JPS5614519B1 - - Google Patents

Info

Publication number
JPS5614519B1
JPS5614519B1 JP2123771A JP2123771A JPS5614519B1 JP S5614519 B1 JPS5614519 B1 JP S5614519B1 JP 2123771 A JP2123771 A JP 2123771A JP 2123771 A JP2123771 A JP 2123771A JP S5614519 B1 JPS5614519 B1 JP S5614519B1
Authority
JP
Japan
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.)
Pending
Application number
JP2123771A
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 filed Critical
Priority to JP2123771A priority Critical patent/JPS5614519B1/ja
Priority to US00235645A priority patent/US3799695A/en
Priority to GB1522272A priority patent/GB1353564A/en
Priority to DE2216414A priority patent/DE2216414C3/de
Priority to FR7211968A priority patent/FR2132466B1/fr
Publication of JPS5614519B1 publication Critical patent/JPS5614519B1/ja
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/54Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Control Devices (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
JP2123771A 1971-04-06 1971-04-06 Pending JPS5614519B1 (ja)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP2123771A JPS5614519B1 (ja) 1971-04-06 1971-04-06
US00235645A US3799695A (en) 1971-04-06 1972-03-17 Control devices of rotorcrafts
GB1522272A GB1353564A (en) 1971-04-06 1972-03-30 Control devices of rotorcrafts
DE2216414A DE2216414C3 (de) 1971-04-06 1972-04-05 Steuersystem für Drehflügelflugzeuge
FR7211968A FR2132466B1 (ja) 1971-04-06 1972-04-05

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2123771A JPS5614519B1 (ja) 1971-04-06 1971-04-06

Publications (1)

Publication Number Publication Date
JPS5614519B1 true JPS5614519B1 (ja) 1981-04-04

Family

ID=12049424

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2123771A Pending JPS5614519B1 (ja) 1971-04-06 1971-04-06

Country Status (5)

Country Link
US (1) US3799695A (ja)
JP (1) JPS5614519B1 (ja)
DE (1) DE2216414C3 (ja)
FR (1) FR2132466B1 (ja)
GB (1) GB1353564A (ja)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1519380A (en) * 1975-11-13 1978-07-26 United Technologies Corp Method and apparatus to control aircraft having dual rigid rotors
US4027999A (en) * 1975-11-13 1977-06-07 United Technologies Corporation Analog mixer to vary helicopter rotor phase angle in flight
US4008979A (en) * 1975-11-13 1977-02-22 United Technologies Corporation Control for helicopter having dual rigid rotors
DE2658828C3 (de) * 1976-12-24 1982-02-25 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Rotor für ein Drehflügelflugzeug
US4525123A (en) * 1982-05-06 1985-06-25 Alfred Curci Rotary wing aircraft
US4697986A (en) * 1984-03-26 1987-10-06 David Constant V Helicopter blade cyclic pitch control system
US4688993A (en) * 1985-03-21 1987-08-25 United Technologies Corporation Tangential link swashplate centering member
US4930988A (en) * 1989-01-02 1990-06-05 Honeywell Inc Individual blade control system for helicopters
AU659491B2 (en) * 1992-09-23 1995-05-18 Elisport Helicopters S.R.L A control mechanism for helicopter rotor blades
US5165854A (en) * 1990-07-12 1992-11-24 Industrias Cicare S.R.L. Mechanism for controlling pitch change in helicopter blades
US5826822A (en) * 1996-04-19 1998-10-27 Rehm; Rehm N. System and method for providing cyclic and collective pitch control in a rotary wing aircraft
JP2000225277A (ja) * 1999-02-05 2000-08-15 Futaba Corp ラジオコントロールヘリコプター
WO2004028901A2 (en) * 2002-09-24 2004-04-08 Bell Helicopter Textron Inc. Rotorcraft control system with stepped mixing linkage
US7262712B2 (en) * 2004-04-12 2007-08-28 Safe Flight Instrument Corporation Helicopter tactile exceedance warning system
FR2946317B1 (fr) * 2009-06-04 2011-06-17 Eurocopter France Guignol a rapport variable pour chaine de commande de vol manuelle d'aeronef a voiture tournante
FR2959205B1 (fr) * 2010-04-27 2012-04-13 Eurocopter France Procede de commande et de regulation de l'angle de braquage d'un empennage d'helicoptere hybride
CN106802659A (zh) * 2017-01-13 2017-06-06 清华大学 变桨距多旋翼飞行器的控制方法
WO2023277847A1 (en) * 2021-06-29 2023-01-05 Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi A control mechanism
EP4363314A4 (en) * 2021-06-29 2024-10-09 Tusas Turk Havacilik Ve Uzay Sanayii Anonim Sirketi CONTROL MECHANISM

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR995459A (fr) * 1945-03-06 1951-12-03 Procédé et dispositif permettant d'améliorer la maniabilité des appareils d'aviation à voilures tournantes articulées
US2599690A (en) * 1945-06-16 1952-06-10 United Aircraft Corp Helicopter control
US2748876A (en) * 1951-01-12 1956-06-05 Vertol Aircraft Corp Means for controlling tip-path of rotors
FR1131074A (fr) * 1954-12-24 1957-02-15 Diretor Geral Do Ct Tecnico De Perfectionnements aux dispositifs de stabilisation des hélicoptères
US2978037A (en) * 1958-02-12 1961-04-04 Ministerio Da Aeronautica Dire Stabilizing means for helicopter aircraft
US3199601A (en) * 1962-02-02 1965-08-10 United Aircraft Corp Flight control system
US3217809A (en) * 1963-02-28 1965-11-16 Kaman Aircraft Corp Rotor blade pitch changing mechanism for rotary wing aircraft
US3589831A (en) * 1969-11-10 1971-06-29 Kaman Corp Control system for rotary wing vehicle

Also Published As

Publication number Publication date
FR2132466B1 (ja) 1975-03-21
FR2132466A1 (ja) 1972-11-17
GB1353564A (en) 1974-05-22
DE2216414A1 (de) 1972-10-19
DE2216414B2 (de) 1974-08-08
US3799695A (en) 1974-03-26
DE2216414C3 (de) 1975-03-27

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