ES2021038B3 - Aparato de control manual para magnitud lanzada y el vector lanzado desde un angulo de una aeronave. - Google Patents

Aparato de control manual para magnitud lanzada y el vector lanzado desde un angulo de una aeronave.

Info

Publication number
ES2021038B3
ES2021038B3 ES87303597T ES87303597T ES2021038B3 ES 2021038 B3 ES2021038 B3 ES 2021038B3 ES 87303597 T ES87303597 T ES 87303597T ES 87303597 T ES87303597 T ES 87303597T ES 2021038 B3 ES2021038 B3 ES 2021038B3
Authority
ES
Spain
Prior art keywords
launched
aircraft
magnitude
angle
control device
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 - Lifetime
Application number
ES87303597T
Other languages
English (en)
Inventor
Neil John 9 Curtis
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
Application granted granted Critical
Publication of ES2021038B3 publication Critical patent/ES2021038B3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/04—Initiating means actuated personally
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G13/00—Manually-actuated control mechanisms provided with two or more controlling members and also two or more controlled members
    • 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
    • Y10T74/20012—Multiple controlled elements
    • Y10T74/20201—Control moves in two planes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Control Devices (AREA)
  • Valve Device For Special Equipments (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
ES87303597T 1986-04-29 1987-04-23 Aparato de control manual para magnitud lanzada y el vector lanzado desde un angulo de una aeronave. Expired - Lifetime ES2021038B3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB868610481A GB8610481D0 (en) 1986-04-29 1986-04-29 Control apparatus

Publications (1)

Publication Number Publication Date
ES2021038B3 true ES2021038B3 (es) 1991-10-16

Family

ID=10597053

Family Applications (1)

Application Number Title Priority Date Filing Date
ES87303597T Expired - Lifetime ES2021038B3 (es) 1986-04-29 1987-04-23 Aparato de control manual para magnitud lanzada y el vector lanzado desde un angulo de una aeronave.

Country Status (6)

Country Link
US (1) US4901952A (es)
EP (1) EP0265035B1 (es)
JP (1) JPS6322799A (es)
DE (1) DE3767276D1 (es)
ES (1) ES2021038B3 (es)
GB (1) GB8610481D0 (es)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8801951D0 (en) * 1988-01-29 1988-02-24 British Aerospace Control apparatus
US5029778A (en) * 1989-09-11 1991-07-09 The Boeing Company Throttle control system having real-time-computed thrust vs throttle position function
US5065962A (en) * 1989-12-27 1991-11-19 Rockwell International Corporation Digital power controller
IT1241178B (it) * 1990-02-16 1993-12-29 Fiat Auto Spa Sistema per il controllo di un cambio automatico per un autoveicolo del tipo comprendente un dispositivo variatore continuo.
GB9008526D0 (en) * 1990-04-17 1990-10-17 British Aerospace Control apparatus
US5768947A (en) * 1996-06-24 1998-06-23 Caterpillar Inc. Implement hand support and control
FR2903204B1 (fr) * 2006-06-30 2011-01-21 Noremat "dispositif formant support reglable de commande manuelle"
US8235330B2 (en) * 2008-03-12 2012-08-07 Usercentrix, Llc Rotational aircraft throttle interface
RU2504682C2 (ru) * 2011-08-03 2014-01-20 Федеральное государственное военное образовательное учреждение высшего профессионального образования "Военный авиационный инженерный университет" (г. Воронеж) Министерства обороны Российской Федерации Ручка управления двигателем для одновременного отклонения сопла в вертикальной и горизонтальной плоскостях
KR200469948Y1 (ko) * 2013-02-08 2013-12-02 영풍전자(주) 엔진추력조절장치
US9126677B1 (en) 2014-10-16 2015-09-08 Sydney Robert Curtis Universal multi-role aircraft protocol
EP3257745B1 (en) 2016-06-15 2019-05-29 Ratier-Figeac SAS Autopilot and manual control switching
US10301009B2 (en) 2016-08-26 2019-05-28 Kitty Hawk Corporation Aircraft hand controller with decoupled throttle
US10011348B1 (en) * 2017-05-02 2018-07-03 Kitty Hawk Corporation Vertical thrust lever
WO2023122111A1 (en) * 2021-12-23 2023-06-29 Electra Aero, Inc. System and method for controlling flight path of a blown lift aircraft

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2923502A (en) * 1949-06-28 1960-02-02 Bendix Aviat Corp Manual controller for automatic steering systems
US2787746A (en) * 1954-07-23 1957-04-02 Chance Vought Aircraft Inc Auxiliary servo control hand grip for a manually operable control lever
US3098628A (en) * 1959-10-30 1963-07-23 Hawker Aircraft Ltd Aircraft
US3599510A (en) * 1969-10-06 1971-08-17 Boeing Co Controlled device comprising alternate manual or power operators
DE2123438A1 (de) * 1970-05-14 1971-11-25 Cge Spa Hebel mit anatomischem Griff für Vielfachsteuerung
US3726497A (en) * 1971-01-15 1973-04-10 Us Federal Aviation Admin Aircraft control handles
US4130259A (en) * 1977-08-10 1978-12-19 Textron Inc. Helicopter collective lever
US4134560A (en) * 1977-09-19 1979-01-16 Messerschmidt Eugene D Helicopter control device
US4191065A (en) * 1978-02-07 1980-03-04 Beugelsdyk Anthony F Throttle twist grip
US4280371A (en) * 1979-02-05 1981-07-28 Jacob Kobelt Control lever assembly
DE3103033C2 (de) * 1981-01-30 1982-10-21 Bayerische Motoren Werke AG, 8000 München Wählhebel für ein programmgesteuertes Automatik-Getriebe, insbesondere für Kraftfahrzeuge
SE431433B (sv) * 1982-06-01 1984-02-06 Saab Scania Ab Spakenhet med flera funktioner
EP0120011B1 (en) * 1982-09-30 1989-03-01 The Boeing Company Modular multi-engine thrust control assembly
US4667909A (en) * 1985-10-10 1987-05-26 Alfred Curci Single-stick control system for helicopters

Also Published As

Publication number Publication date
JPS6322799A (ja) 1988-01-30
GB8610481D0 (en) 1986-11-26
DE3767276D1 (de) 1991-02-14
EP0265035B1 (en) 1991-01-09
US4901952A (en) 1990-02-20
EP0265035A1 (en) 1988-04-27

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