CH244760A - Adjustable foot control on aircraft. - Google Patents

Adjustable foot control on aircraft.

Info

Publication number
CH244760A
CH244760A CH244760DA CH244760A CH 244760 A CH244760 A CH 244760A CH 244760D A CH244760D A CH 244760DA CH 244760 A CH244760 A CH 244760A
Authority
CH
Switzerland
Prior art keywords
aircraft
foot control
adjustable foot
adjustable
control
Prior art date
Application number
Other languages
German (de)
Inventor
Mueller Georg
Original Assignee
Mueller Georg
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 Mueller Georg filed Critical Mueller Georg
Publication of CH244760A publication Critical patent/CH244760A/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
CH244760D 1945-01-27 1945-01-27 Adjustable foot control on aircraft. CH244760A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH244760T 1945-01-27

Publications (1)

Publication Number Publication Date
CH244760A true CH244760A (en) 1946-09-30

Family

ID=4464489

Family Applications (1)

Application Number Title Priority Date Filing Date
CH244760D CH244760A (en) 1945-01-27 1945-01-27 Adjustable foot control on aircraft.

Country Status (1)

Country Link
CH (1) CH244760A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4848708A (en) * 1987-11-13 1989-07-18 The Boeing Company Adjustable assembly for aircraft rudder, brake and nose landing gear steering control
US5056742A (en) * 1987-11-13 1991-10-15 The Boeing Company Modular rudder pedal and brake control assembly for aircraft
EP2626299A1 (en) * 2012-02-10 2013-08-14 Bell Helicopter Textron Inc. Pilot control system with adjustable pedals
US8812177B2 (en) 2012-02-10 2014-08-19 Bell Helicopter Textron Inc. Integrated aircraft flight control units
US9051836B2 (en) 2012-02-10 2015-06-09 Bell Helicopter Textron Inc. Pilot control system with compact gimbal mechanism
US9056675B2 (en) 2012-02-10 2015-06-16 Bell Helicopter Textron Inc. Pilot control system with hand rest
US9067672B2 (en) 2012-02-10 2015-06-30 Bell Helicopter Textron Inc. Pilot control system with pendent grip

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4848708A (en) * 1987-11-13 1989-07-18 The Boeing Company Adjustable assembly for aircraft rudder, brake and nose landing gear steering control
US5056742A (en) * 1987-11-13 1991-10-15 The Boeing Company Modular rudder pedal and brake control assembly for aircraft
EP2626299A1 (en) * 2012-02-10 2013-08-14 Bell Helicopter Textron Inc. Pilot control system with adjustable pedals
US8812177B2 (en) 2012-02-10 2014-08-19 Bell Helicopter Textron Inc. Integrated aircraft flight control units
US9051836B2 (en) 2012-02-10 2015-06-09 Bell Helicopter Textron Inc. Pilot control system with compact gimbal mechanism
US9056675B2 (en) 2012-02-10 2015-06-16 Bell Helicopter Textron Inc. Pilot control system with hand rest
US9067672B2 (en) 2012-02-10 2015-06-30 Bell Helicopter Textron Inc. Pilot control system with pendent grip
US9764830B2 (en) 2012-02-10 2017-09-19 Bell Helicopter Textron Inc. Pilot control system with adjustable pedals

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