NL6711477A - - Google Patents

Info

Publication number
NL6711477A
NL6711477A NL6711477A NL6711477A NL6711477A NL 6711477 A NL6711477 A NL 6711477A NL 6711477 A NL6711477 A NL 6711477A NL 6711477 A NL6711477 A NL 6711477A NL 6711477 A NL6711477 A NL 6711477A
Authority
NL
Netherlands
Application number
NL6711477A
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
Publication of NL6711477A publication Critical patent/NL6711477A/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
NL6711477A 1966-12-22 1967-08-21 NL6711477A (xx)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US60379466A 1966-12-22 1966-12-22

Publications (1)

Publication Number Publication Date
NL6711477A true NL6711477A (xx) 1968-06-24

Family

ID=24416942

Family Applications (1)

Application Number Title Priority Date Filing Date
NL6711477A NL6711477A (xx) 1966-12-22 1967-08-21

Country Status (7)

Country Link
US (1) US3472027A (xx)
JP (1) JPS4840243B1 (xx)
BE (1) BE704187A (xx)
CH (1) CH471965A (xx)
DE (1) DE1601560A1 (xx)
GB (1) GB1184369A (xx)
NL (1) NL6711477A (xx)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1164406A (en) * 1968-06-24 1969-09-17 Rolls Royce Gas Turbine Jet Propulsion Engine
US3517509A (en) * 1968-08-26 1970-06-30 North American Rockwell Integrated aircraft propulsion control system
US3579992A (en) * 1969-01-03 1971-05-25 United Aircraft Corp Power plant variable geometry control
DE1920002A1 (de) * 1969-04-19 1970-11-12 Bodenseewerk Geraetetech Vorrichtung zur Steuerung oder Regelung der Brennstoffzufuhr bei Propeller-Turbinen-Luftstrahltriebwerken
BE755260A (fr) * 1969-11-25 1971-02-01 Gen Electric Systeme de commande du dispositif d'augmentation dans une turbine a ga
GB1519144A (en) * 1974-07-09 1978-07-26 Lucas Industries Ltd Electronic fuel control for a gas turbine engine
US4095420A (en) * 1977-04-26 1978-06-20 The United States Of America As Represented By The Secretary Of The Air Force Augmentor outer segment lockout and fan upmatch
US4292802A (en) * 1978-12-27 1981-10-06 General Electric Company Method and apparatus for increasing compressor inlet pressure
DE2930956C2 (de) * 1979-07-31 1985-07-18 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Regelungsverfahren für eine flächenverstellbare Schubdüse eines Mantelstrom-Gasturbinenstrahltriebwerks mit Nachbrenner
GB2238356B (en) * 1989-11-25 1994-04-13 Rolls Royce Plc Engine fuel control system
GB2240858B (en) * 1990-02-09 1993-08-04 Secr Defence Engine controller for reheated turbofans
US5301500A (en) * 1990-07-09 1994-04-12 General Electric Company Gas turbine engine for controlling stall margin
US20050274115A1 (en) * 2004-06-15 2005-12-15 Pearce Kevin P Method and Apparatus for Prevention of Compressor Stall and Combustion Flameout in a Turbine Engine
US8365513B2 (en) * 2006-10-12 2013-02-05 United Technologies Corporation Turbofan engine operation control
EP2064434B1 (en) * 2006-10-12 2012-06-27 United Technologies Corporation Operational line management of low pressure compressor in a turbofan engine
US7797944B2 (en) * 2006-10-20 2010-09-21 United Technologies Corporation Gas turbine engine having slim-line nacelle
FR3063782B1 (fr) * 2017-03-07 2021-06-18 Safran Aircraft Engines Procede et dispositif de detection de conditions propices a l'apparition d'un pompage en vue de proteger un compresseur d'une turbomachine d'aeronef
CN114233671B (zh) * 2021-12-21 2024-05-03 中国科学院工程热物理研究所 一种超临界二氧化碳离心式压缩机性能测试方法
GB202302422D0 (en) * 2023-02-21 2023-04-05 Rolls Royce Plc Thrust control method for an airbreathing jet engine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2641105A (en) * 1948-10-11 1953-06-09 Marquardt Aircraft Company Temperature control system having means to measure turbine inlet temperature indirectly
US2761280A (en) * 1950-08-31 1956-09-04 Daniel G Russ Fuel-air control mechanism for metering flow of fuel to afterburners in jet or turbine engines
US2693081A (en) * 1951-04-04 1954-11-02 Allen S Atkinson Apparatus for controlling gas turbine engines during transient operation
US2933887A (en) * 1953-07-16 1960-04-26 Rolls Royce Compound gas turbine engine with control for low-pressure rotor
US3041826A (en) * 1959-01-27 1962-07-03 United Aircraft Corp Turbofan afterburner fuel control
US3293847A (en) * 1963-09-13 1966-12-27 Bendix Corp Coordinated main and afterburner fuel controls for gas turbine engines
US3342031A (en) * 1965-06-23 1967-09-19 Gen Motors Corp Gas turbine fuel control
US3316713A (en) * 1965-12-27 1967-05-02 United Aircraft Corp Closed-loop fuel control for gas turbine engines

Also Published As

Publication number Publication date
CH471965A (de) 1969-04-30
GB1184369A (en) 1970-03-18
JPS4840243B1 (xx) 1973-11-29
DE1601560A1 (de) 1970-02-12
BE704187A (xx) 1968-02-01
US3472027A (en) 1969-10-14

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