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DE602006000051D1 - Triebwerkslärm - Google Patents

Triebwerkslärm

Info

Publication number
DE602006000051D1
DE602006000051D1 DE602006000051T DE602006000051T DE602006000051D1 DE 602006000051 D1 DE602006000051 D1 DE 602006000051D1 DE 602006000051 T DE602006000051 T DE 602006000051T DE 602006000051 T DE602006000051 T DE 602006000051T DE 602006000051 D1 DE602006000051 D1 DE 602006000051D1
Authority
DE
Germany
Prior art keywords
engine noise
noise
engine
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
DE602006000051T
Other languages
English (en)
Other versions
DE602006000051T2 (de
Inventor
Rory Douglas Stieger
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of DE602006000051D1 publication Critical patent/DE602006000051D1/de
Application granted granted Critical
Publication of DE602006000051T2 publication Critical patent/DE602006000051T2/de
Anticipated expiration legal-status Critical
Active legal-status Critical Current

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
    • F02K1/46Nozzles 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
    • F02K1/48Corrugated nozzles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • B64D33/06Silencing exhaust or propulsion jets
    • 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
    • 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
    • F02K1/78Other construction of jet pipes
    • F02K1/82Jet pipe walls, e.g. liners
    • F02K1/827Sound absorbing structures or liners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/10Stators
    • F05D2240/12Fluid guiding means, e.g. vanes
    • F05D2240/127Vortex generators, turbulators, or the like, for mixing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/96Preventing, counteracting or reducing vibration or noise
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Nozzles (AREA)
  • Fuel-Injection Apparatus (AREA)
DE602006000051T 2005-03-15 2006-03-02 Triebwerkslärm Active DE602006000051T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0505246 2005-03-15
GBGB0505246.9A GB0505246D0 (en) 2005-03-15 2005-03-15 Engine noise

Publications (2)

Publication Number Publication Date
DE602006000051D1 true DE602006000051D1 (de) 2007-09-13
DE602006000051T2 DE602006000051T2 (de) 2007-11-22

Family

ID=34509061

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006000051T Active DE602006000051T2 (de) 2005-03-15 2006-03-02 Triebwerkslärm

Country Status (4)

Country Link
US (1) US7735601B1 (de)
EP (1) EP1703114B1 (de)
DE (1) DE602006000051T2 (de)
GB (1) GB0505246D0 (de)

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EP2064433B1 (de) * 2006-10-12 2013-11-20 United Technologies Corporation Gasturbinentriebwerksystem und zugehöriges Steuerungsverfahren eines Nebenstroms
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US7966826B2 (en) 2007-02-14 2011-06-28 The Boeing Company Systems and methods for reducing noise from jet engine exhaust
US8727267B2 (en) * 2007-05-18 2014-05-20 United Technologies Corporation Variable contraction ratio nacelle assembly for a gas turbine engine
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US9228534B2 (en) 2007-07-02 2016-01-05 United Technologies Corporation Variable contour nacelle assembly for a gas turbine engine
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US8186942B2 (en) * 2007-12-14 2012-05-29 United Technologies Corporation Nacelle assembly with turbulators
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US20130255796A1 (en) * 2012-03-30 2013-10-03 General Electric Company Flow-control device, component having a flow-control device, and method of producing a flow-control device
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US20140083079A1 (en) * 2012-09-26 2014-03-27 United Technologies Corporation Geared turbofan primary and secondary nozzle integration geometry
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EP2837795B1 (de) * 2013-08-14 2019-05-01 Ansaldo Energia IP UK Limited Verbesserte Ansauganordnung in Gasturbinenkraftwerk
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FR3010454B1 (fr) * 2013-09-10 2024-02-16 Snecma Arriere corps de turboreacteur a flux melanges comportant un melangeur a lobes et des chevrons a surface interne non axisymetrique
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CN105464838B (zh) * 2014-09-25 2019-05-21 波音公司 用于被动推力导向和羽流偏转的方法和装置
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FR3070186B1 (fr) * 2017-08-21 2021-06-11 Safran Aircraft Engines Tuyere secondaire modifiee acoustique
FR3095675B1 (fr) * 2019-05-03 2021-04-09 Safran Aircraft Engines Mélangeur à flux séparés de turbomachine
CN110410230B (zh) * 2019-08-07 2020-09-25 北京航空航天大学 一种变循环发动机中的鳞片式整体变形后涵道引射器
CN110448772B (zh) * 2019-09-20 2021-09-14 成都市第二人民医院 基于呼吸科用的深入精准给药装置及给药方法
US11674435B2 (en) 2021-06-29 2023-06-13 General Electric Company Levered counterweight feathering system
US11795964B2 (en) 2021-07-16 2023-10-24 General Electric Company Levered counterweight feathering system
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Also Published As

Publication number Publication date
EP1703114B1 (de) 2007-08-01
US20100170261A1 (en) 2010-07-08
EP1703114A1 (de) 2006-09-20
GB0505246D0 (en) 2005-04-20
DE602006000051T2 (de) 2007-11-22
US7735601B1 (en) 2010-06-15

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Legal Events

Date Code Title Description
8381 Inventor (new situation)

Inventor name: STRANGE, PAUL JONATHAN RAILTON, DUFFIELD, DERB, GB

Inventor name: STIEGER, RORY DOUGLAS, DERBY, GB

Inventor name: BRITCHFORD, KEVIN MARK, LOUGHBOROUGH, LEICESTE, GB

8364 No opposition during term of opposition