GB1353564A - Control devices of rotorcrafts - Google Patents

Control devices of rotorcrafts

Info

Publication number
GB1353564A
GB1353564A GB1522272A GB1522272A GB1353564A GB 1353564 A GB1353564 A GB 1353564A GB 1522272 A GB1522272 A GB 1522272A GB 1522272 A GB1522272 A GB 1522272A GB 1353564 A GB1353564 A GB 1353564A
Authority
GB
United Kingdom
Prior art keywords
lever
control
pitch
stick
rods
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
GB1522272A
Other languages
English (en)
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.)
Kawasaki Heavy Industries Ltd
Kawasaki Motors Ltd
Original Assignee
Kawasaki Heavy Industries Ltd
Kawasaki Jukogyo KK
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 Kawasaki Heavy Industries Ltd, Kawasaki Jukogyo KK filed Critical Kawasaki Heavy Industries Ltd
Publication of GB1353564A publication Critical patent/GB1353564A/en
Expired 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

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)
GB1522272A 1971-04-06 1972-03-30 Control devices of rotorcrafts Expired GB1353564A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
GB1353564A true GB1353564A (en) 1974-05-22

Family

ID=12049424

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1522272A Expired GB1353564A (en) 1971-04-06 1972-03-30 Control devices of rotorcrafts

Country Status (5)

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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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 A control mechanism

Families Citing this family (17)

* 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
US4008979A (en) * 1975-11-13 1977-02-22 United Technologies Corporation Control for helicopter 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
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
BR0313895A (pt) * 2002-09-24 2005-08-30 Bell Helicopter Textron Inc Sistema de controle de aeronave de rotor com ligação de mistura escalonada
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

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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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 A control mechanism
US12466546B2 (en) 2021-06-29 2025-11-11 Tusas—Turk Havacilik Ve Uzay Sanayii Anonim Sirketi Control mechanism for an air vehicle

Also Published As

Publication number Publication date
DE2216414B2 (de) 1974-08-08
JPS5614519B1 (https=) 1981-04-04
FR2132466B1 (https=) 1975-03-21
DE2216414A1 (de) 1972-10-19
US3799695A (en) 1974-03-26
DE2216414C3 (de) 1975-03-27
FR2132466A1 (https=) 1972-11-17

Similar Documents

Publication Publication Date Title
GB1353564A (en) Control devices of rotorcrafts
GB1188345A (en) Rigid Rotor Helicopter and Method of Flying Same
GB1081341A (en) Apparatus for longitudinal stabilization of rotor craft
GB1232243A (https=)
US2424889A (en) Airplane control system
GB1032772A (en) Mechanism from controlling two separate apparatuses
US2664958A (en) Throttle control and pitch synchronizing device
US3002714A (en) Aircraft longitudinal control system
US2685422A (en) Variable stop mechanism for interrelated mechanical surface control systems for aircraft
US3378938A (en) Aviation trainer
US3375605A (en) Model plane flight control device
US3773282A (en) Vehicle control system
US3050276A (en) Automatic stabilization device
US2606622A (en) Helicopter control apparatus
ES212469A1 (es) Perfeccionamientos en aparatos para el control de vuelo en helicopteros
US3205728A (en) Control system for vtol vehicles
US2817483A (en) Aircraft control force modifier
Hall et al. Flight investigation of fighter side-stick force-deflection characteristics
US3067970A (en) Trim force control system
US2948495A (en) Control apparatus for an aircraft
US2801060A (en) Aircraft trim control
GB1010042A (en) Method and apparatus for controlling an aircraft
US2445550A (en) Control system for adjusting the incidence of the blades of the rotor of a rotary-wing aircraft
GB1231642A (https=)
US2518012A (en) Resiliently interconnected aileron and rudder control system for aircraft

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee