TR201310355A2 - Single wing solar panel opening apparatus - Google Patents

Single wing solar panel opening apparatus

Info

Publication number
TR201310355A2
TR201310355A2 TR2013/10355A TR201310355A TR201310355A2 TR 201310355 A2 TR201310355 A2 TR 201310355A2 TR 2013/10355 A TR2013/10355 A TR 2013/10355A TR 201310355 A TR201310355 A TR 201310355A TR 201310355 A2 TR201310355 A2 TR 201310355A2
Authority
TR
Turkey
Prior art keywords
solar panels
solar panel
test
panel opening
opening apparatus
Prior art date
Application number
TR2013/10355A
Other languages
Turkish (tr)
Inventor
Küçükkaya Tolga
Yurtoğlu Emre
Yilmaz Fati̇h
Original Assignee
Tusas Tuerk Havacilik Ve Uzay Sanayii Anonim Sirketi
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 Tusas Tuerk Havacilik Ve Uzay Sanayii Anonim Sirketi filed Critical Tusas Tuerk Havacilik Ve Uzay Sanayii Anonim Sirketi
Priority to TR2013/10355A priority Critical patent/TR201310355A2/en
Publication of TR201310355A2 publication Critical patent/TR201310355A2/en
Priority to PCT/TR2014/000328 priority patent/WO2015034449A2/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G7/00—Simulating cosmonautic conditions, e.g. for conditioning crews
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M99/00—Subject matter not provided for in other groups of this subclass

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Photovoltaic Devices (AREA)

Abstract

Bu buluş, uyduların (S) tek yapraklı güneş panelleri (3) için tasarlanan ve 5 taşınabilir olan bir test düzeneği (1) ile ilgilidir. Buluşu konusu test düzeneği (1), tek yaprak güneş panelleri (3) için kullanım kolaylığı sağlaması, kolay değiştirilebilen denge ağırlığı (8) sayesinde farklı boyut ve ağırlıktaki güneş panellerinin (3) test edilebilmesi ve düşük maliyetli olması gibi avantajlara sahiptir. Bunun yanı sıra, buluş konusu test düzeneği (1) hem uydu (S) üzerindeki 10 güneş panellerinin (3) testinde hem de yalnızca güneş paneli (3) üretimindeki testlerde kullanılabilmektedir.The present invention relates to a test apparatus (1) designed for single-leaf solar panels (3) of satellites (S) and 5 being portable. The test mechanism (1) of the present invention has advantages such as providing ease of use for single-leaf solar panels (3), being able to test solar panels (3) of different sizes and weights thanks to the easily changeable balance weight (8), and being low cost. In addition, the inventive test setup (1) can be used both in testing 10 solar panels (3) on the satellite (S) and only in tests in the production of solar panels (3).

TR2013/10355A 2013-09-03 2013-09-03 Single wing solar panel opening apparatus TR201310355A2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
TR2013/10355A TR201310355A2 (en) 2013-09-03 2013-09-03 Single wing solar panel opening apparatus
PCT/TR2014/000328 WO2015034449A2 (en) 2013-09-03 2014-09-02 Single wing solar panel opening apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TR2013/10355A TR201310355A2 (en) 2013-09-03 2013-09-03 Single wing solar panel opening apparatus

Publications (1)

Publication Number Publication Date
TR201310355A2 true TR201310355A2 (en) 2014-06-23

Family

ID=52130771

Family Applications (1)

Application Number Title Priority Date Filing Date
TR2013/10355A TR201310355A2 (en) 2013-09-03 2013-09-03 Single wing solar panel opening apparatus

Country Status (2)

Country Link
TR (1) TR201310355A2 (en)
WO (1) WO2015034449A2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113479356A (en) * 2021-08-16 2021-10-08 哈尔滨工业大学 Dumbbell-shaped air floatation pulley longitudinal gravity compensation device

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CN105035370B (en) * 2015-07-31 2017-03-29 上海卫星工程研究所 Three-axis air-bearing table platform analog
CN106184835B (en) * 2016-08-12 2018-07-06 浙江工业大学 A kind of 90 degree of hanging expanding units of sun wing plate cantilevered
TR201710461A1 (en) * 2017-07-17 2019-02-21 Tusas Tuerk Havacilik Ve Uzay Sanayii Anonim Sirketi A bearing test apparatus.
CN109080860B (en) * 2018-06-11 2021-07-23 燕山大学 Global self-balancing gravity unloading device
CN110758782A (en) * 2019-11-22 2020-02-07 北京理工大学 Antenna Microgravity Simulation System
CN114701675A (en) * 2022-03-10 2022-07-05 天津航天机电设备研究所 Active following type zero-gravity unloading system for circular solar wing
CN114802832B (en) * 2022-04-19 2025-09-19 北京精密机电控制设备研究所 Microgravity simulation device combining ball bearing and reverse counterweight
CN114771887B (en) * 2022-04-21 2025-07-15 北京精密机电控制设备研究所 A microgravity simulation device based on magnetic constant force spring
CN116065304B (en) * 2023-03-07 2023-06-20 天津航天机电设备研究所 A machine-sewn connection process for composite substrates of a circular flexible solar wing of a spacecraft
CN117087881B (en) * 2023-08-31 2026-02-06 天津航天机电设备研究所 High-precision multistage telescopic mechanism
CN117262261B (en) * 2023-10-13 2025-12-19 北京零重空间技术有限公司 Multi-folded sailboard unfolding experiment testing device and testing method for spacecraft
CN119489955B (en) * 2025-01-20 2025-06-20 中山大学 One-dimensional pointing precision adjustable large mass optical load gravity unloading device

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3931753A1 (en) * 1989-09-22 1991-04-04 Deutsche Forsch Luft Raumfahrt DEVICE FOR SIMULATING ON THE EARTH OF OPERATIONS OF A MANIPULATOR USED IN SPACE ON A MODEL OF A SPACE VEHICLE
JP2000351400A (en) * 1999-06-10 2000-12-19 Toshiba Corp Deployable structure ground test equipment
KR101059441B1 (en) * 2008-11-26 2011-08-25 한국항공우주연구원 Zero gravity state providing device for deployment test of satellite solar panel

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113479356A (en) * 2021-08-16 2021-10-08 哈尔滨工业大学 Dumbbell-shaped air floatation pulley longitudinal gravity compensation device
CN113479356B (en) * 2021-08-16 2022-04-29 哈尔滨工业大学 Dumbbell-shaped air flotation pulley longitudinal gravity compensation device

Also Published As

Publication number Publication date
WO2015034449A2 (en) 2015-03-12
WO2015034449A3 (en) 2015-06-11

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