CN103448917B - A kind of high orbit satellite platform quick assembling service module and application thereof - Google Patents
A kind of high orbit satellite platform quick assembling service module and application thereof Download PDFInfo
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- CN103448917B CN103448917B CN201310345337.1A CN201310345337A CN103448917B CN 103448917 B CN103448917 B CN 103448917B CN 201310345337 A CN201310345337 A CN 201310345337A CN 103448917 B CN103448917 B CN 103448917B
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Abstract
The invention discloses a kind of high orbit satellite platform quick assembling service module and application thereof, the cross section that described quick assembling service module is mainly made up of the deck board docking mechanism of deck board and connection deck board is the column structure of isosceles trapezoid, this quick assembling service module quantity on common platform for satellite is one or more, unit in order to satisfied different satellites is supporting, can carry out parallel quick assembling.Each deck board of the present invention can be employed as the installed surface of unit, solve under high orbit remote sensing of the earth satellite different task, the versatility of common platform and autgmentability, decrease the common platform amended subject for different task platform, decrease the assembling of whole star unit, testing time, shorten the satellite lead time.
Description
Technical field
The present invention relates to aerospace vehicle field, in particular, relate to a kind of high orbit satellite platform fast
Quick-mounting joins service module configuration.
Background technology
Satellite platform in early days provides unit installed surface to be satellite auxiliary load-carrying construction or inherently satellite master
Load-carrying construction, also exists the problem that can not dismount at any time and change.But, in order to meet the supporting list of platform
The installation requirement of machine, and the variation of unit is minimum on the impact of platform, needs to develop a kind of public satellite
Platform service cabin, it is possible to meet and install variety classes unit, and platform ingredient can be to greatest extent
Concurrent assembly, each system of platform can the requirement of electrical measurement etc. parallel, to meet different mission requirements.
Summary of the invention
For technical problem present in above-mentioned prior art, the present invention provides a kind of high orbit satellite platform
Quick assembling service module and application thereof, by system just can realize satellite platform service module quick assembling, unit
Nearly layout, the assembling of service module independent, the test of whole star module bodyization.Solve high orbit remote sensing of the earth to defend
Under star different task, the versatility of common platform and autgmentability, decrease common platform for different task
The amended subject of Shi Pingtai, decreases the assembling of whole star unit, testing time, shortens the satellite lead time.
To achieve the above object of the invention, the technical solution adopted in the present invention is as follows:
A kind of high orbit satellite platform quick assembling service module, described service module is mainly by deck board and connection
The cross section of the deck board docking mechanism composition of deck board is the column structure of isosceles trapezoid.
Described deck board includes: front side board, back side panel, upper mounting plate, lower installation board, left plate, right side
Plate, described deck board docking mechanism includes in the front left of front side board, left plate and upper mounting plate docking fast
Speed installing mechanism, for front side board, left plate and lower installation board docking front left under quick installation mechanism,
For front side board, right plate and upper mounting plate docking front right on quick installation mechanism, for front side board,
Right plate and lower installation board docking front right under quick installation mechanism, for back side panel, left plate and upper peace
Fill quick installation mechanism in the rear left of plate docking, after back side panel, left plate and lower installation board dock
Lower-left quick installation mechanism, for back side panel, right plate and upper mounting plate docking rear right on Fast Installation
Mechanism, for back side panel, right plate and lower installation board docking rear right under quick installation mechanism.
Installed by screw between described each deck board and between quick installation mechanism and deck board.
Described front side board can be as main radiating surface, and described left plate and right plate can be as auxiliary heat dissipation faces.
The application on satellite platform of the above-mentioned high orbit satellite platform quick assembling service module, described fast quick-mounting
It is one or more for joining service module quantity on satellite platform, installs in order to the unit of satisfied different satellites
Requirement.
The configuration of high orbit satellite platform quick assembling service module provided by the present invention, have employed standardization,
Integrated design philosophy, the cylinder structure that satellite platform quick assembling service module uses cross section to be isosceles trapezoid
Type, can utilize the enveloping space of high orbit satellite common platform to greatest extent, and for public flat
Platform different task demand, can increase the quantity of satellite platform quick assembling service module further, for public flat
The installation requirements that when platform meets different task demand, unit product is different provide possibility.Quick assembling services
Cabin height is that 0.27m(can further expand), effective installed surface area is 0.7m2, bearing capacity is
100kg, can meet the installation requirement of major part unit.Quick assembling service module uses quick installation mechanism
Can be installed to easily on common platform for satellite, whole star concurrent assembly and testing requirement can be met, contracting
The short satellite lead time.
Accompanying drawing explanation
Fig. 1 is the structural representation of quick assembling service module provided by the present invention；
Fig. 2 is the exploded view of Fig. 1；
Fig. 3 is that quick assembling service module provided by the present invention is assemblied on certain high rail common platform for satellite
Schematic diagram.
Detailed description of the invention
With specific embodiment, technical solution of the present invention is described in further detail below in conjunction with the accompanying drawings.
Fig. 1, Fig. 2 are the configurations of quick assembling service module provided by the present invention, mainly by deck board and company
The cross section of the deck board docking mechanism composition connecing deck board is the column structure of isosceles trapezoid.The present embodiment quick
The assembling a length of 500mm in the upper end in isosceles trapezoid cross section of service module, a length of 1330mm that goes to the bottom, highly
For 270mm.
Deck board includes: front side board 6, back side panel 12, upper mounting plate 2, lower installation board 3, left plate 1,
Right plate 9, deck board docking mechanism includes before front side board 6, left plate 1 and upper mounting plate 2 dock
Upper left quick installation mechanism 4, fast under the front left of front side board 6, left plate 1 and lower installation board 3 docking
Speed installing mechanism 5, for front side board 6, right plate 9 and upper mounting plate 2 docking front right on Fast Installation
Mechanism 8, for front side board 6, right plate 9 and lower installation board 3 docking front right under quick installation mechanism 7,
For back side panel 12, left plate 1 and upper mounting plate 2 docking rear left on quick installation mechanism 14, be used for
Back side panel 12, left plate 1 and lower installation board 3 docking rear left under quick installation mechanism 13, for rear side
Plate 12, right plate 9 and upper mounting plate 2 docking rear right on quick installation mechanism 11, for back side panel 12,
Quick installation mechanism 10 under the rear right of right plate 9 and lower installation board 3 docking.Between each deck board and quickly pacify
All installed by screw between mounting mechanism and deck board.
Quick assembling service module provided by the present invention, for the different task demand of common platform, can enter
One step increases the quantity of satellite platform quick assembling service module, meets different payload for common platform
Unit is supporting provides possibility.It is public flat shown in Fig. 3 to be that quick assembling service module is assemblied in certain high rail satellite
Schematic diagram on platform, the embodiment shown in Fig. 3, it is mounted with two quick assembling service modules 100.
High orbit satellite platform quick assembling service module provided by the present invention, its front side board can be as instrument
Main radiating surface, left plate and right plate can be as auxiliary heat dissipation faces.
The foregoing is only embodiments of the invention, not in order to limit the present invention, all essences in the present invention
Any amendment, equivalent and the improvement etc. made within god and principle, should be included in the guarantor of the present invention
Within the scope of protecting.
Claims (3)
1. a high orbit satellite platform quick assembling service module, it is characterised in that described service module is main
The cross section being made up of the deck board docking mechanism of deck board and connection deck board is the column structure of isosceles trapezoid, institute
State quick assembling service module quantity on common platform for satellite be one or can independently dismount multiple, use
Supporting to meet the unit of different task satellite.
High orbit satellite platform quick assembling service module the most according to claim 1, it is characterised in that
Described deck board includes: front side board, back side panel, upper mounting plate, lower installation board, left plate, right plate,
Described deck board docking mechanism includes quickly pacifying in the front left of front side board, left plate and upper mounting plate docking
Mounting mechanism, for front side board, left plate and lower installation board docking front left under quick installation mechanism, be used for
Front side board, right plate and upper mounting plate docking front right on quick installation mechanism, for front side board, right side
Plate and lower installation board docking front right under quick installation mechanism, for back side panel, left plate and upper mounting plate
Docking rear left on quick installation mechanism, for back side panel, left plate and lower installation board docking rear left under
Quick installation mechanism, for back side panel, right plate and upper mounting plate docking rear right on quick installation mechanism,
Quick installation mechanism under the rear right of back side panel, right plate and lower installation board docking.
High orbit satellite platform quick assembling service module the most according to claim 2, it is characterised in that
Installed by screw between described each deck board and between quick installation mechanism and deck board.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310345337.1A CN103448917B (en) | 2013-08-08 | 2013-08-08 | A kind of high orbit satellite platform quick assembling service module and application thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310345337.1A CN103448917B (en) | 2013-08-08 | 2013-08-08 | A kind of high orbit satellite platform quick assembling service module and application thereof |
Publications (2)
| Publication Number | Publication Date |
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| CN103448917A CN103448917A (en) | 2013-12-18 |
| CN103448917B true CN103448917B (en) | 2016-12-28 |
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Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104176272A (en) * | 2014-08-06 | 2014-12-03 | 上海卫星工程研究所 | Eight rod connection type non-contact satellite platform configuration |
| CN104787359B (en) * | 2014-12-30 | 2018-01-19 | 上海新跃仪表厂 | A kind of miniaturized surveillance satellite configuration |
| CN104842219B (en) * | 2015-02-12 | 2018-10-23 | 上海卫星装备研究所 | A kind of satellite structure platform multi-process intensive style repair System and method for |
| CN106043741B (en) * | 2016-08-05 | 2018-08-07 | 深圳航天东方红海特卫星有限公司 | A kind of satellite configuration design method adapting to several satellite in a rocket transmitting |
| CN109969429B (en) * | 2019-02-13 | 2022-03-18 | 上海卫星工程研究所 | Switching mechanism |
| CN109878761B (en) * | 2019-02-14 | 2020-09-08 | 上海卫星工程研究所 | Wedge-shaped space physical field measurement satellite configuration and assembling method thereof |
| CN109850186B (en) * | 2019-02-28 | 2021-02-09 | 中国空间技术研究院 | Plate frame type satellite structure for one-rocket multi-satellite parallel transmission and assembly method |
| CN110217409B (en) * | 2019-05-30 | 2020-10-23 | 北京卫星制造厂有限公司 | On-orbit quick dismounting micro-nano satellite platform structure |
| CN110683077A (en) * | 2019-09-19 | 2020-01-14 | 上海卫星工程研究所 | Trapezoidal satellite structure suitable for radar antenna and manufacturing method |
| CN114476125B (en) * | 2021-12-08 | 2023-08-15 | 浙江时空道宇科技有限公司 | Satellite platform structure |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2823182B1 (en) * | 2001-04-05 | 2004-06-04 | Cit Alcatel | DEPLOYABLE RADIATOR FOR SPACE ENGINE |
| CN201460303U (en) * | 2009-06-24 | 2010-05-12 | 总装备部工程设计研究总院 | Rapid-loading type multi-functional platform cabin |
| CN202439910U (en) * | 2012-02-21 | 2012-09-19 | 陈超 | Combining box |
| CN102717899B (en) * | 2012-06-26 | 2014-10-29 | 上海卫星工程研究所 | Venus probe configuration |
| CN102975867B (en) * | 2012-11-13 | 2014-12-31 | 上海微小卫星工程中心 | Satellite module and modularized satellite |
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