JPH0254700U - - Google Patents

Info

Publication number
JPH0254700U
JPH0254700U JP13233888U JP13233888U JPH0254700U JP H0254700 U JPH0254700 U JP H0254700U JP 13233888 U JP13233888 U JP 13233888U JP 13233888 U JP13233888 U JP 13233888U JP H0254700 U JPH0254700 U JP H0254700U
Authority
JP
Japan
Prior art keywords
rotor blade
lifting device
rotary
hydraulic cylinder
frame
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
JP13233888U
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 JP13233888U priority Critical patent/JPH0254700U/ja
Publication of JPH0254700U publication Critical patent/JPH0254700U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Emergency Lowering Means (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に係る回転翼機の吊
り上げ装置の正面図、第2図はその要部詳細図、
第3図aは従来の回転翼機の吊り上げ装置の機構
説明図、同図bはその要部詳細図である。 1……ダミー用のロータブレード、2……バン
ジーコード、3……油圧シリンダー、4……油圧
ポンプ、5……架構、6……機体。
Fig. 1 is a front view of a lifting device for a rotary wing aircraft according to an embodiment of the present invention, Fig. 2 is a detailed view of its main parts,
FIG. 3a is a mechanical explanatory diagram of a conventional lifting device for a rotary-wing aircraft, and FIG. 3b is a detailed diagram of its main parts. 1... Dummy rotor blade, 2... Bungee cord, 3... Hydraulic cylinder, 4... Hydraulic pump, 5... Frame, 6... Airframe.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 機体にロータブレードの代わりに装着されるダ
ミー用のロータブレードと、該ロータブレードを
架構上に設けられた油圧シリンダーに結合するバ
ンジーコードとを備えてなることを特徴とする回
転翼機の吊り上げ装置。
A lifting device for a rotary-wing aircraft, comprising: a dummy rotor blade that is attached to the aircraft body in place of the rotor blade; and a bungee cord that connects the rotor blade to a hydraulic cylinder provided on a frame. .
JP13233888U 1988-10-12 1988-10-12 Pending JPH0254700U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13233888U JPH0254700U (en) 1988-10-12 1988-10-12

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13233888U JPH0254700U (en) 1988-10-12 1988-10-12

Publications (1)

Publication Number Publication Date
JPH0254700U true JPH0254700U (en) 1990-04-20

Family

ID=31389208

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13233888U Pending JPH0254700U (en) 1988-10-12 1988-10-12

Country Status (1)

Country Link
JP (1) JPH0254700U (en)

Similar Documents

Publication Publication Date Title
JPS6264806U (en)
JPS6447498U (en)
JPH01130899U (en)
JPS6196984U (en)
JPS6441267U (en)
JPH0441499U (en)
JPH03103078U (en)
JPS61163798U (en)
JPS6186308U (en)
JPS6196986U (en)
JPS61165201U (en)
JPS62111095U (en)
JPH01171209U (en)
JPS6312499U (en)
JPS63172726U (en)
JPH0232497U (en)
JPS62148655U (en)
JPS6265118U (en)
JPS61206596U (en)
JPH021118U (en)
JPS631095U (en)
JPS62156643U (en)
JPS648945U (en)
JPS63154061U (en)
JPH0243188U (en)