JPH034440B2 - - Google Patents

Info

Publication number
JPH034440B2
JPH034440B2 JP59183693A JP18369384A JPH034440B2 JP H034440 B2 JPH034440 B2 JP H034440B2 JP 59183693 A JP59183693 A JP 59183693A JP 18369384 A JP18369384 A JP 18369384A JP H034440 B2 JPH034440 B2 JP H034440B2
Authority
JP
Japan
Prior art keywords
link
flap
trailing edge
edge flap
point
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.)
Expired - Lifetime
Application number
JP59183693A
Other languages
English (en)
Japanese (ja)
Other versions
JPS6164599A (ja
Inventor
Tooru Kawamura
Toshio Sato
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.)
Japan Aircraft Manufacturing Co Ltd
Original Assignee
Japan Aircraft Manufacturing Co Ltd
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 Japan Aircraft Manufacturing Co Ltd filed Critical Japan Aircraft Manufacturing Co Ltd
Priority to JP18369384A priority Critical patent/JPS6164599A/ja
Publication of JPS6164599A publication Critical patent/JPS6164599A/ja
Publication of JPH034440B2 publication Critical patent/JPH034440B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Body Structure For Vehicles (AREA)
  • Transmission Devices (AREA)
JP18369384A 1984-09-04 1984-09-04 飛行機翼後縁フラツプのリンク式作動機構 Granted JPS6164599A (ja)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18369384A JPS6164599A (ja) 1984-09-04 1984-09-04 飛行機翼後縁フラツプのリンク式作動機構

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18369384A JPS6164599A (ja) 1984-09-04 1984-09-04 飛行機翼後縁フラツプのリンク式作動機構

Publications (2)

Publication Number Publication Date
JPS6164599A JPS6164599A (ja) 1986-04-02
JPH034440B2 true JPH034440B2 (enrdf_load_stackoverflow) 1991-01-23

Family

ID=16140285

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18369384A Granted JPS6164599A (ja) 1984-09-04 1984-09-04 飛行機翼後縁フラツプのリンク式作動機構

Country Status (1)

Country Link
JP (1) JPS6164599A (enrdf_load_stackoverflow)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7520465B2 (en) * 2003-11-21 2009-04-21 Airbus Aircraft fluid cooling system and aircraft provided with said system
DE102005061750A1 (de) * 2005-12-21 2007-07-05 Eads Deutschland Gmbh Flexible Steuerfläche für ein Luftfahrzeug

Also Published As

Publication number Publication date
JPS6164599A (ja) 1986-04-02

Similar Documents

Publication Publication Date Title
JP3213752B2 (ja) ティルト回転翼用フラッペロン・システム
US4444368A (en) Slotted variable camber flap
US5158252A (en) Three-position variable camber Krueger leading edge flap
US4172575A (en) Airfoil flap conical extension mechanism
US4448375A (en) Folding truss mechanism for trailing edge flaps
US4262868A (en) Three-position variable camber flap
EP0239138B1 (en) Aircraft wings with aileron-supported ground speed spoilers and trailing edge flaps
US4049219A (en) Variable pivot trailing edge flap
US3968946A (en) Extendable aerodynamic fairing
US4542869A (en) Flap mechanism
US3985319A (en) Variable pivot trailing edge flap
US3743219A (en) High lift leading edge device
JPH04503495A (ja) ティルト回転翼用フラッペロン・システム
US7661630B2 (en) High lift longitudinal axis control system
JPH09512515A (ja) ヘリコプター用の主回転翼システム
US4398683A (en) Aircraft with thrust and lift augmenting airfoil
JPH08258795A (ja) フラップ付きヘリコプタロータ
US6164598A (en) Adaptive control surface apparatus
EP0075966A2 (en) Aileron system for aircraft and method of operating the same
US4365774A (en) Convertible delta wing aircraft
JPS62157896A (ja) 可変キヤンバを有する可動翼
JPH03176297A (ja) 飛行機
JPH0523240B2 (enrdf_load_stackoverflow)
US3586262A (en) Foreflapped airfoil
US5236149A (en) Boundary layer control device for tilt rotor configuration

Legal Events

Date Code Title Description
EXPY Cancellation because of completion of term