CA942408A - Integrated control for a turbopropulsion system - Google Patents

Integrated control for a turbopropulsion system

Info

Publication number
CA942408A
CA942408A CA138,725A CA138725A CA942408A CA 942408 A CA942408 A CA 942408A CA 138725 A CA138725 A CA 138725A CA 942408 A CA942408 A CA 942408A
Authority
CA
Canada
Prior art keywords
turbopropulsion
integrated control
integrated
control
turbopropulsion system
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
CA138,725A
Other versions
CA138725S (en
Inventor
William L. Webb
Thomas R. Warwick
Ronald D. Hackney
Robert L. Price
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 Aircraft 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
Application filed by United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of CA942408A publication Critical patent/CA942408A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CA138,725A 1971-04-28 1972-03-30 Integrated control for a turbopropulsion system Expired CA942408A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13816371A 1971-04-28 1971-04-28

Publications (1)

Publication Number Publication Date
CA942408A true CA942408A (en) 1974-02-19

Family

ID=22480733

Family Applications (1)

Application Number Title Priority Date Filing Date
CA138,725A Expired CA942408A (en) 1971-04-28 1972-03-30 Integrated control for a turbopropulsion system

Country Status (4)

Country Link
CA (1) CA942408A (en)
DE (1) DE2220832A1 (en)
FR (1) FR2134717A1 (en)
GB (1) GB1363956A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3848636A (en) * 1972-09-15 1974-11-19 Bendix Corp Control apparatus particularly for a plurality of compressor bleed valves of a gas turbine engine
EP1444428B1 (en) * 2001-11-15 2009-01-07 Goodrich Pump & Engine Control Systems, Inc. Method and system for preventing surge events in a gas turbine engine

Also Published As

Publication number Publication date
FR2134717A1 (en) 1972-12-08
GB1363956A (en) 1974-08-21
DE2220832A1 (en) 1972-11-09

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