FR941556A - Method for adjusting turbo-reactors and apparatus for implementing this method - Google Patents

Method for adjusting turbo-reactors and apparatus for implementing this method

Info

Publication number
FR941556A
FR941556A FR941556DA FR941556A FR 941556 A FR941556 A FR 941556A FR 941556D A FR941556D A FR 941556DA FR 941556 A FR941556 A FR 941556A
Authority
FR
France
Prior art keywords
reactors
implementing
turbo
adjusting
adjusting turbo
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)
Inventor
Hermann Oestrich
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 filed Critical
Application granted granted Critical
Publication of FR941556A publication Critical patent/FR941556A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/15Control or regulation
    • F02K1/16Control or regulation conjointly with another control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR941556D 1947-02-06 1947-02-06 Method for adjusting turbo-reactors and apparatus for implementing this method Expired FR941556A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR941556T 1947-02-06

Publications (1)

Publication Number Publication Date
FR941556A true FR941556A (en) 1949-01-14

Family

ID=9470175

Family Applications (1)

Application Number Title Priority Date Filing Date
FR941556D Expired FR941556A (en) 1947-02-06 1947-02-06 Method for adjusting turbo-reactors and apparatus for implementing this method

Country Status (1)

Country Link
FR (1) FR941556A (en)

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2693081A (en) * 1951-04-04 1954-11-02 Allen S Atkinson Apparatus for controlling gas turbine engines during transient operation
US2694290A (en) * 1951-07-25 1954-11-16 United Aircraft Corp Regulator for limiting compressor pressure rise
US2713767A (en) * 1949-06-30 1955-07-26 Gen Electric Fuel and variable area nozzle regulating apparatus for thermal powerplant
US2738644A (en) * 1950-04-15 1956-03-20 Gen Electric Surge control for axial flow compressors
US2743051A (en) * 1950-07-03 1956-04-24 Power Jets Res & Dev Ltd Gas turbine plant
US2763986A (en) * 1950-10-27 1956-09-25 Bendix Aviat Corp Emergency control system, regulator and computer mechanism
US2766580A (en) * 1952-07-22 1956-10-16 Westinghouse Electric Corp Gas turbine apparatus
US2774215A (en) * 1949-04-22 1956-12-18 Bendix Aviat Corp Tailpipe or afterburning control for turbojet engines
US2780424A (en) * 1951-10-19 1957-02-05 Lockheed Aircraft Corp Airplane for vertical take-off in horizontal attitude
US2780914A (en) * 1951-12-20 1957-02-12 Gen Electric Ambient pressure responsive control for fuel oxidizer and nozzle exhaust area of reaction motors
US2782595A (en) * 1952-08-29 1957-02-26 Westinghouse Electric Corp Fuel system for a gas turbine engine
US2789417A (en) * 1949-03-22 1957-04-23 Bendix Aviat Corp Tailpipe or afterburning control for turbojet engines
US2805546A (en) * 1952-01-31 1957-09-10 Gen Electric Control system having dynamic limit controls
US2811830A (en) * 1952-12-24 1957-11-05 Bronzavia Sa Automatic speed regulator for turbojet engines having a controllable nozzle
US2828606A (en) * 1950-11-18 1958-04-01 United Aircraft Corp Afterburner fuel metering device for turbojet engines
US2830436A (en) * 1952-04-26 1958-04-15 United Aircraft Corp Fuel control system for turbojet engine with afterburner
US2832193A (en) * 1948-09-04 1958-04-29 Garrett Corp Gas turbine fuel control system responsive to speed and compressor load
US2836957A (en) * 1952-06-21 1958-06-03 United Aircraft Corp Fuel control for a gas turbine power plant
US2846846A (en) * 1951-06-14 1958-08-12 Bendix Aviat Corp Fuel system for gas turbine engines having means for avoiding compressor instability
US2857739A (en) * 1951-04-06 1958-10-28 Pratt & Whitney Co Inc Control system for turbo-jet engine
US2865166A (en) * 1952-06-11 1958-12-23 Gen Motors Corp Afterburner fuel system with pump unloader
US2873754A (en) * 1952-05-02 1959-02-17 Garrett Corp Temperature compensated pneumatic governor
US2971336A (en) * 1952-03-15 1961-02-14 Bendix Corp Fuel feed and power control system for gas turbine engines having means for avoidingcompressor stall
US2989849A (en) * 1951-08-04 1961-06-27 United Aircraft Corp Fuel control system for a twin spool gas turbine power plant
EP0005135A1 (en) * 1978-04-26 1979-10-31 United Technologies Corporation Exhaust nozzle control and core engine fuel control for turbofan engine

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2832193A (en) * 1948-09-04 1958-04-29 Garrett Corp Gas turbine fuel control system responsive to speed and compressor load
US2789417A (en) * 1949-03-22 1957-04-23 Bendix Aviat Corp Tailpipe or afterburning control for turbojet engines
US2774215A (en) * 1949-04-22 1956-12-18 Bendix Aviat Corp Tailpipe or afterburning control for turbojet engines
US2713767A (en) * 1949-06-30 1955-07-26 Gen Electric Fuel and variable area nozzle regulating apparatus for thermal powerplant
US2738644A (en) * 1950-04-15 1956-03-20 Gen Electric Surge control for axial flow compressors
US2743051A (en) * 1950-07-03 1956-04-24 Power Jets Res & Dev Ltd Gas turbine plant
US2763986A (en) * 1950-10-27 1956-09-25 Bendix Aviat Corp Emergency control system, regulator and computer mechanism
US2828606A (en) * 1950-11-18 1958-04-01 United Aircraft Corp Afterburner fuel metering device for turbojet engines
US2693081A (en) * 1951-04-04 1954-11-02 Allen S Atkinson Apparatus for controlling gas turbine engines during transient operation
US2857739A (en) * 1951-04-06 1958-10-28 Pratt & Whitney Co Inc Control system for turbo-jet engine
US2846846A (en) * 1951-06-14 1958-08-12 Bendix Aviat Corp Fuel system for gas turbine engines having means for avoiding compressor instability
US2694290A (en) * 1951-07-25 1954-11-16 United Aircraft Corp Regulator for limiting compressor pressure rise
US2989849A (en) * 1951-08-04 1961-06-27 United Aircraft Corp Fuel control system for a twin spool gas turbine power plant
US2780424A (en) * 1951-10-19 1957-02-05 Lockheed Aircraft Corp Airplane for vertical take-off in horizontal attitude
US2780914A (en) * 1951-12-20 1957-02-12 Gen Electric Ambient pressure responsive control for fuel oxidizer and nozzle exhaust area of reaction motors
US2805546A (en) * 1952-01-31 1957-09-10 Gen Electric Control system having dynamic limit controls
US2971336A (en) * 1952-03-15 1961-02-14 Bendix Corp Fuel feed and power control system for gas turbine engines having means for avoidingcompressor stall
US2830436A (en) * 1952-04-26 1958-04-15 United Aircraft Corp Fuel control system for turbojet engine with afterburner
US2873754A (en) * 1952-05-02 1959-02-17 Garrett Corp Temperature compensated pneumatic governor
US2865166A (en) * 1952-06-11 1958-12-23 Gen Motors Corp Afterburner fuel system with pump unloader
US2836957A (en) * 1952-06-21 1958-06-03 United Aircraft Corp Fuel control for a gas turbine power plant
US2766580A (en) * 1952-07-22 1956-10-16 Westinghouse Electric Corp Gas turbine apparatus
US2782595A (en) * 1952-08-29 1957-02-26 Westinghouse Electric Corp Fuel system for a gas turbine engine
US2811830A (en) * 1952-12-24 1957-11-05 Bronzavia Sa Automatic speed regulator for turbojet engines having a controllable nozzle
EP0005135A1 (en) * 1978-04-26 1979-10-31 United Technologies Corporation Exhaust nozzle control and core engine fuel control for turbofan engine

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