FR2996258B1 - Melangeur a rotation alternative pour tuyere a flux confluents de turbomachine et son procede de pilotage - Google Patents

Melangeur a rotation alternative pour tuyere a flux confluents de turbomachine et son procede de pilotage

Info

Publication number
FR2996258B1
FR2996258B1 FR1259281A FR1259281A FR2996258B1 FR 2996258 B1 FR2996258 B1 FR 2996258B1 FR 1259281 A FR1259281 A FR 1259281A FR 1259281 A FR1259281 A FR 1259281A FR 2996258 B1 FR2996258 B1 FR 2996258B1
Authority
FR
France
Prior art keywords
turbomachine
confluent
steering process
flux tube
alternative rotation
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
FR1259281A
Other languages
English (en)
Other versions
FR2996258A1 (fr
Inventor
Norman Jodet
Guillaume Bodard
Cyprien Henry
Maxime Koenig
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SAS filed Critical SNECMA SAS
Priority to FR1259281A priority Critical patent/FR2996258B1/fr
Priority to US14/035,113 priority patent/US8881502B2/en
Priority to GB1317411.5A priority patent/GB2508699B/en
Publication of FR2996258A1 publication Critical patent/FR2996258A1/fr
Application granted granted Critical
Publication of FR2996258B1 publication Critical patent/FR2996258B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02K1/34—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 for attenuating noise
    • 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
    • F02K1/46—Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing
    • F02K1/48—Corrugated nozzles
    • 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
    • F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary 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
    • F02K1/44—Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction
    • 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)
  • Toys (AREA)
  • Control Of Turbines (AREA)
  • Mixers Of The Rotary Stirring Type (AREA)
FR1259281A 2012-10-01 2012-10-01 Melangeur a rotation alternative pour tuyere a flux confluents de turbomachine et son procede de pilotage Active FR2996258B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1259281A FR2996258B1 (fr) 2012-10-01 2012-10-01 Melangeur a rotation alternative pour tuyere a flux confluents de turbomachine et son procede de pilotage
US14/035,113 US8881502B2 (en) 2012-10-01 2013-09-24 Mixer that performs reciprocating rotary motion for a confluent-flow nozzle of a turbine engine, and a method of controlling it
GB1317411.5A GB2508699B (en) 2012-10-01 2013-10-01 A mixer that performs reciprocating rotary motion for a confluent-flow nozzle of a turbine engine, and a method of controlling it

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1259281A FR2996258B1 (fr) 2012-10-01 2012-10-01 Melangeur a rotation alternative pour tuyere a flux confluents de turbomachine et son procede de pilotage

Publications (2)

Publication Number Publication Date
FR2996258A1 FR2996258A1 (fr) 2014-04-04
FR2996258B1 true FR2996258B1 (fr) 2014-10-17

Family

ID=47295033

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1259281A Active FR2996258B1 (fr) 2012-10-01 2012-10-01 Melangeur a rotation alternative pour tuyere a flux confluents de turbomachine et son procede de pilotage

Country Status (3)

Country Link
US (1) US8881502B2 (fr)
FR (1) FR2996258B1 (fr)
GB (1) GB2508699B (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11473780B2 (en) 2018-02-26 2022-10-18 General Electric Company Engine with rotating detonation combustion system
US11320147B2 (en) 2018-02-26 2022-05-03 General Electric Company Engine with rotating detonation combustion system
US11486579B2 (en) 2018-02-26 2022-11-01 General Electric Company Engine with rotating detonation combustion system
CN113586281B (zh) * 2021-07-15 2022-08-02 哈尔滨工程大学 一种带非均匀波瓣引射混合器的船舶燃气轮机
US11828248B1 (en) * 2022-06-27 2023-11-28 Pratt & Whitney Canada Corp. Rotatably driven exhaust mixer

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3060681A (en) * 1958-03-13 1962-10-30 Rolls Royce Jet propulsion engine with adjustable nozzle
FR1547756A (fr) * 1967-10-19 1968-11-29 Snecma Silencieux pour réacteurs aéronautiques
US3514955A (en) * 1968-03-28 1970-06-02 Gen Electric Mixing structures and turbofan engines employing same
US4335573A (en) * 1970-09-02 1982-06-22 General Electric Company Gas turbine engine mixer
US3780827A (en) * 1972-12-19 1973-12-25 Nasa Gas turbine exhaust nozzle
FR2241695B1 (fr) * 1973-08-21 1978-03-17 Bertin & Cie
US4686826A (en) * 1980-05-14 1987-08-18 The United States Of America As Represented By The Secretary Of The Air Force Mixed flow augmentor incorporating a fuel/air tube
GB2372779A (en) * 2001-03-03 2002-09-04 Rolls Royce Plc Gas turbine engine nozzle with noise reducing tabs
SE527788C2 (sv) * 2004-11-05 2006-06-07 Volvo Aero Corp Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordning
GB0608093D0 (en) * 2006-04-25 2006-05-31 Short Brothers Plc Variable area exhaust nozzle
DE102006019299B3 (de) * 2006-04-26 2007-11-08 Deutsches Zentrum für Luft- und Raumfahrt e.V. Ummanteltes Turbofan-Flugzeugtriebwerk
EP2115289B1 (fr) * 2006-10-12 2015-03-25 United Technologies Corporation Moteur à turbine à gaz à tuyère de soufflante à section variable à segments rotatifs superposés
FR2934875B1 (fr) * 2008-08-06 2010-08-13 Aircelle Sa Nacelle de turboreacteur a chevrons mobiles.
US8104260B2 (en) * 2009-05-22 2012-01-31 Pratt & Whitney Canada Corp. Deswirling exhaust mixer
DE102010014910A1 (de) * 2010-04-14 2011-10-20 Rolls-Royce Deutschland Ltd & Co Kg Mischvorrichtung für ein Turbofantriebwerk
US8549834B2 (en) * 2010-10-21 2013-10-08 United Technologies Corporation Gas turbine engine with variable area fan nozzle

Also Published As

Publication number Publication date
GB201317411D0 (en) 2013-11-13
US8881502B2 (en) 2014-11-11
FR2996258A1 (fr) 2014-04-04
GB2508699B (en) 2019-11-06
GB2508699A (en) 2014-06-11
US20140090359A1 (en) 2014-04-03

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