ES8206333A1 - Aparato de control utilizable particularmente en aviacion. - Google Patents

Aparato de control utilizable particularmente en aviacion.

Info

Publication number
ES8206333A1
ES8206333A1 ES500327A ES500327A ES8206333A1 ES 8206333 A1 ES8206333 A1 ES 8206333A1 ES 500327 A ES500327 A ES 500327A ES 500327 A ES500327 A ES 500327A ES 8206333 A1 ES8206333 A1 ES 8206333A1
Authority
ES
Spain
Prior art keywords
rider
aircraft
control
rod
motor
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
ES500327A
Other languages
English (en)
Other versions
ES500327A0 (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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Publication of ES500327A0 publication Critical patent/ES500327A0/es
Publication of ES8206333A1 publication Critical patent/ES8206333A1/es
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control; Arrangement thereof
    • B64D31/02—Initiating means
    • B64D31/04—Initiating means actuated personally

Abstract

UNIDAD DE DEMANDA DE EMPUJE PARA UN AVION. ESTA FORMADA POR UNA ESTRUCTURA METALICA (1) QUE ALOJA EN SU INTERIOR DOS EJES (7) CORRESPONDIENTES CADA UNO AL ESTATOR DE UN MOTOR LINEAL, SOPORTADOS EN TALADROS ENCASQUILLADOS (6). CADA MOTOR LINEAL COMPRENDE ADEMAS UN CUERPO DESLIZANTE (8), CON COJINETES DE CASQUILLO (10) Y UN ELEMENTO ELECTRICO (22) EN SU INTERIOR, QUE SE UNE POR MEDIO DE UN YUGO (12) CON UNA PALANCA DE ACCIONAMIENTO (15). CON LA PALANCA, EL PILOTO PUEDE MOVER LOS DESLIZADORES SOBRE LOS EJES Y CONTROLAR EL MANDO DE GASES DEL MOTOR. EN EL FONDO DE LA ESTRUCTURA METALICA SE MONTA UN CONECTOR ELECTRICO HEMBRA (20) QUE REVIBE UN ENCHUFE MACHO Y CONECTA LA UNIDAD CON LA CIRCUITERIA NECESARIA.
ES500327A 1980-03-15 1981-03-13 Aparato de control utilizable particularmente en aviacion. Expired ES8206333A1 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8008846 1980-03-15
GB8031102 1980-09-26

Publications (2)

Publication Number Publication Date
ES500327A0 ES500327A0 (es) 1982-08-16
ES8206333A1 true ES8206333A1 (es) 1982-08-16

Family

ID=26274841

Family Applications (1)

Application Number Title Priority Date Filing Date
ES500327A Expired ES8206333A1 (es) 1980-03-15 1981-03-13 Aparato de control utilizable particularmente en aviacion.

Country Status (9)

Country Link
US (1) US4494061A (es)
CA (1) CA1189047A (es)
DE (1) DE3109780A1 (es)
ES (1) ES8206333A1 (es)
FR (1) FR2478021B1 (es)
GB (1) GB2073887B (es)
IT (1) IT1142347B (es)
NL (1) NL8101246A (es)
SE (1) SE449844B (es)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58132812A (ja) * 1982-01-22 1983-08-08 ブリテイツシユ・エアロスペイス・パブリツク・リミテツド・カンパニ− 制御装置
DE3382431D1 (de) * 1982-01-22 1991-11-14 British Aerospace Steuerungsgeraet.
EP0265738B1 (en) * 1982-01-22 1991-10-09 British Aerospace Public Limited Company Control apparatus
SE431433B (sv) * 1982-06-01 1984-02-06 Saab Scania Ab Spakenhet med flera funktioner
GB8321376D0 (en) * 1983-08-09 1983-09-28 British Aerospace Control apparatus
GB8801951D0 (en) * 1988-01-29 1988-02-24 British Aerospace Control apparatus
GB8908012D0 (en) * 1989-04-10 1989-09-20 British Aerospace Acceleration-sensitive friction device
US5199535A (en) * 1989-04-10 1993-04-06 British Aerospace Public Limited Company Acceleration-sensitive friction device
US5076517A (en) * 1989-08-14 1991-12-31 United Technologies Corporation Programmable, linear collective control system for a helicopter
GB8919453D0 (en) * 1989-08-26 1990-05-30 British Aerospace Control apparatus
US5797564A (en) * 1995-05-15 1998-08-25 The Boeing Company System for backdrive of flight deck controls during autopilot operation
DE19926800A1 (de) * 1999-06-11 2000-12-14 Wittenstein Gmbh & Co Kg Vorrichtung zum Steuern eines Triebwerkes
DE19926563A1 (de) * 1999-06-11 2000-12-14 Wittenstein Gmbh & Co Kg Vorrichtung zum Steuern eines Triebwerkes
DE10208504A1 (de) * 2002-02-27 2003-09-04 Siemens Ag Fahrpedaleinheit
DE10310717A1 (de) * 2003-03-10 2004-09-23 Wittenstein Ag Vorrichtung zum Steuern eines Fahrzeuges
WO2006032928A1 (en) * 2004-04-27 2006-03-30 Bae Systems Plc Control apparatus
US7742846B2 (en) * 2006-06-02 2010-06-22 Sikorsky Aircraft Corporation Surface contact override landing scheme for a FBW rotary-wing aircraft
FR3014844A1 (fr) * 2013-12-12 2015-06-19 Airbus Operations Sas Dispositif de commande de gaz pour aeronef, comprenant un bras de commande concu pour etre extrait vers l'arriere de son boitier, en fonction de la puissance desiree
GB2549271B (en) * 2016-04-11 2021-07-14 Bae Systems Plc An aircraft
DE102016114576B4 (de) 2016-08-05 2021-07-01 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugzeug mit einer mechanischen primären Flugsteuereinrichtung und einer elektrischen Flugstabilisierungseinrichtung
GB2583464A (en) 2019-04-18 2020-11-04 Airbus Operations Ltd System and method for landing gear retraction

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1119236A (fr) * 1954-12-29 1956-06-18 Sfena Dispositif de sensations artificielles pour le pilotage des aérodynes
DE1261581B (de) * 1963-06-11 1968-02-22 Bodenseewerk Perkin Elmer Co Steuerknueppelanordnung, insbesondere fuer Flugzeugsteuerungen, bei welcher die Lage des Steuerknueppels elektromagnetisch abgetastet wird
SE332899B (es) * 1968-09-13 1971-02-22 Jungner Instrument Ab
US3832610A (en) * 1972-09-08 1974-08-27 Fujitsu Ltd Pulse operated surface motor
DE2309750B2 (de) * 1973-02-27 1976-08-05 Siemens AG, 1000 Berlin und 8000 München Vorrichtung zum antrieb von schreiboder druckerwagen in datenschreibern
US3771037A (en) * 1973-03-15 1973-11-06 Nasa Solid state controller three-axes controller
JPS591057B2 (ja) * 1979-04-18 1984-01-10 パイオニア株式会社 リニアモ−タ
US4283764A (en) * 1979-10-12 1981-08-11 Nordson Corporation Manually programmable robot with power-assisted motion during programming
US4367532A (en) * 1979-10-12 1983-01-04 Nordson Corporation Manually programmable robot with power-assisted motion during programming
US4359677A (en) * 1981-03-02 1982-11-16 Dennon Jack D Linear indexer

Also Published As

Publication number Publication date
FR2478021A1 (fr) 1981-09-18
GB2073887B (en) 1984-04-26
DE3109780A1 (de) 1982-01-14
ES500327A0 (es) 1982-08-16
SE8101601L (sv) 1981-09-16
CA1189047A (en) 1985-06-18
NL8101246A (nl) 1981-10-01
IT8148020A0 (it) 1981-03-13
US4494061A (en) 1985-01-15
SE449844B (sv) 1987-05-25
IT1142347B (it) 1986-10-08
GB2073887A (en) 1981-10-21
FR2478021B1 (fr) 1986-02-28

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