RU2010151175A - SOLAR BATTERY DISPLAY TEST STAND - Google Patents
SOLAR BATTERY DISPLAY TEST STAND Download PDFInfo
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- RU2010151175A RU2010151175A RU2010151175/11A RU2010151175A RU2010151175A RU 2010151175 A RU2010151175 A RU 2010151175A RU 2010151175/11 A RU2010151175/11 A RU 2010151175/11A RU 2010151175 A RU2010151175 A RU 2010151175A RU 2010151175 A RU2010151175 A RU 2010151175A
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- strut
- panel
- fixed
- rotation
- axis
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- Photovoltaic Devices (AREA)
Abstract
Стенд для раскрытия батареи солнечной, состоящий из фермы неподвижно установленной и закрепленной на основании стенда, в верхней части которой имеется неподвижная балка, с шарнирными рычагами, имитирующими кинематические характеристики створок испытуемых панелей батарей солнечных и соединенными со створками при помощи тросов, отличающийся тем, что на ферме соосно оси вращения панели БС по тангажу шарнирно установлена технологическая рама с балансировочным грузом и моментом инерции, равным моменту инерции панели БС относительно ее оси вращения, на которой по штатным посадочным местам закреплена панель БС, которая взаимодействует с двухзвенным шарнирным подкосом, второе звено которого закреплено шарнирно на технологической раме, которая снабжена пружиной, взаимодействующей с шарниром подкоса, при этом панель БС и технологическая рама подвижно закреплены на одном валу, который также посредством кулачка, охватывающего вал, взаимодействует с пружинным компенсатором, жестко закрепленным на основании, а троса, соединяющие шарнирные рычаги со створками БС, снабжены демпферами, причем длины тросов имеют длину не более 0,5 м, а жесткость пружинных компенсаторов рассчитывается по формуле: ! ! где А=G1-ΔH1+G2-ΔH2 - работа сил тяжести звеньев подкоса при ! раскладывании; ! G1, G2-вec звеньев подкоса; ! ΔН1, ΔН2 - изменение высоты центра тяжести звеньев подкоса; ! Мо=G1 ·ℓ1+G2 ·ℓ2 - начальный момент от веса звеньев подкоса; ! ℓ1, ℓ2 - плечо силы веса звеньев подкоса относительно оси вращения технологической рамы; ! R - радиус сектора. A stand for opening a solar battery, consisting of a farm fixedly mounted and fixed on the base of the stand, in the upper part of which there is a fixed beam, with articulated levers that simulate the kinematic characteristics of the shutters of the tested solar panels and connected to the shutters by cables, characterized in that the farm frame coaxially with the axis of rotation of the BS panel has a pivotally mounted technological frame with a balancing weight and moment of inertia equal to the moment of inertia of the BS panel relative to its axis and rotation, on which the BS panel is fixed at regular seats, which interacts with a two-link articulated strut, the second link of which is pivotally mounted on the technological frame, which is equipped with a spring interacting with the strut hinge, while the BS panel and the technological frame are movably fixed on one shaft , which also interacts with a spring compensator rigidly fixed to the base by means of a cam covering the shaft, and the cables connecting the articulated levers with the BS shutters are equipped with a damper ferey, and the cable lengths have a length of not more than 0.5 m, and the stiffness of the spring compensators is calculated by the formula: ! where A = G1-ΔH1 + G2-ΔH2 is the work of the gravity of the strut links at! folding out; ! G1, G2-vec strut units; ! ΔН1, ΔН2 - change in the height of the center of gravity of the strut links; ! Mo = G1 · ℓ1 + G2 · ℓ2 - the initial moment of the weight of the strut links; ! ℓ1, ℓ2 - shoulder of the force of the weight of the strut links relative to the axis of rotation of the technological frame; ! R is the radius of the sector.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2010151175/11A RU2468969C2 (en) | 2010-12-13 | 2010-12-13 | Solar battery opening test bench |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2010151175/11A RU2468969C2 (en) | 2010-12-13 | 2010-12-13 | Solar battery opening test bench |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2010151175A true RU2010151175A (en) | 2012-06-20 |
RU2468969C2 RU2468969C2 (en) | 2012-12-10 |
Family
ID=46680713
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2010151175/11A RU2468969C2 (en) | 2010-12-13 | 2010-12-13 | Solar battery opening test bench |
Country Status (1)
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RU (1) | RU2468969C2 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103879570B (en) * | 2014-04-08 | 2016-01-20 | 哈尔滨工业大学 | Fork roller reciprocating solar wing assisting overturn mechanism |
CN103879569B (en) * | 2014-04-08 | 2016-01-20 | 哈尔滨工业大学 | Oscillating block slider reciprocating solar wing assisting overturn mechanism |
RU2567678C1 (en) * | 2014-07-03 | 2015-11-10 | Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации | Bench for solar battery deployment |
CN106184832B (en) * | 2016-08-01 | 2018-11-13 | 哈尔滨工业大学 | Mars gravitation simulation system based on electromagnetic principles |
RU168492U1 (en) * | 2016-08-29 | 2017-02-06 | федеральное государственное бюджетное образовательное учреждение высшего образования "Южно-Российский государственный политехнический университет (НПИ) имени М.И. Платова" | Solar Battery Test Bench |
RU2745126C1 (en) * | 2020-03-27 | 2021-03-22 | Акционерное общество «Информационные спутниковые системы» имени академика М.Ф.Решетнёва» | Multilink rod for spacecraft solar battery |
RU2757942C1 (en) * | 2021-02-26 | 2021-10-25 | Акционерное общество «Информационные спутниковые системы» имени академика М.Ф.Решетнёва» | Spacecraft cable temperature compensator |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0260900A (en) * | 1988-08-29 | 1990-03-01 | Toshiba Corp | Ground simulation test device for solar paddle |
JPH04139000A (en) * | 1990-09-29 | 1992-05-13 | Mitsubishi Electric Corp | Simulated testing method for extension testing device |
RU1803351C (en) * | 1991-05-24 | 1993-03-23 | Конструкторское бюро "Салют" | Plant for testing sizable solar cell batteries |
JPH0712687A (en) * | 1993-06-22 | 1995-01-17 | Natl Space Dev Agency Japan<Nasda> | Development testing apparatus for developing type solar battery paddle |
DE19933379B4 (en) * | 1999-07-20 | 2005-03-10 | Aerolas Gmbh | Bearing arrangement for supporting tensile forces and bearing head for the bearing assembly |
RU2293961C2 (en) * | 2004-09-07 | 2007-02-20 | Фгуп Производственное Объединение "Полет" (Фгуп По "Полет") | Method of testing spacecraft multi-member mechanical system for functioning and device for realization of this method |
RU2299840C1 (en) * | 2005-09-20 | 2007-05-27 | Закрытое Акционерное Общество "Конструкторское Бюро "Полет" (Зао "Кб "Полет") | Device for simulation of weightlessness of sectional collapsible panels of spacecraft solar batteries |
GB2455311B (en) * | 2007-12-04 | 2012-08-01 | Europ Agence Spatiale | Deployable panel structure |
RU2376217C1 (en) * | 2008-05-27 | 2009-12-20 | Александр Николаевич Евтеев | Device to make weightless horizontally moving multi-link mechanical system of spacecraft |
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2010
- 2010-12-13 RU RU2010151175/11A patent/RU2468969C2/en active
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Publication number | Publication date |
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RU2468969C2 (en) | 2012-12-10 |
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PC43 | Official registration of the transfer of the exclusive right without contract for inventions |
Effective date: 20150623 |
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PD4A | Correction of name of patent owner |