JPS6248640B2 - - Google Patents

Info

Publication number
JPS6248640B2
JPS6248640B2 JP53132065A JP13206578A JPS6248640B2 JP S6248640 B2 JPS6248640 B2 JP S6248640B2 JP 53132065 A JP53132065 A JP 53132065A JP 13206578 A JP13206578 A JP 13206578A JP S6248640 B2 JPS6248640 B2 JP S6248640B2
Authority
JP
Japan
Prior art keywords
arm
control element
control
arm member
spring
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
JP53132065A
Other languages
English (en)
Japanese (ja)
Other versions
JPS5470599A (en
Inventor
Aasaa Daano Ronarudo
Aaru Kuupaa Deiin
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.)
RTX 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 JPS5470599A publication Critical patent/JPS5470599A/ja
Publication of JPS6248640B2 publication Critical patent/JPS6248640B2/ja
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/26Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/341Transmitting means without power amplification or where power amplification is irrelevant mechanical having duplication or stand-by provisions
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/18Mechanical movements
    • Y10T74/18856Oscillating to oscillating
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/20Control lever and linkage systems
    • Y10T74/20396Hand operated
    • Y10T74/20402Flexible 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)
  • Catching Or Destruction (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
JP13206578A 1977-10-27 1978-10-26 Flight control apparatus Granted JPS5470599A (en)

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
JPS5470599A JPS5470599A (en) 1979-06-06
JPS6248640B2 true JPS6248640B2 (en]) 1987-10-14

Family

ID=25296924

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13206578A Granted JPS5470599A (en) 1977-10-27 1978-10-26 Flight control apparatus

Country Status (12)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02138834U (en]) * 1989-04-24 1990-11-20

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
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 (en) 2008-12-11 2018-09-12 Sikorsky Aircraft Corporation Tail rotor blade assembly and elastomeric bearing system motion limiter
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
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

Family Cites Families (10)

* 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
US3277738A (en) * 1964-01-20 1966-10-11 Pacific Scientific Co Control line regulator
US3316775A (en) * 1965-06-01 1967-05-02 Pacific Scientific Co Control line regulator

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02138834U (en]) * 1989-04-24 1990-11-20

Also Published As

Publication number Publication date
DE2845788A1 (de) 1979-05-03
NO144999C (no) 1981-12-28
BE871502A (fr) 1979-02-15
CA1094037A (en) 1981-01-20
IT7829132A0 (it) 1978-10-26
NO783563L (no) 1979-04-30
US4170147A (en) 1979-10-09
AU517367B2 (en) 1981-07-23
NO144999B (no) 1981-09-14
BR7806707A (pt) 1979-05-08
FR2407130A1 (fr) 1979-05-25
IL55776A (en) 1980-10-26
FR2407130B1 (en]) 1983-09-30
DE2845788C2 (en]) 1989-07-06
AU4049878A (en) 1980-04-17
GB2006699B (en) 1982-01-13
IT1099801B (it) 1985-09-28
JPS5470599A (en) 1979-06-06
GB2006699A (en) 1979-05-10

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