IT8324209A0 - Sistema di controllo per turbomotori a gas di aereo. - Google Patents

Sistema di controllo per turbomotori a gas di aereo.

Info

Publication number
IT8324209A0
IT8324209A0 IT8324209A IT2420983A IT8324209A0 IT 8324209 A0 IT8324209 A0 IT 8324209A0 IT 8324209 A IT8324209 A IT 8324209A IT 2420983 A IT2420983 A IT 2420983A IT 8324209 A0 IT8324209 A0 IT 8324209A0
Authority
IT
Italy
Prior art keywords
control system
aircraft gas
gas turbo
turbo engines
engines
Prior art date
Application number
IT8324209A
Other languages
English (en)
Inventor
Edwin William Coldewey
Leonardo Petti
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 IT8324209A0 publication Critical patent/IT8324209A0/it

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0083Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots to help an aircraft pilot in the rolling phase
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements

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)
  • Safety Devices In Control Systems (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
IT8324209A 1982-12-20 1983-12-16 Sistema di controllo per turbomotori a gas di aereo. IT8324209A0 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US45095482A 1982-12-20 1982-12-20

Publications (1)

Publication Number Publication Date
IT8324209A0 true IT8324209A0 (it) 1983-12-16

Family

ID=23790196

Family Applications (1)

Application Number Title Priority Date Filing Date
IT8324209A IT8324209A0 (it) 1982-12-20 1983-12-16 Sistema di controllo per turbomotori a gas di aereo.

Country Status (5)

Country Link
JP (1) JPS59131729A (it)
DE (1) DE3344915A1 (it)
FR (1) FR2538032A1 (it)
GB (1) GB2132384A (it)
IT (1) IT8324209A0 (it)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4655414A (en) * 1985-12-06 1987-04-07 United Technologies Corporation Preventing inadvertent downthrottling of the operative engine in a multi-engine aircraft
DE3741891A1 (de) * 1987-12-10 1989-06-22 Man Nutzfahrzeuge Gmbh Kraftfahrzeug mit umschaltautomatik fuer zwei leistungsgleiche verbrennungsmotoren
US5027769A (en) * 1989-08-25 1991-07-02 Mitsubishi Jidosha Kogya Kabushiki Kaisha Throttle valve control apparatus
US10106269B1 (en) * 2017-03-17 2018-10-23 Rockwell Collins, Inc. System and method for inadvertent engine shutdown prevention

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3106062A (en) * 1959-12-18 1963-10-08 Gen Electric Torque and power sensing and control system for gas turbine engines

Also Published As

Publication number Publication date
GB8331014D0 (en) 1983-12-29
GB2132384A (en) 1984-07-04
DE3344915A1 (de) 1984-06-20
FR2538032A1 (fr) 1984-06-22
JPS59131729A (ja) 1984-07-28

Similar Documents

Publication Publication Date Title
IT8122555A0 (it) Sistema di controllo di gioco per turbomotori a gas.
IT8119944A0 (it) Sistema ausiliario di ventilazione per turbomotori a gas.
IT8022083A0 (it) Sistema di controllo per turbomotore a gas.
IT8424116A0 (it) Sistema di raffreddamento di componenti di turbomotore a gas.
IT1131770B (it) Impianto di controllo di spinta perfezionato per un turbomotore a gas
IT8220759A0 (it) Sistema di rifornimento dicombustibile per turbina a gas.
IT8420753A0 (it) Impianto di comando per motore a turbina a gas.
IT8222204A0 (it) Per turbomotori a gas.struttura di tenuta particolarmente
GB2126382B (en) Gas turbine engine control system
IT8620137A0 (it) Sistema di controllo di aria particolarmente per motori di aereo.
IT8619250A0 (it) Sistema di controllo del combustibile per motori a turbina a gas.
IT8123662A0 (it) Impianto misuratore di coppia per turbomotori a gas, per aerei a due motori.
IT8119348A0 (it) Complesso di aspirazione per turbomotori a gas.
IT8021276A0 (it) Sistema antighiaccio per ogiva di motore a turbina a gas.
IT8025428A0 (it) Sistema di controllo di carico ciclico per turbina a gas.
IT7825923A0 (it) Sistema di controllo integrato per un turbomotore a gas.
IT8521319A0 (it) Sistema di controllo di turbomotore a gas.
IT8024211A0 (it) Sistema di controllo privo di regolatore per il combustibile di turbine a gas.
GB2121986B (en) Gas turbine engine fuel control systems
IT7919728A0 (it) Controllo di combustibile per un sistema di ricombustione di motore a turbina a gas.
IT8324209A0 (it) Sistema di controllo per turbomotori a gas di aereo.
IT8220265A0 (it) Sistema di turbina a gas.
IT8023082A0 (it) Sistema di controllo dicombustibile per un motore a turbina a gas.
IT1174123B (it) Sistema di comando per inserire e disinserire un turbocompressore a gas di scarico
IT1178575B (it) Sistema di controllo di aria particolarmente per turbomotore a gas