CN106392536A - Cabin loading method of large overall equipment cabinet of space station working cabin - Google Patents
Cabin loading method of large overall equipment cabinet of space station working cabin Download PDFInfo
- Publication number
- CN106392536A CN106392536A CN201610944966.XA CN201610944966A CN106392536A CN 106392536 A CN106392536 A CN 106392536A CN 201610944966 A CN201610944966 A CN 201610944966A CN 106392536 A CN106392536 A CN 106392536A
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- Prior art keywords
- rack
- space station
- cabin
- equipment cabinet
- work chamber
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Types And Forms Of Lifts (AREA)
Abstract
The invention discloses a cabin loading method of a large overall equipment cabinet of a space station working cabin. The cabin loading method includes the following steps that (1) the equipment cabinet is conveyed; (2) radial posture alignment of the equipment cabinet is carried out; (3) axial conveying of the equipment cabinet is carried out; (4) axial and radial posture alignment of the equipment cabinet is carried out; and (5) assembling of the equipment cabinet is completed. By means of the cabin loading method of the large overall equipment cabinet of the space station working cabin, the problems in intra-cabin conveying and intra-cabin installation of the large overall equipment cabinet of the certain-type space station working cabin can be effectively solved, and the functions of automatic detection, posture alignment, positioning and the like are achieved; and meanwhile, the installation reliability and safety of the equipment cabinet are guaranteed, and rapid and accurate intra-cabin assembling of the overall equipment cabinet is achieved.
Description
Technical field
The present invention relates to a kind of main equipment assembly method, a kind of especially large-scale integrating cabinet stowage of space station work chamber
Method.
Background technology
Space station be a kind of in LEO long-play, be available for spacefarer's life, work and ground spacefarer and seek
The manned spacecraft visited, represent current space industry the most comprehensively, the most complicated, most advanced and the most comprehensive scientific and technological level, in sky
Between life science, manned deep space explore and many Environment Science fields such as new material processing play important, other spacecrafts
Irreplaceable effect.The inside integrating cabinet of space station has the features such as large volume, large inertia, high accuracy, and is subject to domestic fire
Arrow load-carrying ability, narrow space in station module, causes that equipment installation difficulty is big, inefficiency.
For breaking through the technological difficulties of the internal integrating cabinet ground-mounted in space station, international space station associated specialist proposes machine
Tool arm enter cabin scheme realize large-scale integrating cabinet enter cabin assembling, the program employs to be held with multiple degrees of freedom, multi-functional end
Row device, its complex structure, equipment volume are huge.Because work chamber nacelle internal actual space available in domestic space station is more empty than international
Between stand much smaller, robot arm end effector wants execution complicated, and equipment mechanism can be excessively huge, uses beyond nacelle inside
Space；On the other hand, program infusion of financial resources is more, and utilization rate of equipment and installations is low.
Therefore, industry needs a kind of space station work chamber large-scale integrating cabinet stowage method, to efficiently solving
The internal integrating cabinet ground-mounted difficult problem in domestic space station.
Content of the invention
For the deficiencies in the prior art, the present invention provides a kind of space station work chamber large-scale integrating cabinet stowage method, can
To efficiently solve the internal integrating cabinet ground-mounted difficult problem in domestic space station.By controlling four steel wire ropes of four groups of winding plants
Length and axial location, make large-scale integrating cabinet carry out radial and axial posture adjustment relative to work chamber, and then realize the fast quick-mounting of rack
Join.
In order to reach foregoing invention purpose, by solving its technical problem, the present invention be employed technical scheme comprise that offer is a kind of
Space station work chamber large-scale integrating cabinet stowage method, comprises the steps：
Step 1), rack radially delivers；
Step 2), rack radial direction posture adjustment；
Step 3), rack axially conveys；
Step 4), rack axially with radial direction posture adjustment；
Step 5), rack assembles, and finally realizes integrating cabinet and quickly positions assembling.
Further, rack radially delivers using four groups of winding plant synchronization four steel wire ropes of drive control, makes four steel wires
Rope elevator equal length, and control rack radial direction vertical height, make rack center close to nacelle axis.
Further, when rack axially conveys, underslung trolley axially-movable adopts servomotor driving gear rack form, makes
Rack and hatch door axial location about 50mm.Rack radial direction posture adjustment adopts asynchronous four length of steel ropes of drive control of four groups of winding plants
Degree, adjustment rack with respect to work cabin door relative position it is ensured that rack external envelope and hatch door internal diameter minimum spacing be 15 ~
30mm.After completing rack radial direction posture adjustment, control underslung trolley to make rack pass through hatch door at a slow speed, and travel designated mounting axial direction position
Put.Four groups of winding plants of synchronous driving, control rack radial direction vertical height, make rack close to installation site；Asynchronous driving four again
Group winding plant, makes rack carry out radial direction posture adjustment, and installs rack.
Further, axially conveying adopts servomotor driving gear rack form to rack, realizes rack axial location and controls.
Described step 4) pass through axial direction electric machine driving gear rack drives underslung trolley and rack, pass through at a slow speed hatch door, machine
Cabinet, close to designated mounting position, carries out complex controll rack axial location and footpath by four groups of winding plants and axial servomotor
To attitude.
Further, described four groups of winding plants and axial direction electric machine adopt servomotor to drive.
Further, described four groups of winding plants and axial direction electric machine have multi gear speed-regulating function.
Further, described four groups of winding plants [4] have synchronous versus asynchronous control function.
The present invention can efficiently solve the internal integrating cabinet ground-mounted difficult problem in certain space station domestic, with existing assembling hand
Section is compared, and has the advantages that compact conformation, workable, good economy performance, realizes integrating cabinet ground quick assembling.
Brief description
Fig. 1 is work cabin door and the rack relative position structure chart of the embodiment of the present invention.
Specific embodiment
The present invention is further detailed explanation below in conjunction with the accompanying drawings.
Fig. 1 is work cabin door and the rack relative position structure chart of the embodiment of the present invention.In figure, 1 is hatch door border, 5
It is guide rail, 9 is intravehicular activity space；A kind of space station work chamber large-scale integrating cabinet stowage method, comprises the following steps
Step 1, rack radially delivers operation out of my cabin
Rack 2 passes through synchronous four groups of winding plants 4 of drive control, makes four steel wire ropes 3 elevator equal length it is ensured that rack 2 footpath
Steady to delivering, and control rack radial direction vertical height, make rack center close to nacelle axis.
Step 2, rack axial advancement operation out of my cabin
Underslung trolley axially-movable adopts servomotor driving gear rack form, and rack is followed underslung trolley and moved to hatch door 1
Axial location about 50mm.
Step 3, the rack operation of radial direction posture adjustment out of my cabin
Asynchronous four steel wire rope 3 length of drive control of four groups of winding plants 4, adjustment rack is with respect to work cabin door 1 position relatively
Put it is ensured that rack external envelope and hatch door 1 internal diameter minimum spacing are 15 ~ 30mm.
Step 4, axial advancement operation in rack cabin
Underslung trolley and rack are driven by the axial tooth bar 8 of axial direction electric machine 6 driving axial gear 7, passes through hatch door 1 at a slow speed, and
Reach designated mounting axial location.
Decline operation in step 5. rack cabin
By synchronous four groups of winding plants 4 of drive control, rack is made to drop to close to designated mounting position.
Radial direction posture adjustment operation in step 6. rack cabin
Asynchronous four steel wire rope 1 length of drive control of four groups of winding plants 4, adjustment rack attitude is to work chamber designated mounting position
Put.
Fixed work order in step 7. rack cabin
Rack is carried out fixing in cabin.
Step 8. underslung trolley goes out cabin operation
Four groups of winding plants 4 reclaim four steel wire ropes 3, and underslung trolley moves on to out of my cabin, carry out next group rack and install.
Every content without departing from technical solution of the present invention, is made to above example according to the technical spirit of the present invention
Any simple modification, equivalent variations and modification, belong to the protection domain of technical solution of the present invention.
Claims (8)
1. a kind of space station work chamber large-scale integrating cabinet stowage method is it is characterised in that comprise the steps：
Step 1), rack radially delivers；
Step 2), rack radial direction posture adjustment；
Step 3), rack axially conveys；
Step 4), rack axially with radial direction posture adjustment；
Step 5), rack assembles, and finally realizes integrating cabinet and quickly positions assembling.
2. a kind of space station according to claim 1 work chamber large-scale integrating cabinet stowage method is it is characterised in that rack
Radially deliver using four groups of winding plant [4] synchronization four steel wire ropes [3] of drive control, make four steel wire rope [3] elevator length
Equal it is ensured that rack motion state, and control rack radial direction vertical height.
3. a kind of space station according to claim 1 work chamber large-scale integrating cabinet stowage method is it is characterised in that rack
Radial direction posture adjustment adopts asynchronous four steel wire ropes [3] of drive control of four groups of winding plants [4], and adjustment rack is with respect to work cabin door
[1] relative position, makes rack external envelope and hatch door [1] internal diameter minimum spacing be 15 ~ 30mm.
4. a kind of space station according to claim 1 work chamber large-scale integrating cabinet stowage method is it is characterised in that rack
Axially conveying adopts servomotor driving gear rack form, realizes rack axial location and controls.
5. a kind of space station according to claim 1 work chamber large-scale integrating cabinet stowage method is it is characterised in that described
Step 4) pass through axial direction electric machine [6] driving gear rack drives underslung trolley and rack, pass through hatch door [1] at a slow speed, rack is close
Designated mounting position, carries out complex controll rack axial location and footpath by four groups of winding plants [4] and axial servomotor [6]
To attitude.
6. a kind of space station according to claim 5 work chamber large-scale integrating cabinet stowage method is it is characterised in that described
Four groups of winding plants [4] adopt servomotor to drive with axial direction electric machine [6].
7. a kind of space station according to claim 5 work chamber large-scale integrating cabinet stowage method is it is characterised in that described
Four groups of winding plants [4] have multi gear speed-regulating function with axial direction electric machine [6].
8. a kind of space station according to claim 7 work chamber large-scale integrating cabinet stowage method is it is characterised in that described
Four groups of winding plants [4] have synchronous versus asynchronous control function.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610944966.XA CN106392536A (en) | 2016-11-02 | 2016-11-02 | Cabin loading method of large overall equipment cabinet of space station working cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610944966.XA CN106392536A (en) | 2016-11-02 | 2016-11-02 | Cabin loading method of large overall equipment cabinet of space station working cabin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106392536A true CN106392536A (en) | 2017-02-15 |
Family
ID=58014160
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610944966.XA Pending CN106392536A (en) | 2016-11-02 | 2016-11-02 | Cabin loading method of large overall equipment cabinet of space station working cabin |
Country Status (1)
| Country | Link |
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| CN (1) | CN106392536A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109050873A (en) * | 2018-08-31 | 2018-12-21 | 上海宇航系统工程研究所 | A kind of aircraft section structure with large size opening |
| CN112676880A (en) * | 2020-12-17 | 2021-04-20 | 中航沈飞民用飞机有限责任公司 | Integrated process equipment suitable for automatically drilling and riveting multiple cabin doors |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19614366A1 (en) * | 1996-04-11 | 1997-11-20 | Martin Krusche | Tube bundle drawing apparatus for drawing heat exchanger tubes |
| CN101607674A (en) * | 2008-06-17 | 2009-12-23 | 卫华集团有限公司 | Dolly on the hoisting crane and the driving device between I-beam section |
| CN102764972A (en) * | 2012-07-18 | 2012-11-07 | 山东电力建设第二工程公司 | Method for penetrating inner stator to outer stator of split turbine generator |
| CN103511179A (en) * | 2012-06-21 | 2014-01-15 | 邓允河 | Wind wheel structure of vertical axis wind turbine and installation method thereof |
| CN104148931A (en) * | 2014-07-04 | 2014-11-19 | 上海拓璞数控科技有限公司 | Multipoint servo adjustment device for alignment of large barrel-section member and method thereof |
| CN105197206A (en) * | 2015-10-23 | 2015-12-30 | 极视成像科技（武汉）有限公司 | Rope-driven underwater detection robot |
| CN105775991A (en) * | 2016-05-16 | 2016-07-20 | 兰州兰石重型装备股份有限公司 | Large-diameter tube bundle hoisting assembly tooling and using method thereof |
| CN205465050U (en) * | 2016-03-04 | 2016-08-17 | 郑州纺机工程技术有限公司 | Be used for dresser warp beam device that falls on automatic |
-
2016
- 2016-11-02 CN CN201610944966.XA patent/CN106392536A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19614366A1 (en) * | 1996-04-11 | 1997-11-20 | Martin Krusche | Tube bundle drawing apparatus for drawing heat exchanger tubes |
| CN101607674A (en) * | 2008-06-17 | 2009-12-23 | 卫华集团有限公司 | Dolly on the hoisting crane and the driving device between I-beam section |
| CN103511179A (en) * | 2012-06-21 | 2014-01-15 | 邓允河 | Wind wheel structure of vertical axis wind turbine and installation method thereof |
| CN102764972A (en) * | 2012-07-18 | 2012-11-07 | 山东电力建设第二工程公司 | Method for penetrating inner stator to outer stator of split turbine generator |
| CN104148931A (en) * | 2014-07-04 | 2014-11-19 | 上海拓璞数控科技有限公司 | Multipoint servo adjustment device for alignment of large barrel-section member and method thereof |
| CN105197206A (en) * | 2015-10-23 | 2015-12-30 | 极视成像科技（武汉）有限公司 | Rope-driven underwater detection robot |
| CN205465050U (en) * | 2016-03-04 | 2016-08-17 | 郑州纺机工程技术有限公司 | Be used for dresser warp beam device that falls on automatic |
| CN105775991A (en) * | 2016-05-16 | 2016-07-20 | 兰州兰石重型装备股份有限公司 | Large-diameter tube bundle hoisting assembly tooling and using method thereof |
Non-Patent Citations (5)
| Title |
|---|
| 宋立博主编: "《运动控制系统原理、结构与设计》", 30 January 2009 * |
| 徐伟 主编: "《建筑工程施工》", 30 August 2013 * |
| 沈阳市机电工业局编辑: "《机电产品目录 第8册 大中小电机、控制驱动微电机、汽轮机、工业锅炉》", 28 February 1980 * |
| 秦顺全编著: "《海上长桥整孔箱梁预制架设技术》", 31 October 2006 * |
| 高钦和 编著: "《机电检测与控制》", 28 February 2015 * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109050873A (en) * | 2018-08-31 | 2018-12-21 | 上海宇航系统工程研究所 | A kind of aircraft section structure with large size opening |
| CN112676880A (en) * | 2020-12-17 | 2021-04-20 | 中航沈飞民用飞机有限责任公司 | Integrated process equipment suitable for automatically drilling and riveting multiple cabin doors |
| CN112676880B (en) * | 2020-12-17 | 2021-12-03 | 中航沈飞民用飞机有限责任公司 | Integrated process equipment suitable for automatically drilling and riveting multiple cabin doors |
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Application publication date: 20170215 |