FR1105537A - Fuel supply and power control device for gas turbine engines - Google Patents

Fuel supply and power control device for gas turbine engines

Info

Publication number
FR1105537A
FR1105537A FR1105537DA FR1105537A FR 1105537 A FR1105537 A FR 1105537A FR 1105537D A FR1105537D A FR 1105537DA FR 1105537 A FR1105537 A FR 1105537A
Authority
FR
France
Prior art keywords
control device
power control
gas turbine
fuel supply
turbine engines
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
Other languages
French (fr)
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation 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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Application granted granted Critical
Publication of FR1105537A publication Critical patent/FR1105537A/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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1105537D 1953-05-27 1954-05-26 Fuel supply and power control device for gas turbine engines Expired FR1105537A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1105537XA 1953-05-27 1953-05-27

Publications (1)

Publication Number Publication Date
FR1105537A true FR1105537A (en) 1955-12-05

Family

ID=22333646

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1105537D Expired FR1105537A (en) 1953-05-27 1954-05-26 Fuel supply and power control device for gas turbine engines

Country Status (1)

Country Link
FR (1) FR1105537A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1075897B (en) * 1956-04-25 1960-02-18 United Aircraft Corp Pressure control device for maintaining a certain working gas pressure in the combustion chamber, in particular the optimal pressure, preferably for jet engines
DE1106118B (en) * 1957-12-19 1961-05-04 Habil Fritz A F Schmidt Dr Ing Fuel control device for gas turbine engines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1075897B (en) * 1956-04-25 1960-02-18 United Aircraft Corp Pressure control device for maintaining a certain working gas pressure in the combustion chamber, in particular the optimal pressure, preferably for jet engines
DE1106118B (en) * 1957-12-19 1961-05-04 Habil Fritz A F Schmidt Dr Ing Fuel control device for gas turbine engines

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