CN105857640B - A kind of connection cornual plate and satellite for satellite modules - Google Patents
A kind of connection cornual plate and satellite for satellite modules Download PDFInfo
- Publication number
- CN105857640B CN105857640B CN201610218059.7A CN201610218059A CN105857640B CN 105857640 B CN105857640 B CN 105857640B CN 201610218059 A CN201610218059 A CN 201610218059A CN 105857640 B CN105857640 B CN 105857640B
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- satellite modules
- satellite
- plate
- modules
- inner sheet
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- 230000015572 biosynthetic process Effects 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 6
- 239000002360 explosive Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000007596 consolidation process Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/223—Modular spacecraft systems
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- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Joining Of Building Structures In Genera (AREA)
- Connection Of Plates (AREA)
Abstract
The present invention provides a kind of connection cornual plates and satellite for satellite modules.The connection cornual plate includes inner sheet and outer plate, the outer surface of the outer plate and the outer surface of satellite modules are in the same plane, outer surface to ensure the satellite modules is smooth, and the inner sheet is arranged on the inside of the edge of the outer plate, and parallel with the setting outer plate of inner sheet；The interior on piece is provided with inner bolt hole, and the inner bolt hole is used to connection cornual plate being solidly connected between the frame of satellite modules, and the outer plate is provided with outer screw hole, and the outer screw hole is used between different satellite modules be connected with each other.
Description
Technical field
The present invention relates to space technology field more particularly to a kind of connection cornual plates and satellite for satellite modules.
Background technology
The miniaturization of satellite is one of the trend of current space technology development.Satellite, which is resolved into several function modules, is
A kind of effective means of satellite weight and volume is reduced in the prior art.And how to connect multiple satellite modules, being must
The problem that must be solved.Common methods are slotted or are punched on the side wall of satellite modules, and different modules is connected
Come.But the distribution of force of satellite modules side wall can be destroyed in this way, therefore different satellite modules need respectively to design different companies
Binding structure.This improves design difficulty.Therefore, a kind of mode of the simple and effective different satellite modules of connection is designed, is existing
Technology urgent problem to be solved.
Invention content
The technical problem to be solved by the invention is to provide a kind of connection cornual plate and satellite for satellite modules, energy
Enough simple and effective different satellite modules of connection.
To solve the above-mentioned problems, the present invention provides a kind of connection cornual plate for satellite modules, including inner sheet and outer
Piece, the outer surface of the outer plate and the outer surface of satellite modules in the same plane, to ensure the appearance of the satellite modules
Face is smooth, and the inner sheet is arranged on the inside of the edge of the outer plate, and parallel with the setting outer plate of inner sheet；The interior on piece setting
There are inner bolt hole, the inner bolt hole to be used to connection cornual plate being solidly connected between the frame of satellite modules, the outer plate is provided with outer
Screw hole, the outer screw hole are used between different satellite modules be connected with each other.
Optionally, the edge of the inner sheet extends to one extension of formation being arranged other than the outer plate edge of the inner sheet, institute
The inner bolt hole for stating inner sheet is arranged in extension.
Optionally, the connection cornual plate includes two orthogonal outer plates, for connecting upper and lower two satellite modules
Edge.
Optionally, the connection cornual plate includes three orthogonal outer plates, is placed in three or three or more satellite modules
Stitching portion, for connecting multiple satellite modules.
Optionally, the connection cornual plate includes the apex angle that three orthogonal outer plates are constituted, and it is sudden and violent to be placed in satellite modules
The vertex of dew, for fixing the apex angle.
The present invention also provides a kind of satellites, are spliced to form by multiple satellite modules, between the satellite modules at least
It is to be formed by connecting using the connection cornual plate described in any one of above-mentioned technical proposal at one.
It is an advantage of the current invention that the inner sheet of connection cornual plate is used for multiple satellite modules for connecting satellite modules, outer plate
Between interconnection, therefore satellite modules can be simply securely attached to together, and it is standardized to be that one kind is easily achieved
Connecting method.On the outline border of satellite modules only need to according to the standard of cornual plate reserve screw hole, so that it may with realize different satellite modules it
Between free splicing combination.
Description of the drawings
Attached drawing 1 is the structural schematic diagram of connection the first specific implementation mode of cornual plate of the present invention.
Attached drawing 2 is the structural schematic diagram of connection the second specific implementation mode of cornual plate of the present invention.
Attached drawing 3 is the structural schematic diagram of connection cornual plate third specific implementation mode of the present invention.
Attached drawing 4A is the explosive view using a satellite of connection cornual plate described in multiple first and second specific implementation modes.
Attached drawing 4B is the assembling figure of attached drawing 4A.
Attached drawing 5A is using the satellite for connecting cornual plate described in multiple above-mentioned first, second and third specific implementation mode
Explosive view.
Attached drawing 5B is the assembling figure of attached drawing 5A.
Specific implementation mode
Below in conjunction with the accompanying drawings to a kind of specific reality for connecting cornual plate and satellite for satellite modules provided by the invention
The mode of applying elaborates.
It is the structural schematic diagram of connection the first specific implementation mode of cornual plate of the present invention, the first joint angle shown in attached drawing 1
Piece 10 includes inner sheet and outer plate.Wherein outer plate includes two orthogonal outer plates 121 and 122, correspondingly, each outer plate corresponds to
One inner sheet, including inner sheet 111 and 112 are set.The outer surface of the outer plate 121 and 122 and the outer surface of satellite modules exist
In same plane, the outer surface to ensure the satellite modules is smooth.The inner sheet 111 is arranged at the edge of the outer plate 121
Inside, and it is parallel with the setting outer plate 121 of inner sheet 111.Inner sheet 112 also has similar structure.
In present embodiment, the connection cornual plate includes two orthogonal outer plates 121 and 122, for connecting
The edge of upper and lower two satellite modules.Be provided with inner bolt hole on the inner sheet 111, present embodiment with inner bolt hole 114 with
115 indicate.The inner bolt hole is used to connection cornual plate being solidly connected between the frame of satellite modules.It is set on corresponding outer plate 121
It is equipped with outer screw hole, screw hole 124,125 and 126 indicates other than present embodiment.The outer screw hole is used for different satellite modules
Between be connected with each other.Can also include more or less inner bolt hole and outer screw hole in other specific implementation modes.Separately
Also same screw hole is arranged on one group of inner sheet 112 and outside 122.
In this embodiment, the edge of the inner sheet 111 extends to 121 edge of outside that the inner sheet 111 is arranged
The inner bolt hole 114 and 115 of one extension of formation in addition, the inner sheet 111 is arranged in extension.In other specific embodiment parties
In formula, the installation position of inner bolt hole can be adjusted according to the screwhole position of satellite modules.
Above structure is used to connect the edge of a satellite modules with another satellite modules.Inner sheet is used for satellite mould
It is consolidated between the frame of block, and outer plate is for connecting another satellite modules.And another satellite modules is only needed in frame
Screw hole is arranged in position corresponding with the outer screw hole of this connection cornual plate on frame.
It is the structural schematic diagram of connection the second specific implementation mode of cornual plate of the present invention, the second joint angle shown in attached drawing 2
Piece 20 includes inner sheet and outer plate.Wherein outer plate includes three orthogonal outer plates 221,222 and 223.The folder of three outer plates
One inner sheet 211 is set at angle.In other specific implementation modes, it can also be set according to the shape of connected satellite modules
Set more inner sheets.The outer surface of the outer plate 221,222 and 223 and the outer surface of satellite modules in the same plane,
Outer surface to ensure the satellite modules is smooth.Three orthogonal outer plates of present embodiment are placed in three satellites
The stitching portion of module, for connecting three satellite modules.In other specific implementation modes, outer plate 221,222 and 223 is prolonged
It stretches, you can for connecting more satellite modules.Inner sheet and the screwhole position of outer on piece please refer to the first specific implementation mode, this
Place repeats no more.
Above structure is used for multiple satellite modules stitching portions.Inner sheet is used to consolidate between the frame of satellite modules, and outer
Piece is used for the consolidation between multiple satellite modules.Satellite modules only need corresponding with the outer screw hole of this connection cornual plate on frame
Screw hole is arranged in position.
It is the structural schematic diagram of connection cornual plate third specific implementation mode of the present invention, third joint angle shown in attached drawing 3
Piece 30 includes inner sheet and outer plate.Wherein outer plate includes three orthogonal outer plates 321,322 and 323.The folder of three outer plates
One inner sheet 311 is set at angle.The outer surface of the outer plate 321,322 and 323 and the outer surface of satellite modules are same
In plane, the outer surface to ensure the satellite modules is smooth.Three orthogonal outer plates 321 of present embodiment,
322 and 323 apex angles constituted, are placed in the vertex of satellite modules exposure, for fixing the apex angle.Inner sheet and outer on piece
Screwhole position please refers to the first specific implementation mode, and details are not described herein again.
It is using the first connection cornual plate 10 described in multiple above-mentioned first and second specific implementation modes and the shown in attached drawing 4A
The explosive view of one satellite of two connection cornual plates 20.Attached drawing 4B is the assembling figure of attached drawing 4A.
It is using the first connection cornual plate described in multiple above-mentioned first, second and third specific implementation mode shown in attached drawing 5A
10, the explosive view of a satellite of the second connection cornual plate 20 and third connection cornual plate 30.Attached drawing 5B is the assembling figure of attached drawing 5A.
It can be seen from the above description that the connection cornual plate that the above specific implementation mode provides can be simply firm by satellite modules
Solid link together, and be that one kind being easily achieved standardized connecting method.It only need to be according to mark on the outline border of satellite modules
The reserved screw hole of standard, so that it may to realize that the free splicing between different satellite modules combines.
The above is only a preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art
Member, various improvements and modifications may be made without departing from the principle of the present invention, these improvements and modifications also should be regarded as
Protection scope of the present invention.
Claims (5)
1. a kind of connection cornual plate for satellite modules, which is characterized in that including inner sheet and outer plate, the outer surface of the outer plate with
In the same plane, the outer surface to ensure the satellite modules is smooth for the outer surface of satellite modules, and the inner sheet setting exists
On the inside of the edge of the outer plate, and it is parallel with the setting outer plate of inner sheet；The interior on piece is provided with inner bolt hole, and the inner bolt hole is used
It is solidly connected between the frame of satellite modules in by connection cornual plate, the outer plate is provided with outer screw hole, and the outer screw hole is not for
It is connected with each other between satellite modules；The edge of the inner sheet extends to the formation one being arranged other than the outer plate edge of the inner sheet and prolongs
The inner bolt hole of extending portion, the inner sheet is arranged in extension.
2. the connection cornual plate according to claim 1 for satellite modules, which is characterized in that the connection cornual plate includes two
A orthogonal outer plate, the edge for connecting upper and lower two satellite modules.
3. the connection cornual plate according to claim 1 for satellite modules, which is characterized in that the connection cornual plate includes three
A orthogonal outer plate is placed in the stitching portion of three or three or more satellite modules, for connecting multiple satellite modules.
4. the connection cornual plate according to claim 1 for satellite modules, which is characterized in that the connection cornual plate includes three
The apex angle that a orthogonal outer plate is constituted, is placed in the vertex of satellite modules exposure, for fixing the apex angle.
5. a kind of satellite is spliced to form by multiple satellite modules, which is characterized in that be at least one between the satellite modules
It is formed by connecting using the connection cornual plate described in any one of the claims 1-4.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610218059.7A CN105857640B (en) | 2016-04-08 | 2016-04-08 | A kind of connection cornual plate and satellite for satellite modules |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610218059.7A CN105857640B (en) | 2016-04-08 | 2016-04-08 | A kind of connection cornual plate and satellite for satellite modules |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105857640A CN105857640A (en) | 2016-08-17 |
| CN105857640B true CN105857640B (en) | 2018-10-16 |
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ID=56637346
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610218059.7A Active CN105857640B (en) | 2016-04-08 | 2016-04-08 | A kind of connection cornual plate and satellite for satellite modules |
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| Country | Link |
|---|---|
| CN (1) | CN105857640B (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109941458A (en) * | 2019-02-25 | 2019-06-28 | 航天科工空间工程发展有限公司 | A kind of cornual plate suitable for criticizing production satellite assembly |
| CN110143293B (en) * | 2019-06-06 | 2020-11-24 | 北京理工大学 | Method for reconstructing and destructuring morphology topology of variable micro-nano satellite |
| CN111762338A (en) * | 2020-05-25 | 2020-10-13 | 航天科工空间工程发展有限公司 | Folding flat satellite structure |
| CN113815901B (en) * | 2021-10-18 | 2022-04-26 | 北京微纳星空科技有限公司 | Satellite frame and satellite |
| CN114313311B (en) * | 2022-03-04 | 2022-05-27 | 中国人民解放军战略支援部队航天工程大学 | Topological structure of multi-body allosteric satellite |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202208413U (en) * | 2011-09-06 | 2012-05-02 | 苏州良才物流科技股份有限公司 | Enhanced type hollow plate container |
| CN102975867A (en) * | 2012-11-13 | 2013-03-20 | 上海微小卫星工程中心 | Satellite module and modularized satellite |
| CN103935529A (en) * | 2014-04-29 | 2014-07-23 | 上海卫星工程研究所 | Rapid response satellite structure |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110011982A1 (en) * | 2009-07-20 | 2011-01-20 | Jason Herman | Modular control moment gyroscope (cmg) system for spacecraft attitude control |
-
2016
- 2016-04-08 CN CN201610218059.7A patent/CN105857640B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202208413U (en) * | 2011-09-06 | 2012-05-02 | 苏州良才物流科技股份有限公司 | Enhanced type hollow plate container |
| CN102975867A (en) * | 2012-11-13 | 2013-03-20 | 上海微小卫星工程中心 | Satellite module and modularized satellite |
| CN103935529A (en) * | 2014-04-29 | 2014-07-23 | 上海卫星工程研究所 | Rapid response satellite structure |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105857640A (en) | 2016-08-17 |
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