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FR2971553B1 - REACTOR WITH REDUCED ACOUSTIC SIGNATURE - Google Patents

REACTOR WITH REDUCED ACOUSTIC SIGNATURE

Info

Publication number
FR2971553B1
FR2971553B1 FR1151066A FR1151066A FR2971553B1 FR 2971553 B1 FR2971553 B1 FR 2971553B1 FR 1151066 A FR1151066 A FR 1151066A FR 1151066 A FR1151066 A FR 1151066A FR 2971553 B1 FR2971553 B1 FR 2971553B1
Authority
FR
France
Prior art keywords
reactor
acoustic signature
reduced acoustic
reduced
signature
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
FR1151066A
Other languages
French (fr)
Other versions
FR2971553A1 (en
Inventor
Michel Aguilar
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.)
Airbus Group SAS
Original Assignee
European Aeronautic Defence and Space Company EADS France
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 European Aeronautic Defence and Space Company EADS France filed Critical European Aeronautic Defence and Space Company EADS France
Priority to FR1151066A priority Critical patent/FR2971553B1/en
Publication of FR2971553A1 publication Critical patent/FR2971553A1/en
Application granted granted Critical
Publication of FR2971553B1 publication Critical patent/FR2971553B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/28Plants 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
    • F02K1/34Plants 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38Introducing air inside the jet
    • F02K1/386Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/46Nozzles 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
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Physical Or Chemical Processes And Apparatus (AREA)
FR1151066A 2011-02-10 2011-02-10 REACTOR WITH REDUCED ACOUSTIC SIGNATURE Active FR2971553B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1151066A FR2971553B1 (en) 2011-02-10 2011-02-10 REACTOR WITH REDUCED ACOUSTIC SIGNATURE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1151066A FR2971553B1 (en) 2011-02-10 2011-02-10 REACTOR WITH REDUCED ACOUSTIC SIGNATURE

Publications (2)

Publication Number Publication Date
FR2971553A1 FR2971553A1 (en) 2012-08-17
FR2971553B1 true FR2971553B1 (en) 2015-05-29

Family

ID=44318212

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1151066A Active FR2971553B1 (en) 2011-02-10 2011-02-10 REACTOR WITH REDUCED ACOUSTIC SIGNATURE

Country Status (1)

Country Link
FR (1) FR2971553B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3009027B1 (en) * 2013-07-26 2018-04-06 Airbus Operations AIRCRAFT TURBOMACHINE ASSEMBLY WITH ATTENUATED JET NOISE.
CN103569373B (en) * 2013-11-13 2016-03-09 中国航空工业集团公司西安飞机设计研究所 The method of calculating of whirlpool oar aircraft under static state tail jet velocity field

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1157063A (en) * 1956-07-30 1958-05-27 Bertin & Cie Mufflers for engines, in particular for jet engines
US3599749A (en) * 1969-07-28 1971-08-17 Rohr Corp Jet noise control system
US6971229B2 (en) * 2003-02-26 2005-12-06 The Nordam Group, Inc. Confluent exhaust nozzle
US7870722B2 (en) * 2006-12-06 2011-01-18 The Boeing Company Systems and methods for passively directing aircraft engine nozzle flows

Also Published As

Publication number Publication date
FR2971553A1 (en) 2012-08-17

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