CN106744068A - The rope storage of spacecraft and release device - Google Patents
The rope storage of spacecraft and release device Download PDFInfo
- Publication number
- CN106744068A CN106744068A CN201611025086.9A CN201611025086A CN106744068A CN 106744068 A CN106744068 A CN 106744068A CN 201611025086 A CN201611025086 A CN 201611025086A CN 106744068 A CN106744068 A CN 106744068A
- Authority
- CN
- China
- Prior art keywords
- reel
- rope
- main shaft
- protective cover
- coiling main
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
- B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
- B65H75/34—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables
- B65H75/38—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables involving the use of a core or former internal to, and supporting, a stored package of material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
- B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
- B65H75/34—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables
- B65H75/38—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables involving the use of a core or former internal to, and supporting, a stored package of material
- B65H75/44—Constructional details
- B65H75/4457—Arrangements of the frame or housing
- B65H75/4471—Housing enclosing the reel
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2701/00—Handled material; Storage means
- B65H2701/30—Handled filamentary material
- B65H2701/35—Ropes, lines
Abstract
The invention provides a kind of for the rope storage of spacecraft and release device; including coiling main shaft, housing screw, reel protective cover, reel capping and spring bearing, the reel protective cover is connected with reel capping and forms a reel close to closing；The quantity of the spring bearing is two, using deep groove ball bearing, is separately mounted to the center of reel protective cover and reel capping, is that coiling main shaft is provided a supporting role；Equipped with the housing screw for rope end to be fixed on the coiling main shaft, rope realizes that it is tightened up or discharges by turning on spring bearing.The present invention solve executing agency on the spacecraft of part need rope carry out tensioning release start function, simultaneously the device also have light weight, structure composition simple, small volume and it is compatible good the features such as, the safety and reliability that rope draws release in is effectively guaranteed, is had broad application prospects.
Description
Technical field
The present invention relates to a kind of rope executing agency, in particular it relates to a kind of rope storage and release for spacecraft
Device.
Background technology
With the development of spacecraft technology, the movable part used on spacecraft is increasingly extensive, it is desirable to use flexible rope
Also produced therewith as the requirement of executing agency：
1) rope is used as executive component, realizes the correlation functions such as mechanism's driving；
2) line frequency is adjusted and flexible accessory launches etc. is entered using flexible rope.
Release and gathering of the technical problem above to rope on spacecraft propose the requirement of dependable with function.
The content of the invention
In order to solve the above technical problems, from product applicability, rope flexibility characteristics, product weight and connecting occupation mode
Angularly consider, the invention provides a kind of rope storage of spacecraft and release device.
The purpose of the present invention is achieved through the following technical solutions：
It is a kind of to be protected for the rope storage of spacecraft and release device, including coiling main shaft, housing screw, reel
Cover, reel capping and spring bearing, the capping of the reel protective cover and reel be connected formed one it is close close around
Spool；The quantity of the spring bearing is two, using deep groove ball bearing, is separately mounted to reel protective cover and reel envelope
The center of lid, is that coiling main shaft is provided a supporting role；Equipped with the pressure for rope end to be fixed on the coiling main shaft
Tight screw, rope realizes that it is tightened up or discharges by turning on spring bearing.
Preferably, the outer rim of the coiling main shaft 1 is the outer stupefied side of two for stretching out, two outer stupefied sides and reel protective cover
3 form an approximate closing space, used as the region that rope stores.
Preferably, the outer rim central region of the coiling main shaft 1 is provided with unthreaded hole and screwed hole, and rope end penetrates unthreaded hole,
Housing screw 2 is compressed by the screw hole orthogonal with unthreaded hole and by rope end, plays fixed effect.
Preferably, the outer rim of coiling main shaft 1 is the cylindrical section and reel protective cover endoporus on the outer stupefied side of two for stretching out
Shell of column small―gap suture hole axle coordinates, and can not only ensure that coiling main shaft was freely rotated but also can ensure that rope reliably stores, Bu Huicong
The gap abjection that both coordinate.
Preferably, two deep groove ball bearings are pacified by way of repair reel protective cover 3 and reel cover 4
Dress, it is ensured that bearing has certain axial pretightening, it is ensured that coiling main shaft axial restraint, will not random play, it is ensured that rope discharge with
The reliability of gathering.
Preferably, the reel protective cover designs eel-like figure shape wire hole in outer rim so that rope lay out from reel and
Draw in move and will not produce friction
The present invention is reliably drawn in and discharge in ground foundation realizing space product rope, alleviates product weight, raising
The scope of application of product, so as to improve the reliability of product, reaches the effect for improving spacecraft performance.
Compared with prior art, the present invention has following beneficial effect：Simple structure, rope fixes reliability, work
It is reliable, at the same the device also have light weight, small volume and it is compatible good the features such as, be effectively guaranteed rope on spacecraft
The reliability of start, has broad application prospects.
Brief description of the drawings
The detailed description made to non-limiting example with reference to the following drawings by reading, further feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is rope storage and the release device structural representation that the embodiment of the present invention is used for spacecraft.
Fig. 2 is rope storage and the profile of release device that the embodiment of the present invention is used for spacecraft.
Fig. 3 is rope storage and the appearance schematic diagram of release device that the embodiment of the present invention is used for spacecraft.
In figure：1- coiling main shafts；2- housing screws；3- reel protective covers；4- reels are covered；5- spring bearings.
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 to the ordinary skill of this area
For personnel, without departing from the inventive concept of the premise, various modifications and improvements can be made.These belong to the present invention
Protection domain.
Refering to Fig. 1-Fig. 3, the embodiment of the invention provides a kind of rope for spacecraft and receive and release device, including
Coiling main shaft 1, housing screw 2, reel protective cover 3, reel cover 4 and spring bearing 5, the reel protective cover 3 with
The connection of reel capping 4 forms a reel close to closing；The quantity of the spring bearing 5 is two, using deep-groove ball
Bearing, is separately mounted to the center of reel protective cover 3 and reel capping 4, is that coiling main shaft is provided a supporting role；Institute
State equipped with the housing screw 2 for rope end to be fixed on coiling main shaft 1, rope realizes that it is received by turning on spring bearing 5
Tight or release.
The outer rim of the coiling main shaft 1 is the outer stupefied side of two for stretching out, and two outer stupefied sides form one with reel protective cover 3
Individual approximate closing space, as the region that rope stores.
The outer rim central region of the coiling main shaft 1 is provided with unthreaded hole and screwed hole, and rope end penetrates unthreaded hole, housing screw
2 are compressed by the screw hole orthogonal with unthreaded hole and by rope end, play fixed effect, and the diameter of unthreaded hole is according to using
The diameter of rope determines, can be designed by rope diameter+0.5mm.
The outer rim of coiling main shaft 1 be stretch out two outer stupefied sides cylindrical section and reel protective cover endoporus shell of column it is small between
Lyriform pore axle coordinates, and can not only ensure that coiling main shaft was freely rotated but also can ensure that rope reliably stores, and will not coordinate from both
Gap abjection；The unilateral gap for coordinating is 0.1mm, it is ensured that use the rope of 0.2mm~1.6mm diameters.
Two deep groove ball bearings are installed by way of repair reel protective cover 3 and reel cover 4, it is ensured that axle
Hold certain axial pretightening, it is ensured that coiling main shaft axial restraint, axial pre tightening force is determined by moment of friction, is tightly rubbed in advance
Torque is that can be identified as reliably Pre strained state to three times equivalent to the twice of free state.
The reel protective cover 3 designs eel-like figure shape wire hole in outer rim so that rope lays out from reel and draws dynamic in
Friction will not be produced；The width of wire hole can be designed by rope diameter+0.5mm, and the circumferential angle for hole occur can be according to rope
Maximum outlet angle two ends respectively increase by 5 ° and are designed in the course of the work.
At present, the force measuring device has been applied to certain spaceborne Zeng Pin mechanism, and its function meets use requirement, reaches
To design objective.
Specific embodiment of the invention is described above.It is to be appreciated that the invention is not limited in above-mentioned
Particular implementation, those skilled in the art can within the scope of the claims make various deformations or amendments, this not shadow
Sound substance of the invention.
Claims (6)
1. a kind of rope storage and release device for spacecraft, it is characterised in that including coiling main shaft, housing screw, around
Spool protective cover, reel capping and spring bearing, the reel protective cover are connected formation one and approach with reel capping
The reel of closing；The quantity of the spring bearing be two, using deep groove ball bearing, be separately mounted to reel protective cover and
The center of reel capping, is that coiling main shaft is provided a supporting role；Being equipped with the coiling main shaft is used for rope end
Fixed housing screw, rope realizes that it is tightened up or discharges by turning on spring bearing.
2. the rope of spacecraft according to claim 1 is received and release device, it is characterised in that the coiling main shaft
Outer rim is the outer stupefied side of two for stretching out, and two outer stupefied sides form an approximate closing space with reel protective cover, used as rope
The region of storage.
3. the rope of spacecraft according to claim 1 is received and release device, it is characterised in that the coiling main shaft
Outer rim central region is provided with unthreaded hole and screwed hole, and rope end penetrates unthreaded hole, and housing screw is by the screwed hole orthogonal with unthreaded hole
It is spirally connected and compresses rope end.
4. the rope of spacecraft according to claim 2 is received and release device, it is characterised in that outside the coiling main shaft
Edge is that the cylindrical section on the outer stupefied side of two for stretching out coordinates with reel protective cover endoporus shell of column small―gap suture hole axle.
5. the rope of spacecraft according to claim 1 is received and release device, it is characterised in that two deep groove ball bearings
Installed by way of repair reel protective cover and reel are covered.
6. the rope of spacecraft according to claim 1 is received and release device, it is characterised in that the reel protection
Cover on outer rim design eel-like figure shape wire hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611025086.9A CN106744068A (en) | 2016-11-17 | 2016-11-17 | The rope storage of spacecraft and release device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611025086.9A CN106744068A (en) | 2016-11-17 | 2016-11-17 | The rope storage of spacecraft and release device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106744068A true CN106744068A (en) | 2017-05-31 |
Family
ID=58968108
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611025086.9A Pending CN106744068A (en) | 2016-11-17 | 2016-11-17 | The rope storage of spacecraft and release device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106744068A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108163644A (en) * | 2017-12-26 | 2018-06-15 | 大连函量科技发展有限公司 | A kind of ocean engineering anchor mooring cable stationary storage means |
| CN108415449A (en) * | 2018-05-21 | 2018-08-17 | 北京航空航天大学 | A kind of device applied to the expansion of Aerospace Satellite system tether, recycling and tension force |
| CN110758773A (en) * | 2019-11-21 | 2020-02-07 | 上海卫星工程研究所 | Spacecraft and spring pre-tightening high-rigidity locking device thereof |
| CN112518712A (en) * | 2020-10-29 | 2021-03-19 | 中国科学院深圳先进技术研究院 | Exoskeleton robot |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1726137A (en) * | 1926-11-17 | 1929-08-27 | Tomas Suarez Y Bernal | Reel for cables and wire |
| US3212729A (en) * | 1963-04-22 | 1965-10-19 | Gene M Putnam | Wire dispensing apparatus |
| US6517022B1 (en) * | 2001-06-01 | 2003-02-11 | Richard A. Bailey | Cable storage device |
| CN202765986U (en) * | 2012-08-09 | 2013-03-06 | 临泉县龙大复合不锈钢管有限责任公司 | Hose winding machine |
| CN203255809U (en) * | 2013-04-09 | 2013-10-30 | 泰州市强达不锈钢丝绳有限公司 | Steel wire rope collecting device |
| CN103991756A (en) * | 2014-06-05 | 2014-08-20 | 江苏五洲电磁线有限公司 | Cable take-up reel |
| CN203794372U (en) * | 2014-05-05 | 2014-08-27 | 福州庆佳金属制品有限公司 | Tube coiler |
| CN104003255A (en) * | 2014-06-05 | 2014-08-27 | 江苏五洲电磁线有限公司 | Take-up reel |
| US8882016B1 (en) * | 2012-06-11 | 2014-11-11 | Kimberly J. Melvin | Cable and cord winding and storage system |
| CN204624857U (en) * | 2015-05-07 | 2015-09-09 | 德阳旌特线缆有限公司 | A kind of improved type cable take-up |
| CN204643394U (en) * | 2015-04-30 | 2015-09-16 | 福州庆佳金属制品有限公司 | Tube coiling appts |
-
2016
- 2016-11-17 CN CN201611025086.9A patent/CN106744068A/en active Pending
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1726137A (en) * | 1926-11-17 | 1929-08-27 | Tomas Suarez Y Bernal | Reel for cables and wire |
| US3212729A (en) * | 1963-04-22 | 1965-10-19 | Gene M Putnam | Wire dispensing apparatus |
| US6517022B1 (en) * | 2001-06-01 | 2003-02-11 | Richard A. Bailey | Cable storage device |
| US8882016B1 (en) * | 2012-06-11 | 2014-11-11 | Kimberly J. Melvin | Cable and cord winding and storage system |
| CN202765986U (en) * | 2012-08-09 | 2013-03-06 | 临泉县龙大复合不锈钢管有限责任公司 | Hose winding machine |
| CN203255809U (en) * | 2013-04-09 | 2013-10-30 | 泰州市强达不锈钢丝绳有限公司 | Steel wire rope collecting device |
| CN203794372U (en) * | 2014-05-05 | 2014-08-27 | 福州庆佳金属制品有限公司 | Tube coiler |
| CN103991756A (en) * | 2014-06-05 | 2014-08-20 | 江苏五洲电磁线有限公司 | Cable take-up reel |
| CN104003255A (en) * | 2014-06-05 | 2014-08-27 | 江苏五洲电磁线有限公司 | Take-up reel |
| CN204643394U (en) * | 2015-04-30 | 2015-09-16 | 福州庆佳金属制品有限公司 | Tube coiling appts |
| CN204624857U (en) * | 2015-05-07 | 2015-09-09 | 德阳旌特线缆有限公司 | A kind of improved type cable take-up |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108163644A (en) * | 2017-12-26 | 2018-06-15 | 大连函量科技发展有限公司 | A kind of ocean engineering anchor mooring cable stationary storage means |
| CN108415449A (en) * | 2018-05-21 | 2018-08-17 | 北京航空航天大学 | A kind of device applied to the expansion of Aerospace Satellite system tether, recycling and tension force |
| CN110758773A (en) * | 2019-11-21 | 2020-02-07 | 上海卫星工程研究所 | Spacecraft and spring pre-tightening high-rigidity locking device thereof |
| CN110758773B (en) * | 2019-11-21 | 2021-07-30 | 上海卫星工程研究所 | Spacecraft and spring pre-tightening high-rigidity locking device thereof |
| CN112518712A (en) * | 2020-10-29 | 2021-03-19 | 中国科学院深圳先进技术研究院 | Exoskeleton robot |
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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 | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170531 |