FR1132452A - Flight control system for airplanes or aerodynes - Google Patents

Flight control system for airplanes or aerodynes

Info

Publication number
FR1132452A
FR1132452A FR1132452DA FR1132452A FR 1132452 A FR1132452 A FR 1132452A FR 1132452D A FR1132452D A FR 1132452DA FR 1132452 A FR1132452 A FR 1132452A
Authority
FR
France
Prior art keywords
aerodynes
airplanes
control system
flight control
flight
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
Application number
Other languages
French (fr)
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.)
HM Hobson Ltd
Original Assignee
HM Hobson 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 HM Hobson Ltd filed Critical HM Hobson Ltd
Application granted granted Critical
Publication of FR1132452A publication Critical patent/FR1132452A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H21/00—Gearings comprising primarily only links or levers, with or without slides
    • F16H21/10—Gearings comprising primarily only links or levers, with or without slides all movement being in, or parallel to, a single plane
    • F16H21/44—Gearings comprising primarily only links or levers, with or without slides all movement being in, or parallel to, a single plane for conveying or interconverting oscillating or reciprocating motions
    • 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
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/345—Transmitting means without power amplification or where power amplification is irrelevant mechanical with artificial feel
FR1132452D 1954-06-03 1955-05-31 Flight control system for airplanes or aerodynes Expired FR1132452A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1132452X 1954-06-03

Publications (1)

Publication Number Publication Date
FR1132452A true FR1132452A (en) 1957-03-12

Family

ID=10876445

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1132452D Expired FR1132452A (en) 1954-06-03 1955-05-31 Flight control system for airplanes or aerodynes

Country Status (1)

Country Link
FR (1) FR1132452A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2261119A1 (en) 2009-06-04 2010-12-15 Eurocopter Method for directional control of a hybrid helicopter and hybrid helicopter provided with a directional control device suitable for implementing said method
EP2279941A1 (en) 2009-07-28 2011-02-02 Eurocopter Variable damping of haptic feedback for kinematic linkage to change the flight attitude of an aircraft
US8196857B2 (en) 2009-06-04 2012-06-12 Eurocopter Variable ratio crank for a manual flight control linkage of a rotary wing aircraft
EP3162706A1 (en) 2015-10-15 2017-05-03 Airbus Helicopters Combiner of yaw and thrust commands for a hybrid helicopter
EP3170744A1 (en) 2015-11-20 2017-05-24 Airbus Helicopters An adaptive flight control system for the yaw and thrust flight controls of a hybrid helicopter

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2261119A1 (en) 2009-06-04 2010-12-15 Eurocopter Method for directional control of a hybrid helicopter and hybrid helicopter provided with a directional control device suitable for implementing said method
US8196857B2 (en) 2009-06-04 2012-06-12 Eurocopter Variable ratio crank for a manual flight control linkage of a rotary wing aircraft
US8376266B2 (en) 2009-06-04 2013-02-19 Eurocopter Method of controlling a hybrid helicopter in yaw, and a hybrid helicopter provided with a yaw control device suitable for implementing said method
EP2279941A1 (en) 2009-07-28 2011-02-02 Eurocopter Variable damping of haptic feedback for kinematic linkage to change the flight attitude of an aircraft
EP3162706A1 (en) 2015-10-15 2017-05-03 Airbus Helicopters Combiner of yaw and thrust commands for a hybrid helicopter
EP3170744A1 (en) 2015-11-20 2017-05-24 Airbus Helicopters An adaptive flight control system for the yaw and thrust flight controls of a hybrid helicopter
US10507905B2 (en) 2015-11-20 2019-12-17 Airbus Helicopters Adaptive flight control system for the yaw and thrust flight controls of a hybrid helicopter

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