CN101994663A - Rotor device fixing shaft seat - Google Patents

Rotor device fixing shaft seat Download PDF

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Publication number
CN101994663A
CN101994663A CN2009101095879A CN200910109587A CN101994663A CN 101994663 A CN101994663 A CN 101994663A CN 2009101095879 A CN2009101095879 A CN 2009101095879A CN 200910109587 A CN200910109587 A CN 200910109587A CN 101994663 A CN101994663 A CN 101994663A
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CN
China
Prior art keywords
axle bed
flapping wing
sprocket wheel
rotor arrangement
flapping
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
Application number
CN2009101095879A
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Chinese (zh)
Inventor
周跃平
周红球
周星果
周文珺
尹雄鹰
Original Assignee
周文珺
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 周文珺 filed Critical 周文珺
Priority to CN2009101095879A priority Critical patent/CN101994663A/en
Publication of CN101994663A publication Critical patent/CN101994663A/en
Pending legal-status Critical Current

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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

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  • Wind Motors (AREA)

Abstract

The invention relates to a rotor device fixing shaft seat on wind power and water power flapping-wing device power equipment, which is characterized by comprising a shaft seat, and the shaft seat is provided with a cantilever and a shaft hole. The shaft hole is used for assembling a central shaft of a rotating wheel, and the shaft seat can be fixed on a support of the flapping-wing device through the cantilever. The invention can optimize the structure of a planet winnowing linkage device on the flapping-wing device so as to realize higher power, high efficiency and high reliability of the flapping-wing device power equipment.

Description

Rotor arrangement is axle bed fixedly
Technical field
The present invention relates to the fixing axle bed of a kind of rotor arrangement on wind-force, the waterpower flapping wing device power equipment.
Technical background
The scheme that I provide a kind of revolving flapping wings reducing machine on December 14th, 2008, application number is 2008101884409, this scheme provides a kind of new power technologies such as can be used for wind-power electricity generation, hydroelectric power and communications and transportation, adopt flexible material such as parachute fabric etc. to rotatablely move in this scheme, realize power generating equipment or required power-assisted of facilities for transport and communication or transmission of power around same central axis reducing; I provide a kind of planet of flapping wing device to change on April 14th, 2009 and have raised linkage, application number 20091016630.6.More than related to following technological scheme in two kinds of invention schemes: i.e. the sprocket wheel or the gear matched of the chain of rotor arrangement both sides or belt such as Toothed belt and rotor arrangement both sides.Have following deficiency in this technological scheme: the rotating shaft of the central rotating shaft of rotor arrangement and the sprocket wheel of both sides or gear is same rotating shaft, and links to each other with support by same rotating shaft.This deficiency has following one or more defectives: one, the sprocket wheel of rotor arrangement and both sides or gear are all wanted bearing load, rotor arrangement and both sides or wherein the sprocket wheel or the gear of a side can produce certain deformation under external force, can influence each other; Two, this rotating shaft will be passed planet changes the center of raising linkage, causes planet to change the leakage of raising the lubricant oil in the linkage easily; Three, it causes the planet commentaries on classics to raise the linkage complex structure.
Summary of the invention
Purpose of the present invention is exactly to provide fixedly axle bed of a kind of rotor arrangement at the last deficiency of being permitted for the flapping wing device.
The present invention is achieved in that it is characterized in that having axle bed, has axis hole on the axle bed; It is characterized in that axle bed has cantilever.The rotating shaft of rotor arrangement and bearing can directly be assemblied in the axis hole of axle bed, and axle bed is fixed on the support of flapping wing device by cantilever.
One end of the axle of sprocket wheel or gear also can assemble on the axle bed, can ensure that like this sprocket wheel or gear and rotor arrangement rotate along same central axis.
The load that rotor arrangement bore can directly be delivered to support by axle bed and cantilever like this, can not produce bigger influence to sprocket wheel or gear.
Be furnished with planet and change the rotor arrangement of raising linkage, then can by flange shaft etc. and rotor arrangement fixedly axle bed link to each other, planet changes the center raise linkage and does not have axis and pass, help planet and change the optimization of raising the linkage structure, planet changes the center of raising linkage does not have axis to pass,, planet changes the center raise linkage and does not have through hole, can effectively prevent planet change raise linkage in lubricant oil leak from center hole.
The invention will be further described below in conjunction with embodiment.
Description of drawings
Shown in the accompanying drawing 1 is fixedly one of the embodiment of axle bed of rotor arrangement involved in the present invention.
Shown in the accompanying drawing 2 be rotor arrangement involved in the present invention fixedly axle bed embodiment two.
Shown in the accompanying drawing 3 is the fixedly embodiment's one of axle bed one of practical application example of accompanying drawing 1 related rotor arrangement.
Shown in the accompanying drawing 4 is the structural drawing of planet hoisting linkage device related in the related practical application example one of accompanying drawing 3.
Shown in the accompanying drawing 5 is the fixedly embodiment's one of axle bed one of practical application examples of accompanying drawing 2 related rotor arrangements.
In the accompanying drawing 1: 1, axis hole; 2, axle bed; 3, cantilever.
In the accompanying drawing 2: 4, axis hole; 5, sprocket wheel axis hole; 6, axle bed; 7, cantilever.
In the accompanying drawing 3: 8, generator; 9, break; 10, power chain; 11, power chain; 12, synchronous sprocket wheel device; 13, gantry support; 14, wing chain bar; 15, fin; 16, slideway; 17, high-end flapping wing sprocket wheel; 18, synchronous sprocket wheel device; 19, the fixing axle bed of rotor arrangement; 20, flapping wing chain; 21, runner; 22, linkage is raised in the planet commentaries on classics; 23, low side flapping wing sprocket wheel.
In the accompanying drawing 4: 24, low side flapping wing sprocket wheel: 25, flapping wing chain; 26, slideway; 27, the fixing axle bed of rotor arrangement; 28, synchromesh gear device; 29, synchronizing jugged belt; 30, generator; 31, break; 32, high-end flapping wing sprocket wheel; 33, wing chain bar; 34, linkage is raised in the planet commentaries on classics; 35, synchronizing shaft; 36, support; 37, runner; 38, synchromesh gear device; 39, synchronizing jugged belt.
In the accompanying drawing 5: 25, flapping wing chain; 37, runner; 40, gear; B; 41, elevator axle B; 42, center tooth wheels; 43, gear A; 44 elevator axle A; 45 fin A; 46 fin B.
Embodiment
Among the embodiment of accompanying drawing 1, axis hole 1 is used to assemble the central shaft of runner, and axle bed 2 can be fixed on the support of flapping wing device by cantilever 3.
In the accompanying drawing 2, sprocket wheel axis hole 5 is used to assemble the axle of flapping wing sprocket wheel, can ensure effectively that the central shaft of runner is concentric with the axle of flapping wing sprocket wheel.
Shown in the accompanying drawing 3 is a kind of large-scale flapping wing wind generating unit, it is made up of two groups of flapping wing devices, the rotor arrangement that the central shaft at runner 21 two ends is assemblied in two ends is fixedly on the axle bed 19, axle one end of low side flapping wing sprocket wheel 23 is assemblied on the gantry support 13, the other end is assemblied in rotor arrangement fixedly on the axle bed 19, rotor arrangement fixedly axle bed 19 is assemblied on the gantry support 13 by its cantilever, the low side flapping wing sprocket wheel 23 of runner 21 both sides rotates synchronously by synchronous sprocket wheel device 12, the kinetic energy of two groups of flapping wing devices is by synchronous sprocket wheel device 12 and synchronous sprocket wheel device 18, power chain 10, power chain 11 is delivered to generator 8, and break 9 can be realized braking.Wind-force drives the rotation of fin 15, fin 15 drives the motion of flapping wing chain 20 by wing chain bar 14, and drive the rotation of high-end flapping wing sprocket wheel 17 and low side flapping wing sprocket wheel 23, and the rotation of low side flapping wing sprocket wheel 23 drives power chain 10 and rotates, and power chain 10 drives generators 8 and rotates generating.
Fin 15 has many groups with wing chain bar 14, and an end of every links to each other with wing chain bar 14, and the other end links to each other with epitrochanterian planet hoisting device, and planet changes raises the folding and unfolding that linkage 22 can effectively ensure fin 15.
Slideway 26 helps ensureing the motion of flapping wing chain.
The application number that provides in person is provided in detail is 2008101884409 a kind of revolving flapping wings reducing machine and application number and be 20091016630.6 planet changes and raises linkage.
Because the main parts size of this flapping wing wind generating unit is positioned at the low side of electricity generating device, relatively near ground, dismounting is very convenient with maintenance, because fin 15 adopts flexible material, in light weight, cost is low, effective large size capturing wind energy can be fit to the wind-power electricity generation and the deepwater wind-power electricity generation of most lands on the earth.
Shown in the accompanying drawing 4 is a kind of large-scale flapping wing hydroelectric installation, shown in the accompanying drawing 5 is that planet related in the accompanying drawing 4 changes the structural drawing of raising linkage 34, the rotor arrangement that the central shaft at runner 37 two ends is assemblied in two ends is fixedly on the axle bed 27, the axle two ends of high-end flapping wing sprocket wheel 32 are assemblied in rotor arrangement fixedly on the axle bed 27, rotor arrangement fixedly axle bed 27 is assemblied on the support 36 by its cantilever, the high-end flapping wing sprocket wheel 23 of runner 37 both sides is by synchromesh gear device 28, synchronizing jugged belt 29, synchronizing shaft 35, synchromesh gear device 38, synchronizing jugged belt 39 rotates synchronously, the kinetic energy of flapping wing device is by synchromesh gear device 28, synchronizing jugged belt 29, synchronizing shaft 35, synchromesh gear device 38, synchronizing jugged belt 39 is delivered to generator 30, and break 31 can be realized braking.Waterpower drives the rotation of fin A46, fin B47, fin A46 and fin B 47 drive the motion of flapping wing chain 25 by wing chain bar 33, and drive the rotation of high-end flapping wing sprocket wheel 32 and low side flapping wing sprocket wheel 24, the rotation of high-end flapping wing sprocket wheel 32 drives synchronizing shaft 35 and rotates, and synchronizing shaft 35 drives generator 30 and rotates generating.
In the accompanying drawing 5, fin A 46 links to each other with elevator axle A 44, fin B46 links to each other with elevator axle B41, the rotation of stretching out meeting drive elevator axle A44 of fin A45, elevator axle A44 is by gear A 43, gear train 42, the engagement rotation drive elevator axle B41 counter-rotating mutually mutually of gear B 40, the rotation of elevator axle B 41 is regained fin B47 synchronously, fin A46 and fin B47 have certain force of strain all the time under hydraulic action, fin A46 is owing to the frictional force of self twists on the elevator axle A45 tightly, equally, fin B47 is owing to the frictional force of self twists on the elevator axle B41 tightly, this shows, it is very simple that the planet that connects axle changes the structure of raising linkage 34, and can improve planet and change the working efficiency of raising linkage 34, the planet that does not connect axle in addition changes to be raised in the linkage 34, does not also just have center hole, and lubricant oil just can not leak by its center hole yet.
Because flapping wing hydroelectric installation main parts size is positioned at the high-end of electricity generating device, on the water surface, fin is because the frictional force of self twists in the elevator axle tightly, the dismounting of whole generating device is very convenient with maintenance, fin A46 can adopt and be similar to high-intensity corrosion resistant braiding line belt, in light weight, cost is low, effectively large size is caught the water energy, can be fit to the generating of waterpower on most rivers on the earth, control flood, combats a natural disaster, irrigates.

Claims (3)

1. the present invention relates to the fixing axle bed of a kind of rotor arrangement on wind-force, the waterpower flapping wing device power equipment, it is characterized in that having axle bed;
2. a kind of rotor arrangement according to claim 1 is axle bed fixedly, it is characterized in that axle bed has cantilever;
3. a kind of rotor arrangement according to claim 1 is axle bed fixedly, it is characterized in that having axis hole on the axle bed.
CN2009101095879A 2009-08-13 2009-08-13 Rotor device fixing shaft seat Pending CN101994663A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009101095879A CN101994663A (en) 2009-08-13 2009-08-13 Rotor device fixing shaft seat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009101095879A CN101994663A (en) 2009-08-13 2009-08-13 Rotor device fixing shaft seat

Publications (1)

Publication Number Publication Date
CN101994663A true CN101994663A (en) 2011-03-30

Family

ID=43785267

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009101095879A Pending CN101994663A (en) 2009-08-13 2009-08-13 Rotor device fixing shaft seat

Country Status (1)

Country Link
CN (1) CN101994663A (en)

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Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
DD01 Delivery of document by public notice

Addressee: Zhou Wenjun

Document name: Notification of Publication of the Application for Invention

DD01 Delivery of document by public notice

Addressee: Zhou Wenjun

Document name: Notification of before Expiration of Request of Examination as to Substance

C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20110330