FR2407130A1 - Systeme de commande de vol redondant - Google Patents

Systeme de commande de vol redondant

Info

Publication number
FR2407130A1
FR2407130A1 FR7830385A FR7830385A FR2407130A1 FR 2407130 A1 FR2407130 A1 FR 2407130A1 FR 7830385 A FR7830385 A FR 7830385A FR 7830385 A FR7830385 A FR 7830385A FR 2407130 A1 FR2407130 A1 FR 2407130A1
Authority
FR
France
Prior art keywords
quadrant
control system
cables
flight control
pilot
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
FR7830385A
Other languages
English (en)
Other versions
FR2407130B1 (fr
Inventor
Rondald Arthur Durno
Dean Earl Cooper
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 Technologies 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 Technologies Corp filed Critical United Technologies Corp
Publication of FR2407130A1 publication Critical patent/FR2407130A1/fr
Application granted granted Critical
Publication of FR2407130B1 publication Critical patent/FR2407130B1/fr
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
    • B64C13/26—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
    • B64C13/341—Transmitting means without power amplification or where power amplification is irrelevant mechanical having duplication or stand-by provisions
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/18—Mechanical movements
    • Y10T74/18856—Oscillating to oscillating
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/20—Control lever and linkage systems
    • Y10T74/20396—Hand operated
    • Y10T74/20402—Flexible transmitter [e.g., Bowden cable]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Control Devices (AREA)
  • Flexible Shafts (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Catching Or Destruction (AREA)

Abstract

L'INVENTION CONCERNE UN SYSTEME DE COMMANDE DE VOL REDONDANT. DANS CE SYSTEME DE COMMANDE DE VOL 10, ON UTILISE DES CABLES FLEXIBLES 20, 22 MANOEUVRES PAR LE PILOTE POUR DEPLACER SELECTIVEMENT UN QUADRANT DE COMMANDE 16, AINSI QUE DES RESSORTS D'EQUILIBRAGE PRECHARGES 84, 96 QUI SONT RELIES AU QUADRANT 16 AFIN DE SE DETENDRE AUTOMATIQUEMENT ET SELECTIVEMENT SUITE A LA RUPTURE D'UN DES CABLES 20, 22, PERMETTANT AINSI AU PILOTE, DE MANOEUVRER LE QUADRANT 16 DANS TOUT SON REGIME DE COMMANDE EN DEPIT DE LA RUPTURE D'UN DES CABLES 20, 22. L'INVENTION EST UTILISEE POUR PERMETTRE UNE COMMANDE REDONDANTE DU QUADRANT AFIN QUE LE PILOTE PUISSE CONSERVER LE CONTROLE DE CE DERNIER EN CAS DE RUPTURE D'UN DES CABLES.
FR7830385A 1977-10-27 1978-10-25 Systeme de commande de vol redondant Granted FR2407130A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/846,094 US4170147A (en) 1977-10-27 1977-10-27 Redundant flight control system

Publications (2)

Publication Number Publication Date
FR2407130A1 true FR2407130A1 (fr) 1979-05-25
FR2407130B1 FR2407130B1 (fr) 1983-09-30

Family

ID=25296924

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7830385A Granted FR2407130A1 (fr) 1977-10-27 1978-10-25 Systeme de commande de vol redondant

Country Status (12)

Country Link
US (1) US4170147A (fr)
JP (1) JPS5470599A (fr)
AU (1) AU517367B2 (fr)
BE (1) BE871502A (fr)
BR (1) BR7806707A (fr)
CA (1) CA1094037A (fr)
DE (1) DE2845788A1 (fr)
FR (1) FR2407130A1 (fr)
GB (1) GB2006699B (fr)
IL (1) IL55776A (fr)
IT (1) IT1099801B (fr)
NO (1) NO144999C (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2502825A1 (fr) * 2011-03-25 2012-09-26 Eurocopter Pilotage de secours par vérin série pour chaine de commande de vol manuelle d'aéronef et Procédé

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4198877A (en) * 1978-07-07 1980-04-22 The United States Of America As Represented By The Secretary Of The Air Force Control cable fail safe device
FR2444295A1 (fr) * 1978-12-13 1980-07-11 Rech Mecanique Appliquee Regulateur de tension de cables
US4484486A (en) * 1981-12-03 1984-11-27 Westinghouse Electric Corp. Concentric pulley drive assembly
US4540141A (en) * 1983-09-22 1985-09-10 United Technologies Corporation Fail-safe tail rotor control system
US4529155A (en) * 1983-12-09 1985-07-16 United Technologies Corporation Redundant tail rotor control system
US4691584A (en) * 1985-02-20 1987-09-08 Ohi Seisakusho Co., Ltd. Actuator for remote devices or the like
JPH02138834U (fr) * 1989-04-24 1990-11-20
US5551652A (en) * 1994-03-28 1996-09-03 Mcdonnell Douglas Corporation Standby control system
KR100461481B1 (ko) * 1997-04-30 2005-05-17 볼보 컨스트럭션 이키프먼트 홀딩 스웨덴 에이비 링크장치
US5924331A (en) * 1997-07-08 1999-07-20 Mcdonnell Douglas Corporation Cable control system having stored energy fail-safe mechanism
US20090283628A1 (en) * 2008-05-19 2009-11-19 Frederickson Kirk C Directional control arrangement to provide stabilizing feedback to a structural bending mode
EP2367719B1 (fr) 2008-12-11 2018-09-12 Sikorsky Aircraft Corporation Assemblage pour lames de rotor de queue avec dispositif limiteur de mouvement d'un système de palier élastomère
US9584367B2 (en) * 2013-11-05 2017-02-28 Solarwinds Worldwide, Llc Node de-duplication in a network monitoring system
US9562581B2 (en) * 2014-03-28 2017-02-07 Bell Helicopter Textron Inc. Spring tension adjustment mechanism

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1046110A (en) * 1964-01-20 1966-10-19 Pacific Scientific Co Control line regulator
GB1096238A (en) * 1965-06-01 1967-12-20 Pacific Scientific Co Control line regulator

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1996332A (en) * 1933-09-12 1935-04-02 Henry M Grinslade Brake equalizing mechanism
US2304487A (en) * 1939-11-20 1942-12-08 Stinson School Of Aviat Inc Control mechanism for combination flap and aileron for airplanes
US2280106A (en) * 1940-12-24 1942-04-21 Sturgess Inc Cable tension controller
US2430869A (en) * 1945-03-03 1947-11-18 Continental Inc Roadable airplane
US2669401A (en) * 1952-05-17 1954-02-16 Boeing Co Tab control
US2778455A (en) * 1954-05-17 1957-01-22 Stanley G Roach Auxiliary actuating attachment for vehicle brake system
US2921480A (en) * 1956-01-30 1960-01-19 Pacific Scientific Co Control line regulator
US3031036A (en) * 1956-12-03 1962-04-24 Meyers Joseph Emergency brake mechanism

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1046110A (en) * 1964-01-20 1966-10-19 Pacific Scientific Co Control line regulator
GB1096238A (en) * 1965-06-01 1967-12-20 Pacific Scientific Co Control line regulator

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2502825A1 (fr) * 2011-03-25 2012-09-26 Eurocopter Pilotage de secours par vérin série pour chaine de commande de vol manuelle d'aéronef et Procédé
US8684314B2 (en) 2011-03-25 2014-04-01 Airbus Helicopters Emergency piloting by means of a series actuator for a manual flight control system in an aircraft

Also Published As

Publication number Publication date
DE2845788C2 (fr) 1989-07-06
JPS6248640B2 (fr) 1987-10-14
GB2006699A (en) 1979-05-10
AU4049878A (en) 1980-04-17
GB2006699B (en) 1982-01-13
NO783563L (no) 1979-04-30
AU517367B2 (en) 1981-07-23
IT7829132A0 (it) 1978-10-26
NO144999C (no) 1981-12-28
NO144999B (no) 1981-09-14
BR7806707A (pt) 1979-05-08
IT1099801B (it) 1985-09-28
JPS5470599A (en) 1979-06-06
DE2845788A1 (de) 1979-05-03
CA1094037A (fr) 1981-01-20
US4170147A (en) 1979-10-09
BE871502A (fr) 1979-02-15
FR2407130B1 (fr) 1983-09-30
IL55776A (en) 1980-10-26

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Legal Events

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