JPS5453496A - Control device in helicopter for corrective pitch of helicopter and corrective control device for helicopter - Google Patents

Control device in helicopter for corrective pitch of helicopter and corrective control device for helicopter

Info

Publication number
JPS5453496A
JPS5453496A JP9675278A JP9675278A JPS5453496A JP S5453496 A JPS5453496 A JP S5453496A JP 9675278 A JP9675278 A JP 9675278A JP 9675278 A JP9675278 A JP 9675278A JP S5453496 A JPS5453496 A JP S5453496A
Authority
JP
Japan
Prior art keywords
helicopter
control device
corrective
pitch
corrective pitch
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
JP9675278A
Other languages
English (en)
Other versions
JPS6344120B2 (ja
Inventor
Uiriamu Kaarusun Furoido
Mashiyuman Jiyouzuifu
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.)
Textron Inc
Original Assignee
Textron Inc
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 Textron Inc filed Critical Textron Inc
Publication of JPS5453496A publication Critical patent/JPS5453496A/ja
Publication of JPS6344120B2 publication Critical patent/JPS6344120B2/ja
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
  • Toys (AREA)
  • Catching Or Destruction (AREA)
  • Mechanical Control Devices (AREA)
JP9675278A 1977-08-10 1978-08-10 Control device in helicopter for corrective pitch of helicopter and corrective control device for helicopter Granted JPS5453496A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/823,284 US4130259A (en) 1977-08-10 1977-08-10 Helicopter collective lever

Publications (2)

Publication Number Publication Date
JPS5453496A true JPS5453496A (en) 1979-04-26
JPS6344120B2 JPS6344120B2 (ja) 1988-09-02

Family

ID=25238312

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9675278A Granted JPS5453496A (en) 1977-08-10 1978-08-10 Control device in helicopter for corrective pitch of helicopter and corrective control device for helicopter

Country Status (7)

Country Link
US (1) US4130259A (ja)
JP (1) JPS5453496A (ja)
CA (1) CA1112230A (ja)
DE (1) DE2833495C2 (ja)
FR (1) FR2399946A1 (ja)
GB (1) GB2002302B (ja)
IT (1) IT1105477B (ja)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT8052954V0 (it) * 1980-02-19 1980-02-19 Agusta Aeronaut Costr Sistema di comando per elicotteri con barra mobile con il sedile pilota
US4819896A (en) * 1986-01-29 1989-04-11 Narad James L Hand-operated aircraft control system
GB8610481D0 (en) * 1986-04-29 1986-11-26 British Aerospace Control apparatus
US4887782A (en) * 1989-01-12 1989-12-19 The United States Of American As Represented By The Secretary Of The Army Cyclic control sticks for helicopters
WO2001014943A1 (en) * 1999-08-25 2001-03-01 Jae Dong Kim Aerial photography camera system for a helicopter
US8950699B1 (en) * 2010-09-09 2015-02-10 Groen Brothers Aviation, Inc. Heliplane rotor thermal management for maintaining dimensional stability
USD693758S1 (en) * 2012-02-10 2013-11-19 Bell Helicopter Textron Inc. Cyclic control post and grip
USD693757S1 (en) * 2012-02-10 2013-11-19 Bell Helicopter Textron Inc. Combined cyclic and collective controls
USD694168S1 (en) * 2012-02-10 2013-11-26 Bell Helicopter Textron Inc. Collective control post and grip for a rotorcraft
USD701485S1 (en) * 2013-03-03 2014-03-25 Bell Helicopter Textron Inc. Cyclic control post and grip
USD701486S1 (en) * 2013-03-03 2014-03-25 Bell Helicopter Textron Inc. Collective control post and grip
USD701161S1 (en) * 2013-03-03 2014-03-18 Bell Helicopter Textron Inc. Cyclic and collective controls
US10035583B2 (en) * 2015-10-23 2018-07-31 The Boeing Company Rotorcraft controls and rotorcraft including such rotorcraft controls
US11021244B2 (en) * 2017-03-06 2021-06-01 Textron Innovations Inc. Collective control stick mounted throttle control assembly
US10011348B1 (en) * 2017-05-02 2018-07-03 Kitty Hawk Corporation Vertical thrust lever
US12612172B2 (en) 2022-10-14 2026-04-28 Beta Air Llc Lift lever assembly for a vertical takeoff and landing (VTOL) aircraft and a method for its use

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1278462A (en) * 1917-09-20 1918-09-10 John Harris Airplane.
US2505020A (en) * 1946-09-13 1950-04-25 Weisman Charles Control mechanism for aircraft
US2589030A (en) * 1949-04-26 1952-03-11 Alde Murray William Helicopter rotor system
DE1079961B (de) * 1957-11-05 1960-04-14 Curtiss Wright Corp Regleranlage fuer eine Antriebsmaschine, insbesondere fuer einen Hubschrauber-motor
DE1225966B (de) * 1964-11-03 1966-09-29 Wolfgang Mueller Steuereinrichtung fuer Hubschrauber
US3288395A (en) * 1964-12-07 1966-11-29 Krohncke Kenneth Helicopter
US3543599A (en) * 1969-03-20 1970-12-01 Textron Inc Throttle control linkage

Also Published As

Publication number Publication date
IT7850650A0 (it) 1978-08-08
GB2002302A (en) 1979-02-21
GB2002302B (en) 1982-01-27
DE2833495A1 (de) 1979-02-22
CA1112230A (en) 1981-11-10
FR2399946B1 (ja) 1983-10-14
JPS6344120B2 (ja) 1988-09-02
IT1105477B (it) 1985-11-04
FR2399946A1 (fr) 1979-03-09
DE2833495C2 (de) 1987-04-02
US4130259A (en) 1978-12-19

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