IT1186010B - Motore a ciclo variabile - Google Patents

Motore a ciclo variabile

Info

Publication number
IT1186010B
IT1186010B IT22560/85A IT2256085A IT1186010B IT 1186010 B IT1186010 B IT 1186010B IT 22560/85 A IT22560/85 A IT 22560/85A IT 2256085 A IT2256085 A IT 2256085A IT 1186010 B IT1186010 B IT 1186010B
Authority
IT
Italy
Prior art keywords
cycle engine
variable cycle
variable
engine
cycle
Prior art date
Application number
IT22560/85A
Other languages
English (en)
Other versions
IT8522560A0 (it
Inventor
Frank Andrew Schweiger
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT8522560A0 publication Critical patent/IT8522560A0/it
Application granted granted Critical
Publication of IT1186010B publication Critical patent/IT1186010B/it

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
    • F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
    • 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)
  • Valve-Gear Or Valve Arrangements (AREA)
  • Valve Device For Special Equipments (AREA)
IT22560/85A 1984-10-22 1985-10-21 Motore a ciclo variabile IT1186010B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US66351184A 1984-10-22 1984-10-22

Publications (2)

Publication Number Publication Date
IT8522560A0 IT8522560A0 (it) 1985-10-21
IT1186010B true IT1186010B (it) 1987-11-18

Family

ID=24662129

Family Applications (1)

Application Number Title Priority Date Filing Date
IT22560/85A IT1186010B (it) 1984-10-22 1985-10-21 Motore a ciclo variabile

Country Status (5)

Country Link
JP (1) JPS61101658A (it)
DE (1) DE3536549A1 (it)
FR (1) FR2572136A1 (it)
GB (1) GB2165892B (it)
IT (1) IT1186010B (it)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3932791A1 (de) * 1989-09-30 1991-04-11 Mtu Muenchen Gmbh Gasturbinenstrahltriebwerk mit mindestens einem axial verfahrbar angeordneten schieber
US5201801A (en) * 1991-06-04 1993-04-13 General Electric Company Aircraft gas turbine engine particle separator
US5261227A (en) * 1992-11-24 1993-11-16 General Electric Company Variable specific thrust turbofan engine
US5345760A (en) * 1993-02-05 1994-09-13 General Electric Company Turboprop booster
DE4403469A1 (de) * 1994-02-04 1994-07-21 Alexander Schaefer Auf Düsen-oder-Raketenantrieb in dem wird verwendet Schubdüse mit bestimmten gekrümmten Trajektorie Ausstrahlung des Gases, auf einen Beschleunigungsprinzip nach dem wird der Strom beschleunigt mit Hilfe einer Bewegung nach bestimmten gekrümmten Trajektorie
GB2308866B (en) * 1996-01-04 1999-09-08 Rolls Royce Plc Ducted fan gas turbine engine with secondary duct
JPWO2005085620A1 (ja) * 2004-03-02 2008-01-24 根本　勇 亜音速機推進用可変サイクルエンジン
US20070000232A1 (en) * 2005-06-29 2007-01-04 General Electric Company Gas turbine engine and method of operating same
GB201412189D0 (en) 2014-07-09 2014-08-20 Rolls Royce Plc A nozzle arrangement for a gas turbine engine
RU2730562C1 (ru) * 2019-11-21 2020-08-24 Публичное Акционерное Общество "Одк-Сатурн" Винтовентиляторный газотурбинный двигатель
US20210262416A1 (en) * 2020-02-20 2021-08-26 General Electric Company Turbofan engine with core exhaust and bypass flow mixing
US11781506B2 (en) * 2020-06-03 2023-10-10 Rtx Corporation Splitter and guide vane arrangement for gas turbine engines
CN115263598B (zh) * 2022-07-28 2024-11-19 北京航空航天大学 一种双变涵道、宽速域、高通流变循环发动机构型
US12065937B1 (en) 2023-12-22 2024-08-20 Rtx Corporation Variable area nozzle assembly for an aircraft propulsion system

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB633695A (en) * 1946-02-15 1949-12-19 Louis Breguet Rotary propeller
GB711846A (en) * 1950-01-26 1954-07-14 Rateau Soc Control device for gas turbine aircraft propulsion units
GB832641A (en) * 1956-12-28 1960-04-13 Power Jets Res & Dev Ltd Jet propulsion power plant
GB871016A (en) * 1957-06-12 1961-06-21 Power Jets Res & Dev Ltd Gas turbine jet propulsion engines
FR1373227A (fr) * 1962-09-03 1964-09-25 Bristol Siddeley Engines Ltd Perfectionnements apportés aux moteurs de propulsion par réaction
US4043121A (en) * 1975-01-02 1977-08-23 General Electric Company Two-spool variable cycle engine
GB1535765A (en) * 1975-01-02 1978-12-13 Gen Electric Variable cycle turbofan engines
US4069661A (en) * 1975-06-02 1978-01-24 The United States Of America As Represented By The United States National Aeronautics And Space Administration Variable mixer propulsion cycle
US4068471A (en) * 1975-06-16 1978-01-17 General Electric Company Variable cycle engine with split fan section
US4039146A (en) * 1975-12-01 1977-08-02 General Electric Company Variable cycle plug nozzle and flap and method of operating same
US4142365A (en) * 1976-11-01 1979-03-06 General Electric Company Hybrid mixer for a high bypass ratio gas turbofan engine
US4175384A (en) * 1977-08-02 1979-11-27 General Electric Company Individual bypass injector valves for a double bypass variable cycle turbofan engine
US4254619A (en) * 1978-05-01 1981-03-10 General Electric Company Partial span inlet guide vane for cross-connected engines

Also Published As

Publication number Publication date
GB8522330D0 (en) 1985-10-16
GB2165892A (en) 1986-04-23
JPS61101658A (ja) 1986-05-20
IT8522560A0 (it) 1985-10-21
GB2165892B (en) 1988-10-26
FR2572136A1 (fr) 1986-04-25
DE3536549A1 (de) 1986-04-24

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