JPS63104394U - - Google Patents

Info

Publication number
JPS63104394U
JPS63104394U JP19775086U JP19775086U JPS63104394U JP S63104394 U JPS63104394 U JP S63104394U JP 19775086 U JP19775086 U JP 19775086U JP 19775086 U JP19775086 U JP 19775086U JP S63104394 U JPS63104394 U JP S63104394U
Authority
JP
Japan
Prior art keywords
wire
ring portion
steady rest
aircraft
rest member
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
JP19775086U
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 JP19775086U priority Critical patent/JPS63104394U/ja
Publication of JPS63104394U publication Critical patent/JPS63104394U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Guides For Winding Or Rewinding, Or Guides For Filamentary Materials (AREA)

Description

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

第1,2図は本考案の一実施例としての航空機
用ワイヤ揺動防止装置を示すもので、第1図はそ
の全体の概要を示す立面図、第2図はその要部を
拡大して示す斜視図である。 1……巻き上げ機、2……機体、3,3′……
ワイヤ振れ止め部材、3a……リング部、3b…
…支持アーム、3c……出入口、4……ワイヤ、
5……減摩部材、A……荷物。
Figures 1 and 2 show an aircraft wire swing prevention device as an embodiment of the present invention. Figure 1 is an elevational view showing the overall outline of the device, and Figure 2 is an enlarged view of the main parts. FIG. 1...Hoisting machine, 2...Airframe, 3,3'...
Wire steady rest member, 3a...Ring part, 3b...
...Support arm, 3c...Entrance/exit, 4...Wire,
5... Anti-friction member, A... Baggage.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 航空機の機体に折りたたみ可能に枢着されたワ
イヤ振れ止め部材をそなえ、同ワイヤ振れ止め部
材が、ワイヤを挿通されるリング部と、同リング
部に一端を結合されるとともに他端を上記機体に
枢着された支持アームとで構成されて、上記リン
グ部に上記ワイヤの出入口が形成されていること
を特徴とする、航空機用ワイヤ揺動防止装置。
A wire steady rest member is foldably pivotally attached to the fuselage of an aircraft, and the wire steady rest member has a ring portion through which a wire is inserted, one end of which is connected to the ring portion, and the other end of the wire steady rest member is connected to the aircraft body. 1. A wire swing prevention device for an aircraft, comprising a support arm pivotally mounted, and an entrance/exit for the wire is formed in the ring portion.
JP19775086U 1986-12-23 1986-12-23 Pending JPS63104394U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19775086U JPS63104394U (en) 1986-12-23 1986-12-23

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19775086U JPS63104394U (en) 1986-12-23 1986-12-23

Publications (1)

Publication Number Publication Date
JPS63104394U true JPS63104394U (en) 1988-07-06

Family

ID=31157796

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19775086U Pending JPS63104394U (en) 1986-12-23 1986-12-23

Country Status (1)

Country Link
JP (1) JPS63104394U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009037872A1 (en) * 2007-09-18 2009-03-26 Aero Asahi Corporation Cable protection device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009037872A1 (en) * 2007-09-18 2009-03-26 Aero Asahi Corporation Cable protection device
JP2009073223A (en) * 2007-09-18 2009-04-09 Asahi Koyo Kk Cable protection device
JP4576413B2 (en) * 2007-09-18 2010-11-10 朝日航洋株式会社 Cable protector

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