JPS5747298A - Electric command spoiler device - Google Patents

Electric command spoiler device

Info

Publication number
JPS5747298A
JPS5747298A JP56086315A JP8631581A JPS5747298A JP S5747298 A JPS5747298 A JP S5747298A JP 56086315 A JP56086315 A JP 56086315A JP 8631581 A JP8631581 A JP 8631581A JP S5747298 A JPS5747298 A JP S5747298A
Authority
JP
Japan
Prior art keywords
spoiler device
electric command
command
electric
spoiler
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.)
Granted
Application number
JP56086315A
Other languages
English (en)
Other versions
JPH0362596B2 (ja
Inventor
Buusu Heiningu
Debitsudo Matsukufuii Toomasu
Jiyasutatsudo Otsudo
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.)
Boeing Co
Original Assignee
Boeing Co
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=22585707&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=JPS5747298(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co filed Critical Boeing Co
Publication of JPS5747298A publication Critical patent/JPS5747298A/ja
Priority to EP82105030A priority Critical patent/EP0067407A1/en
Publication of JPH0362596B2 publication Critical patent/JPH0362596B2/ja
Granted 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
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/503—Fly-by-Wire
    • 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
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
JP56086315A 1980-06-24 1981-06-04 Electric command spoiler device Granted JPS5747298A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP82105030A EP0067407A1 (en) 1981-06-04 1982-06-08 Vehicle body with enclosed space for containing auxiliary devices

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/162,458 US4363098A (en) 1980-06-24 1980-06-24 Electric command spoiler system

Publications (2)

Publication Number Publication Date
JPS5747298A true JPS5747298A (en) 1982-03-18
JPH0362596B2 JPH0362596B2 (ja) 1991-09-26

Family

ID=22585707

Family Applications (1)

Application Number Title Priority Date Filing Date
JP56086315A Granted JPS5747298A (en) 1980-06-24 1981-06-04 Electric command spoiler device

Country Status (4)

Country Link
US (1) US4363098A (ja)
EP (1) EP0042653B1 (ja)
JP (1) JPS5747298A (ja)
DE (1) DE3175945D1 (ja)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63235194A (ja) * 1987-03-24 1988-09-30 防衛庁技術研究本部長 飛行制御装置
JPH0429693U (ja) * 1990-06-30 1992-03-10
JP2009515750A (ja) * 2005-11-15 2009-04-16 エアバス・ドイチュラント・ゲーエムベーハー 航空機用ブレーキフラップ
CN104108472A (zh) * 2013-04-16 2014-10-22 通用电气航空系统有限公司 用于预测速度制动系统故障的方法

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4472780A (en) * 1981-09-28 1984-09-18 The Boeing Company Fly-by-wire lateral control system
EP0237650B1 (en) * 1986-03-14 1990-03-14 The Boeing Company Avionic control system
US4739469A (en) * 1984-04-19 1988-04-19 Nissan Motor Company, Limited Fail-safe circuit for a control system
US4899284A (en) * 1984-09-27 1990-02-06 The Boeing Company Wing lift/drag optimizing system
US4821193A (en) * 1985-08-26 1989-04-11 General Electric Company Digital control for gas turbine engine
EP0218021B1 (de) * 1985-08-29 1988-06-08 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Klappenanordnung für einen Flugzeugtragflügel
US5087866A (en) * 1991-05-22 1992-02-11 Lucas Industries Temperature compensating circuit for LVDT and control system
US5493497A (en) * 1992-06-03 1996-02-20 The Boeing Company Multiaxis redundant fly-by-wire primary flight control system
US5458304A (en) * 1992-08-26 1995-10-17 Gilbert; Raymond D. Disk spoiler system
US5588620A (en) * 1992-08-26 1996-12-31 Gilbert; Raymond D. Radial-force spoiler system
US5564656A (en) * 1994-08-29 1996-10-15 Gilbert; Raymond D. Segmented spoilers
US5489830A (en) * 1994-09-09 1996-02-06 Mcdonnell Douglas Corporation Control system with loadfeel and backdrive
US6561463B1 (en) * 2000-07-14 2003-05-13 Honeywell International Inc. Flight control module with integrated spoiler actuator control electronics
US20030183728A1 (en) * 2002-03-29 2003-10-02 The Boeing Company Aircraft control surface controller and associated method
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
DE10249967B4 (de) * 2002-10-26 2006-03-09 Airbus Deutschland Gmbh Vorrichtung zur Ansteuerung der Vorflügel und Landeklappen eines Flugzeuges
EP1599383A4 (en) 2003-02-15 2011-08-24 Gulfstream Aerospace Corp SYSTEM AND METHOD FOR CONTROLLING THE ATMOSPHERIC COMPOSITION OF AN AIRCRAFT CABIN
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
FR2870819B1 (fr) * 2004-05-28 2006-08-25 Airbus France Sas Systeme de commande des aerofreins d'un avion
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
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
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
WO2007084679A2 (en) * 2006-01-17 2007-07-26 Gulfstream Aerospace Corporation Apparatus and method for backup control in a distributed flight control system
EP1977292A2 (en) * 2006-01-17 2008-10-08 Gulfstream Aerospace Corporation System and method for an integrated backup control system
GB2444742B (en) * 2006-12-11 2011-06-08 Embraer Aeronautica Sa Flight Control System
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
US10183738B2 (en) * 2014-04-08 2019-01-22 Marc Arnold Flight control augmentation system and method for high aspect ratio aircraft including motorglider aircraft, optionally piloted vehicles (OPVs) and unpiloted air vehicles (UAVs)
US20150321748A1 (en) * 2014-05-08 2015-11-12 Honeywell International Inc. Speed brake alerting system and method
US10196131B2 (en) * 2016-02-16 2019-02-05 The Boeing Company Hydraulic system and method for an aircraft flight control system
JP2021142974A (ja) 2020-03-10 2021-09-24 ナブテスコ株式会社 スポイラ制御装置、スポイラ制御方法、及びスポイラ制御プログラム

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR978031A (fr) * 1948-11-09 1951-04-09 Perfectionnements aux dispositifs stabilisateurs d'engins se déplaçant dans les fluides
US2612329A (en) * 1948-11-13 1952-09-30 Northrop Aircraft Inc Aileron, flap, and dive brake
US3589648A (en) * 1969-01-02 1971-06-29 Lockheed Aircraft Corp Means for controlling the vertical path of an aircraft
US3636324A (en) * 1970-01-28 1972-01-18 Us Federal Aviation Admin Air data lateral-directional stability augmentation system
US3787009A (en) * 1970-08-24 1974-01-22 Northrop Corp Direct side force control device
FR2344063A1 (fr) * 1976-03-10 1977-10-07 Smiths Industries Ltd Circuit numerique de commande a deux voies au moins
US4087065A (en) * 1977-02-04 1978-05-02 The Boeing Company Electrical control system for actuating inboard spoilers on aircraft
US4143839A (en) * 1977-08-29 1979-03-13 Antonov Oleg K Apparatus for combating rolling movements of aircraft
US4261537A (en) * 1979-02-28 1981-04-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Velocity vector control system augmented with direct lift control

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63235194A (ja) * 1987-03-24 1988-09-30 防衛庁技術研究本部長 飛行制御装置
JPH0429693U (ja) * 1990-06-30 1992-03-10
JP2009515750A (ja) * 2005-11-15 2009-04-16 エアバス・ドイチュラント・ゲーエムベーハー 航空機用ブレーキフラップ
CN104108472A (zh) * 2013-04-16 2014-10-22 通用电气航空系统有限公司 用于预测速度制动系统故障的方法
JP2014210574A (ja) * 2013-04-16 2014-11-13 ジーイー・アビエイション・システムズ・リミテッドＧｅ Ａｖｉａｔｉｏｎ Ｓｙｓｔｅｍｓ Ｌｉｍｉｔｅｄ スピードブレーキシステムの障害を予測する方法

Also Published As

Publication number Publication date
DE3175945D1 (en) 1987-04-09
JPH0362596B2 (ja) 1991-09-26
EP0042653A1 (en) 1981-12-30
EP0042653B1 (en) 1987-03-04
US4363098A (en) 1982-12-07

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