CN106404029A - Satellite composite material planar frame hanging debugging tool - Google Patents
Satellite composite material planar frame hanging debugging tool Download PDFInfo
- Publication number
- CN106404029A CN106404029A CN201610756152.3A CN201610756152A CN106404029A CN 106404029 A CN106404029 A CN 106404029A CN 201610756152 A CN201610756152 A CN 201610756152A CN 106404029 A CN106404029 A CN 106404029A
- Authority
- CN
- China
- Prior art keywords
- satellite
- cantilever
- debugging tool
- main frame
- plane framework
- 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.)
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
- G01D11/00—Component parts of measuring arrangements not specially adapted for a specific variable
- G01D11/30—Supports specially adapted for an instrument; Supports specially adapted for a set of instruments
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Clamps And Clips (AREA)
- Sampling And Sample Adjustment (AREA)
Abstract
The invention provides a satellite composite material planar frame hanging debugging tool. The satellite composite material planar frame hanging debugging tool comprises a supporting main frame, wherein the supporting main frame is provided with a cantilever and a fixed arm, the fixed arm is arranged at a lower side of the cantilever, the cantilever is provided with hanging points, the fixed arm is provided with supporting points, and the supporting main frame is formed through welding metal pipes or assembling the metal pipes through screws and positioning pins. According to the tool, the multiple hanging points are set, the hanging points of a satellite plane frame can be utilized, and adaptation to the spacing position of the hanging points can be realized through adjustment.
Description
Technical field
The present invention relates to debugging tool, in particular it relates to a kind of satellite hangs debugging tool with composite plane framework.
Background technology
Plane framework is a kind of antenna carrier that satellite is commonly used, and typically adopts composite material parts to pass through splicing and has assembled
Become, by the sheet metal glueing joint on the composite is integrally machined with guarantee installed surface precision, the antenna frame in satellite launch
Frame draws in together in a folded fashion, reinflated after satellier injection.Due to there is the larger area of plane and relatively in plane framework
Little thickness, poor rigidity in face, its flatness exist gravity impact and space state of weightlessness be difficult to be consistent.
For solving the impact to plane framework flatness for the gravity, ground test is general to be passed through vertically to hang product installed surface
Hang, from reducing the component gravity vertical mounting surface to the full extent.Product is carried out hang test and debugging requirement product suspension
During can be disposed vertically as far as possible, fixing point can not to product produce power of enforcement, simultaneously frock can adapt to various sizes of
Plane framework, has versatility.Before the present invention, plane framework is typically hung by easy 2 points or multi-point suspended is fixed,
2 points are suspended on state when product contact type measurement is debugged and can shift, and the multiple spot fixation exceeding three-point fix easily makes framework
Stress deformation, is simultaneous for the different appearance and sizes of Different Plane framework, poor universality.
Content of the invention
For defect of the prior art, it is an object of the invention to provide a kind of satellite is hung with composite plane framework
Debugging tool.
Debugging tool is hung with composite plane framework according to the satellite that the present invention provides, including the main frame of support；
Wherein, the main frame of described support is provided with cantilever and fixed arm；Described fixed arm is arranged on the downside of described cantilever；
The suspension suspension centre being provided with cantilever, is provided with the strong point on fixed arm.
Preferably, support main frame be welded using metal tube or metal tube between by screw, shop bolt assembling and
Become.
Preferably, described cantilever carries out Y-direction regulation and fixation by following any one mode on supporting main frame：
- hydraulic drive；
- chain connection；
- gear drives；
- positioning pin connection.
Preferably, described fixed arm carries out Y-direction regulation and fixation by following any one mode on supporting main frame：
- hydraulic drive；
- chain connection；
- gear drives；
- positioning pin connection.
Preferably, hang suspension centre, on cantilever, X is carried out to regulation and fixation by following any one mode：
- hydraulic drive；
- chain connection；
- gear drives；
- positioning pin connection.
Preferably, the strong point can carry out X to the regulation with Z-direction and fixation by following any one mode on fixed arm：
- hydraulic drive；
- chain connection；
- gear drives；
- positioning pin connection.
Preferably, hang suspension centre and be provided with bidirectional helical structure；
Preferably, the strong point is provided with clamping and locking device.
Preferably, cantilever, fixed arm and can be mobile along the vertical direction supporting main frame, fixing；Hanging suspension centre being capable of edge
Cantilever transverse shifting, fixation；The strong point can be along fixed arm transverse shifting, fixation.
Preferably, described suspension suspension centre is provided with the square snap ring being connected with cantilever；Described square snap ring passes through fixing screws
Cantilever connects.
Compared with prior art, the present invention has following beneficial effect：
1st, the present invention is provided with multiple suspension suspension centres, can utilize the suspension centre of satellite plane framework, and can adjust adaptation
The spaced position of suspension centre；
2nd, the present invention is capable of the plumbness of convenient adjustment plane framework, makes the component of gravity vertical frame mounting plane
Little；
3rd, the present invention can adapt to the plane framework suspension measurement of various appearance and sizes, and provides three-point mount effectively,
While ensureing that framework clamping is stablized, it is prevented effectively from clamping and imposed deformation is produced to framework.
Brief description
The detailed description with reference to the following drawings, non-limiting example made by reading, the further feature of the present invention,
Objects and advantages will become more apparent upon：
Fig. 1 is the structural representation that embodiment of the present invention Satellite composite plane framework hangs debugging tool；
Fig. 2 is to support main frame schematic diagram in the embodiment of the present invention；
Fig. 3 is cantilever, the connection diagram of fixed arm in the embodiment of the present invention；
Fig. 4 is the structural representation hanging suspension centre in the embodiment of the present invention；
Fig. 5 is the structural representation of the strong point in the embodiment of the present invention.
Specific embodiment
With reference to specific embodiment, the present invention is described in detail.Following examples will be helpful to the technology of this area
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill to this area
For personnel, without departing from the inventive concept of the premise, some deformation can also be made and improve.These broadly fall into the present invention
Protection domain.
In the present embodiment, the satellite that the present invention provides hangs debugging tool with composite plane framework, including support
Main frame 1；Wherein, the main frame 1 of described support is provided with cantilever 4 and fixed arm 5；Described fixed arm 5 is arranged under described cantilever 4
Side；The suspension suspension centre 2 being provided with cantilever 4, is provided with the strong point 3 on fixed arm 5.
Support main frame 1 to be welded using metal tube or metal tube between assembled by screw, shop bolt.
Described cantilever 4 carries out Y-direction regulation and fixation by following any one mode on supporting main frame 1：
- hydraulic drive；
- chain connection；
- gear drives；
- positioning pin connection.
Described fixed arm 5 carries out Y-direction regulation and fixation by following any one mode on supporting main frame 1：
- hydraulic drive；
- chain connection；
- gear drives；
- positioning pin connection.
Suspension suspension centre 2 carries out X by following any one mode on cantilever 4 to regulation and to be fixed：
- hydraulic drive；
- chain connection；
- gear drives；
- positioning pin connection.
The strong point 3 can carry out X to the regulation with Z-direction and fixation by following any one mode on fixed arm 5：
- hydraulic drive；
- chain connection；
- gear drives；
- positioning pin connection.
Hang suspension centre 2 and be provided with bidirectional helical structure；The strong point 3 is provided with clamping and locking device.
Cantilever 4, fixed arm 5 with can be mobile, fixing along the vertical direction supporting main frame 1；Hanging suspension centre 2 can be along cantilever
Transverse shifting, fixation；The strong point can be along fixed arm 5 transverse shifting, fixation.
In the present embodiment, main frame 1 is supported to be welded by seamless cold rectangular steel pipe, using the material of model Q235A
Material is made it is ensured that supporting the lightweight of main frame, and rigidity is good；
As shown in Fig. 2 supporting main frame 1 both sides to be provided with screwed hole, for adjusting the height of cantilever 4, fixed arm 5 to adapt to treat
The different profiles of debugging product；In other examples, the version of main frame 1 and height adjusting holes are supported can also to take
Other designs；
As shown in figure 3, cantilever 4, fixed arm 5 pass through screw and the installation being arranged on three relevant position with supporting main frame 1
Hole is fixed and adjusts, and adjusts the adjustment making to be fixed distance according to the pitch-row supporting on main frame 1 in this example；At other
In embodiment, the connection of cantilever 4, fixed arm 5 and the main frame 1 of support and regulation can also take other designs；
As shown in figure 4, hanging suspension centre 2 to be provided with the square snap ring being connected with cantilever 4 and fixing screws it is ensured that hanging
Suspension centre 2 is slidably and fixing in cantilever 4, and lower section is provided with the two-way bolt of many specifications, for the suspension centre spiral shell with product dimension
Pit connects；In other examples, snap ring, fixing screws and two-way bolt also can take other designs；
As shown in figure 5, the strong point 3 is provided with the square snap ring being connected with fixed arm 5 and fixing screws it is ensured that supporting
Point 3 is slidably and fixing in fixed arm 5, and upper end is provided with product draw-in groove and adjustment screw, can be consolidated by bilateral screw
Fixed output quota product, control the amount of screwing of bilateral screw can adjust the side-play amount perpendicular to installed surface direction at this for the product simultaneously it is ensured that
The plumbness that product hangs；In other examples, snap ring, draw-in groove, fixing screws, adjusting screw also can take other to set
Meter mode.
Above the specific embodiment of the present invention is described.It is to be appreciated that the invention is not limited in above-mentioned
Particular implementation, those skilled in the art can make various modifications or modification within the scope of the claims, this not shadow
Ring the flesh and blood of the present invention.
Claims (10)
1. a kind of satellite hangs debugging tool with composite plane framework it is characterised in that including supporting main frame (1)；
Wherein, the main frame of described support (1) is provided with cantilever (4) and fixed arm (5)；Described fixed arm (5) is arranged on described outstanding
The downside of arm (4)；
The suspension suspension centre (2) being provided with cantilever (4), is provided with the strong point (3) on fixed arm (5).
2. satellite as claimed in claim 1 hangs debugging tool with composite plane framework it is characterised in that supporting main frame
(1) be welded using metal tube or metal tube between assembled by screw, shop bolt.
3. satellite as claimed in claim 1 composite plane framework hangs debugging tool it is characterised in that described cantilever
(4) on supporting main frame (1), Y-direction regulation and fixation are carried out by following any one mode：
- hydraulic drive；
- chain connection；
- gear drives；
- positioning pin connection.
4. satellite as claimed in claim 1 composite plane framework hangs debugging tool it is characterised in that described fixation
Arm (5) carries out Y-direction regulation and fixation by following any one mode on supporting main frame (1)：
- hydraulic drive；
- chain connection；
- gear drives；
- positioning pin connection.
5. satellite as claimed in claim 1 hangs debugging tool with composite plane framework it is characterised in that hanging suspension centre
(2) carry out X by following any one mode on cantilever (4) to regulation and to fix：
- hydraulic drive；
- chain connection；
- gear drives；
- positioning pin connection.
6. satellite as claimed in claim 1 composite plane framework hangs debugging tool it is characterised in that the strong point
(3) X can be carried out to the regulation with Z-direction and fixation by following any one mode on fixed arm (5)：
- hydraulic drive；
- chain connection；
- gear drives；
- positioning pin connection.
7. satellite as claimed in claim 1 hangs debugging tool with composite plane framework it is characterised in that hanging suspension centre
(2) it is provided with bidirectional helical structure.
8. satellite as claimed in claim 1 composite plane framework hangs debugging tool it is characterised in that the strong point
(3) it is provided with clamping and locking device.
9. satellite as claimed in claim 1 with composite plane framework hang debugging tool it is characterised in that cantilever (4),
Fixed arm (5) with can be mobile, fixing along the vertical direction supporting main frame (1)；Hang suspension centre (2) laterally to move along cantilever
Dynamic, fixing；The strong point can be along fixed arm (5) transverse shifting, fixation.
10. satellite as claimed in claim 1 with composite plane framework hang debugging tool it is characterised in that
Described suspension suspension centre (2) is provided with the square snap ring being connected with cantilever (4)；Described square snap ring passes through fixing screws cantilever
(4) connect.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610756152.3A CN106404029B (en) | 2016-08-29 | 2016-08-29 | Satellite hangs debugging tool with composite material plane framework |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610756152.3A CN106404029B (en) | 2016-08-29 | 2016-08-29 | Satellite hangs debugging tool with composite material plane framework |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106404029A true CN106404029A (en) | 2017-02-15 |
| CN106404029B CN106404029B (en) | 2018-11-23 |
Family
ID=58002569
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610756152.3A Active CN106404029B (en) | 2016-08-29 | 2016-08-29 | Satellite hangs debugging tool with composite material plane framework |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106404029B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107486734A (en) * | 2017-07-19 | 2017-12-19 | 上海复合材料科技有限公司 | A kind of method that satellite machines clamping with carbon fibre composite plane framework suspension status |
| CN109883662A (en) * | 2017-12-06 | 2019-06-14 | 红塔烟草(集团)有限责任公司 | The experimental provision of knife sharpener assembly debugging on a kind of tobacco cutting machine |
| CN113752055A (en) * | 2021-09-01 | 2021-12-07 | 上海复合材料科技有限公司 | Clamping tool and method for vertical suspension machining of planar frame |
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| JPS61124838A (en) * | 1984-11-22 | 1986-06-12 | Toshiba Corp | Apparatus for supporting object to be tested used in testing vibration test of cosmic structure |
| DE20213955U1 (en) * | 2002-09-09 | 2003-05-15 | Bolik Torsten | Experimental equipment for determining the effect on motion behavior in space, comprises capsule suspended from frame on flexible spring line |
| CN1612953A (en) * | 2001-09-14 | 2005-05-04 | 埃托特克德国有限公司 | Device for the transport and wet-chemical or electrolytic treatment of very thin and planar items to be treated |
| CN201144297Y (en) * | 2007-11-29 | 2008-11-05 | 比亚迪股份有限公司 | Combined hanger |
| CN102145755A (en) * | 2010-02-10 | 2011-08-10 | 上海卫星工程研究所 | Zero-gravity suspension type deployment test device |
| CN102842745A (en) * | 2011-06-22 | 2012-12-26 | 鸿富锦精密工业（深圳）有限公司 | Antenna support |
| CN202836967U (en) * | 2012-08-21 | 2013-03-27 | 中国航天科技集团公司第四研究院四0一所 | Hanging test device employing flexible fixed connection method |
| CN203056076U (en) * | 2012-12-12 | 2013-07-10 | 中国华冶科工集团有限公司 | Auxiliary apparatus for geological radar detection |
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2016
- 2016-08-29 CN CN201610756152.3A patent/CN106404029B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS61124838A (en) * | 1984-11-22 | 1986-06-12 | Toshiba Corp | Apparatus for supporting object to be tested used in testing vibration test of cosmic structure |
| CN1612953A (en) * | 2001-09-14 | 2005-05-04 | 埃托特克德国有限公司 | Device for the transport and wet-chemical or electrolytic treatment of very thin and planar items to be treated |
| DE20213955U1 (en) * | 2002-09-09 | 2003-05-15 | Bolik Torsten | Experimental equipment for determining the effect on motion behavior in space, comprises capsule suspended from frame on flexible spring line |
| CN201144297Y (en) * | 2007-11-29 | 2008-11-05 | 比亚迪股份有限公司 | Combined hanger |
| CN102145755A (en) * | 2010-02-10 | 2011-08-10 | 上海卫星工程研究所 | Zero-gravity suspension type deployment test device |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107486734A (en) * | 2017-07-19 | 2017-12-19 | 上海复合材料科技有限公司 | A kind of method that satellite machines clamping with carbon fibre composite plane framework suspension status |
| CN107486734B (en) * | 2017-07-19 | 2019-02-15 | 上海复合材料科技有限公司 | A kind of method that satellite machines clamping with carbon fibre composite plane framework suspension status |
| CN109883662A (en) * | 2017-12-06 | 2019-06-14 | 红塔烟草(集团)有限责任公司 | The experimental provision of knife sharpener assembly debugging on a kind of tobacco cutting machine |
| CN109883662B (en) * | 2017-12-06 | 2024-05-07 | 红塔烟草(集团)有限责任公司 | Experimental device for debugging knife grinder assembly on tobacco cutter |
| CN113752055A (en) * | 2021-09-01 | 2021-12-07 | 上海复合材料科技有限公司 | Clamping tool and method for vertical suspension machining of planar frame |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106404029B (en) | 2018-11-23 |
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