SE343643B - - Google Patents

Info

Publication number
SE343643B
SE343643B SE5303/68A SE530368A SE343643B SE 343643 B SE343643 B SE 343643B SE 5303/68 A SE5303/68 A SE 5303/68A SE 530368 A SE530368 A SE 530368A SE 343643 B SE343643 B SE 343643B
Authority
SE
Sweden
Application number
SE5303/68A
Inventor
L Urban
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
Publication of SE343643B publication Critical patent/SE343643B/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F02K1/18—Control or regulation automatic
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • 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
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Control Of Turbines (AREA)
SE5303/68A 1967-04-21 1968-04-19 SE343643B (xx)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US632805A US3401524A (en) 1967-04-21 1967-04-21 Control for ducted fan engine

Publications (1)

Publication Number Publication Date
SE343643B true SE343643B (xx) 1972-03-13

Family

ID=24537015

Family Applications (1)

Application Number Title Priority Date Filing Date
SE5303/68A SE343643B (xx) 1967-04-21 1968-04-19

Country Status (5)

Country Link
US (1) US3401524A (xx)
DE (1) DE1751199B2 (xx)
FR (1) FR1567367A (xx)
GB (1) GB1184779A (xx)
SE (1) SE343643B (xx)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3517509A (en) * 1968-08-26 1970-06-30 North American Rockwell Integrated aircraft propulsion control system
US4068469A (en) * 1975-05-29 1978-01-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Variable thrust nozzle for quiet turbofan engine and method of operating same
US4294069A (en) * 1978-04-26 1981-10-13 United Technologies Corporation Exhaust nozzle control and core engine fuel control for turbofan engine
US4242864A (en) * 1978-05-25 1981-01-06 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Integrated control system for a gas turbine engine
DE2930956C2 (de) * 1979-07-31 1985-07-18 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Regelungsverfahren für eine flächenverstellbare Schubdüse eines Mantelstrom-Gasturbinenstrahltriebwerks mit Nachbrenner
EP2064434B1 (en) * 2006-10-12 2012-06-27 United Technologies Corporation Operational line management of low pressure compressor in a turbofan engine
US8387389B2 (en) * 2007-12-20 2013-03-05 Volvo Aero Corporation Gas turbine engine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3269114A (en) * 1966-08-30 Marchant etal j et propulsion engines
US2672726A (en) * 1950-09-19 1954-03-23 Bell Aircraft Corp Ducted fan jet aircraft engine
GB757981A (en) * 1952-02-06 1956-09-26 Rolls Royce Improvements in or relating to gas turbine engines
US3060680A (en) * 1957-12-30 1962-10-30 Rolls Royce By-pass gas-turbine engine and control therefor
FR1379642A (fr) * 1963-06-04 1964-11-27 Snecma Dispositif de régulation à commande unique pour turboréacteurs multiflux à postcombustion

Also Published As

Publication number Publication date
US3401524A (en) 1968-09-17
DE1751199B2 (de) 1972-07-20
FR1567367A (xx) 1969-05-16
GB1184779A (en) 1970-03-18
DE1751199A1 (de) 1970-10-22

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