CN107053103A - A kind of attitude of satellite adjusts frock - Google Patents
A kind of attitude of satellite adjusts frock Download PDFInfo
- Publication number
- CN107053103A CN107053103A CN201710384568.1A CN201710384568A CN107053103A CN 107053103 A CN107053103 A CN 107053103A CN 201710384568 A CN201710384568 A CN 201710384568A CN 107053103 A CN107053103 A CN 107053103A
- Authority
- CN
- China
- Prior art keywords
- bearing
- bracket
- product
- bracket base
- 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.)
- Pending
Links
- 229910000831 Steel Inorganic materials 0.000 claims description 24
- 239000010959 steel Substances 0.000 claims description 24
- 239000000758 substrate Substances 0.000 claims description 13
- 238000003466 welding Methods 0.000 claims description 10
- 235000004443 Ricinus communis Nutrition 0.000 claims description 6
- 229910000838 Al alloy Inorganic materials 0.000 claims description 4
- 238000010276 construction Methods 0.000 claims description 2
- 238000007493 shaping process Methods 0.000 claims description 2
- 238000000034 method Methods 0.000 abstract description 9
- 230000013011 mating Effects 0.000 abstract description 8
- 238000004519 manufacturing process Methods 0.000 abstract description 4
- 230000000149 penetrating effect Effects 0.000 abstract description 3
- 238000005259 measurement Methods 0.000 abstract description 2
- 229910000906 Bronze Inorganic materials 0.000 description 1
- 241000237858 Gastropoda Species 0.000 description 1
- 240000000528 Ricinus communis Species 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 239000010974 bronze Substances 0.000 description 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25H—WORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
- B25H1/00—Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby
- B25H1/10—Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby with provision for adjusting holders for tool or work
Abstract
Frock is adjusted the invention provides a kind of attitude of satellite, satellite is fixed in the attitude of satellite of the present invention adjustment frock, during adjustment rotation attitude, interface frame, mating frame is directly rotated, product rotates with interface frame, mating frame, when being rotated by 90 °, penetrating alignment pin makes product orientation；When adjusting flipping gesture, handwheel is rotated, drives bracket and product to overturn by worm and gear, is locked using worm and gear auto-lock function in switching process optional position；Clamped one time can realize 360 degree of product rotations and ± 90 degree upsets, in switching process can any angle locking, solve pose adjustment time and effort consuming in such product final assemble, measurement process, there is the problems such as security risk, it is ensured that product quality, reduction production cost.
Description
Technical field
The technical scheme is related to the product final assemble such as satellite field, the pose adjustment frock of specifically a kind of Satellite Product.
Background technology
During Satellite Product general assembly and precision measure, it is often necessary to the pose adjustment such as rotated, overturn to product
Due to lacking suitable frock in operation, Conventional process, pose adjustment work is carried out often by suspender indirect labor,
Cause product safety risk big, labor strength is big, and can not meet production schedule requirement.
The content of the invention
The pose adjustment operations such as rotation, the upsets of product such as the achievable satellite of the present invention, are not take up crane gear, it is ensured that appearance
State adjusts process personnel and product safety, reduces labor strength, improves production efficiency.
This frock includes base, substrate holder, bearing block, bearing, feathering axis one, bracket, feathering axis two, snail
Wheel, worm screw, handwheel, castor, alignment pin, switchover frame, bracket base, vertical rotary shaft, bearing and axle sleeve.
Base is rectangle, using square steel pipe welded structure, and its appearance and size is determined according to the product size adjusted,
Inside is strengthened with square steel pipe welded, and castor is installed in corner location threaded connection in bottom, and the side position of top two passes through welding steel
It is threadedly coupled each 1 of substrate holder；Substrate holder is triangular frame structure, is molded using square steel pipe welded, side matrix
The upside of support is threadedly coupled in bearing block, bearing block by welding steel and installs bearing, connection feathering axis one in bearing,
The upside of opposite side substrate holder is threadedly coupled in bearing block, bearing block by welding steel and installs bearing, connection water in bearing
Flat rotary shaft two, the lateral ends of feathering axis two are connected by flat key with worm and gear, and worm screw is connected with handwheel by nut；
Feathering axis one, feathering axis two are parallel to base, and connecting bracket is distinguished in inner side by screw thread respectively, and bracket uses triangle
Bracket base is threadedly coupled by welding steel on the downside of shape frame structure, square steel pipe welded shaping, bracket；Bracket base is used
Aluminium alloy entirety square structure, symmetrical center positions are provided with axis hole on the upside of it, and axis hole is installed in bracket base, axis hole
Axle sleeve, dowel hole is interval with bracket base circumferential position by 90 degree；Axle sleeve uses the tubular structure with flange, axle sleeve
Outer side flanging is connected through a screw thread with bracket base, and internal diameter is connected by bearing with vertical rotary shaft；Vertical rotary shaft perpendicular to
Switchover frame is connected through a screw thread on the upside of bracket base, vertical rotary shaft；Switchover frame is the tubular construction of two side flangings up and down, flange
Screw thread via is provided with, can be threadedly coupled using via with the passing of satelline, or pass through upper side flanging and passing of satelline band form
Connection, downside is connected by screw thread with vertical rotary shaft, and flange position is interval with dowel hole by 90 degree, its position and bracket
Pin-and-hole position is corresponding on base；Alignment pin is inserted into bracket base dowel hole through dowel hole on switchover frame, is used for
Product rotational positioning.
Frock is fixed by screw in use, satellite is placed on frock interface frame, mating frame.When adjusting rotation attitude, directly
Interface frame, mating frame is rotated, product rotates with interface frame, mating frame, when being rotated by 90 °, and penetrating alignment pin makes product orientation；When adjusting flipping gesture, turn
Start to take turns, drive bracket and product to overturn by worm and gear, using worm and gear auto-lock function in switching process optional position
Locking.
The technical program can realize product for the design of the pose adjustments such as rotation, the upsets of product such as satellite, clamped one time
360 degree rotation and ± 90 degree upset, in switching process can any angle lock, solve such product final assemble, measurement process
Middle pose adjustment time and effort consuming, there is the problems such as security risk, it is ensured that product quality, reduce production cost.
Brief description of the drawings
Fig. 1 attitudes of satellite adjust frock front view
Fig. 2 attitudes of satellite adjust frock right view
Fig. 3 attitudes of satellite adjustment frock product overturns 90 ° of right views
1- bases, 2- substrate holders, 3- bearing blocks, 4- bearings, 5- feathering axis one, 6- brackets, 7- feathering axis
2nd, 8- worm gears, 9- worm screws, 10- handwheels, 11- castors, 12- alignment pins, 13- switchover frames, 14- bracket bases, 15- rotate vertically
Axle, 16- bearings, 17- axle sleeves
Embodiment
Specific embodiment：Certain satellite overall dimensions 1000mm × 1000mm × 1000mm, interface is 4 uniform M8 screw threads
Hole, nominal diameter 400mm, barycenter is product geometric center.Design frock is required according to product pose adjustment：Base is using square
Steel-pipe welding structure, steel pipe specification be 50mm × 32mm × 2mm, after welding monnolithic case size be 2000mm × 1500mm ×
Castor is installed in 32mm, bottom corner location threaded connection.Top both sides pass through 8 M10 mode connects for screw substrate holders, substrate holder
For triangular frame structure, it is molded using with base same size square steel pipe welded, height 1200mm, both sides are symmetrically installed axle
Connection feathering axis in bearing, Selection of Bearings angular contact ball bearing 7208AC, bearing, feathering axis is using diameter 40
40Cr steel, with bracket using 4 M8 mode connects for screw, wherein side feathering axis is connected with worm and gear, and worm screw uses 40Cr
Steel material, worm gear uses tin bronze, speed reducing ratio 1：9, worm screw is connected with handwheel；Two brackets are arranged on the inside of substrate holder, are used
Triangular frame structure, is molded, height 800mm, downside passes through 8 M8 screws using with base same size square steel pipe welded
Connecting bracket base；Bracket base uses aluminium alloy overall structure, appearance and size 1500mm × 600mm × 80mm, on the upside of it
Symmetrical center positions, which are provided with diameter 100mm axis holes, axis hole, is provided with axle sleeve, and 90 are pressed in bracket base circle diameter 400mm positions
Degree is interval with diameter 10mm dowel holes；Axle sleeve uses 45 steel, and external diameter 100mm, internal diameter 80mm are symmetrically installed by two
Angular contact ball bearing 7208AC bearings are connected with vertical rotary shaft；Vertical rotary shaft uses 40Cr forged steel, and hierarchic structure, downside is straight
Footpath 40mm, is connected with bearing, upside diameter 500mm, passes through 6 M8 mode connects for screw switchover frames；Switchover frame is two side flangings up and down
Barrel shaped structure, using aluminium alloy, upside diameter 400mm is provided with screw thread via, be connected using 4 M8 with satellite, downside and erects
Direct rotary rotating shaft is connected, and flange position is by 90 degree of interval setting diameter 10mm dowel holes, its position and pin-and-hole position on bracket base
Put corresponding；Alignment pin use 45 steel, diameter 10mm, through switchover frame on dowel hole be inserted into bracket base dowel hole
In.
Frock is fixed by 4 M8 screws in use, satellite is placed on frock interface frame, mating frame.When adjusting rotation attitude,
Interface frame, mating frame is directly rotated, product rotates with interface frame, mating frame, when being rotated by 90 °, and penetrating alignment pin makes product orientation；Adjust flipping gesture
When, handwheel is rotated, drives bracket and product to overturn by worm and gear, it is any in switching process using worm and gear auto-lock function
Position is locked.
Claims (1)
1. a kind of attitude of satellite adjusts frock, it is characterised in that including base, substrate holder, bearing block, bearing, horizontal rotation
Axle one, bracket, feathering axis two, worm gear, worm screw, handwheel, castor, alignment pin, switchover frame, bracket base, vertical rotary shaft,
Bearing and axle sleeve；Base is rectangle, using square steel pipe welded structure, and inside is strengthened with square steel pipe welded, bottom corner
Castor is installed in position threaded connection, and the side position of top two is threadedly coupled each 1 of substrate holder by welding steel；Substrate holder is
Triangular frame structure, is molded using square steel pipe welded, and the upside of side substrate holder passes through welding steel thread cnnecting shaft
Connection feathering axis one in bearing, bearing is installed, the upside of opposite side substrate holder passes through welding steel in bearing, bearing block
It is threadedly coupled in bearing block, bearing block and bearing is installed, connection feathering axis two in bearing, the lateral ends of feathering axis two leads to
Cross flat key to be connected with worm and gear, worm screw is connected with handwheel by nut；Feathering axis one, feathering axis two are the bottom of parallel to
Connecting bracket is distinguished in seat, inner side by screw thread respectively, and bracket uses triangular frame structure, square steel pipe welded shaping, bracket
Downside is threadedly coupled bracket base by welding steel；Bracket base is symmetrical on the upside of it using the overall square structure of aluminium alloy
Center is provided with axis hole, and axis hole mounting sleeve in bracket base, axis hole, bracket base circumferential position is spaced by 90 degree
Provided with dowel hole；Axle sleeve uses the tubular structure with flange, and the outer side flanging of axle sleeve is connected through a screw thread with bracket base, interior
Footpath is connected by bearing with vertical rotary shaft；Vertical rotary shaft is connected on the upside of bracket base, vertical rotary shaft by screw thread
Connect switchover frame；Switchover frame is the tubular construction of two side flangings up and down, and flange is provided with screw thread via, using via and the passing of satelline
Threaded connection, or be connected by upper side flanging with passing of satelline band form, downside is connected by screw thread with vertical rotary shaft, is turned over
Side position is interval with dowel hole by 90 degree, and its position is corresponding with pin-and-hole position on bracket base；Alignment pin passes through switching
Dowel hole is inserted into bracket base dowel hole on frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710384568.1A CN107053103A (en) | 2017-05-26 | 2017-05-26 | A kind of attitude of satellite adjusts frock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710384568.1A CN107053103A (en) | 2017-05-26 | 2017-05-26 | A kind of attitude of satellite adjusts frock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107053103A true CN107053103A (en) | 2017-08-18 |
Family
ID=59610533
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710384568.1A Pending CN107053103A (en) | 2017-05-26 | 2017-05-26 | A kind of attitude of satellite adjusts frock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107053103A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107639419A (en) * | 2017-11-19 | 2018-01-30 | 黄石市华天自动化设备有限公司 | Automatic carriage pipeline automobile instrument panel suspender |
| CN108020566A (en) * | 2017-11-30 | 2018-05-11 | 中国航发航空科技股份有限公司 | A kind of auxiliary mould equipment for casing welding quality ray detection |
| CN108044573A (en) * | 2017-12-29 | 2018-05-18 | 中国航发中传机械有限公司 | For the mounting plate of bevel gear box |
| CN108662380A (en) * | 2018-04-24 | 2018-10-16 | 南京淳泰控制设备有限公司 | A kind of pedestal fixed structure of moment gyro |
| CN108856629A (en) * | 2018-07-26 | 2018-11-23 | 四川广旺能源发展（集团）有限责任公司机械制造分公司 | A kind of tramcar chassis riveting rotary tooling |
| CN109605299A (en) * | 2019-01-21 | 2019-04-12 | 北京卫星环境工程研究所 | Three Degree Of Freedom posture adjustment platform for the assembly of spacecraft large scale bay section |
| CN109822477A (en) * | 2019-02-28 | 2019-05-31 | 中航华东光电有限公司 | Multiple degrees of freedom rotary clamp |
| CN112555643A (en) * | 2020-12-17 | 2021-03-26 | 中国航空工业集团公司北京航空精密机械研究所 | Satellite posture adjusting device |
| CN115072342A (en) * | 2022-06-16 | 2022-09-20 | 北京遥感设备研究所 | General frock is transported in calibration of optics seeker |
| CN116765776A (en) * | 2023-06-30 | 2023-09-19 | 北京新风航天装备有限公司 | Device and method for entering cabin of transverse and vertical mixed equipment |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0074517A2 (en) * | 1981-09-15 | 1983-03-23 | Wilhelm Severt | Work fixture and handling device |
| JPS60184491A (en) * | 1984-03-02 | 1985-09-19 | ヴイルヘルム・ゼ−ヴエルト | Multispindle type rotary machine functioning as positioning in combination |
| CN102589804A (en) * | 2011-11-15 | 2012-07-18 | 上海卫星工程研究所 | Satellite attitude transformation device for testing quality characteristics of satellite |
| CN202667996U (en) * | 2012-06-05 | 2013-01-16 | 沙洲职业工学院 | Welding table |
| TW201338905A (en) * | 2012-03-21 | 2013-10-01 | China Steel Machinery Corp | Workpiece overturning device for welding assistance |
| CN205148264U (en) * | 2015-08-17 | 2016-04-13 | 上海航天精密机械研究所 | A rotatory device that shifts of two freedoms for spherical conduit head |
| CN206899183U (en) * | 2017-05-26 | 2018-01-19 | 北京航天新风机械设备有限责任公司 | A kind of attitude of satellite adjusts frock |
-
2017
- 2017-05-26 CN CN201710384568.1A patent/CN107053103A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0074517A2 (en) * | 1981-09-15 | 1983-03-23 | Wilhelm Severt | Work fixture and handling device |
| JPS60184491A (en) * | 1984-03-02 | 1985-09-19 | ヴイルヘルム・ゼ−ヴエルト | Multispindle type rotary machine functioning as positioning in combination |
| CN102589804A (en) * | 2011-11-15 | 2012-07-18 | 上海卫星工程研究所 | Satellite attitude transformation device for testing quality characteristics of satellite |
| TW201338905A (en) * | 2012-03-21 | 2013-10-01 | China Steel Machinery Corp | Workpiece overturning device for welding assistance |
| CN202667996U (en) * | 2012-06-05 | 2013-01-16 | 沙洲职业工学院 | Welding table |
| CN205148264U (en) * | 2015-08-17 | 2016-04-13 | 上海航天精密机械研究所 | A rotatory device that shifts of two freedoms for spherical conduit head |
| CN206899183U (en) * | 2017-05-26 | 2018-01-19 | 北京航天新风机械设备有限责任公司 | A kind of attitude of satellite adjusts frock |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107639419A (en) * | 2017-11-19 | 2018-01-30 | 黄石市华天自动化设备有限公司 | Automatic carriage pipeline automobile instrument panel suspender |
| CN107639419B (en) * | 2017-11-19 | 2023-08-22 | 湖北天华智能装备股份有限公司 | Automobile instrument panel lifting appliance for self-propelled trolley conveying line |
| CN108020566A (en) * | 2017-11-30 | 2018-05-11 | 中国航发航空科技股份有限公司 | A kind of auxiliary mould equipment for casing welding quality ray detection |
| CN108044573A (en) * | 2017-12-29 | 2018-05-18 | 中国航发中传机械有限公司 | For the mounting plate of bevel gear box |
| CN108662380A (en) * | 2018-04-24 | 2018-10-16 | 南京淳泰控制设备有限公司 | A kind of pedestal fixed structure of moment gyro |
| CN108856629A (en) * | 2018-07-26 | 2018-11-23 | 四川广旺能源发展（集团）有限责任公司机械制造分公司 | A kind of tramcar chassis riveting rotary tooling |
| CN109605299A (en) * | 2019-01-21 | 2019-04-12 | 北京卫星环境工程研究所 | Three Degree Of Freedom posture adjustment platform for the assembly of spacecraft large scale bay section |
| CN109822477A (en) * | 2019-02-28 | 2019-05-31 | 中航华东光电有限公司 | Multiple degrees of freedom rotary clamp |
| CN109822477B (en) * | 2019-02-28 | 2024-03-19 | 中航华东光电有限公司 | Multi-freedom-degree rotating clamp |
| CN112555643A (en) * | 2020-12-17 | 2021-03-26 | 中国航空工业集团公司北京航空精密机械研究所 | Satellite posture adjusting device |
| CN115072342A (en) * | 2022-06-16 | 2022-09-20 | 北京遥感设备研究所 | General frock is transported in calibration of optics seeker |
| CN116765776A (en) * | 2023-06-30 | 2023-09-19 | 北京新风航天装备有限公司 | Device and method for entering cabin of transverse and vertical mixed equipment |
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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 | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170818 |
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| WD01 | Invention patent application deemed withdrawn after publication |