CN109927944A - Micro-nano satellite intelligent design platform - Google Patents
Micro-nano satellite intelligent design platform Download PDFInfo
- Publication number
- CN109927944A CN109927944A CN201910376318.2A CN201910376318A CN109927944A CN 109927944 A CN109927944 A CN 109927944A CN 201910376318 A CN201910376318 A CN 201910376318A CN 109927944 A CN109927944 A CN 109927944A
- Authority
- CN
- China
- Prior art keywords
- micro
- nano satellite
- design platform
- intelligent design
- installation frame
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Landscapes
- Details Of Aerials (AREA)
- Particle Accelerators (AREA)
Abstract
The invention discloses a kind of installation site convenient for each functional component of micro-nano satellite, overall performance carries out assembling test, is easy to implement the micro-nano satellite intelligent design platform of different function micro-nano satellite design.The micro-nano satellite intelligent design platform, including pedestal and cuboid installation frame are provided with turntable on the pedestal；The cuboid installation frame is mounted on turntable, and is clamped by clamping jaw；The cuboid installation frame has bottom plate and top plate；Side plate is provided on four sides of the bottom plate；One end of the side plate and bottom plate are hinged；The other end is provided with fixture block；The dismountable horizontal baffle of multilayer is provided in the cuboid installation frame；The roof center position is provided with center mounting hole；Mounting cylinder is slidably fitted in the center mounting hole.It can be improved the efficiency of micro-nano satellite test using the micro-nano satellite intelligent design platform, the design of micro-nano satellite can be convenient for.
Description
Technical field
The present invention relates to the design of micro-nano satellite, especially a kind of micro-nano satellite intelligent design platform.
Background technique
Well-known: micro-nano satellite is often referred to quality less than 10 kilograms, the satellite with actual use function.With height
The development of new technology and the promotion of demand, micro-nano satellite is with small in size, low in energy consumption, the development cycle is short, and can form into columns networking, with lower
Cost complete the advantages of many complicated space tasks, played an important role in fields such as scientific research, national defence and commercializations.
Micro-nano satellite technology is considered as the commanding elevation of 21 century National Technical and economic development.Developed country all attaches great importance to
Microminiature technology space industry application and formulated corresponding development plan, such as the stellar chain plan of SpaceX, Amazon
Kuiper plan, the internet satellite constellation plan of OneWeb, " dove group " Project Constellation of Planet lab etc., and show good
Technology well, economic and social benefit.
Modular micro-nano satellite, at the whole star of satellite, is achieved communication, appearance by the block combiner with different function
The functions such as control, energy storage.But existing micro-nano satellite is in an assembling process, the interface standard and disunity of each functional module, it can
It is alternative not strong.Therefore cost of manufacture is higher, and satellite platform versatility is poor.
In the design process of micro-nano satellite, need to debug different function module, the installation to each functional module
It is required to constantly be debugged, so that each spaceborne functional module reaches optimal state and optimal installation site, thus
The volume of satellite can effectively be reduced while guaranteeing micro-nano satellite the operation is stable.
Existing micro-nano satellite design platform is not easy to carry out the installation and debugging of each functional component of satellite, and debugging needs every time
Satellite is dismantled, the position of each functional component is adjusted, or is assembled again after substituting certain functional components, group
It is debugged, therefore complicated for operation, and is assembled cumbersome again after the completion of dress.
Summary of the invention
Technical problem to be solved by the invention is to provide a kind of installation positions convenient for each functional component of micro-nano satellite
It sets, overall performance carries out assembling test, is easy to implement the micro-nano satellite intelligent design platform of different function micro-nano satellite design.
The technical solution adopted by the present invention to solve the technical problems is: micro-nano satellite intelligent design platform, including pedestal
And cuboid installation frame, turntable is provided on the pedestal；There are four circumferentially equally distributed for setting on the turntable
Radial groove；Clamping jaw is slidably fitted on the radial groove；It is provided on the clamping jaw and clamping jaw is fixed on radial groove
Lock-screw；
The cuboid installation frame is mounted on turntable, and is clamped by clamping jaw；The cuboid installation frame has
Bottom plate and top plate；The cuboid installation frame two is to being provided with vertical equally distributed slot on the column of side；
Side plate is provided on four sides of the bottom plate；One end of the side plate and bottom plate are hinged；The other end is provided with fixture block；
Horizontal baffle is provided in the slot of the cuboid installation frame；The horizontal baffle is slidably mounted on slot
It is interior；Card slot and regulating tank are provided on four sides of the top plate；The card slot is matched with fixture block, is set in the card slot
It is equipped with the slide post for blocking fixture block；One end of the slide post passes through card slot and extends in regulating tank；
The roof center position is provided with center mounting hole；Mounting cylinder is slidably fitted in the center mounting hole.
Further, the upper end of the clamping jaw is provided with horizontal supporting plate.
Further, changeover base is provided with below the bottom plate.
Further, air hole is provided on the side wall of the mounting cylinder.
Further, solar array is installed on the outside of the side plate.
Specifically, being provided with universal communication connectivity port on every layer of horizontal baffle.
Specifically, being separately installed with different satellite load devices on every layer of horizontal baffle.
Further, installation threaded hole is provided on the horizontal baffle.
Further, two of the cuboid installation frame are to being provided with second on two crossbeams up and down on side
Slot.
The beneficial effects of the present invention are:
1) micro-nano satellite intelligent design platform of the present invention, since side plate is hinged with bottom plate, by the way that side plate is unfolded,
So as to which micro-nano satellite internal component is installed and is replaced.
2) horizontal baffle of internal components installation simultaneously can be extracted out, consequently facilitating realizing to each function in micro-nano satellite inside
The installation and replacement of energy device, consequently facilitating the micro-nano satellite to different function carries out assembling test.Therefore, it can be improved micro-nano
The efficiency of satellite test can be convenient for the design of micro-nano satellite.
3) it is provided with turntable on pedestal, therefore in Installation And Test micro-nano satellite when all parts, micro-nano can be rotated
Satellite frame, consequently facilitating all parts of installation micro-nano satellite.
4) it further, is provided with slot on two crossbeams up and down of same side, so as to be convenient for vertical baffle
Installation, be easy to implement satellite function element different location installation test.
5) secondly, micro-nano satellite intelligent design platform structure of the present invention is simple, convenient for operation.
6) finally, the center of micro-nano satellite intelligent design platform upper of the present invention is provided with mounting hole, from
And the installation test of micro-nano satellite core component can be easy to implement；It can be convenient for the more preferable debugging of core component.
7) micro-nano satellite intelligent design platform of the present invention can simplify the design of micro-nano satellite, can be improved design
Efficiency has biggish economic value.
Detailed description of the invention
Fig. 1 is the perspective view of the explosion of micro-nano satellite intelligent design platform in the embodiment of the present invention；
Perspective view when Fig. 2 is the side plate expansion of micro-nano satellite intelligent design platform in the embodiment of the present invention；
Fig. 3 is the perspective view when horizontal baffle of micro-nano satellite intelligent design platform in the embodiment of the present invention stretches out；
Structural schematic diagram when Fig. 4 is the side plate expansion of micro-nano satellite intelligent design platform in the embodiment of the present invention；
Fig. 5 is the perspective view when side plate of micro-nano satellite intelligent design platform in the embodiment of the present invention is packed up；
Fig. 6 is the main view when side plate of micro-nano satellite intelligent design platform in the embodiment of the present invention is packed up；
Fig. 7 is the A-A cross-sectional view in Fig. 6；
It is indicated in figure: 1- pedestal, 2- turntable, 3- radial groove, 4- clamping jaw, 5- cuboid installation frame, 6- bottom plate, the side 7-
Plate, 8- through-hole, 9- top plate, 10- horizontal baffle, 11- mounting cylinder, 12- center mounting hole.
Specific embodiment
Present invention will be further explained below with reference to the attached drawings and examples.
As shown in Figures 1 to 7, micro-nano satellite intelligent design platform of the present invention, including pedestal 1 and cuboid peace
Frame up frame 5, is provided with turntable 2 on the pedestal 1；There are four circumferentially equally distributed radial grooves for setting on the turntable 2
3；Clamping jaw 4 is slidably fitted on the radial groove 3；It is provided on the clamping jaw 4 and clamping jaw 4 is fixed on radial groove 3
Lock-screw 41；
The cuboid installation frame 5 is mounted on turntable 2, and is clamped by clamping jaw 4；The cuboid installation frame 5
With bottom plate 6 and top plate 9；The cuboid installation frame 5 two is vertically uniformly distributed to being provided on the column of side
Slot 51；Side plate 7 is provided on four sides of the bottom plate 6；One end of the side plate 7 and bottom plate 6 are hinged；The other end
It is provided with fixture block 71；
Horizontal baffle 10 is provided in the slot 51 of the cuboid installation frame 5；The horizontal baffle 10 is slidably installed
In slot 51；Card slot 91 and regulating tank 92 are provided on four sides of the top plate 9；The card slot 91 and fixture block 71
It matches, is provided with the slide post 93 for blocking fixture block 71 in the card slot 91；One end of the slide post 93 extends across card slot 91
Into regulating tank 92；
9 center of top plate is provided with center mounting hole 12；Installation is slidably fitted in the center mounting hole 12
Cylinder 11.
During application, since the cuboid installation frame 5 two is vertical to being provided on the column of side
Equally distributed slot 51；Horizontal baffle 10 is provided in the slot 51 of the cuboid installation frame 5；The horizontal baffle 10
It is slidably mounted in slot 51；Therefore multiple-layer horizontal partition 10 can be inserted into cuboid installation frame 5；Can level every
Respective satellite load device is installed, while can be according to the layer of the big minor adjustment horizontal baffle 10 of satellite load device on plate 10
Number；Convenient for the installation of satellite load device.
During the installation process, as shown in figure 3, side plate 7 is unfolded, while horizontal baffle 10 being pulled out, so as to be convenient for
Satellite load device is installed on horizontal baffle 10.Further it can be provided with bolt hole on horizontal baffle 10, thus just
It is fixed on horizontal baffle 10 in by star load device.Further, since the cuboid installation frame 5 is mounted on turntable 2
On, and clamped by clamping jaw 4；Therefore in installation process, cuboid installation frame 5 can be rotated, so as to carry convenient for satellite
The installation of lotus device.After corresponding satellite load device is installed on horizontal baffle, other can be installed by mounting cylinder 11 and defended
Star function element.Therefore the design platform can satisfy the installation test of a variety of satellite function elements.
When corresponding function part is installed in mounting cylinder 11, function element can be installed to by taking out mounting cylinder 11
Then mounting cylinder 11 is inserted into mounting cylinder 11.It specifically can be by the way that bolt hole be arranged on mounting cylinder 11, consequently facilitating function
It can installation of the device on mounting cylinder 11.
After being installed, horizontal baffle 10 is inserted into cuboid installation frame 5, while by the number of each function element
After being attached according to line, side plate 7 is packed up, so that fixture block 71 is located in card slot 91, and passes through the slide post 93 in card slot 91
Block fixture block 71；As shown in Figure 5.Then the entirety of micro-nano satellite can be tested accordingly.
In conclusion micro-nano satellite intelligent design platform of the present invention has the advantages that
1) micro-nano satellite intelligent design platform of the present invention, since side plate is hinged with bottom plate, by the way that side plate is unfolded,
So as to which micro-nano satellite internal component is installed and is replaced.
2) horizontal baffle of internal components installation simultaneously can be extracted out, consequently facilitating realizing to each function in micro-nano satellite inside
The installation and replacement of energy device, consequently facilitating the micro-nano satellite to different function carries out assembling test.Therefore, it can be improved micro-nano
The efficiency of satellite test can be convenient for the design of micro-nano satellite.
3) it is provided with turntable on pedestal, therefore in Installation And Test micro-nano satellite when all parts, micro-nano can be rotated
Satellite frame, consequently facilitating all parts of installation micro-nano satellite.
4) it further, is provided with slot on two crossbeams up and down of same side, so as to be convenient for vertical baffle
Installation, be easy to implement satellite function element different location installation test.
5) secondly, micro-nano satellite intelligent design platform structure of the present invention is simple, convenient for operation.
6) finally, the center of micro-nano satellite intelligent design platform upper of the present invention is provided with installation through-hole,
So as to be easy to implement the installation test of micro-nano satellite core component；It can be convenient for the more preferable debugging of core component.
7) micro-nano satellite intelligent design platform of the present invention can simplify the design of micro-nano satellite, can be improved design
Efficiency has biggish economic value.
For the ease of the expansion of side plate 7, further, the upper end of the clamping jaw 4 is provided with horizontal supporting plate 42.In clamping jaw
Horizontal supporting plate 42 is set on 4, consequently facilitating realizing the support to side plate 7.
For the ease of accordingly being tested, convenient for being connected with test component, further side, under the bottom plate 6
Side is provided with changeover base.
For the ease of the ventilative of mounting cylinder 11, further, air hole is provided on the side wall of the mounting cylinder 11.
For the ease of the test to realizing in micro-nano satellite surface setting solar battery, further, the side plate 7
Outside is equipped with solar array.
For the ease of the installation of each function element, or substitute, further, is provided on every layer of horizontal baffle 10
Universal communication connectivity port.
In order to realize that the test to different satellite function elements is verified, further, pacify respectively on every layer of horizontal baffle 10
Equipped with different satellite load devices.
For the ease of installation of the satellite function element on horizontal baffle, further, it is provided on the horizontal baffle
Threaded hole is installed.
For the ease of installing vertical baffle, further, two of the cuboid installation frame 5 are to upper and lower on side
The second slot is provided on two crossbeams.By the way that the second slot is arranged, so as to convenient for setting vertical baffle；It replaces original
Horizontal baffle.
Claims (9)
1. micro-nano satellite intelligent design platform, it is characterised in that: including pedestal (1) and cuboid installation frame (5), the bottom
Turntable (2) are provided on seat (1)；There are four circumferentially equally distributed radial grooves (3) for setting on the turntable (2)；It is described
Clamping jaw (4) are slidably fitted on radial groove (3)；It is provided on the clamping jaw (4) and clamping jaw (4) is fixed on radial groove (3)
On lock-screw (41)；
The cuboid installation frame (5) is mounted on turntable (2), and is clamped by clamping jaw (4)；The cuboid installation frame
(5) there is bottom plate (6) and top plate (9)；The cuboid installation frame (5) two vertical to being provided on the column of side
Equally distributed slot (51)；Side plate (7) are provided on four sides of the bottom plate (6)；One end of the side plate (7) with
Bottom plate (6) is hinged；The other end is provided with fixture block (71)；
Horizontal baffle (10) are provided in the slot (51) of the cuboid installation frame (5)；Horizontal baffle (10) sliding
It is mounted in slot (51)；Card slot (91) and regulating tank (92) are provided on four sides of the top plate (9)；The card
Slot (91) is matched with fixture block (71), is provided with the slide post (93) for blocking fixture block (71) in the card slot (91)；The slide post
(93) one end passes through card slot (91) and extends in regulating tank (92)；
Top plate (9) center is provided with center mounting hole (12)；Peace is slidably fitted in the center mounting hole (12)
Fitted tube (11).
2. micro-nano satellite intelligent design platform as described in claim 1, it is characterised in that: the upper end of the clamping jaw (4) is arranged
There are horizontal supporting plate (42).
3. micro-nano satellite intelligent design platform as claimed in claim 2, it is characterised in that: be provided with below the bottom plate (6)
Changeover base.
4. micro-nano satellite intelligent design platform as claimed in claim 3, it is characterised in that: on the side wall of the mounting cylinder (11)
It is provided with air hole.
5. micro-nano satellite intelligent design platform as claimed in claim 4, it is characterised in that: install in the outside of the side plate (7)
There is solar array.
6. micro-nano satellite intelligent design platform as claimed in claim 5, it is characterised in that: be all provided on every layer of horizontal baffle (10)
It is equipped with universal communication connectivity port.
7. micro-nano satellite intelligent design platform as claimed in claim 6, it is characterised in that: on every layer of horizontal baffle (10) respectively
Different satellite load devices is installed.
8. micro-nano satellite intelligent design platform as claimed in claim 6, it is characterised in that: be provided with peace on the horizontal baffle
Fill threaded hole.
9. micro-nano satellite intelligent design platform as claimed in claim 6, it is characterised in that: the cuboid installation frame (5)
Two to being provided with the second slot on two crossbeams up and down on side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910376318.2A CN109927944B (en) | 2019-05-07 | 2019-05-07 | Micro-nano satellite intelligent design platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910376318.2A CN109927944B (en) | 2019-05-07 | 2019-05-07 | Micro-nano satellite intelligent design platform |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109927944A true CN109927944A (en) | 2019-06-25 |
| CN109927944B CN109927944B (en) | 2021-01-12 |
Family
ID=66991453
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910376318.2A Active CN109927944B (en) | 2019-05-07 | 2019-05-07 | Micro-nano satellite intelligent design platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109927944B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112249364A (en) * | 2020-10-28 | 2021-01-22 | 哈尔滨工业大学 | Structural system of a minisatellite, a minisatellite and a method of assembling a minisatellite |
| CN114037912A (en) * | 2022-01-07 | 2022-02-11 | 成都国星宇航科技有限公司 | Method and device for detecting change of remote sensing image and computer readable storage medium |
| RU2825164C1 (en) * | 2024-01-31 | 2024-08-21 | Федеральное Государственное Автономное Образовательное Учреждение Высшего Образования "Самарский Национальный Исследовательский Университет Имени Академика С.П. Королева" (Самарский Университет) | Spacecraft automated assembly complex |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0488872A1 (en) * | 1990-11-30 | 1992-06-03 | AEROSPATIALE Société Nationale Industrielle | Device for temporal holding of an object to a support with a monobloc holding socket |
| CN104290920A (en) * | 2014-10-08 | 2015-01-21 | 上海微小卫星工程中心 | Modular reconfigurable micro-nano satellite structure |
| US9875091B1 (en) * | 2016-11-16 | 2018-01-23 | Vector Launch Inc. | User-initiated software application deployment to an orbital satellite platform |
| CN108733897A (en) * | 2018-04-28 | 2018-11-02 | 上海烜翊科技有限公司 | Attack-defense Confrontation Simulation System based on architectural framework model and emulation mode |
| US20190028181A1 (en) * | 2016-10-19 | 2019-01-24 | Vector Launch Inc. | State Transfer Among Satellite Platforms |
| CN109335023A (en) * | 2018-08-31 | 2019-02-15 | 南京理工大学 | A kind of no cable high density cube star and its assembly method |
-
2019
- 2019-05-07 CN CN201910376318.2A patent/CN109927944B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0488872A1 (en) * | 1990-11-30 | 1992-06-03 | AEROSPATIALE Société Nationale Industrielle | Device for temporal holding of an object to a support with a monobloc holding socket |
| CN104290920A (en) * | 2014-10-08 | 2015-01-21 | 上海微小卫星工程中心 | Modular reconfigurable micro-nano satellite structure |
| US20190028181A1 (en) * | 2016-10-19 | 2019-01-24 | Vector Launch Inc. | State Transfer Among Satellite Platforms |
| US9875091B1 (en) * | 2016-11-16 | 2018-01-23 | Vector Launch Inc. | User-initiated software application deployment to an orbital satellite platform |
| CN108733897A (en) * | 2018-04-28 | 2018-11-02 | 上海烜翊科技有限公司 | Attack-defense Confrontation Simulation System based on architectural framework model and emulation mode |
| CN109335023A (en) * | 2018-08-31 | 2019-02-15 | 南京理工大学 | A kind of no cable high density cube star and its assembly method |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112249364A (en) * | 2020-10-28 | 2021-01-22 | 哈尔滨工业大学 | Structural system of a minisatellite, a minisatellite and a method of assembling a minisatellite |
| CN114037912A (en) * | 2022-01-07 | 2022-02-11 | 成都国星宇航科技有限公司 | Method and device for detecting change of remote sensing image and computer readable storage medium |
| RU2825164C1 (en) * | 2024-01-31 | 2024-08-21 | Федеральное Государственное Автономное Образовательное Учреждение Высшего Образования "Самарский Национальный Исследовательский Университет Имени Академика С.П. Королева" (Самарский Университет) | Spacecraft automated assembly complex |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109927944B (en) | 2021-01-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109927944A (en) | Micro-nano satellite intelligent design platform | |
| CN107800371A (en) | A kind of photovoltaic module group mount structure for being easy to splicing | |
| CN109600943A (en) | A kind of modular functionality case with scalability | |
| CN217156241U (en) | Road simulation experiment device for engineering detection | |
| CN109411866A (en) | A kind of 5G antenna holder | |
| CN109466799A (en) | A kind of modular microfluidic Nano satellite platform | |
| CN201270314Y (en) | Multi-unit connector capable of unit disassembly | |
| CN210281434U (en) | Support device and support assembly for automobile clay model | |
| CN208839085U (en) | Prepare the modular construction of chromatographic column | |
| CN209896966U (en) | Solar energy component mounting bracket | |
| CN208621371U (en) | One kind dividing sampling device and acquisition and analysis device | |
| CN221705067U (en) | Total station for space resource planning | |
| CN204485922U (en) | A kind of Multifunctional test tube rack | |
| CN206627620U (en) | A kind of multiple-unit crosses knot adjustment device | |
| CN212830345U (en) | Constant temperature and humidity box | |
| CN116388653B (en) | Automatic regulating device for solar photovoltaic panel | |
| CN201724958U (en) | Package type solar module exposure rack | |
| CN219225181U (en) | Vibration isolation optical mechanism and device | |
| CN110886395A (en) | Support with adjustable net rack assembly lower chord | |
| CN215155794U (en) | 2U &3U cube star quality simulator | |
| CN220254444U (en) | Photovoltaic power station without rain leakage | |
| CN221597988U (en) | Road safety monitoring equipment | |
| CN221707693U (en) | Test power supply device | |
| CN215540271U (en) | Liquid preparation container for pharmaceutical and pharmacological research | |
| CN209104346U (en) | A kind of 5G antenna holder |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20200918 Address after: 610000 No.16, 1st floor, building 7, No.333, middle Shuangnan Avenue, Dongsheng Street, Shuangliu District, Chengdu, Sichuan Province 610000 Applicant after: CHENGDU GUOXING AEROSPACE TECHNOLOGY Co.,Ltd. Address before: 100071 Beijing Fengtai District, Donggaodi South Dahongmen Road, No. 1, No. 38, No. 428 Applicant before: Zhao Hongjie Applicant before: CHENGDU GUOXING AEROSPACE TECHNOLOGY Co.,Ltd. |
|
| TA01 | Transfer of patent application right | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: No. 200, building 16, middle section of shuangshenggang Avenue, Shuangliu District, Chengdu, Sichuan Province Patentee after: Chengdu Guoxing Aerospace Technology Co.,Ltd. Address before: No.16, 1st floor, building 7, No.333, middle section of Shuangnan Avenue, Dongsheng Street, Shuangliu District, Chengdu, Sichuan 610000 Patentee before: CHENGDU GUOXING AEROSPACE TECHNOLOGY Co.,Ltd. |
|
| CP03 | Change of name, title or address |