IL62132A0 - Inlet cowl for a two-dimensional inlet - Google Patents

Inlet cowl for a two-dimensional inlet

Info

Publication number
IL62132A0
IL62132A0 IL62132A IL6213281A IL62132A0 IL 62132 A0 IL62132 A0 IL 62132A0 IL 62132 A IL62132 A IL 62132A IL 6213281 A IL6213281 A IL 6213281A IL 62132 A0 IL62132 A0 IL 62132A0
Authority
IL
Israel
Prior art keywords
inlet
dimensional
cowl
inlet cowl
dimensional inlet
Prior art date
Application number
IL62132A
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 IL62132A0 publication Critical patent/IL62132A0/en

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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • 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)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Filtering Of Dispersed Particles In Gases (AREA)
IL62132A 1980-02-26 1981-02-13 Inlet cowl for a two-dimensional inlet IL62132A0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12499580A 1980-02-26 1980-02-26

Publications (1)

Publication Number Publication Date
IL62132A0 true IL62132A0 (en) 1981-03-31

Family

ID=22417761

Family Applications (1)

Application Number Title Priority Date Filing Date
IL62132A IL62132A0 (en) 1980-02-26 1981-02-13 Inlet cowl for a two-dimensional inlet

Country Status (6)

Country Link
JP (1) JPS56143315A (en)
DE (1) DE3106644A1 (en)
FR (1) FR2476743A1 (en)
GB (1) GB2070139B (en)
IL (1) IL62132A0 (en)
IT (1) IT1212501B (en)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4763858A (en) * 1986-02-05 1988-08-16 Grumman Aerospace Corporation Deflectable jet engine inlet
DE3720318A1 (en) * 1987-06-19 1989-01-05 Mtu Muenchen Gmbh GONDOLA FOR JET ENGINES
FR2680831A1 (en) * 1991-08-28 1993-03-05 Gen Electric PROCESS FOR ESTABLISHING THE ENTRY PROFILE OF THE NACELLE OF AN AIRPLANE GAS TURBINE ENGINE AND INTAKE OF THE NACELLE AS WELL AS NACELLE OBTAINED USING THIS PROCESS.
FR2763098B1 (en) * 1997-05-07 1999-06-11 Snecma AIR INTAKE SYSTEM IN A TURBOMACHINE VEIN
EP1478569B1 (en) 2002-01-30 2009-09-23 Gulfstream Aerospace Corporation Fuselage shaping and inclusion of spike on a supersonic aircraft for controlling and reducing sonic boom
DE10361722B4 (en) * 2003-12-30 2009-06-10 Airbus Deutschland Gmbh Ram air duct for ambient air supply in an aircraft
WO2008045108A2 (en) 2005-12-15 2008-04-17 Gulfstream Aerospace Corporation Isentropic compression inlet for supersonic aircraft
US8393158B2 (en) 2007-10-24 2013-03-12 Gulfstream Aerospace Corporation Low shock strength inlet
CN102748135B (en) * 2012-07-29 2013-12-25 西北工业大学 Method for designing fixed-geometry two-dimensional mixed-compression type supersonic velocity air inlet channel
CN102828832B (en) * 2012-08-14 2014-05-14 西北工业大学 Method for improving starting capability of fixed-geometry two-dimensional mixed-compression inlet
CN105156212B (en) * 2015-10-09 2017-08-29 西北工业大学 A kind of rocket based combined cycle engine becomes geometry Sidewall-compression inlet
RU2677828C1 (en) * 2018-01-19 2019-01-21 Федеральное государственное бюджетное образовательное учреждение высшего образования Иркутский государственный университет путей сообщения (ФГБОУ ВО ИрГУПС) Onboard device of engine protection against ingress of foreign objects
RU2677841C1 (en) * 2018-01-19 2019-01-21 Федеральное государственное бюджетное образовательное учреждение высшего образования Иркутский государственный университет путей сообщения (ФГБОУ ВО ИрГУПС) On-board device for engine protection from ingress of foreign objects
CN110043367A (en) * 2019-04-22 2019-07-23 南京航空航天大学 A kind of super/hypersonic inlet of side plate openings
CN110486168B (en) * 2019-09-18 2020-07-28 南京航空航天大学 Binary supersonic inlet duct with step type side plate
CN113247279B (en) * 2021-06-30 2022-06-07 中国人民解放军国防科技大学 Scheme for realizing separation of hypersonic air inlet duct fairing by utilizing gap flow
CN113247276B (en) * 2021-06-30 2022-06-07 中国人民解放军国防科技大学 Two-stage pneumatic separation type hypersonic air inlet duct fairing
CN115585062B (en) * 2022-09-15 2023-06-20 南京航空航天大学 Air inlet channel based on oscillation type Ramp type vortex generator capable of adjusting frequency

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699906A (en) * 1949-10-25 1955-01-18 Northrop Aircraft Inc Air inlet for airplane gaseous combustion turbine engines
US3430640A (en) * 1964-02-17 1969-03-04 Gen Electric Supersonic inlet
GB1166733A (en) * 1967-02-14 1969-10-08 Minster Of Technology London Aircraft Engine Intake Ducts
SE318194B (en) * 1968-06-24 1969-12-01 Saab Ab
DE1944472A1 (en) * 1969-09-02 1971-03-18 Messerschmitt Boelkow Blohm Double-walled closure flap for an auxiliary inlet opening of a jet engine
US3664612A (en) * 1969-12-22 1972-05-23 Boeing Co Aircraft engine variable highlight inlet
US3955782A (en) * 1973-07-11 1976-05-11 Rolls-Royce (1971) Limited Turbine engines
GB1479023A (en) * 1975-07-28 1977-07-06 Secr Defence Aircraft engine intakes

Also Published As

Publication number Publication date
JPS56143315A (en) 1981-11-09
IT8119945A0 (en) 1981-02-24
IT1212501B (en) 1989-11-22
GB2070139A (en) 1981-09-03
DE3106644A1 (en) 1982-01-07
FR2476743A1 (en) 1981-08-28
GB2070139B (en) 1983-06-22

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