JPS6370213U - - Google Patents

Info

Publication number
JPS6370213U
JPS6370213U JP16383686U JP16383686U JPS6370213U JP S6370213 U JPS6370213 U JP S6370213U JP 16383686 U JP16383686 U JP 16383686U JP 16383686 U JP16383686 U JP 16383686U JP S6370213 U JPS6370213 U JP S6370213U
Authority
JP
Japan
Prior art keywords
frame
spacecraft
rollers
suspended
support plate
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
JP16383686U
Other languages
Japanese (ja)
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 JP16383686U priority Critical patent/JPS6370213U/ja
Publication of JPS6370213U publication Critical patent/JPS6370213U/ja
Pending legal-status Critical Current

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  • Electric Cable Installation (AREA)

Description

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

第1図は宙乗機の斜面図、第2図は使用状態の
正面図、第3図は使用状態の側面図、第4図は使
用状態の背面図、第5図は背もたれベルト6の取
付け部の平面図、第6図は従来例の正面図である
。 2……主フレーム、3……補助フレーム、4…
…腰掛け部、5……ブレーキ装置。
Figure 1 is a slope view of the spacecraft, Figure 2 is a front view in use, Figure 3 is a side view in use, Figure 4 is a rear view in use, and Figure 5 is the installation of the backrest belt 6. FIG. 6 is a front view of a conventional example. 2...Main frame, 3...Auxiliary frame, 4...
... Seat part, 5... Brake device.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 送電線9に懸架して使用され、送電線9上を転
動するローラ24を具えたフレーム上に作業者8
が座る腰掛け部4を配備した宙乗機に於て、フレ
ーム1はローラ24を具える主フレーム2と該主
フレーム2の下部中央に補助フレーム3を吊して
構成され、補助フレーム3の下部に形成した横向
き支持板33上に宙乗機の走行方向と平行な面内
でシーソー式に揺動可能に腰掛け部4が取り付け
られている宙乗機。
A worker 8 is placed on a frame that is suspended from the power transmission line 9 and is equipped with rollers 24 that roll on the power transmission line 9.
The frame 1 is composed of a main frame 2 equipped with rollers 24 and an auxiliary frame 3 suspended from the center of the lower part of the main frame 2. A spacecraft in which a seat part 4 is attached to a horizontal support plate 33 formed on a horizontal support plate 33 so as to be swingable in a seesaw manner in a plane parallel to the running direction of the spacecraft.
JP16383686U 1986-10-25 1986-10-25 Pending JPS6370213U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16383686U JPS6370213U (en) 1986-10-25 1986-10-25

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16383686U JPS6370213U (en) 1986-10-25 1986-10-25

Publications (1)

Publication Number Publication Date
JPS6370213U true JPS6370213U (en) 1988-05-11

Family

ID=31092404

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16383686U Pending JPS6370213U (en) 1986-10-25 1986-10-25

Country Status (1)

Country Link
JP (1) JPS6370213U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH059113U (en) * 1991-07-09 1993-02-05 藤井電工株式会社 Tight line air carrier

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6158812B2 (en) * 1980-03-20 1986-12-13 Marwitz & Hausner

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6158812B2 (en) * 1980-03-20 1986-12-13 Marwitz & Hausner

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH059113U (en) * 1991-07-09 1993-02-05 藤井電工株式会社 Tight line air carrier

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