JPH0480800U - - Google Patents

Info

Publication number
JPH0480800U
JPH0480800U JP12275290U JP12275290U JPH0480800U JP H0480800 U JPH0480800 U JP H0480800U JP 12275290 U JP12275290 U JP 12275290U JP 12275290 U JP12275290 U JP 12275290U JP H0480800 U JPH0480800 U JP H0480800U
Authority
JP
Japan
Prior art keywords
space equipment
mounting surface
space
base plate
tightening
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.)
Granted
Application number
JP12275290U
Other languages
Japanese (ja)
Other versions
JP2503678Y2 (en
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 filed Critical
Priority to JP1990122752U priority Critical patent/JP2503678Y2/en
Publication of JPH0480800U publication Critical patent/JPH0480800U/ja
Application granted granted Critical
Publication of JP2503678Y2 publication Critical patent/JP2503678Y2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

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  • Connection Of Plates (AREA)

Description

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本考案の一実施例の縦断面図、第2図
は他の実施例を示す縦断面図である。 図中、1は宇宙機器、2はベースプレート、3
は締付ねじ、4は雄ねじ部、7は宇宙ステーシヨ
ン、8は宇宙機器取付表面、10はナツト部材、
14はスプリング、17はナツト部材、18は締
付ねじ、19は外側部材、20は締付部、21は
先端部、23はスプリングを示す。
FIG. 1 is a longitudinal cross-sectional view of one embodiment of the present invention, and FIG. 2 is a longitudinal cross-sectional view showing another embodiment. In the figure, 1 is space equipment, 2 is base plate, 3 is
is a tightening screw, 4 is a male threaded part, 7 is a space station, 8 is a space equipment mounting surface, 10 is a nut member,
14 is a spring, 17 is a nut member, 18 is a tightening screw, 19 is an outer member, 20 is a tightening part, 21 is a tip, and 23 is a spring.

Claims (1)

【実用新案登録請求の範囲】 1 宇宙ステーシヨンの宇宙機器取付表面の内方
に配設された複数のナツト部材と、該ナツト部材
を前記宇宙機器取付表面に向けて付勢するスプリ
ングと、宇宙機器を備え前記宇宙機器取付表面に
当接するベースプレートに取付けられ前記ナツト
部材に螺合する複数の締付ねじとを備えたことを
特徴とする宇宙機器締付機構の着脱装置。 2 宇宙ステーシヨンの宇宙機器取付表面に配設
された複数のナツト部材と、宇宙機器を備え前記
宇宙機器取付表面に当接するベースプレート及び
該ベースプレートに間隔を隔てて設けた外側部材
を貫通し、該外側部材の外方に締付部を有すると
共に前記ベースプレートを貫通する先端部に前記
ナツト部材に螺合する雄ねじ部を有した複数の締
付ねじと、該締付ねじを前記先端部方向に向けて
付勢するスプリングとを備えたことを特徴とする
宇宙機器締付機構の着脱装置。
[Claims for Utility Model Registration] 1. A plurality of nut members disposed inside a space equipment mounting surface of a space station, a spring that biases the nut members toward the space equipment mounting surface, and a space equipment. An attachment/detachment device for a space equipment tightening mechanism, comprising: a plurality of tightening screws that are attached to a base plate that abuts the space equipment mounting surface and are threadedly engaged with the nut member. 2. A plurality of nut members disposed on the space equipment mounting surface of the space station, a base plate that is equipped with space equipment and comes into contact with the space equipment mounting surface, and an outer member provided at intervals on the base plate, and A plurality of tightening screws each having a tightening portion on the outside of the member and having a male threaded portion at a tip portion that penetrates the base plate and is screwed into the nut member, and the tightening screws are directed toward the tip portion. An attachment/detachment device for a space equipment tightening mechanism, characterized by comprising a biasing spring.
JP1990122752U 1990-11-22 1990-11-22 Detaching device for space equipment tightening mechanism Expired - Fee Related JP2503678Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1990122752U JP2503678Y2 (en) 1990-11-22 1990-11-22 Detaching device for space equipment tightening mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1990122752U JP2503678Y2 (en) 1990-11-22 1990-11-22 Detaching device for space equipment tightening mechanism

Publications (2)

Publication Number Publication Date
JPH0480800U true JPH0480800U (en) 1992-07-14
JP2503678Y2 JP2503678Y2 (en) 1996-07-03

Family

ID=31870506

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1990122752U Expired - Fee Related JP2503678Y2 (en) 1990-11-22 1990-11-22 Detaching device for space equipment tightening mechanism

Country Status (1)

Country Link
JP (1) JP2503678Y2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102803858B1 (en) * 2022-12-07 2025-05-08 한국항공우주연구원 Modular electronics connecting assembly for replacing electronics in client satellites

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63179295A (en) * 1987-01-20 1988-07-23 富士電機株式会社 Remote control type bolt screwing device
JPH01164038U (en) * 1988-05-07 1989-11-15
JPH01314699A (en) * 1988-06-16 1989-12-19 Ishikawajima Harima Heavy Ind Co Ltd Space equipment attachment/detachment device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63179295A (en) * 1987-01-20 1988-07-23 富士電機株式会社 Remote control type bolt screwing device
JPH01164038U (en) * 1988-05-07 1989-11-15
JPH01314699A (en) * 1988-06-16 1989-12-19 Ishikawajima Harima Heavy Ind Co Ltd Space equipment attachment/detachment device

Also Published As

Publication number Publication date
JP2503678Y2 (en) 1996-07-03

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