CN103030061A - Circular ring lifting tool based on satellite bearing cylinder lifting - Google Patents
Circular ring lifting tool based on satellite bearing cylinder lifting Download PDFInfo
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- CN103030061A CN103030061A CN2012105952401A CN201210595240A CN103030061A CN 103030061 A CN103030061 A CN 103030061A CN 2012105952401 A CN2012105952401 A CN 2012105952401A CN 201210595240 A CN201210595240 A CN 201210595240A CN 103030061 A CN103030061 A CN 103030061A
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- lifting
- satellite
- annulus
- bearing cylinder
- circular ring
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Abstract
The invention discloses a circular ring lifting tool based on satellite bearing cylinder lifting. Different from a general support rod type lifting tool, a circular ring lifting tool is used between a lifting beam and a satellite. Before the lifting tool is used, a lifting beam component is connected with a circular ring component by a quick-release stop pin, and then the circular ring component is connected with a frame at the upper end of a bearing cylinder through a plurality of fasteners, so that the lifting of the whole satellite or a single compartment is achieved. The quick-release stop pin can simplify the assembly of the lifting tool, and the fasteners can reinforce the frame at the upper end of the bearing cylinder in a lifting process of the whole satellite or the single compartment, so that stresses of connection points are relatively uniform, and the difficulty for designing a lifting point on the frame at the upper end of the bearing cylinder is reduced.
Description
Technical field
The present invention relates to the lifting conveying device in the whole star of a kind of satellite or single cabin, particularly a kind of annulus suspender based on the lifting of the satellite bearing cylinder take loaded cylinder as the main force support structure configuration.
Background technology
The satellite suspender is that satellite is in important general assembly operate ground frock of AIT stage, be used for the lifting whole star of satellite or single cabin, making the whole star of satellite or single cabin realize vertical, parallel motion, for carrying out of the follow-up AIT work of satellite facilitates, is satellite requisite ground frock in development process.
Usually, the satellite suspender adopts beam type suspender or Jackstay type suspender according to satellite configuration and force-applied situation, takes advantage of the advantage of the method for hanging to be for these two kinds, and the suspender load-carrying capacity is better.But the defective in implementation process has: 1) structure relative complex is higher to matching requirements; 2) use a word beam that satellite is born in the lifting process because so that satellite revolves slowly in the lifting process, there is potential safety hazard in the moment of torsion that the suspension centre unbalance stress produces, also be unfavorable for the general assembly operation; 3) use a word beam that satellite suspension centre local strength is had relatively high expectations, may to the damage of satellite suspension centre, affect the satellite lifting.
Summary of the invention
The technical matters that the present invention solves is: provide that a kind of load-carrying capacity is good, stressed uniform suspender design in the lifting process, this design can realize the lifting of the whole star of satellite or cabin section by simple operations.
Technical scheme of the present invention is: a kind of annulus suspender based on the satellite bearing cylinder lifting comprises hanging beam assembly, annulus assembly, quick-release stop pin and shackle; The hanging beam assembly comprises suspension ring, link, upper end suspender belt, lower end suspender belt, cross flange, support beam, hinge and turnbuckle; Two hollow cylinder support beams are by cross flange quadrature captive joint, and the two ends of every support beam are connected with an end of upper end suspender belt by hinge respectively, and the other end of upper end suspender belt links to each other with circular suspension ring by circular link; The two ends of every support beam also link to each other with an end of turnbuckle by hinge respectively, and the other end of turnbuckle links to each other with an end of lower end suspender belt, and the other end of lower end suspender belt links to each other with the annulus assembly with shackle by the quick-release stop pin; The annulus assembly comprises the connection annulus, connects annulus inside and is carved with groove, uniform the screw that is used for assembling on the groove; The quick-release stop pin is connected with shackle and connects on the annulus.
The present invention's advantage compared with prior art is:
1) design of the annular arrangement of annulus suspender is little to the constraint of satellite design of lifting points, and annulus assembly and annulus suspender are reasonable in design, simple in structure, uses safety, reliable;
2) it is stressed evenly that the structure that connects annulus has guaranteed that satellite holds suspension centre, improves the safety in the satellite lifting process, in the lifting process satellite upper end frame played reinforcement effect simultaneously;
3) introducing of quick-release stop pin has reduced in the satellite suspender installation process to introduce the possibility of superfluity;
4) the annulus suspender is compared with the beam type suspender, in use, can realize separating of suspender and satellite by separating hanging beam assembly and annulus assembly, has reduced the interface operation between suspender and the satellite, and satellite upper end frame has been played protective effect.
Description of drawings
Fig. 1 is the structural representation of annulus suspender of the present invention.
The specific embodiment
As shown in Figure 1, according to weight, the lifting state of satellite, determine the setting of annulus unit construction point of connection, and evenly arrange that its effect is that each point of connection was stressed evenly when the annulus suspender was connected with loaded cylinder upper end frame.When the satellite suspender is installed, assemble first the hanging beam assembly, make hanging beam assembly lower end and annulus assembly junction substantially be in same plane, behind quick-release stop pin 10 connecting hanging beam assemblies and annulus assembly, the assembling of annulus suspender is finished.Lifting annulus suspender makes by bolt that suspension centre reliably is connected on annulus assembly and the satellite to satellite, unified tightening locks quick-release stop pin 10, check the annulus assembly be connected with satellite errorless after, lift by crane satellite, the lifting in the realization whole star of satellite or single cabin.Suspension ring 1 used in the present invention, link 2, upper end suspender belt 3, lower end suspender belt 8, quick-release stop pin 10, shackle 9, turnbuckle 7 are huge power group product, cross flange 4, hinge 6, connection annulus 11 all adopt the 20# Steel material, support beam 6 adopts solid drawn pipe, and the quick-release stop pin can adopt the 30CrMnSi material.
The content that is not described in detail in the specification sheets of the present invention belongs to those skilled in the art's known technology.
Claims (1)
1. the annulus suspender based on the satellite bearing cylinder lifting is characterized in that: comprise hanging beam assembly, annulus assembly, quick-release stop pin (10) and shackle (9); The hanging beam assembly comprises suspension ring (1), link (2), upper end suspender belt (3), lower end suspender belt (8), cross flange (4), support beam (5), hinge (6) and turnbuckle (7); Two hollow cylinder support beams (5) are by cross flange (4) quadrature captive joint, the two ends of every support beam (5) are connected with an end of upper end suspender belt (3) by hinge (6) respectively, and the other end of upper end suspender belt (3) links to each other with circular suspension ring (1) by circular link (2); The two ends of every support beam (5) also link to each other with an end of turnbuckle (7) by hinge (6) respectively, the other end of turnbuckle (7) links to each other with an end of lower end suspender belt (8), and the other end of lower end suspender belt (8) links to each other with the annulus assembly with shackle (9) by quick-release stop pin (10); The annulus assembly comprises and connects annulus (11), connects annulus (11) inside and is carved with groove, uniform the screw that is used for assembling on the groove; Quick-release stop pin (10) is connected 9 with shackle) be distributed on the connection annulus (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012105952401A CN103030061A (en) | 2012-12-28 | 2012-12-28 | Circular ring lifting tool based on satellite bearing cylinder lifting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012105952401A CN103030061A (en) | 2012-12-28 | 2012-12-28 | Circular ring lifting tool based on satellite bearing cylinder lifting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103030061A true CN103030061A (en) | 2013-04-10 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012105952401A Pending CN103030061A (en) | 2012-12-28 | 2012-12-28 | Circular ring lifting tool based on satellite bearing cylinder lifting |
Country Status (1)
| Country | Link |
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| CN (1) | CN103030061A (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103287965A (en) * | 2013-06-24 | 2013-09-11 | 保定天威保变电气股份有限公司 | Shunt reactor core column lifting method and special tool |
| CN103879882A (en) * | 2014-03-15 | 2014-06-25 | 奇瑞汽车股份有限公司 | Lifting appliance for lifting longitudinal beam wheel cover assemblies |
| CN103964295A (en) * | 2014-05-26 | 2014-08-06 | 北京卫星环境工程研究所 | Lever structure-based special-shaped spacecraft lifting device |
| CN104044994A (en) * | 2014-05-26 | 2014-09-17 | 北京航天发射技术研究所 | Assembly fixture |
| CN106044543A (en) * | 2016-03-30 | 2016-10-26 | 上海市建筑装饰工程集团有限公司 | Contactless lifting sling system for towering precious metal tower mast |
| CN107381322A (en) * | 2017-07-10 | 2017-11-24 | 北京航天发射技术研究所 | A kind of satellite fairing assembly hanging basket |
| CN107538391A (en) * | 2017-02-17 | 2018-01-05 | 北京卫星环境工程研究所 | Foldable arris rod mechanism and its soft shade of the satellite of composition |
| CN111634793A (en) * | 2020-04-26 | 2020-09-08 | 北京空间飞行器总体设计部 | Hoisting device and hoisting method for satellite |
| CN112591597A (en) * | 2020-12-17 | 2021-04-02 | 德阳九鼎电气有限公司 | Rotor base hoisting tool and using method |
| CN112875486A (en) * | 2021-01-12 | 2021-06-01 | 航天科工空间工程发展有限公司 | Satellite hoisting equipment |
| CN114955825A (en) * | 2021-02-19 | 2022-08-30 | 北京九天微星科技发展有限公司 | Satellite lifting appliance |
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| JPH08303642A (en) * | 1995-05-10 | 1996-11-22 | Masaru Masuda | Buried pipe hanging tool |
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| CN202414958U (en) * | 2012-01-05 | 2012-09-05 | 湖南南方搏云新材料有限责任公司 | Multifunctional lifting appliance |
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2012
- 2012-12-28 CN CN2012105952401A patent/CN103030061A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH08303642A (en) * | 1995-05-10 | 1996-11-22 | Masaru Masuda | Buried pipe hanging tool |
| US7252315B2 (en) * | 2003-05-02 | 2007-08-07 | Pugh Acquisition Co. | System and method for personnel transfer |
| EP1669316B1 (en) * | 2004-12-10 | 2010-01-27 | GM Global Technology Operations, Inc. | Transport device |
| CN201376833Y (en) * | 2009-02-24 | 2010-01-06 | 曹振邦 | Manned hanging basket |
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Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103287965A (en) * | 2013-06-24 | 2013-09-11 | 保定天威保变电气股份有限公司 | Shunt reactor core column lifting method and special tool |
| CN103879882A (en) * | 2014-03-15 | 2014-06-25 | 奇瑞汽车股份有限公司 | Lifting appliance for lifting longitudinal beam wheel cover assemblies |
| CN103879882B (en) * | 2014-03-15 | 2016-01-27 | 奇瑞汽车股份有限公司 | A kind of suspender for lifting longeron wheel cover assembly |
| CN104044994B (en) * | 2014-05-26 | 2017-01-04 | 北京航天发射技术研究所 | Assembly jig |
| CN103964295A (en) * | 2014-05-26 | 2014-08-06 | 北京卫星环境工程研究所 | Lever structure-based special-shaped spacecraft lifting device |
| CN104044994A (en) * | 2014-05-26 | 2014-09-17 | 北京航天发射技术研究所 | Assembly fixture |
| CN103964295B (en) * | 2014-05-26 | 2016-06-01 | 北京卫星环境工程研究所 | Based on the special-shaped spacecraft lifting appliance of lever construction |
| CN106044543A (en) * | 2016-03-30 | 2016-10-26 | 上海市建筑装饰工程集团有限公司 | Contactless lifting sling system for towering precious metal tower mast |
| CN107538391A (en) * | 2017-02-17 | 2018-01-05 | 北京卫星环境工程研究所 | Foldable arris rod mechanism and its soft shade of the satellite of composition |
| CN107381322A (en) * | 2017-07-10 | 2017-11-24 | 北京航天发射技术研究所 | A kind of satellite fairing assembly hanging basket |
| CN111634793A (en) * | 2020-04-26 | 2020-09-08 | 北京空间飞行器总体设计部 | Hoisting device and hoisting method for satellite |
| CN112591597A (en) * | 2020-12-17 | 2021-04-02 | 德阳九鼎电气有限公司 | Rotor base hoisting tool and using method |
| CN112875486A (en) * | 2021-01-12 | 2021-06-01 | 航天科工空间工程发展有限公司 | Satellite hoisting equipment |
| CN112875486B (en) * | 2021-01-12 | 2023-03-24 | 航天科工空间工程发展有限公司 | Satellite hoisting equipment |
| CN114955825A (en) * | 2021-02-19 | 2022-08-30 | 北京九天微星科技发展有限公司 | Satellite lifting appliance |
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Application publication date: 20130410 |