CN108820263A - The nested layering staged satellite platform configuration of mixing - Google Patents
The nested layering staged satellite platform configuration of mixing Download PDFInfo
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- CN108820263A CN108820263A CN201810631166.1A CN201810631166A CN108820263A CN 108820263 A CN108820263 A CN 108820263A CN 201810631166 A CN201810631166 A CN 201810631166A CN 108820263 A CN108820263 A CN 108820263A
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- 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
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
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Abstract
The invention discloses a kind of nested layering staged satellite platform configuration of mixing, which is configured as the closing cabin staged satellite platform configuration for promoting service module with load cabin by rule layering nested with the mixing that special-shaped deck board overlap joint is realized.The nested layering stepped configuration of mixing according to the present invention, when not changing the propulsion intrinsic envelope of service module ontology and mature configuration layouts, so that it may the area ratio over the ground for promoting service module and load cabin be adjusted flexibly, significantly improve satellite platform scalability and adaptability；It can increase on demand and promote service module to ground area, and the effectively vertical height of control satellite platform and height of center of mass, improve the mechanical characteristics such as mechanical environment and the satellite bending stiffness of mounting of roof plate load.Satellite platform configuration of the invention can be widely applied to the comprehensive remote sensing satellite that there is large volume envelope, big lumped mass, high accuracy install, the collaboration fusion observation of multi-load wide visual field to require.
Description
Technical field
The present invention relates to a kind of satellite platforms, and in particular, to a kind of nested layering staged satellite platform configuration of mixing.
Background technique
Mature satellite platform can satisfy multiple-task demand, adapt to different payload installation forms, can be effective
Satellite developing risk is controlled, satellite development cost is reduced and shortens the satellite lead time.With meteorology, environment, ocean, land etc.
The continuous upgrading of field space-based quantitative remote sensing observation mission, remote sensing load volume and quality are increasing, and detection accuracy requires to get over
Carry out higher, multi-load collaboration fusion observation new tool emergence, it is higher and higher to the composite request of satellite platform.In order to meet
The installation of more remote sensing load list stars and use that large volume envelope, big lumped mass, high accuracy install, wide visual field collaboration fusion are observed
It is required that having invented a kind of nested layering staged satellite platform configuration of mixing.
Summary of the invention
For above-mentioned the technical problems existing in the prior art, the present invention provides a kind of nested layering staged satellite of mixing
Platform configuration.
The present invention is realized by following technical proposals：
A kind of nested layering staged satellite platform configuration of mixing, the satellite platform are configured as promoting service module and load cabin
Pass through the closing cabin staged satellite platform configuration of rule layering nested with the mixing that special-shaped deck board overlap joint is realized.
Preferably, described two layers that promotes service module to be formed by overlapping for concave-convex type, stretching type and the combination of regular rectangular shape deck board
Or multilayer cabin configuration, including to ground lower part protruding plate, it is embedded in-stretches out plate to ground top, sunny slope L-type stretches out plate, back
Sunny side L-type stretches out plate, laminate, partition, side plate and the loaded cylinder of regular rectangular shape；It is embedding to ground lower part protruding plate and to ground top
Enter-stretch out plate and complete propulsion service module is constituted to ground by concaveconvex shape matching insertion docking
Preferably, described horizontal to ground lower part protruding plate lower end and concordant with service module ontology lower end bottom plate is promoted, it is right
Ground lower part protruding plate upper end is convex.
Preferably, described to be embedded in-stretch out plate lower end to ground top as concave, plate upper end is embedded in-stretched out to ground top
Part-structure be stretch out promote service module ontology upper end.
Preferably, the upper end protrusion part stretching that the sunny slope L-type stretches out plate and opaco L-type stretching plate, which promotes, to be serviced
Cabin ontology upper end.
Preferably, the upper and lower two or more layers enclosure of the load cabin and the semiclosed cludy in ground is composed
Mixing layering cabin configuration.
Preferably, the enclosure is made of laminate, side plate and small baffle rectangle rule deck board, described semiclosed to ground
Cludy utilizes the bottom plate of the enclosure, constitutes to floor and two pieces of small baffles, one piece small top plate.
Preferably, described to be embedded in-stretch out the upper of plate, sunny slope L-type stretching plate and opaco L-type stretching plate to ground top
Hold extension closing cludy nested with the formation mixing of complete closure of the semiclosed cludy of load cabin.
Compared with domestic and international satellite platform configuration at present, the invention has the advantages that：
1) using the nested layering stepped configuration of mixing, do not change and promote the intrinsic envelope of service module ontology and mature configuration cloth
Office, so that it may the area ratio over the ground for promoting service module and load cabin be adjusted flexibly, significantly improve to mature and reliable satellite platform expansion
Malleability and adaptability；
2) using the nested layering stepped configuration of mixing, do not change and promote the intrinsic envelope of service module ontology and mature configuration cloth
Office, so that it may it realizes the increase for promoting service module to ground area, while effectively control satellite platform height, shortens Path of Force Transfer,
Improve satellite platform mounting of roof plate load mechanical environment；
3) using the nested layering stepped configuration of mixing, do not change and promote the intrinsic envelope of service module ontology and mature configuration cloth
Office, so that it may realize the increase for promoting service module to ground area, while effectively control satellite platform height of center of mass, reduce and laterally turn
Dynamic inertia, improves the mechanical characteristics such as satellite platform bending stiffness.
Detailed description of the invention
By reading a detailed description of non-restrictive embodiments in the light of the attached drawings below, of the invention other
Feature, objects and advantages will become more apparent upon：
Fig. 1 is satellite platform configuration picture；
Fig. 2 is to promote service module configuration picture；
Fig. 3 is load cabin configuration picture；
Fig. 4 is satellite platform configuration explosive view.
Specific embodiment
The present invention is described in detail combined with specific embodiments below.Following embodiment will be helpful to the technology of this field
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill of this field
For personnel, without departing from the inventive concept of the premise, various modifications and improvements can be made.These belong to the present invention
Protection scope.
Now in conjunction with attached drawing 1~4, satellite platform configuration example according to an embodiment of the present invention and its installation is described in detail.
As shown in Figure 1, Figure 2, Figure 3, Figure 4, the nested layering staged satellite platform configuration of a kind of mixing provided by the invention,
The satellite platform is configured as mixing the closing cabin staged satellite platform configuration of nested layering, is applied to multi-load wide visual field
The comprehensive remote sensing satellite that collaboration fusion observation requires is taken by propulsion service module 100 and load cabin 200 by rule and special-shaped deck board
It connects；Promote service module 100 mainly include to ground lower part protruding plate 101, ground top is embedded in-is stretched out plate 102, on the sunny side
Face L-type stretches out plate 103, opaco L-type stretches out plate 104, bottom plate 105, laminate 106, partition 107 (16 pieces), side plate 108 (4 pieces)
And loaded cylinder 109；Load cabin 200 mainly include bottom plate 201, to floor 202, laminate 203, partition 204 (10 pieces), top plate 205,
Side plate 206 (3 pieces), small baffle 208 (2 pieces) and small top plate 209.
Propulsion service module 100 is the upper layer and lower layer cabin that the combinations such as concave-convex type, stretching type and regular rectangular shape deck board are formed by overlapping
Body configuration.
Promote service module 100 horizontal to 101 lower end of ground lower part protruding plate and with promote 100 ontology lower end bottom plate of service module
105 is concordant, is convex to 101 upper end of ground lower part protruding plate.
Promoting service module 100 to be embedded in-stretch out 102 lower end of plate to ground top is concave, ground top is embedded in-stretch out plate
The part-structure of 102 upper ends is to stretch out to promote 100 ontology upper end of service module.
Service module 100 is promoted to ground lower part protruding plate 101 and is embedded in-stretches out plate 102 to ground top and pass through concave-convex
Shape matching insertion docking constitute it is complete promote service module 100 to ground.
Promoting 100 sunny slope L-type of service module to stretch out plate 103 and the upper end protrusion part of opaco L-type stretching plate 104 is to stretch
100 ontology upper end of service module is promoted out.
Load cabin 200 is upper and lower two layers of enclosure and is layered cabin structure to the mixing that the semiclosed cludy in ground is composed
Type.
The enclosure of load cabin 200 by bottom plate 201, to floor 202, laminate 203, partition 204 (10 pieces), top plate 205, side
(3 pieces) overlap joints of plate 206 surround.
Load cabin 200 to the semiclosed cludy in ground by bottom plate 201, to floor 202, small baffle 208 (2 pieces), small top plate
209 overlap joints surround.
Promote service module 100 is embedded in-stretches out plate 102, sunny slope L-type stretching plate 103, opaco L-type to ground top
The bottom plate 201 of cabin body part and load cabin 200 is stretched out, to floor 202, small baffle 208 (2 pieces), small in the upper end for stretching out plate 104
The mixing nesting that top plate 209 forms complete closure closes cludy.
Then this satellite platform configuration can implement the docking of two cabins with subdivision concurrent assembly, forming process is as follows.
Promote service module assembly：
Step 1, bottom plate 105 are installed on satellite structure mounting plate；
Step 2 installs loaded cylinder 109 on the basis of step 1；
Step 3 successively installs lower cabin partition 107 (8 pieces) on the basis of step 2；
Step 4 installs laminate 106 on the basis of step 3；
Step 5 successively installs upper-deck cabin partition 107 (8 pieces) on the basis of step 4；
Step 6, on the basis of step 5, the bottom plate 201 in installed load cabin 200；
Step 7 is successively installed to ground lower part protruding plate 101 on the basis of step 6, ground top is embedded in-is stretched
Ejecting plate 102；
Step 8 successively installs sunny slope L-type and stretches out plate 103, opaco L-type stretching plate on the basis of step 7
104, side plate 108 (4 pieces).
Load cabin assembly：
Step 1 first removes the bottom plate 201 for being already installed on and promoting the load cabin 200 on service module 100；
Step 2, bottom plate 201 are installed on satellite structure mounting plate；
Step 3 successively installs lower cabin partition 204 (5 pieces) on the basis of step 2；
Step 4 installs laminate 203 on the basis of step 3；
Step 5 successively installs upper-deck cabin partition 204 (5 pieces) on the basis of step 4；
Step 6 installs top plate 205 on the basis of step 5；
Step 7 is installed on the basis of step 6 to floor 202；
Step 8, on the basis of step 7, successively installation side plate 206 (3 pieces)；
Step 9 successively installs small baffle 208 (2 pieces), small top plate 209 on the basis of step 8.
Two cabin general assemblies：
Step 1, successively dismounting, which is already installed on to promote, is embedded in-stretches out plate 102, side to ground top on service module 100
Plate 108 (upper-deck cabin), sunny slope L-type stretch out plate 103, opaco L-type stretches out plate 104；
Step 2 promotes service module and two cabin Butt Assembling of load cabin；
Step 3, on the basis of step 2, successively installation promote service module 100 on to ground top insertion-stretching
Plate 102, sunny slope L-type stretch out plate 103, opaco L-type stretches out plate 104, side plate 108 (upper-deck cabin), and it is nested to form complete mixing
It is layered staged satellite platform configuration.
It is obvious to a person skilled in the art that invention is not limited to the details of the above exemplary embodiments, Er Qie
In the case where without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the present invention is by appended power
Benefit requires rather than above description limits, it is intended that all by what is fallen within the meaning and scope of the equivalent elements of the claims
Variation is included within the present invention.Any reference signs in the claims should not be construed as limiting the involved claims.This
Outside, it is clear that one word of " comprising " does not exclude other units or steps, and odd number is not excluded for plural number.That states in system claims is multiple
Unit or device can also be implemented through software or hardware by a unit or device.The first, the second equal words are used to table
Show title, and does not indicate any particular order.
Claims (8)
1. a kind of nested layering staged satellite platform configuration of mixing, which is characterized in that the satellite platform is configured as promoting service
Cabin passes through the closing cabin staged satellite platform structure of rule layering nested with the mixing that special-shaped deck board overlap joint is realized with load cabin
Type.
2. the nested layering staged satellite platform configuration of mixing according to claim 1, which is characterized in that the propulsion clothes
Business cabin is the two or more layers cabin configuration that concave-convex type, stretching type and the combination of regular rectangular shape deck board are formed by overlapping, including to ground
Lower part protruding plate is embedded in-stretches out plate to ground top, and sunny slope L-type stretches out plate, and opaco L-type stretches out plate, the layer of regular rectangular shape
Plate, partition, side plate and loaded cylinder；To ground lower part protruding plate and to ground top be embedded in-stretch out plate pass through concaveconvex shape match
Insertion docking constitutes complete propulsion service module to ground.
3. the nested layering staged satellite platform configuration of mixing according to claim 2, which is characterized in that described to ground
Lower part protruding plate lower end is horizontal and concordant with service module ontology lower end bottom plate is promoted, and is convex to ground lower part protruding plate upper end.
4. the nested layering staged satellite platform configuration of mixing according to claim 2, which is characterized in that described to ground
It is concave that top, which is embedded in-stretches out plate lower end, is to stretch out to promote service module to the part-structure that ground top was embedded in-stretched out plate upper end
Ontology upper end.
5. the nested layering staged satellite platform configuration of mixing according to claim 2, which is characterized in that the sunny slope
L-type stretches out plate and the upper end protrusion part stretching of opaco L-type stretching plate promotes service module ontology upper end.
6. the nested layering staged satellite platform configuration of mixing according to claim 1, which is characterized in that the load cabin
Cabin configuration is layered for upper and lower two or more layers enclosure and to the mixing that the semiclosed cludy in ground is composed.
7. the nested layering staged satellite platform configuration of mixing according to claim 6, which is characterized in that the enclosure
It is made of rectangle rule deck board, it is described that the bottom plate, small to floor and two pieces of the enclosure is utilized to the semiclosed cludy in ground
Partition, one piece small top plate are constituted.
8. the nested layering staged satellite platform configuration of mixing according to claim 2, which is characterized in that described to ground
Top is embedded in-stretches out plate, sunny slope L-type stretches out plate and opaco L-type stretches out the upper end extension of plate and half envelope of load cabin
Close the mixing nesting closing cludy that cludy forms complete closure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810631166.1A CN108820263B (en) | 2018-06-19 | 2018-06-19 | Mixed nested layered stepped satellite platform configuration |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810631166.1A CN108820263B (en) | 2018-06-19 | 2018-06-19 | Mixed nested layered stepped satellite platform configuration |
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| CN108820263A true CN108820263A (en) | 2018-11-16 |
| CN108820263B CN108820263B (en) | 2020-03-06 |
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| CN201810631166.1A Active CN108820263B (en) | 2018-06-19 | 2018-06-19 | Mixed nested layered stepped satellite platform configuration |
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| CN109466799A (en) * | 2018-11-20 | 2019-03-15 | 赵宏杰 | A kind of modular microfluidic Nano satellite platform |
| CN110217409A (en) * | 2019-05-30 | 2019-09-10 | 北京卫星制造厂有限公司 | In-orbit fast assembling-disassembling micro-nano satellite platform structure |
| CN112319851A (en) * | 2020-10-20 | 2021-02-05 | 北京空间飞行器总体设计部 | Large-scale boxboard formula communication cabin structure |
| CN114537709A (en) * | 2022-01-14 | 2022-05-27 | 上海卫星工程研究所 | Load embedded type installation satellite platform structure and assembling method thereof |
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| CN114537709B (en) * | 2022-01-14 | 2023-10-10 | 上海卫星工程研究所 | Load embedded type installation satellite platform configuration and assembly method thereof |
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| Publication number | Publication date |
|---|---|
| CN108820263B (en) | 2020-03-06 |
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