CA993851A - Fas actuation system - Google Patents

Fas actuation system

Info

Publication number
CA993851A
CA993851A CA201,747A CA201747A CA993851A CA 993851 A CA993851 A CA 993851A CA 201747 A CA201747 A CA 201747A CA 993851 A CA993851 A CA 993851A
Authority
CA
Canada
Prior art keywords
fas
actuation system
actuation
fas actuation
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
CA201,747A
Other versions
CA201747S (en
Inventor
Harold G. Heiney
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of CA993851A publication Critical patent/CA993851A/en
Expired legal-status Critical Current

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
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/40—Transmitting means with power amplification using fluid pressure
    • B64C13/46—Transmitting means with power amplification using fluid pressure with artificial feel
CA201,747A 1973-10-23 1974-06-05 Fas actuation system Expired CA993851A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US408876A US3862730A (en) 1973-10-23 1973-10-23 Fas actuation system

Publications (1)

Publication Number Publication Date
CA993851A true CA993851A (en) 1976-07-27

Family

ID=23618138

Family Applications (1)

Application Number Title Priority Date Filing Date
CA201,747A Expired CA993851A (en) 1973-10-23 1974-06-05 Fas actuation system

Country Status (10)

Country Link
US (1) US3862730A (en)
JP (1) JPS5072400A (en)
BR (1) BR7408722A (en)
CA (1) CA993851A (en)
DE (1) DE2450158A1 (en)
FR (1) FR2248194B1 (en)
GB (1) GB1478524A (en)
IL (1) IL45617A (en)
IT (1) IT1025111B (en)
MY (1) MY7800298A (en)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3960348A (en) * 1975-08-04 1976-06-01 United Technologies Corporation Aerodynamic surface control feel augmentation system
US4477043A (en) * 1982-12-15 1984-10-16 The United States Of America As Represented By The Secretary Of The Air Force Biodynamic resistant control stick
US4477044A (en) * 1983-01-17 1984-10-16 The Boeing Company Elevator feel actuator
JP2536508Y2 (en) * 1990-11-22 1997-05-21 三菱農機株式会社 Moving agricultural machine
WO1998017529A1 (en) 1996-10-22 1998-04-30 The Boeing Company Airplane with unswept slotted cruise wing airfoil
JP3995752B2 (en) * 1997-03-14 2007-10-24 アビックス株式会社 Man-machine interface input device
US7258308B2 (en) * 2002-07-02 2007-08-21 The Boeing Company Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
US7059563B2 (en) * 2003-06-03 2006-06-13 The Boeing Company Systems, apparatuses, and methods for moving aircraft control surfaces
US7243881B2 (en) 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
US6799739B1 (en) * 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7424350B2 (en) 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
US7357358B2 (en) * 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US6978971B1 (en) * 2004-06-15 2005-12-27 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
US7270305B2 (en) * 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding methods
US7494094B2 (en) * 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) * 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7322547B2 (en) * 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) * 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7309043B2 (en) * 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7300021B2 (en) * 2005-05-20 2007-11-27 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7721999B2 (en) * 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
US7500641B2 (en) * 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body systems and associated methods
US7611099B2 (en) * 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
US7475854B2 (en) 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US7708231B2 (en) * 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US7578484B2 (en) * 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) * 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8382045B2 (en) * 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
US10196131B2 (en) * 2016-02-16 2019-02-05 The Boeing Company Hydraulic system and method for an aircraft flight control system

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3450375A (en) * 1967-02-02 1969-06-17 Bertea Corp Load feel computer
US3438306A (en) * 1967-02-07 1969-04-15 Lear Siegler Inc Preloaded servo actuator controls for redundant systems
US3733039A (en) * 1971-05-20 1973-05-15 United Aircraft Corp Feel augmentation control system for helicopters

Also Published As

Publication number Publication date
IT1025111B (en) 1978-08-10
IL45617A0 (en) 1975-03-13
IL45617A (en) 1977-06-30
MY7800298A (en) 1978-12-31
JPS5072400A (en) 1975-06-14
BR7408722A (en) 1975-11-04
US3862730A (en) 1975-01-28
AU7295174A (en) 1976-03-11
FR2248194A1 (en) 1975-05-16
GB1478524A (en) 1977-07-06
FR2248194B1 (en) 1981-11-20
DE2450158A1 (en) 1975-09-04

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