CN101744429A - Method for placing object on spacecraft and space station - Google Patents

Method for placing object on spacecraft and space station Download PDF

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Publication number
CN101744429A
CN101744429A CN200810231125A CN200810231125A CN101744429A CN 101744429 A CN101744429 A CN 101744429A CN 200810231125 A CN200810231125 A CN 200810231125A CN 200810231125 A CN200810231125 A CN 200810231125A CN 101744429 A CN101744429 A CN 101744429A
Authority
CN
China
Prior art keywords
spacecraft
space station
cloth
coupling
self
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
Application number
CN200810231125A
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Chinese (zh)
Inventor
马遂根
袁长宝
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN200810231125A priority Critical patent/CN101744429A/en
Publication of CN101744429A publication Critical patent/CN101744429A/en
Pending legal-status Critical Current

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Abstract

The invention relates to a method for placing an object on a spacecraft and a space station. Self-coupling viscose cloth is adhered on the object to be placed and moved on the spacecraft and the space station and on the position for placing and moving the object, the object is adhered by the self-coupling viscose cloth when being placed so as to lead the object on the spacecraft and the space station not to float in weightlessness, and the self-coupling viscose cloth is pulled open under the tensile force when the object is moved. The invention adopts the technical scheme that the self-coupling viscose cloth is cloth which is woven and raised by fibers with different thicknesses and is provided with holes and hooks, the quantity of the holes is more than that of the hooks and the hooks slightly protrude out of the holes.

Description

Method for placing object on spacecraft and the space station
Technical field the present invention relates to method for placing object on a kind of spacecraft and the space station.
The object utilization group that present known spacecraft of background technology and space station need be moved and place pricks, the method for padlock is fixed object, prevents when weightlessness elegant.
Summary of the invention utilizes on existing spacecraft and the space station for solving that group pricks, padlock prevents object elegant defective when weightlessness, the invention provides method for placing object on a kind of spacecraft and the space station: go up from the coupling sticky cloth boning on the object that needs on spacecraft and the space station to put, moves and on the position of storing, mobile object, it is bonding when putting object from the coupling sticky cloth, do not make the object on spacecraft and the space station elegant when weightlessness; During mobile object, under pulling force, drawn back from the coupling sticky cloth.The technical solution adopted for the present invention to solve the technical problems is: from the coupling sticky cloth is to knit the cloth that deduction has hole and hook with the different fiber of thickness, and the quantity of hole is more than hook, and hook slightly protrudes from hole.
The invention has the beneficial effects as follows: the group that reduces object on spacecraft and the space station pricks, snap lock feature, conveniently moving.
The specific embodiment elaborates to the specific embodiment of the present invention below in conjunction with concrete condition.
Technical scheme requires: knit the cloth that deduction has hole and hook with the different fiber of thickness, the quantity of hole is more than hook, and hook slightly protrudes from hole.
The specific embodiment is as follows:
Knit deduction from the coupling sticky cloth by the different fiber of thickness, knit when carrying, wherein a part of fine fibre is knitted and is proposed cloth cover formation hole, and the fiber that another part is thicker is knitted and proposed cloth cover formation hook, and the quantity of hole is more than hook, and hook slightly protrudes from hole.
The present invention not only is used for the storing of the weightless object of spacecraft, also can be widely used in the bonding of industry articles for use such as industrial or agricultural, medical treatment, packing, life.

Claims (2)

1. method for placing object on spacecraft and the space station is characterized in that: need on the object of putting, moving on spacecraft and the space station and the position of storing, mobile object on bond on from the coupling sticky cloth.
2. on spacecraft according to claim 1 and the space station in the method for placing object from the coupling sticky cloth, it is characterized in that: knit on the sticky cloth and carried hole and hook.
CN200810231125A 2008-11-28 2008-11-28 Method for placing object on spacecraft and space station Pending CN101744429A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN200810231125A CN101744429A (en) 2008-11-28 2008-11-28 Method for placing object on spacecraft and space station

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN200810231125A CN101744429A (en) 2008-11-28 2008-11-28 Method for placing object on spacecraft and space station

Publications (1)

Publication Number Publication Date
CN101744429A true CN101744429A (en) 2010-06-23

Family

ID=42472501

Family Applications (1)

Application Number Title Priority Date Filing Date
CN200810231125A Pending CN101744429A (en) 2008-11-28 2008-11-28 Method for placing object on spacecraft and space station

Country Status (1)

Country Link
CN (1) CN101744429A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3009235A (en) * 1957-10-02 1961-11-21 Internat Velcro Company Separable fastening device
JPS4933745A (en) * 1972-07-31 1974-03-28
CN87102459A (en) * 1987-03-29 1988-10-12 刘义民 Personnel's walking and article move and placement technique under the weightless situation
US5231738A (en) * 1991-12-12 1993-08-03 Kuraray Co., Ltd. Mixed hook/loop separable fastener and process for its production
CN1141234A (en) * 1995-05-09 1997-01-29 Ykk株式会社 Molded surface fastener
CN1158714A (en) * 1995-12-22 1997-09-10 Ykk株式会社 Surface fastener

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3009235A (en) * 1957-10-02 1961-11-21 Internat Velcro Company Separable fastening device
JPS4933745A (en) * 1972-07-31 1974-03-28
CN87102459A (en) * 1987-03-29 1988-10-12 刘义民 Personnel's walking and article move and placement technique under the weightless situation
US5231738A (en) * 1991-12-12 1993-08-03 Kuraray Co., Ltd. Mixed hook/loop separable fastener and process for its production
CN1141234A (en) * 1995-05-09 1997-01-29 Ykk株式会社 Molded surface fastener
CN1158714A (en) * 1995-12-22 1997-09-10 Ykk株式会社 Surface fastener

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Legal Events

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20100623