IT8619848A1 - Metodo e apparato per controllare aerei a motori multipli - Google Patents

Metodo e apparato per controllare aerei a motori multipli

Info

Publication number
IT8619848A1
IT8619848A1 IT1986A19848A IT1984886A IT8619848A1 IT 8619848 A1 IT8619848 A1 IT 8619848A1 IT 1986A19848 A IT1986A19848 A IT 1986A19848A IT 1984886 A IT1984886 A IT 1984886A IT 8619848 A1 IT8619848 A1 IT 8619848A1
Authority
IT
Italy
Prior art keywords
engine aircraft
controlling multi
controlling
aircraft
engine
Prior art date
Application number
IT1986A19848A
Other languages
English (en)
Other versions
IT1188600B (it
IT8619848A0 (it
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT8619848A0 publication Critical patent/IT8619848A0/it
Publication of IT8619848A1 publication Critical patent/IT8619848A1/it
Application granted granted Critical
Publication of IT1188600B publication Critical patent/IT1188600B/it

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
IT19848/86A 1985-03-25 1986-03-24 Metodo e apparato per controllare aerei a motori multipli IT1188600B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/715,569 US4787201A (en) 1985-03-25 1985-03-25 Method and apparatus for controlling multiple engine aircraft

Publications (3)

Publication Number Publication Date
IT8619848A0 IT8619848A0 (it) 1986-03-24
IT8619848A1 true IT8619848A1 (it) 1987-09-24
IT1188600B IT1188600B (it) 1988-01-20

Family

ID=24874594

Family Applications (1)

Application Number Title Priority Date Filing Date
IT19848/86A IT1188600B (it) 1985-03-25 1986-03-24 Metodo e apparato per controllare aerei a motori multipli

Country Status (6)

Country Link
US (1) US4787201A (it)
JP (1) JPS61253298A (it)
DE (1) DE3609457A1 (it)
FR (1) FR2579172B1 (it)
GB (1) GB2172860B (it)
IT (1) IT1188600B (it)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4991393A (en) * 1986-05-15 1991-02-12 Trw Inc. Spacecraft guidance and control system
EP2151730A1 (en) * 2008-08-05 2010-02-10 The Boeing Company Four-dimensional navigation of an aircraft
FR2938302B1 (fr) * 2008-11-13 2010-12-31 Snecma Dispositif d'ajustement d'une variable de fonctionnement d'un moteur
JP5123964B2 (ja) 2010-02-26 2013-01-23 三菱重工業株式会社 航空機の制御システム、航空機の制御方法、及び航空機
US9889944B2 (en) * 2013-08-28 2018-02-13 United Technologies Corporation Multi-engine aircraft thrust balancing
US10005561B2 (en) * 2016-06-16 2018-06-26 Ge Aviation Systems Llc Controlling aircraft using thrust differential trim
DE102019205152A1 (de) * 2019-04-10 2020-10-15 Rolls-Royce Deutschland Ltd & Co Kg Elektrisches Antriebssystem für ein Flugzeug mit minimalem Giermoment

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2737015A (en) * 1948-05-07 1956-03-06 Pratt & Whitney Co Inc Jet engine control
US3120359A (en) * 1959-11-04 1964-02-04 Lester E Sprecher Aircraft with equi-spaced power plants
US3286143A (en) * 1962-07-31 1966-11-15 Aircraft Radio Corp Autopilot for maintaining attitude and heading including rate integration and memorymeans
US3231223A (en) * 1962-11-16 1966-01-25 Thiokol Chemical Corp Flight attitude control system
US3218800A (en) * 1963-06-27 1965-11-23 Holley Carburetor Co Reaction control valve and system
US3311130A (en) * 1963-10-25 1967-03-28 Marquardt Corp Thrust vectoring system and control valve therefor
US3304721A (en) * 1964-09-08 1967-02-21 George U Oppel Aircraft thrust vector control assembly
US3515361A (en) * 1966-09-12 1970-06-02 Albert W Blackburn Control of aircraft by deflection of propulsion gases
JPS5327559A (en) * 1976-08-17 1978-03-14 Mitsubishi Chem Ind Soil conditioner

Also Published As

Publication number Publication date
IT1188600B (it) 1988-01-20
FR2579172A1 (fr) 1986-09-26
GB2172860B (en) 1988-06-29
JPS61253298A (ja) 1986-11-11
DE3609457A1 (de) 1986-09-25
US4787201A (en) 1988-11-29
GB2172860A (en) 1986-10-01
FR2579172B1 (fr) 1989-12-22
GB8606631D0 (en) 1986-04-23
IT8619848A0 (it) 1986-03-24

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19930323