CN205327442U - Large tracts of land can be opened up solar energy and turned over board - Google Patents
Large tracts of land can be opened up solar energy and turned over board Download PDFInfo
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- CN205327442U CN205327442U CN201620029714.XU CN201620029714U CN205327442U CN 205327442 U CN205327442 U CN 205327442U CN 201620029714 U CN201620029714 U CN 201620029714U CN 205327442 U CN205327442 U CN 205327442U
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- straight pin
- set square
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- compound hinges
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Abstract
The utility model provides a large tracts of land can be opened up solar energy and turned over board, the base that this solar energy turned over the board welds in the satellite main part, the second side lever is connected with the base through the 12 cylindric lock, first side lever is connected with the second side lever through the 9th cylindric lock, first rotor plate and second rotor plate are installed on the 9th cylindric lock, and can rotate around the 9th cylindric lock, the second cylindric lock welds in first side lever top, the multiple hinge is by the first rotator of multiple hinge, multiple hinge second rotator, multiple hinge third rotator and the combination of multiple hinge fourth rotator form. This solar energy turns over the board and adopts the form that becomes born of the same parents mechanism, has stronger controllability, and it not only has the function that the secondary expanded, and sunshine is received better to the angle that can adjust solar panel moreover in a flexible way.
Description
Technical field
This utility model relates to a kind of space flight mechanical field, and particularly a kind of large area can open up solar energy turnover panel。
Background technology
In recent years, along with the development of human society, the dependence of satellite is also become increasingly stronger by people, and the satellite of purposes of all kinds is issued in space by the mankind, have equipped with astronomical observation equipment, be used for carrying out astronomical observation；Have equipped with communication relay equipment, be used for relay the communication signals such as broadcast, TV, data communication, phone；Have equipped with scientific research equipment, can be used to carry out the special producing under the agravic condition of scientific research and space, therefore, the status of satellite is also more and more important, but the premise that satellite has needed these tasks is to have energy supply endlessly, these energy sources in solar energy turnover panel, so, the status of solar energy turnover panel is also indispensable。Current solar energy turnover panel all adopts the form that plane is pulled open mostly, there is certain defect in developed area and motility, it is therefore necessary to design the solar energy turnover panel of a kind of energy large area expansion and flexible overturning。
Have not yet to see and a kind of can large area launch overturn flexibly again, and there is the innovation design of the solar energy turnover panel of higher controllability。
Summary of the invention
The purpose of this utility model is to provide a kind of large area can open up solar energy turnover panel, it can large area launch again can flexible angle adjustment, and there is higher controllability, allow solar energy turnover panel absorb the energy better。
This utility model is achieved through the following technical solutions above-mentioned purpose: a kind of large area can open up solar energy turnover panel, the base of this solar energy turnover panel is welded in satellite main body, second side lever is connected with base by the 12nd straight pin, first side lever is connected by the 9th straight pin and the second side lever, first swivel plate and the second swivel plate are arranged on the 9th straight pin, and can rotate around the 9th straight pin, second straight pin is welded in the little coffin at the first side lever top, compound hinges is by compound hinges the first rotary body, compound hinges the second rotary body, compound hinges the 3rd rotary body and compound hinges the 4th rotary body combine, compound hinges the first rotary body and compound hinges the second rotary body are connected by the second straight pin and the first side lever, compound hinges the 3rd rotary body is connected with compound hinges the first rotary body by the 8th straight pin, compound hinges the 4th rotary body is connected with compound hinges the second rotary body by the 7th straight pin, straight-bar is connected with compound hinges the 4th rotary body by the tenth straight pin, triangle pole is connected with compound hinges the 3rd rotary body by the 11st straight pin, straight-bar is connected by the first straight pin with triangle pole, solar panels can be opened up be connected with triangle pole by the 3rd straight pin, solar panels can be opened up by the first set square, second set square, 3rd set square, 4th set square and the 5th set square composition, first set square is connected by the 3rd straight pin and the second set square, second set square is connected by the 4th straight pin and the 3rd set square, 3rd set square is connected by the 5th straight pin and the 4th set square, 4th set square is connected by the 6th straight pin and the 5th set square, runner fixed body is welded in satellite main body, runner is installed on the circular trough of runner fixed body by the round key of self, and can rotate around runner fixed body, first Hooke's hinge one end is connected on runner, the other end is connected with Hooke's hinge connecting rod, second Hooke's hinge one end is connected with the second side lever, the other end is connected with Hooke's hinge connecting rod。
Described first side lever top is provided with a coffin, and the second straight pin is welded in this coffin。
Described straight-bar side is milled with elongated slot。
The side of described triangle pole the first side lever is milled with long key, and this long key coordinates with the elongated slot on straight-bar。
It is milled with round key inside described runner。
Being milled with circular trough on described runner fixed body, this circular trough matches with the round key on runner。
Of the present utility model have the prominent advantages that:
1, this solar energy turnover panel has the function of second outspread; first it is be transformed into flat state from spatiality; then deploying solar energy plate on the basis of flat state; form large-area solar panels; this solar energy turnover panel has extremely strong ductile; and when closure state, take up room little, it is possible to effectively protect panel when vile weather。
2, the solar panels opened up of this solar energy turnover panel rotate within the scope of 0 °～180 ° under the drive of side lever, and the first swivel plate and the second swivel plate can rotate around side lever, to adapt to the irradiating angle of sunlight, have extremely strong motility and adaptability。
3, this solar energy turnover panel is in the process opened or close, and mechanism is become single-degree-of-freedom from two-freedom, and movement locus is more accurate, moves more steady。
Accompanying drawing explanation
Fig. 1 is the front view that large area described in the utility model can open up under solar energy turnover panel half deployed condition。
Fig. 2 is the top view that large area described in the utility model can open up under solar energy turnover panel fully closed condition。
Fig. 3 is the schematic diagram opened up under solar panels deployed condition described in the utility model。
Fig. 4 is the front view of triangle pole described in the utility model。
Fig. 5 is the top view of compound hinges described in the utility model。
Fig. 6 is the front view of compound hinges described in the utility model。
Fig. 7 is the assembling schematic diagram of the first swivel plate described in the utility model and the second swivel plate。
Fig. 8 is the front view of straight-bar described in the utility model。
Fig. 9 is the front view of rotating disk fixed body described in the utility model。
Figure 10 is the front view of rotating disk described in the utility model。
Figure 11 is the top view that large area described in the utility model can open up solar energy turnover panel its fully unfolded position。
Figure 12 is that large area described in the utility model can open up solar energy turnover panel state transition diagram。
Figure is labeled as: 1. the first straight pin；2. triangle pole；3. can open up solar panels；4. straight-bar；5. compound hinges；6. the second swivel plate；7. the first swivel plate；8. the first side lever；9. the first Hooke's hinge；10. Hooke's hinge connecting rod；11. the second Hooke's hinge；12. base；13. satellite main body；14. runner；15. runner fixed body；16. the second straight pin；17. the first set square；18. the 3rd straight pin；19. the second set square；20. the 4th straight pin；21. the 3rd set square；22. the 5th straight pin；23. the 4th set square；24. the 6th straight pin；25. the 5th set square；26. the 7th straight pin；27. compound hinges the 4th rotary body；28. the 8th straight pin；29. compound hinges the 3rd rotary body；30. compound hinges the first rotary body；31. compound hinges the second rotary body；32. the second side lever；33. the 9th straight pin；34. the tenth straight pin；35. the 11st straight pin；36. the 12nd straight pin。
Detailed description of the invention:
Below in conjunction with drawings and Examples, the technical solution of the utility model is further described。
As shown in Figure 1, Figure 2, shown in Fig. 3, Fig. 5 and Fig. 6, large area described in the utility model can be opened up solar energy turnover panel, concrete structure and annexation and is:
The base 12 of this solar energy turnover panel is welded in satellite main body 13, second side lever 32 is connected with base 12 by the 12nd straight pin 36, first side lever 8 is connected with the second side lever 32 by the 9th straight pin 33, first swivel plate 7 and the second swivel plate 6 are arranged on the 9th straight pin 33, and can rotate around the 9th straight pin 33, second straight pin 16 is welded in the first side lever 8 top, compound hinges 5 is by compound hinges the first rotary body 30, compound hinges the second rotary body 31, compound hinges the 3rd rotary body 29 and compound hinges the 4th rotary body 27 combine, compound hinges the first rotary body 30 and compound hinges the second rotary body 31 are connected with the first side lever 8 by the second straight pin 16, compound hinges the 3rd rotary body 29 is connected with compound hinges the first rotary body 30 by the 8th straight pin 28, compound hinges the 4th rotary body 27 is connected with compound hinges the second rotary body 31 by the 7th straight pin 26, straight-bar 4 is connected with compound hinges the 4th rotary body 27 by the tenth straight pin 34, triangle pole 2 is connected with compound hinges the 3rd rotary body 29 by the 11st straight pin 35, straight-bar 4 is connected by the first straight pin 1 with triangle pole 2, solar panels 3 can be opened up be connected with triangle pole 2 by the 3rd straight pin 18, solar panels 3 can be opened up by the first set square 17, second set square 19, 3rd set square 21, 4th set square 23 and the 5th set square 25 form, first set square 17 is connected with the second set square 19 by the 3rd straight pin 18, second set square 19 is connected with the 3rd set square 21 by the 4th straight pin 20, 3rd set square 21 is connected with the 4th set square 23 by the 5th straight pin 22, 4th set square 23 is connected with the 5th set square 25 by the 6th straight pin 24, runner fixed body 15 is welded in satellite main body 13, runner 14 is installed on the circular trough of runner fixed body 15 by the round key of self, and can rotate around runner fixed body 15, first Hooke's hinge 9 one end is connected on runner 14, the other end is connected with Hooke's hinge connecting rod 10, second Hooke's hinge 11 one end is connected with the second side lever 32, the other end is connected with Hooke's hinge connecting rod 10。
Operation principle of the present utility model is:
Owing to this solar energy turnover panel has symmetrical structure, being made up of six identical unit, the structure of each unit is all identical with motion mode, therefore, here only analyzes the operation principle of a unit, and the operation principle of remaining element is all identical。Unit is by first Hooke's hinge the 9, second Hooke's hinge 11, Hooke's hinge connecting rod the 10, first side lever the 8, second side lever the 32, first swivel plate the 7, second swivel plate 6, compound hinges 5, triangle pole 2, straight-bar 4 and can open up solar panels 3 and forms, when satellite is not transmitted in space, solar energy turnover panel is in fully closed condition；After satellite launch success, solar energy turnover panel needs to launch, first triangle pole 2 and straight-bar 4 is made to rotate from inside to outside respectively around the tenth straight pin the 34 and the 11st straight pin 35, turn to the plane residing for triangle pole 2 parallel with the plane residing for the first side lever 8 time stop operating, then rotating wheel 14, runner 14 is by pulling Hooke's hinge connecting rod 10 to rotate with the annexation of the second Hooke's hinge 11, thus pulling the second side lever 32 around the 12nd straight pin 36 to external rotation, can rotate in the scope of 0 °～180 °, stop operating when turning to suitable angle, solar energy turnover panel completes first time expansion, now to launch to open up solar panels 3 and complete second time expansion, second set square 19 can rotate around the 3rd straight pin 18, 3rd set square 21 can rotate around the 4th straight pin 20, 4th set square 23 can rotate around the 5th straight pin 22, 5th set square 25 can rotate around the 6th straight pin 24, rotate the second set square 19 successively, 3rd set square 21, 4th set square 23 and the 5th set square 25 make to open up solar energy turnover panel to launch, solar energy turnover panel completes second time to launch。First swivel plate 7 and the second swivel plate 6 can rotate around the 9th straight pin 33, to adjust the angle of absorbing light photograph。Otherwise, when solar energy turnover panel needs to close, opposite direction rotating wheel 14, runner 14 is by pulling Hooke's hinge connecting rod 10 to rotate with the annexation of the second Hooke's hinge 11, thus pulling the second side lever 32 inwardly to rotate around the 12nd straight pin 36, in the process rotated, long key on triangle pole 2 overlaps with the elongated slot on straight-bar 4 gradually, when being completely superposed, mechanism's topological structure changes, now degree of freedom becomes one from two, second side lever 32 cannot be further continued for inside rotation, only triangle pole 2 and straight-bar 4 rotate respectively around the tenth straight pin the 34 and the 11st straight pin 35 ecto-entad, directly forward fully closed condition to。In the process that mechanism runs, compound hinges 5 act as the effect that ball is secondary, and it is to be combined along the revolute pair of x-axis, y-axis and z-axis by axis, as shown in Figure 5 and Figure 6。
Claims (6)
1. a large area can open up solar energy turnover panel, it is characterized in that, the base of this solar energy turnover panel is welded in satellite main body, second side lever is connected with base by the 12nd straight pin, first side lever is connected by the 9th straight pin and the second side lever, first swivel plate and the second swivel plate are arranged on the 9th straight pin, and can rotate around the 9th straight pin, second straight pin is welded in the coffin at the first side lever top, compound hinges is by compound hinges the first rotary body, compound hinges the second rotary body, compound hinges the 3rd rotary body and compound hinges the 4th rotary body combine, compound hinges the first rotary body and compound hinges the second rotary body are connected by the second straight pin and the first side lever, compound hinges the 3rd rotary body is connected with compound hinges the first rotary body by the 8th straight pin, compound hinges the 4th rotary body is connected with compound hinges the second rotary body by the 7th straight pin, straight-bar is connected with compound hinges the 4th rotary body by the tenth straight pin, triangle pole is connected with compound hinges the 3rd rotary body by the 11st straight pin, straight-bar is connected by the first straight pin with triangle pole, solar panels can be opened up be connected with triangle pole by the 3rd straight pin, solar panels can be opened up by the first set square, second set square, 3rd set square, 4th set square and the 5th set square composition, first set square is connected by the 3rd straight pin and the second set square, second set square is connected by the 4th straight pin and the 3rd set square, 3rd set square is connected by the 5th straight pin and the 4th set square, 4th set square is connected by the 6th straight pin and the 5th set square, runner fixed body is welded in satellite main body, runner is installed on the circular trough of runner fixed body by the round key of self, and can rotate around runner fixed body, first Hooke's hinge one end is connected on runner, the other end is connected with Hooke's hinge connecting rod, second Hooke's hinge one end is connected with the second side lever, the other end is connected with Hooke's hinge connecting rod。
2. large area according to claim 1 can open up solar energy turnover panel, it is characterised in that: described first side lever top is provided with a coffin, and the second straight pin is welded in this coffin。
3. large area according to claim 1 can open up solar energy turnover panel, it is characterised in that: described straight-bar side is milled with elongated slot。
4. large area according to claim 1 can open up solar energy turnover panel, it is characterised in that: the side of described triangle pole the first side lever is milled with long key, and this long key coordinates with the elongated slot on straight-bar。
5. large area according to claim 1 can open up solar energy turnover panel, it is characterised in that: it is milled with round key inside described runner。
6. large area according to claim 1 can open up solar energy turnover panel, it is characterised in that: being milled with circular trough on described runner fixed body, this circular trough matches with the round key on runner。
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620029714.XU CN205327442U (en) | 2016-01-13 | 2016-01-13 | Large tracts of land can be opened up solar energy and turned over board |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620029714.XU CN205327442U (en) | 2016-01-13 | 2016-01-13 | Large tracts of land can be opened up solar energy and turned over board |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205327442U true CN205327442U (en) | 2016-06-22 |
Family
ID=56196773
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620029714.XU Withdrawn - After Issue CN205327442U (en) | 2016-01-13 | 2016-01-13 | Large tracts of land can be opened up solar energy and turned over board |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205327442U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539880A (en) * | 2016-01-13 | 2016-05-04 | 广西大学 | Large-area unfoldable solar energy turnover plate |
| CN106965169A (en) * | 2017-04-06 | 2017-07-21 | 广西大学 | A kind of driving auxiliary equipment of mechanism type variable topological packaging robot |
| CN107792395A (en) * | 2017-09-25 | 2018-03-13 | 上海卫星工程研究所 | The deployable spacecraft of radome fairing primary integration heavy caliber |
| CN112550776A (en) * | 2020-12-10 | 2021-03-26 | 中国科学院空间应用工程与技术中心 | Foldable and unfoldable space platform |
-
2016
- 2016-01-13 CN CN201620029714.XU patent/CN205327442U/en not_active Withdrawn - After Issue
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539880A (en) * | 2016-01-13 | 2016-05-04 | 广西大学 | Large-area unfoldable solar energy turnover plate |
| CN106965169A (en) * | 2017-04-06 | 2017-07-21 | 广西大学 | A kind of driving auxiliary equipment of mechanism type variable topological packaging robot |
| CN107792395A (en) * | 2017-09-25 | 2018-03-13 | 上海卫星工程研究所 | The deployable spacecraft of radome fairing primary integration heavy caliber |
| CN107792395B (en) * | 2017-09-25 | 2021-02-19 | 上海卫星工程研究所 | Radome fairing main satellite integrated large-caliber deployable spacecraft |
| CN112550776A (en) * | 2020-12-10 | 2021-03-26 | 中国科学院空间应用工程与技术中心 | Foldable and unfoldable space platform |
| CN112550776B (en) * | 2020-12-10 | 2022-06-07 | 中国科学院空间应用工程与技术中心 | Foldable and unfoldable space platform |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20160622 Effective date of abandoning: 20171013 |