ES8206331A1 - Perfeccionamientos en los dispositivos de posicionado e in- movilizacion automatico de palas plegables de helicoptero - Google Patents

Perfeccionamientos en los dispositivos de posicionado e in- movilizacion automatico de palas plegables de helicoptero

Info

Publication number
ES8206331A1
ES8206331A1 ES506143A ES506143A ES8206331A1 ES 8206331 A1 ES8206331 A1 ES 8206331A1 ES 506143 A ES506143 A ES 506143A ES 506143 A ES506143 A ES 506143A ES 8206331 A1 ES8206331 A1 ES 8206331A1
Authority
ES
Spain
Prior art keywords
positions
stored
response
trim
references
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
ES506143A
Other languages
English (en)
Other versions
ES506143A0 (es
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
Priority claimed from US06/195,723 external-priority patent/US4376979A/en
Priority claimed from US06/195,808 external-priority patent/US4354234A/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of ES506143A0 publication Critical patent/ES506143A0/es
Publication of ES8206331A1 publication Critical patent/ES8206331A1/es
Expired 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • B64C27/473Constructional features
    • B64C27/50Blades foldable to facilitate stowage of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)

Abstract

DISPOSITIVO DE POSICIONADO E INMOVLILIZACION AUTOMATICA DE PALAS PLEGABLES DE HELICOPTEROS. LAS PALAS (12) DEL ROTOR PRINCIPAL SON PIVOTABLES ALREDEDOR DE UN EJE LONGITUDINAL, EN RESPUESTA A LA POSICION DE UNAS BARRAS DE EMPUJE QUE CONTACTAN CON UN PLATO OSCILANTE (13) QUE ESTA CONECTADO A UNA SERIE DE SERVOMECANISMOS (17-19) QUE CONTROLAN EL EMPLAZAMIENTO DEL EJE DE INCLINACION, EL GRADO DE INCLINACION Y LA POSICION VERTICAL DEL PLATO OSCILANTE. CADA SERVOMECANISMO TIENE UN ELEMENTO DE ENTRADA MECANICO (23-25) DE UN MEZCLADOR (26) QUE RECIBE LAS ENTRADAS MECANICAS (27-29) DE CADA UNO DE LOS TRES EJES DE MANDO DE VUELO: PASO, DESPLAZAMIENTO Y ELEVACION. LA ENTRADA DE CADA SERVOMECANISMO (31-33) TIENE UN ACCIONADOR COMPENSADOR (39-41) QUE RESPONDE A UNA CONEXION ELECTRICA (42-44) DESDE UN COMPUTADOR DE MANDO DE VUELO AUTOMATICO (45).
ES506143A 1980-10-10 1981-10-09 Perfeccionamientos en los dispositivos de posicionado e in- movilizacion automatico de palas plegables de helicoptero Expired ES8206331A1 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/195,723 US4376979A (en) 1980-10-10 1980-10-10 Updated lock-positioning of foldable helicopter blades
US06/195,808 US4354234A (en) 1980-10-10 1980-10-10 Automatic lock-positioning of foldable helicopter blades

Publications (2)

Publication Number Publication Date
ES506143A0 ES506143A0 (es) 1982-08-16
ES8206331A1 true ES8206331A1 (es) 1982-08-16

Family

ID=26891271

Family Applications (1)

Application Number Title Priority Date Filing Date
ES506143A Expired ES8206331A1 (es) 1980-10-10 1981-10-09 Perfeccionamientos en los dispositivos de posicionado e in- movilizacion automatico de palas plegables de helicoptero

Country Status (8)

Country Link
AU (1) AU540743B2 (es)
CA (1) CA1161413A (es)
CH (1) CH652673A5 (es)
DE (1) DE3139720C2 (es)
ES (1) ES8206331A1 (es)
FR (1) FR2491865A1 (es)
GB (1) GB2085194B (es)
IT (1) IT1138938B (es)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4696445A (en) * 1986-09-18 1987-09-29 United Technologies Corporation Collective control system for a helicopter
AU587363B1 (en) * 1988-07-27 1989-08-10 Richard Henry Tollervey Improvements to helicopter rotor blades
FR2754779B1 (fr) * 1996-10-22 1998-12-31 Eurocopter France Procede de repliage des pales d'un rotor principal de giravion et dispositif de mise en oeuvre
FR2931132B1 (fr) 2008-05-19 2010-04-23 Eurocopter France Systeme de commande assiste d'un giravon
US9682771B2 (en) 2013-08-14 2017-06-20 Sikorsky Aircraft Corporation Controlling rotor blades of a swashplateless rotor
CN114465065B (zh) * 2022-01-06 2023-11-03 广东汇天航空航天科技有限公司 飞行器主轴滑环装置、飞行器旋翼系统及飞行器
CN114802739B (zh) * 2022-06-09 2023-04-07 广东汇天航空航天科技有限公司 飞行器的旋翼定位方法、飞行器和存储介质

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3698662A (en) * 1970-10-12 1972-10-17 Lockheed Aircraft Corp Apparatus and method for sequencing the folding and unfolding of rotor blades in a compound vehicle
US4103848A (en) * 1977-03-08 1978-08-01 United Technologies Corporation Variable incidence helicopter stabilator and fail safe actuator
US4284387A (en) * 1979-05-02 1981-08-18 United Technologies Corp. Blade fold restraint system

Also Published As

Publication number Publication date
IT1138938B (it) 1986-09-17
GB2085194A (en) 1982-04-21
CA1161413A (en) 1984-01-31
GB2085194B (en) 1984-03-07
FR2491865A1 (fr) 1982-04-16
AU7622781A (en) 1982-04-22
FR2491865B1 (es) 1983-12-23
CH652673A5 (de) 1985-11-29
ES506143A0 (es) 1982-08-16
AU540743B2 (en) 1984-11-29
DE3139720A1 (de) 1982-05-19
DE3139720C2 (de) 1994-02-10
IT8124415A0 (it) 1981-10-09

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19990503