IL174977A0 - Exhaust nozzle for an engine of a flying craft - Google Patents

Exhaust nozzle for an engine of a flying craft

Info

Publication number
IL174977A0
IL174977A0 IL174977A IL17497706A IL174977A0 IL 174977 A0 IL174977 A0 IL 174977A0 IL 174977 A IL174977 A IL 174977A IL 17497706 A IL17497706 A IL 17497706A IL 174977 A0 IL174977 A0 IL 174977A0
Authority
IL
Israel
Prior art keywords
engine
exhaust nozzle
flying craft
craft
flying
Prior art date
Application number
IL174977A
Other versions
IL174977A (en
Original Assignee
Snecma
Beutin Bruno
Fert Jeremy
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 Snecma, Beutin Bruno, Fert Jeremy filed Critical Snecma
Publication of IL174977A0 publication Critical patent/IL174977A0/en
Publication of IL174977A publication Critical patent/IL174977A/en

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
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • 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
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/006—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only
    • 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
    • F02K1/38—Introducing air inside the jet
    • 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
    • F02K1/40—Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet
    • 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • F02K1/825—Infrared radiation suppressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/12—Two-dimensional rectangular

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
  • Toys (AREA)
  • Supercharger (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Exhaust-Gas Circulating Devices (AREA)
  • Testing Of Engines (AREA)
IL174977A 2005-04-14 2006-04-11 Exhaust nozzle for an engine of a flying craft IL174977A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0503716A FR2884560B1 (en) 2005-04-14 2005-04-14 EJECTION TUBE OF A FLYING ENGINE ENGINE

Publications (2)

Publication Number Publication Date
IL174977A0 true IL174977A0 (en) 2006-08-20
IL174977A IL174977A (en) 2010-04-29

Family

ID=35124629

Family Applications (1)

Application Number Title Priority Date Filing Date
IL174977A IL174977A (en) 2005-04-14 2006-04-11 Exhaust nozzle for an engine of a flying craft

Country Status (7)

Country Link
EP (1) EP1712769B1 (en)
JP (1) JP4711876B2 (en)
CA (1) CA2542717C (en)
DE (1) DE602006001423D1 (en)
FR (1) FR2884560B1 (en)
IL (1) IL174977A (en)
RU (1) RU2374478C2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103899432A (en) * 2014-03-31 2014-07-02 西北工业大学 Improved pneumatic vectoring nozzle structure with function of injecting double secondary flow branches
GB2615794A (en) * 2022-02-18 2023-08-23 Bae Systems Plc Exhaust nozzle

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3048974A (en) * 1952-04-23 1962-08-14 Snecma Jet deflecting device for jet propulsion units
GB744196A (en) * 1953-08-12 1956-02-01 Rolls Royce Improvements in or relating to silencing means
US3239150A (en) * 1961-11-29 1966-03-08 Continental Aviat & Eng Corp Thrust vector control
FR1456926A (en) * 1965-09-17 1966-07-08 Bertin & Cie Improvements made to fluid deflection devices and their application at dilution
US5435489A (en) * 1994-01-13 1995-07-25 Bell Helicopter Textron Inc. Engine exhaust gas deflection system
US6679048B1 (en) * 2000-10-24 2004-01-20 Lockheed Martin Corporation Apparatus and method for controlling primary fluid flow using secondary fluid flow injection

Also Published As

Publication number Publication date
CA2542717C (en) 2013-10-22
EP1712769A1 (en) 2006-10-18
DE602006001423D1 (en) 2008-07-24
IL174977A (en) 2010-04-29
RU2374478C2 (en) 2009-11-27
RU2006112319A (en) 2007-11-20
JP2006290341A (en) 2006-10-26
CA2542717A1 (en) 2006-10-14
EP1712769B1 (en) 2008-06-11
FR2884560A1 (en) 2006-10-20
FR2884560B1 (en) 2007-05-25
JP4711876B2 (en) 2011-06-29

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Legal Events

Date Code Title Description
FF Patent granted
MM9K Patent not in force due to non-payment of renewal fees
NE Application for restoration - patent lapsed through non-payment of renewal fees (section 60, patents law, 5727-1967)
KB Patent renewed
KB Patent renewed