CN205034356U - A simple and easy manual hold -down mechanism that is used for sun wing boxboard assembly - Google Patents

A simple and easy manual hold -down mechanism that is used for sun wing boxboard assembly Download PDF

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Publication number
CN205034356U
CN205034356U CN201520695657.4U CN201520695657U CN205034356U CN 205034356 U CN205034356 U CN 205034356U CN 201520695657 U CN201520695657 U CN 201520695657U CN 205034356 U CN205034356 U CN 205034356U
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China
Prior art keywords
boxboard
handle
latch hook
rotating shaft
hook
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CN201520695657.4U
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Chinese (zh)
Inventor
梁世杰
杨巧龙
任守志
闫泽红
马静雅
王举
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Beijing Institute of Spacecraft System Engineering
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Beijing Institute of Spacecraft System Engineering
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Abstract

The utility model discloses a simple and easy manual hold -down mechanism that is used for sun wing boxboard assembly, including compressing tightly handle, handle stand, handle base, handle pivot, latch hook pivot, latch hook, going up boxboard couple and lower boxboard couple, need to be changed during the sun wing when in orbit, draw in flexible sun blanket 12 in through drive arrangement etc. Earlier. Flexible sun blanket 12 draws the back that puts in place in, and the certain distance is drawn close to the boxboard of flexible 12 both sides of sun blanket, at this moment, by spaceman manually operation, will compress tightly handle 1 and lift, and it is 5 upwards rotatory around the handle pivot to compress tightly handle 1, and then drives latch hook 7 and throw off from boxboard couple 9 down, the utility model discloses a pure mechanical means realize compressing tightly the manual of sun blanket and boxboard, simple structure, the reliability is high, light in weight, the manual hold -down mechanism of boxboard, easy operation, reliable need not to utilize appurtenance, operates outside the spaceman's of being convenient for the cabin.

Description

A kind of manual simplified hold-down mechanism for solar wing boxboard fabricate block
Technical field
The utility model relates to space technology field, particularly relates to a kind of manual simplified hold-down mechanism for solar wing boxboard fabricate block.
Background technology
Existing large-scale flexible solar wing, has two cover boxboard fabricate blocks, often overlaps boxboard fabricate block and is made up of upper boxboard, lower boxboard and flexible sun blanket, and flexible sun blanket is held by upper boxboard and nowel plate holder after drawing in and folding.Boxboard fabricate block needs to have the function can manually changed in-orbit, and more changing jobs manually is completed out of my cabin by astronaut.In solar wing Renewal process, first sun blanket need be drawn in, and tentatively compress, sun blanket and outer side box plate thereof is made to be fixed as an entirety, unified replacing, therefore, needs to study the connection between upper boxboard and lower boxboard, separate mode again, make in Renewal process, boxboard fabricate block becomes as a whole.
Utility model content
In view of this, the utility model provides a kind of manual simplified hold-down mechanism for solar wing boxboard fabricate block, and the manual gathering be applicable in large-scale flexible solar wing between sun blanket boxboard compresses, and can not pass through the situation of instrument and M/C compression.There is the features such as structure is simple, reliability is high, lightweight, easy to operate.
A kind of manual simplified hold-down mechanism for solar wing boxboard fabricate block, wherein boxboard fabricate block is made up of upper boxboard, lower boxboard and flexible sun blanket, flexible sun blanket is held by upper boxboard and nowel plate holder after drawing in and folding, and described manual hold-down mechanism comprises compression handle, handle column, handle base, handle rotating shaft, latch hook rotating shaft, latch hook, upper boxboard hook and lower boxboard hook;
Described lower boxboard hook and handle base are fixed on the side of lower boxboard; Upper boxboard hook is fixed on boxboard side, and corresponding with the position of described handle base; The opening of described lower boxboard hook and upper boxboard hook towards all back to handle base;
Described handle column bottom has disc projection, is embedded in cylindrical grooves corresponding in handle base, and can around the central axis of handle column; Handle column stretches out the part of described groove along being processed with through hole with central axis direction; The bottom compressing handle is connected with described through hole by handle rotating shaft; The middle part compressing handle is provided with the cylindrical hole with handle shaft parallel, and latch hook rotating shaft is through described cylindrical hole, and the two ends vertical centre direction of principal axis exposed is processed with through hole; Described latch hook is U-shaped structure, and two free ends are each passed through the through hole at latch hook rotating shaft two ends, and is fixedly connected with latch hook rotating shaft, and latch hook can around the central axis of latch hook rotating shaft.
Preferably, described latch hook two free end is processed with screw thread, and each free end is clamped to latch hook rotating shaft both sides by two setting nuts.
The utility model has following beneficial effect:
The utility model have employed the manual compression that pure mechanical means realizes sun blanket and boxboard, and structure is simple, and reliability is high, lightweight; The manual hold-down mechanism of boxboard, simple to operate, reliable, without using accessory appliances, be convenient to the operation out of my cabin of astronaut.
Accompanying drawing explanation
Fig. 1 is the structural representation of the boxboard fabricate block of existing flexible solar wing.
Fig. 2 is the utility model boxboard manual hold-down mechanism structure composition schematic diagram;
Fig. 3 be the manual hold-down mechanism of the utility model boxboard standby time position;
Fig. 4 is the state of the utility model boxboard manual hold-down mechanism when boxboard and sun blanket manually being compressed;
Fig. 5 is that the utility model raising middle flask wrench moves hold-down mechanism cutaway view.
Wherein, under 1-compresses handle, 2-handle column, 3-setting nut, 4-handle base, the rotating shaft of 5-handle, the rotating shaft of 6-latch hook, 7-latch hook, the upper boxboard hook of 8-, 9-, boxboard is linked up with, the upper boxboard of 10-, boxboard under 11-, the flexible sun blanket of 12-.
Detailed description of the invention
To develop simultaneously embodiment below in conjunction with accompanying drawing, the utility model is described in detail.
As shown in Figure 1, boxboard fabricate block is made up of upper boxboard 10, lower boxboard 11 and flexible sun blanket 12, and flexible sun blanket 12 is clamped by upper boxboard 10 and lower boxboard 11 after drawing in and folding.
As Fig. 2,3, shown in 4 and 5, the manual hold-down mechanism of boxboard of the present utility model mainly comprises and compresses handle 1, handle column 2, handle base 4, handle rotating shaft 5, latch hook rotating shaft 6, latch hook 7, upper boxboard hook 8, lower boxboard hook 9 and corresponding fastening gauge member.Except upper boxboard hook 8, remaining part is all fixed on the side of lower boxboard 10.
Lower boxboard hook 9 and handle base 4 are fixed on the side of lower boxboard; Upper boxboard hook 8 is fixed on boxboard side, and corresponding with the position of described handle base 4.The opening of lower boxboard hook 9 and upper boxboard hook 8 towards all back to handle base 4.Handle column 2 bottom has disc projection, is embedded in cylindrical grooves corresponding in handle base 4, and can rotates around body central axle; Handle column 2 stretches out the part of groove along being processed with through hole with central axis direction; The bottom compressing handle 1 is connected with described through hole by handle rotating shaft 5, and compressing handle 1 can around the central axis of handle rotating shaft 5.The middle part compressing handle 1 is provided with the cylindrical hole parallel with handle rotating shaft 5, and latch hook rotating shaft 6 is through described cylindrical hole, and the two ends vertical centre direction of principal axis exposed is processed with through hole; Latch hook 7 is U-shaped structure, and two free ends are each passed through the through hole at latch hook rotating shaft 6 two ends, and is fixedly connected with latch hook rotating shaft 6, and latch hook 7 can around the central axis of latch hook rotating shaft 6.Wherein fixed form is: latch hook 7 liang of free ends are processed with screw thread, and each free end is clamped to latch hook rotating shaft 6 both sides by two setting nuts 3.
In the Spacecraft Launch stage, manual hold-down mechanism does not work, and just uses, therefore be fixed in the side of lower boxboard 10 when it just needs to change solar wing in-orbit, independent placement.In order to avoid its affect flexible sun blanket 12 in-orbit time Automatic-expanding motion, be provided with lower boxboard hook 9, at ordinary times latch hook 7 is linked up with 9 with lower boxboard and is connected, its position is fixed, as shown in Figure 2 state.
When needing in-orbit to change solar wing, first by actuating device etc., flexible sun blanket 12 is drawn in.After flexible sun blanket 12 draws in and puts in place, the boxboard of flexible sun blanket 12 both sides is brought to certain distance, now, by astronaut's M/C, compression handle 1 is lifted, compresses handle 1 and rotate up around handle rotating shaft 5, and then band moveable lock hook 7 is thrown off from lower boxboard hook 9.
Compress the parts such as handle 1 and latch hook 7, be fixed on handle column 2 by handle rotating shaft 5,360 ° can be done with handle column 2 around its center shaft and rotate freely.Astronaut now, manually will compress handle 1 around handle column 2 half-twist, and band moveable lock hook 7 rotates the position of supreme boxboard hook 8, latch hook head be caught on upper boxboard hook 8.Manual depression compresses handle 1, compress handle 1 to be rotated down around handle rotating shaft 5, and then band moveable lock hook 7 moves backward, upper boxboard 10 and lower boxboard 11 is strained, compress inner flexible sun blanket 12, reach and make boxboard and the as a whole object of flexible sun blanket 12 one-tenth.
In latch hook 7 and latch hook rotating shaft 6 junction, be provided with latch hook setting nut 3, by the collapsing length of its adjustable latch hook 7, to adapt to the thickness deviation demand of sun blanket, the also clamping load of adjustable flexible sun blanket 12.
In sum, these are only preferred embodiment of the present utility model, be not intended to limit protection domain of the present utility model.All within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.

Claims (2)

1. the manual simplified hold-down mechanism for solar wing boxboard fabricate block, wherein boxboard fabricate block is by upper boxboard (10), lower boxboard (11) and flexible sun blanket (12) composition, by upper boxboard (10) and lower boxboard (11) clamping after flexible sun blanket (12) gathering in folds, it is characterized in that, described manual hold-down mechanism comprises compression handle (1), handle column (2), handle base (4), handle rotating shaft (5), latch hook rotating shaft (6), latch hook (7), upper boxboard hook (8) and lower boxboard hook (9),
Described lower boxboard hook (9) and handle base (4) are fixed on the side of lower boxboard (11); Upper boxboard hook (8) is fixed on boxboard (10) side, and corresponding with the position of described handle base (4); Described lower boxboard hook (9) and upper boxboard link up with the opening of (8) towards all back to handle base (4);
Described handle column (2) bottom has disc projection, is embedded in the upper corresponding cylindrical grooves of handle base (4), and can around the central axis of handle column (2); Handle column (2) stretches out the part of described groove along being processed with through hole with central axis direction; The bottom compressing handle (1) is connected with described through hole by handle rotating shaft (5); The middle part compressing handle (1) is provided with the cylindrical hole parallel with handle rotating shaft (5), and latch hook rotating shaft (6) is through described cylindrical hole, and the two ends vertical centre direction of principal axis exposed is processed with through hole; Described latch hook (7) is U-shaped structure, two free ends are each passed through the through hole at latch hook rotating shaft (6) two ends, and be fixedly connected with latch hook rotating shaft (6), latch hook (7) can around the central axis of latch hook rotating shaft (6).
2. a kind of manual simplified hold-down mechanism for solar wing boxboard fabricate block as claimed in claim 1, it is characterized in that, described latch hook (7) two free end is processed with screw thread, and each free end is clamped to latch hook rotating shaft (6) both sides by two setting nuts (3).
CN201520695657.4U 2015-09-09 2015-09-09 A simple and easy manual hold -down mechanism that is used for sun wing boxboard assembly Active CN205034356U (en)

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CN201520695657.4U CN205034356U (en) 2015-09-09 2015-09-09 A simple and easy manual hold -down mechanism that is used for sun wing boxboard assembly

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Application Number Priority Date Filing Date Title
CN201520695657.4U CN205034356U (en) 2015-09-09 2015-09-09 A simple and easy manual hold -down mechanism that is used for sun wing boxboard assembly

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106546365A (en) * 2016-09-22 2017-03-29 北京空间飞行器总体设计部 A kind of sun blanket pressure calibration method of flexible solar wing
CN109229431A (en) * 2018-09-11 2019-01-18 北京空间机电研究所 A kind of non-firer's tripper and locking unlocking method
CN112224617A (en) * 2020-10-26 2021-01-15 国网山东省电力公司昌邑市供电公司 Electric energy meter week packing box
CN112936125A (en) * 2020-12-22 2021-06-11 深圳市魔方卫星科技有限公司 Mechanism for increasing integral clamping load of solar carpet
CN113864583A (en) * 2021-09-24 2021-12-31 北京无线电测量研究所 Quick locking device, quick detach radar assembly and radar car
CN116374211A (en) * 2023-06-01 2023-07-04 天津航天机电设备研究所 Ultra-large type spaceflight flexible structure whole-star integrated auxiliary device

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106546365A (en) * 2016-09-22 2017-03-29 北京空间飞行器总体设计部 A kind of sun blanket pressure calibration method of flexible solar wing
CN106546365B (en) * 2016-09-22 2019-03-12 北京空间飞行器总体设计部 A kind of sun blanket pressure calibration method of flexibility solar wing
CN109229431A (en) * 2018-09-11 2019-01-18 北京空间机电研究所 A kind of non-firer's tripper and locking unlocking method
CN112224617A (en) * 2020-10-26 2021-01-15 国网山东省电力公司昌邑市供电公司 Electric energy meter week packing box
CN112936125A (en) * 2020-12-22 2021-06-11 深圳市魔方卫星科技有限公司 Mechanism for increasing integral clamping load of solar carpet
CN113864583A (en) * 2021-09-24 2021-12-31 北京无线电测量研究所 Quick locking device, quick detach radar assembly and radar car
CN116374211A (en) * 2023-06-01 2023-07-04 天津航天机电设备研究所 Ultra-large type spaceflight flexible structure whole-star integrated auxiliary device

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