (2)

Country Link
CN (1) CN101457745A (fr)
WO (1) WO2010066156A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102287335A (zh) * 2011-07-21 2011-12-21 卢国林 帆板串联式风力发电装置
EA023510B1 (ru) * 2012-08-13 2016-06-30 Александр Васильевич Колесов Гидроэлектростанция конвейерного типа

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101457745A (zh) * 2008-12-14 2009-06-17 周文珺 回转扑翼变径器
CN102052257A (zh) * 2009-11-02 2011-05-11 周文珺 一种卷扬翼链杆装置
CN201687651U (zh) * 2010-02-08 2010-12-29 周跃平 一种转动变径扑翼
CN102400842A (zh) * 2010-09-15 2012-04-04 刘文晏 辅助发电系统
CN201963458U (zh) * 2011-02-21 2011-09-07 周跃平 一种往复扑翼流体能量转换装置

Citations (5)

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Publication number Priority date Publication date Assignee Title
JP2004138015A (ja) * 2002-10-21 2004-05-13 Tamio Nakamura 流体車
CN1740560A (zh) * 2005-08-15 2006-03-01 石运达 圆弧齿形链式风力环保发电制氢装置
CN101100974A (zh) * 2007-06-29 2008-01-09 陈崟 转叶车式流体机
US20080007069A1 (en) * 2006-05-05 2008-01-10 Jurgen Diederich Fluid Energy-Harnessing Apparatus
CN101457745A (zh) * 2008-12-14 2009-06-17 周文珺 回转扑翼变径器

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004138015A (ja) * 2002-10-21 2004-05-13 Tamio Nakamura 流体車
CN1740560A (zh) * 2005-08-15 2006-03-01 石运达 圆弧齿形链式风力环保发电制氢装置
US20080007069A1 (en) * 2006-05-05 2008-01-10 Jurgen Diederich Fluid Energy-Harnessing Apparatus
CN101100974A (zh) * 2007-06-29 2008-01-09 陈崟 转叶车式流体机
CN101457745A (zh) * 2008-12-14 2009-06-17 周文珺 回转扑翼变径器

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102287335A (zh) * 2011-07-21 2011-12-21 卢国林 帆板串联式风力发电装置
EA023510B1 (ru) * 2012-08-13 2016-06-30 Александр Васильевич Колесов Гидроэлектростанция конвейерного типа

Also Published As

Publication number Publication date
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