CN100554816C - Heliostat device - Google Patents

Heliostat device Download PDF

Info

Publication number
CN100554816C
CN100554816C CN 200510039114 CN200510039114A CN100554816C CN 100554816 C CN100554816 C CN 100554816C CN 200510039114 CN200510039114 CN 200510039114 CN 200510039114 A CN200510039114 A CN 200510039114A CN 100554816 C CN100554816 C CN 100554816C
Authority
CN
China
Prior art keywords
level crossing
guiding mechanism
general frame
axle sleeve
heliostat device
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.)
Expired - Fee Related
Application number
CN 200510039114
Other languages
Chinese (zh)
Other versions
CN1687669A (en
Inventor
张耀明
张文进
张振远
孙利国
刘晓晖
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ZHANG YAOMING ZHANG ZHENYUAN ZHANG WENJIN
ZHANG YAOMING ZHANG ZHENYUAN Z
Original Assignee
ZHANG YAOMING ZHANG ZHENYUAN ZHANG WENJIN
ZHANG YAOMING ZHANG ZHENYUAN Z
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 ZHANG YAOMING ZHANG ZHENYUAN ZHANG WENJIN, ZHANG YAOMING ZHANG ZHENYUAN Z filed Critical ZHANG YAOMING ZHANG ZHENYUAN ZHANG WENJIN
Priority to CN 200510039114 priority Critical patent/CN100554816C/en
Publication of CN1687669A publication Critical patent/CN1687669A/en
Application granted granted Critical
Publication of CN100554816C publication Critical patent/CN100554816C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • 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
    • Y02E10/40Solar thermal energy, e.g. solar towers
    • Y02E10/47Mountings or tracking

Landscapes

  • Mounting And Adjusting Of Optical Elements (AREA)

Abstract

The present invention relates to a kind of heliostat device, belong to application of solar.This device comprises level crossing group, azimuth guiding mechanism, elevation angle guiding mechanism, alignment sensor and control circuit, wherein the axis of transverse axis and vertical shaft is positioned at same plane and intersects vertically, the geometric center of level crossing group is positioned at the intersection point of two axial lines, and the line between the center line of alignment sensor and two axial lines intersection point and the projection target's center's point overlaps.After adopting the present invention, how does not move at each position of pipe unit, the geometric center physical location of level crossing is motionless all the time, had real motionless physical space central point just because of single unit system, and between heart point and the impact point alignment sensor has been installed hereinto, therefore eliminated the intrinsic systematic error that prior art exists, there is not theoretical error in the mechanism design that had both realized whole device, thereby the sunshine that is guaranteed to incide on the level crossing can accurately be invested impact point after reflection all the time.

Description

Heliostat device
Technical field
The present invention relates to a kind of plane mirror devices of directed projection sunshine, promptly be commonly referred to the device of heliostat, belong to application of solar.
Background technology
Heliostat device as its name suggests, its effect is that sunshine is accurately positioned on certain target, is commonly used to the optically focused parts as solar energy light collecting lighting device or heat generating system.
Along with the continuous development of solar utilization technique,, wish during design that heliostat device has enough tracking accuracies in order to obtain desirable daylighting effect.Yet, to understand according to the applicant, the tracking of existing heliostat device all has approximation, can't satisfy the instructions for use of scientific and technological progress to the tracking accuracy increasingly stringent.
Finding the geneogenous systematic error of design ubiquity of existing heliostat device through intensive research back.Concrete condition is as follows:
In general, when using, need place by heliostat the device of solar receiver and so at the target place that sets, because its tracking accuracy is to the receiver performance or utilize effect can produce direct influence, therefore in order to satisfy the requirement on settled date, should require a bit in the heliostat device operation process, maintaining static all the time in the level crossing, otherwise will there be inherent shortcoming in heliostat device, influence tracking accuracy.
Existing heliostat device generally adopts the two intersecting axle mechanical transmission mechanisms that can produce compound motion to drive, and the transverse axis mechanism in two intersecting axles is superimposed upon in the vertical shaft mechanism.Because structure limited (for example in order to avoid transverse axis), the geometric center point of level crossing can only be designed to the position of as far as possible close two intersecting axle intersection points, does not therefore all satisfy above-mentioned requirements basically--a bit in the heliostat device operation process, maintaining static all the time in the level crossing.As a result, in operation process, can only ignore the error that causes thus in fact, can only allow receiver tolerate this error when designing in other words.
This level crossing departs from the systematic error notion that error that ideal position causes can use in the physics explains, or is further defined as intrinsic systematic error.For example, the heliostat device that adopts in sun I number of building up in the Southern California of the U.S. and the II number tower electricity generation system has adopted typical two intersecting axle mechanical transmission mechanisms, wherein the transverse axis mechanism rack is located in the vertical shaft mechanism, but the level crossing general frame all is installed on the transverse axis, about 150 millimeters away from distance of transverse axis axis be of level crossings--there is intrinsic systematic error.
When the heliostat device area was big, transverse axis was in order to bear bigger load, the corresponding overstriking of diameter, and the systematic error of device itself will be big more as a result.
In addition, the transverse axis and the vertical shaft two axial lines itself of existing heliostat device also usually are the non-space quadrature, thereby have further aggravated the intrinsic systematic error of heliostat device.
Facts have proved that the existence of this intrinsic systematic error makes heliostat to follow the tracks of the sun by approximate rule, in any case mate the position of alignment sensor and take which kind of remedial measure, all can not satisfy the requirement that pinpoint accuracy is followed the tracks of.
Summary of the invention
The technical problem to be solved in the present invention is: at the shortcoming that above prior art exists, propose a kind of eliminate above-mentioned intrinsic systematic error heliostat device, thereby significantly improve tracking accuracy, satisfy the designing requirement that modernized solar energy utilizes facility.
In order to solve above technical problem, heliostat device of the present invention comprises the level crossing group that is installed on the general frame, drive the azimuth guiding mechanism that general frame rotates around the vertical shaft axis, be superimposed upon on the guiding mechanism of azimuth, drive the elevation angle guiding mechanism that general frame rotates around the transverse axis axis, alignment sensor, and be input with the alignment sensor, control the control circuit of above-mentioned guiding mechanism drive motors corner, it is characterized in that: the axis of described transverse axis and vertical shaft is positioned at same plane and intersects vertically, the geometric center of described level crossing group is positioned at the intersection point of described two axial lines, and the line between the center line of described alignment sensor and two axial lines intersection point and the projection target's center's point overlaps.
After adopting above technical scheme of the present invention, how does not move at each position of pipe unit, the geometric center physical location of level crossing is motionless all the time, had real motionless physical space central point just because of single unit system, and between heart point and the impact point alignment sensor has been installed hereinto, therefore eliminated the intrinsic systematic error that prior art exists, there is not theoretical error in the mechanism design that had both realized whole device, thereby the sunshine that is guaranteed to incide on the level crossing can accurately be invested impact point after reflection all the time.
Description of drawings
The present invention is further illustrated below in conjunction with accompanying drawing.
Fig. 1-1,1-2,2 are the structural representation of the embodiment of the invention one.
Fig. 3,4 is the embodiment of the invention one a magnitude range sensor construction schematic diagram.
Fig. 5 is the embodiment of the invention one a systematic error schematic diagram.
Fig. 6 is the embodiment of the invention one a midplane mirror cross-sectional view.
Fig. 7,8,9 is the embodiment of the invention one a midplane mirror surface radian micro-adjusting mechanism schematic diagram.
Figure 10,11 is the structural representation of the embodiment of the invention two.
Figure 12,13 is the structural representation of the embodiment of the invention three.
Figure 14 is that the A of Figure 11, Figure 13 is to view.
The specific embodiment
Embodiment one
The structural representation of present embodiment heliostat device as shown in Figure 1, 2, comprise 9 plate plane mirrors and general frame 1 thereof, drive the elevation angle guiding mechanism that level crossing and general frame 1 thereof rotate around transverse axis axis AB, drive the azimuth guiding mechanism that level crossing and general frame 1 thereof rotate around vertical shaft axis CD, and alignment sensor.The two axial lines AB of transverse axis and vertical shaft, CD orthogonal space are in an O, and the geometric center of 9 plate plane mirror assemblys is the center of mid-plane mirror 1 ', and O overlaps with orthogonal space point.The central axis of alignment sensor overlaps (its concrete structure is narrated in the back) with the crossing point of axes O of two intersecting axle mechanisms and the line between projection target's center's point.
The azimuth guiding mechanism is made up of the vertical shaft 2 that is fixed in base surface, four runners having two side stands 3,3 ' underframe 4 and be positioned at 4 four jiaos on underframe, one of them runner is motor-driven driving wheel (not shown), driven by worm and gear, other three runners are driven pulley.Worm and gear drives underframe 4 and does azimuthal adjustment around vertical shaft axis CD rotation under drive motors drives.
Be fixed with the transverse axis axle sleeve of two coaxial lines in the member neutral of level crossing general frame 1, two axle sleeves are supported in two side stands 3, the 3 ' upper end of azimuth guiding mechanism respectively by bearing block 5,5 ', and the horizontal geometric center lines of 9 plate plane mirror assemblys overlaps with transverse axis axle sleeve axis AB.
The elevation angle guiding mechanism is made up of leading screw 6, nut 7 and their supporting seat, axle sleeve and bearing block 5,5 ' thereof, the supporting seat of leading screw 6 one ends is connected with general frame 1, the supporting seat of nut 7 is connected with connector 8 between two stands 3,3 ', under the drive of drive motors, leading screw 6 rotates in nut 7, promote general frame 1 and rotate, adjust the elevation angle of general frame 1 around axle sleeve axis AB.
The structure of alignment sensor as shown in Figure 3, Figure 4, central axis O 1O 2Overlap with the crossing point of axes of two intersecting axle mechanisms and the line between projection target's center's point.Sensor is combined by the sensor on a large scale 15 of the sensor among a small circle 14 of surveying the low-angle deviation and detection wide-angle deviation.Sensor 14 mainly is made up of four-quadrant light-sensitive element 17 and lens 16 among a small circle, and four-quadrant light-sensitive element 17 is positioned at around lens 16 focuses.Sensor 15 is made of photoarray I, the II, III, the IV that arrange along four orientation of East, West, South, North on a large scale, and the light-sensitive element in each array is arranged as shown in Figure 4.When the wide-angle deviation appears in heliostat, light-sensitive element in certain an array of sensor 15 or the two adjacent arrays must receive optical signal on a large scale, rotate towards respective direction thereby drive heliostat device, enter the crossing point of axes O of sensor 14 and the line coincidence (its concrete structure is narrated in the back) between the projection target's center point among a small circle.
The azimuth guiding mechanism is made up of the vertical shaft 2 that is fixed in base surface, four runners having two side stands 3,3 ' underframe 4 and be positioned at 4 four jiaos on underframe, one of them runner is motor-driven driving wheel (not shown), driven by worm and gear, other three runners are driven pulley.Worm and gear drives underframe 4 and does azimuthal adjustment around vertical shaft axis CD rotation under drive motors drives.
Be fixed with the transverse axis axle sleeve of two coaxial lines in the member neutral of level crossing general frame 1, two axle sleeves are supported in two side stands 3, the 3 ' upper end of azimuth guiding mechanism respectively by bearing block 5,5 ', and the horizontal geometric center lines of 9 plate plane mirror assemblys overlaps with transverse axis axle sleeve axis AB.
The elevation angle guiding mechanism is made up of leading screw 6, nut 7 and their supporting seat, axle sleeve and bearing block 5,5 ' thereof, the supporting seat of leading screw 6 one ends is connected with general frame 1, the supporting seat of nut 7 is connected with connector 8 between two stands 3,3 ', under the drive of drive motors, leading screw 6 rotates in nut 7, promote general frame 1 and rotate, adjust the elevation angle of general frame 1 around axle sleeve axis AB.Leading screw one end supporting seat is connected with azimuth guiding mechanism stand.
The structure of alignment sensor as shown in Figure 3, Figure 4, central axis O 1O 2Overlap with the crossing point of axes of two intersecting axle mechanisms and the line between projection target's center's point.Sensor is combined by the sensor on a large scale 15 of the sensor among a small circle 14 of surveying the low-angle deviation and detection wide-angle deviation.Sensor 14 mainly is made up of four-quadrant light-sensitive element 17 and lens 16 among a small circle, and four-quadrant light-sensitive element 17 is positioned at around lens 16 focuses.Sensor 15 is made of photoarray I, the II, III, the IV that arrange along four orientation of East, West, South, North on a large scale, and the light-sensitive element in each array is arranged as shown in Figure 4.When the wide-angle deviation appears in heliostat, light-sensitive element in certain an array of sensor 15 or the two adjacent arrays must receive optical signal on a large scale, thereby driving heliostat device rotates towards respective direction, enter sensor 142 among a small circle "; this means that there is unsurmountable systematic error in device itself, improve the precision of other parts in any case and all can't eliminate this error.
Need to prove in addition, when heliostat will incide its surperficial sunshine and reflex to the receiver that the impact point place is provided with, come down to sunshine and be concentrated on the receiver place, in order to make the sunshine of every plate plane mirroring not produce excessive defocusing, level crossing itself preferably has certain surperficial small radian of similar concave mirror, so just the sun optically focused of energy generation rule.Level crossing in the embodiment of the invention relies on glass and the surface curvature micro-adjusting mechanism thereof with special construction, has reached above-mentioned purpose.
Particularly, 9 plate plane mirrors have same double glazing special construction, are made of back side silvered glass and simple glass, accompany the PVB glued membrane between the layer glass, as shown in Figure 6.Adopt this structure that two big benefits are arranged, the one, the silver coating in the middle of having protected is avoided atmospheric corrosion; The 2nd, help taking surface curvature micro-adjusting mechanism as described below to finely tune the surperficial radian of level crossing, make it to produce the spotlight effect of similar concave mirror.
The mechanism of fine setting level crossing surface curvature is a nut bolt mechanism, and shown in Fig. 7,8,9, Fig. 7 is a front view, and Fig. 8 is a rearview, and Fig. 9 is that the A of Fig. 8 is to view.This mechanism is by the shaped as frame carriage 9 with cross member 13, be positioned at 8 pushing tow nut bolt (a of four jiaos on carriage, a ', b, b ', c, c ', d, d '), clamp nut bolt (the A of all frames of carriage, B, C, D, E, F, G, H), the adjusting nut bolt of center, glass blocks 10 compositions such as grade, pushing tow nut bolt and the clamp nut bolt of all frame of every plate plane mirror by four jiaos is supported on separately the shaped as frame carriage 9, the adjusting bolt 11 of center passes cross member 13, fixedly connected with glass blocks 10 in its end, glass blocks 10 is fixedlyed connected with the simple glass layer of level crossing, is combined on two nuts 12 regulating on the bolt 11,12 ' lays respectively at cross member 13 both sides.The effect of the combination adjusting by pushing tow nut bolt and clamp nut bolt and the adjusting nut bolt of center just can obtain the level crossing of certain curvature, produces the optically focused hot spot of similar concave mirror.
Above-mentioned complete heliostat device is because level crossing assembly center overlaps the error of the system of having eliminated own with the crossing point of axes of two intersecting axle mechanisms; And adopted specific glass planar mirror and curvature micro-adjusting mechanism thereof, can realize the optics requirement of level crossing optically focused economically; Adopt large and small range sensor to unite the positioning function of the heliostat device of finishing large and small angular deviation more exactly.Therefore, overall plan science, reasonable, practical, economic, strong operability, precision height.
Embodiment two
The basic condition of present embodiment is identical with embodiment one, the main distinction is: (1) is as Figure 10, shown in Figure 11, general frame 1 is limited between two stands 3,3 ' of azimuth guiding mechanism, general frame 1 both sides are fixed two coaxial axle sleeves respectively, and be supported in two side stands 3,3 ' upper end by bearing block 5,5 ' respectively, and keep the horizontal geometric center lines of all level crossing assemblys to overlap equally with axle sleeve axis AB, the center of all level crossing assemblys is the center of mid-plane mirror, overlaps with the intersection point O of two intersecting axle pivot centers of orthogonal space.(2) this heliostat device also comprises an anti-wind mechanism that depends on feed screw nut elevation angle guiding mechanism, mainly forms (referring to the A of Figure 11 to enlarged drawing) by a cover electromagnetic clutch mechanism 18, axle sleeve 19 and steel wire rope 20.Its bottom bracket axle 19 is connected with motor output shaft by key, electromagnetic clutch mechanism 18 is placed on the motor output shaft, steel wire rope 20 1 ends are connected with general frame 1, the screw-nut body of this moment is installed on the lateral location of general frame shown in Figure 10 1, and is connected by latch 21 between leading screw one end and the axle sleeve.When weather was normal, electromagnetic clutch mechanism 18 threw off with axle sleeve 19, and the screw-nut body proper function satisfies the power needs that general frame 1 elevation angle is adjusted; When learning that from weather forecast the strong wind bad weather may occur, the latch 21 that is connected between leading screw one end and the axle sleeve 19 is pulled out, in electromagnetic clutch mechanism 18 and axle sleeve 19 adhesives, this moment, the driven by motor steel wire rope was constantly reeled, rotate to horizontal level until level crossing and general frame 1 thereof, flat mirror reflects faces down.Like this, both can guarantee heliostat device front face area minimum, again can be so that minute surface is avoided foreign matter attack and dust coverings such as hail.
Can inference, the device of present embodiment can reach the locating effect that embodiment one brings fully, eliminates systematic error.
Embodiment three
The basic condition of present embodiment is identical with embodiment two, and the main distinction is: shown in Figure 12,13, the azimuth guiding mechanism is not the underframe form, but directly adopts worm and gear, and worm-wheel shaft 14 is connected in vertical shaft; Be fixed with an axle sleeve in the middle neutral of the member of level crossing general frame 1, axle sleeve is supported in vertical shaft 14 upper ends of azimuth guiding mechanism, the horizontal geometric center lines of all level crossing assemblys and axle sleeve dead in line by bearing block 15.
The elevation angle guiding mechanism still adopts leading screw and nut mechanism, and the center of all level crossing assemblys still overlaps with the two axial lines intersection point.Compare with embodiment one, two, though there is not the level crossing on the practical significance in the center of all level crossing assemblys, but can when design, allow the spacing between the level crossing of both sides dwindle as far as possible, the position of alignment sensor so still can rationally be set, guarantee the certain tracking accuracy of heliostat device.
Except that above embodiment, the present invention also has other numerous embodiments.Every those skilled in the art are done on basis of the present invention is equal to and replaces or similar combined transformation all belongs to this patent protection domain.
In addition to the implementation, the present invention can also have other embodiments.For example, driving level crossing and general frame thereof is hydraulic gear around the elevation angle guiding mechanism that the transverse axis axis rotates.All employings are equal to the technical scheme of replacement or equivalent transformation formation, all drop on the protection domain of requirement of the present invention.

Claims (10)

1. heliostat device, comprise the level crossing group that is installed on the general frame, drive the azimuth guiding mechanism that general frame rotates around the vertical shaft axis, be superimposed upon on the guiding mechanism of azimuth, drive the elevation angle guiding mechanism that general frame rotates around the transverse axis axis, alignment sensor, and be input with the alignment sensor, control the control circuit that above-mentioned guiding mechanism drive motors rotates, it is characterized in that: the axis of described transverse axis and vertical shaft is positioned at same plane and intersects vertically, the geometric center of described level crossing group is positioned at the intersection point of described two axial lines, and the line between the center line of described alignment sensor and two axial lines intersection point and the projection target's center's point overlaps.
2. heliostat device according to claim 1 is characterized in that: described level crossing has double-layer glass structure, is made of back side silvered glass and simple glass, accompanies the PVB glued membrane between the layer glass.
3. heliostat device according to claim 2, it is characterized in that: described level crossing comprises the nut bolt mechanism of fine setting level crossing surface curvature, this mechanism is by the shaped as frame carriage with cross member, be positioned at the pushing tow nut bolt of four jiaos on carriage, the clamp nut bolt of all frames of carriage, the adjusting nut bolt of center, the glass blocks that connects center adjusting nut bolt is formed, pushing tow nut bolt and the clamp nut bolt of all frame of every plate plane mirror by four jiaos is supported on separately the carriage, the adjusting bolt of center passes cross member, fixedly connected with glass blocks in its end, glass blocks is fixedlyed connected with the simple glass of level crossing, and two nuts are combined on respectively on the adjusting bolt that passes cross member.
4, heliostat device according to claim 1, it is characterized in that: the transverse axis axle sleeve that is fixed with two coaxial lines in the member neutral of described level crossing general frame, described two axle sleeves are supported in the two side stands upper end of azimuth guiding mechanism, the horizontal geometric center lines of all level crossing assemblys and axle sleeve dead in line respectively.
5, heliostat device according to claim 1, it is characterized in that: described level crossing general frame both sides are fixed with two coaxial axle sleeves respectively, described axle sleeve is supported in the vertical shaft upper end of azimuth mechanism, the horizontal geometric center lines of level crossing assembly and axle sleeve dead in line respectively.
6, heliostat device according to claim 1, it is characterized in that: be fixed with an axle sleeve in the middle neutral of the member of described level crossing general frame, described axle sleeve is supported in the vertical shaft upper end of azimuth guiding mechanism, the horizontal geometric center lines of all level crossing assemblys and axle sleeve dead in line.
7, heliostat device according to claim 1, it is characterized in that: described alignment sensor is made up of the sensor combination on a large scale of the sensor among a small circle of surveying the low-angle deviation and detection wide-angle deviation, described sensor among a small circle is made up of a four-quadrant light-sensitive element and lens, described four-quadrant light-sensitive element is positioned at around the lens focus, and described sensor on a large scale is made of the photoarray of four orientation layouts along the four corners of the world.
8, heliostat device according to claim 1, it is characterized in that: described driving level crossing and general frame thereof are screw-nut body around the elevation angle guiding mechanism that the transverse axis axis rotates, form by leading screw, nut, leading screw supporting seat, nut support seat and motor, the supporting seat of described leading screw one end is connected with general frame, described nut support seat is connected with connector between two stands, and the supporting seat of leading screw one end is connected with the stand of azimuth guiding mechanism.
9, heliostat device according to claim 1 is characterized in that: described driving level crossing and general frame thereof are hydraulic gear around the elevation angle guiding mechanism that the transverse axis axis rotates.
10, heliostat device according to claim 8, it is characterized in that: described heliostat device comprises an anti-wind mechanism that depends on described screw-nut body, mainly form by a cover electromagnetic clutch mechanism, axle sleeve and steel wire, described axle sleeve is connected with motor output shaft by key, steel wire rope one end is connected with general frame, described screw-nut body is installed on the side of general frame, and is connected by latch between leading screw one end and the axle sleeve.
CN 200510039114 2005-04-27 2005-04-27 Heliostat device Expired - Fee Related CN100554816C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200510039114 CN100554816C (en) 2005-04-27 2005-04-27 Heliostat device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200510039114 CN100554816C (en) 2005-04-27 2005-04-27 Heliostat device

Publications (2)

Publication Number Publication Date
CN1687669A CN1687669A (en) 2005-10-26
CN100554816C true CN100554816C (en) 2009-10-28

Family

ID=35305711

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 200510039114 Expired - Fee Related CN100554816C (en) 2005-04-27 2005-04-27 Heliostat device

Country Status (1)

Country Link
CN (1) CN100554816C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011072449A1 (en) 2009-12-17 2011-06-23 Wang Chengwei Heliostat device

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101187724B (en) * 2007-12-12 2010-06-02 中国科学院电工研究所 Heliostat support device
CN101261046B (en) * 2008-04-21 2012-12-12 北京航空航天大学 Solar energy heliostat gearing device
CN101614445B (en) * 2008-06-23 2010-11-10 中国华电工程(集团)有限公司 Method for improving accuracy of control of automatic sun track following of heliostat
CN101697030B (en) * 2009-10-23 2011-08-31 刘奇灵 Heliostat
DE102010054980A1 (en) * 2010-12-17 2012-06-21 Flabeg Holding Gmbh Fastening system for connecting two components together and method for fixing a mirror element, in particular for a solar collector module, to a support frame using such fastening system
CN103149943A (en) * 2013-01-21 2013-06-12 德州高科力液压有限公司 Solar reflection-type fixed target tracking control method
CN103306919B (en) * 2013-06-06 2016-03-02 国电青松吐鲁番新能源有限公司 Solar groove type heat build-up electricity generation system
CN104143293A (en) * 2014-06-06 2014-11-12 赵勇 Translucent mirror for mirror TV
CN108572665A (en) * 2017-03-13 2018-09-25 郭延达 Settled date tracing system based on sensing technology
CN110174908A (en) * 2019-06-14 2019-08-27 重庆科技学院 Heliostat direction regulating system and its control method
CN113740806B (en) * 2021-08-02 2024-03-22 中国资源卫星应用中心 Three-sided corner reflector and using method thereof
CN114576870A (en) * 2022-03-01 2022-06-03 西安热工研究院有限公司 Tower light and heat power station mirror surface adjusting device of fused salt

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011072449A1 (en) 2009-12-17 2011-06-23 Wang Chengwei Heliostat device

Also Published As

Publication number Publication date
CN1687669A (en) 2005-10-26

Similar Documents

Publication Publication Date Title
CN100554816C (en) Heliostat device
CN201828831U (en) Solar module array and polar shaft tracking device of solar collector
US20100307564A1 (en) Apparatus for two-way tracing and condensing sunlight of roof installation type
CN101236287A (en) Heliostat device
US9224898B2 (en) Coaxial drive tracking system for use with photovoltaic systems
CN1369956A (en) Photovoltaic electric generation system automatically tracking sun
CN111130444B (en) High-precision double-shaft solar tracking system and method for concentrating solar cell
JP2013513817A (en) A heliostat that controls the direction of reflection with a sensor
KR101131482B1 (en) Solar power generation system for high efficient
KR100922238B1 (en) Solar power generator
KR20120126804A (en) Solar Tracking Driver using Electrical Cylinder
CN1982752A (en) Mechanical transmission with light-selector omnibearing motion driven and solar system thereof
CN104699125A (en) Two-dimensional sun tracking device for electric speed reducer drive heliostat
CN201499107U (en) Sunlight autotracking and positioning device
CN104820436A (en) Electric speed reducer driving photovoltaic plate two-dimensional sun tracking apparatus
CN101728980A (en) Polar axis tracking device of solar collector
CN104483979B (en) One kind linkage heliostat
CN202189280U (en) High precision solar energy tracker
CN2518261Y (en) Photovoltaic generating system able to automatically tracking sun
CN101442279B (en) Earth axis type solar condense photovoltaic generating set
CN107178913B (en) Floating type point coke Fresnel optically focused energy-collecting device
CN203070103U (en) Simplified biaxial linkage-type solar photovoltaic power generation system
CN210532719U (en) Novel speed reduction transmission mechanism
CN209590644U (en) A kind of settled date mirror drive and heliostat
CN106026873A (en) Reflective type solar energy tracking bracket system

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20091028

Termination date: 20110427