DE69017042D1 - Doppeltströmungsschalldämpfer für ein turbinentriebwerk. - Google Patents

Doppeltströmungsschalldämpfer für ein turbinentriebwerk.

Info

Publication number
DE69017042D1
DE69017042D1 DE69017042T DE69017042T DE69017042D1 DE 69017042 D1 DE69017042 D1 DE 69017042D1 DE 69017042 T DE69017042 T DE 69017042T DE 69017042 T DE69017042 T DE 69017042T DE 69017042 D1 DE69017042 D1 DE 69017042D1
Authority
DE
Germany
Prior art keywords
turbine engine
double flow
flow silencer
silencer
double
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.)
Expired - Fee Related
Application number
DE69017042T
Other languages
English (en)
Other versions
DE69017042T2 (de
Inventor
David Ross
Charles Royalty
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.)
Honeywell International Inc
Original Assignee
AlliedSignal Inc
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 AlliedSignal Inc filed Critical AlliedSignal Inc
Publication of DE69017042D1 publication Critical patent/DE69017042D1/de
Application granted granted Critical
Publication of DE69017042T2 publication Critical patent/DE69017042T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K1/78Other construction of jet pipes
    • F02K1/82Jet pipe walls, e.g. liners
    • F02K1/827Sound absorbing structures or liners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30Exhaust heads, chambers, or the like
    • 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
    • F05D2220/00Application
    • F05D2220/50Application for auxiliary power units (APU's)

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Exhaust Silencers (AREA)
  • Supercharger (AREA)
DE69017042T 1989-11-28 1990-11-15 Doppeltströmungsschalldämpfer für ein turbinentriebwerk. Expired - Fee Related DE69017042T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/442,378 US5162620A (en) 1989-11-28 1989-11-28 Dual flow turbine engine muffler
PCT/US1990/006686 WO1991008379A1 (en) 1989-11-28 1990-11-15 Dual flow turbine engine muffler

Publications (2)

Publication Number Publication Date
DE69017042D1 true DE69017042D1 (de) 1995-03-23
DE69017042T2 DE69017042T2 (de) 1995-08-10

Family

ID=23756586

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69017042T Expired - Fee Related DE69017042T2 (de) 1989-11-28 1990-11-15 Doppeltströmungsschalldämpfer für ein turbinentriebwerk.

Country Status (6)

Country Link
US (1) US5162620A (de)
EP (1) EP0502924B1 (de)
JP (1) JPH0814244B2 (de)
CA (1) CA2072118C (de)
DE (1) DE69017042T2 (de)
WO (1) WO1991008379A1 (de)

Families Citing this family (54)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1010618B1 (de) * 1996-08-02 2002-05-22 Honeywell International Inc. Integrierter Schalldämpfer und Abgasendstück für Flugzeug
US6039287A (en) 1996-08-02 2000-03-21 Alliedsignal Inc. Detachable integral aircraft tailcone and power assembly
US5916136A (en) * 1997-10-02 1999-06-29 Ettere; Mark Aspiration device for vehicle engine exhaust system
DE19818873C2 (de) * 1998-04-28 2001-07-05 Man B & W Diesel Ag Hubkolbenbrennkraftmaschine
DE19818874C2 (de) * 1998-04-28 2001-06-07 Man B & W Diesel As Kopenhagen Hubkolbenmaschine
US6220387B1 (en) * 1999-10-21 2001-04-24 Mathew S. Hoppes Exhaust muffler
CH691191A5 (de) * 2000-01-06 2001-05-15 Rudolf Ing Htl Gehring Drehverbindung auf Gleitlagerbasis.
AU2001290863A1 (en) * 2000-09-11 2002-03-26 Joseph Zelinski Exhaust system having angled baffle
DE50110932D1 (de) 2000-12-08 2006-10-19 Alstom Technology Ltd Abgassystem mit Helmholtz-Resonator
EP1356193B1 (de) 2000-12-20 2006-11-29 Quiet Storm LLC Vorrichtung zur verbesserten lärmdämpfung in einem absorptionsdämpfer einer brennkraftmaschine
US6615576B2 (en) 2001-03-29 2003-09-09 Honeywell International Inc. Tortuous path quiet exhaust eductor system
US6382347B1 (en) 2001-05-08 2002-05-07 Ghl Motorsports, L.L.C. Exhaust muffler for an internal combustion engine
US6915877B2 (en) 2003-01-13 2005-07-12 Garabed Khayalian Muffler device
US6892853B2 (en) * 2003-05-01 2005-05-17 Agency For Science Technology And Research High performance muffler
US7482705B2 (en) * 2003-05-12 2009-01-27 Piercey Iii Gerald S Generator support plenum
US7080514B2 (en) * 2003-08-15 2006-07-25 Siemens Power Generation,Inc. High frequency dynamics resonator assembly
US7292151B2 (en) * 2004-07-29 2007-11-06 Kevin Ferguson Human movement measurement system
US20060032974A1 (en) * 2004-08-16 2006-02-16 Honeywell International Inc. Modular installation kit for auxiliary power unit
US7267297B2 (en) * 2004-09-02 2007-09-11 The Boeing Company Integrated axially varying engine muffler, and associated methods and systems
US7350619B2 (en) * 2004-09-23 2008-04-01 Honeywell International, Inc. Auxiliary power unit exhaust duct with muffler incorporating an externally replaceable acoustic liner
US7364116B2 (en) * 2004-09-27 2008-04-29 The Boeing Company Automatic control systems for aircraft auxiliary power units, and associated methods
US7344107B2 (en) * 2004-10-26 2008-03-18 The Boeing Company Dual flow APU inlet and associated systems and methods
US7513119B2 (en) 2005-02-03 2009-04-07 The Boeing Company Systems and methods for starting aircraft engines
US7367424B2 (en) * 2005-02-14 2008-05-06 Honeywell International, Inc. Eccentric exhaust muffler for use with auxiliary power units
US7431125B2 (en) 2005-03-15 2008-10-07 Honeywell International Inc. Composite muffler for use with airborne auxiliary power unit
US20070039381A1 (en) * 2005-08-05 2007-02-22 Timmons Suzanne A Secondary Air Injector For Use With Exhaust Gas Simulation System
US7784283B2 (en) * 2006-05-03 2010-08-31 Rohr, Inc. Sound-absorbing exhaust nozzle center plug
US7765784B2 (en) * 2006-09-25 2010-08-03 The Boeing Company Thermally compliant APU exhaust duct arrangements and associated systems and methods
US7762374B2 (en) * 2006-11-22 2010-07-27 Honeywell International Inc. Turbine engine diffusing exhaust muffler
US20080236939A1 (en) * 2007-03-30 2008-10-02 Hamilton Sundstrand Corporation Exhaust silencer assembly
US9194293B2 (en) 2007-09-18 2015-11-24 Hamilton Sundstrand Corporation Air inlet noise attenuation assembly
US7578369B2 (en) 2007-09-25 2009-08-25 Hamilton Sundstrand Corporation Mixed-flow exhaust silencer assembly
DE102008051241B4 (de) 2008-10-10 2011-06-16 Airbus Operations Gmbh Schalldämpfer für ein Hilfstriebwerk eines Flugzeugs
US8025122B2 (en) * 2008-11-06 2011-09-27 The Boeing Company Acoustically treated exhaust centerbody for jet engines and associated methods
US8657227B1 (en) 2009-09-11 2014-02-25 The Boeing Company Independent power generation in aircraft
US8069666B1 (en) * 2010-02-25 2011-12-06 Maxim Silencers, Inc. System for generating shaft horsepower using waste heat
US8307857B2 (en) * 2010-08-04 2012-11-13 Honeywell International Inc. Insulation assembly for use with an auxiliary power unit having an exhaust muffler
CN102022222B (zh) * 2010-12-08 2013-05-29 中国商用飞机有限责任公司 消声器
US8738268B2 (en) 2011-03-10 2014-05-27 The Boeing Company Vehicle electrical power management and distribution
US8596568B2 (en) 2011-04-26 2013-12-03 Hamilton Sundstrand Corporation Exhaust silencer with baffles
US8556027B2 (en) 2011-06-28 2013-10-15 United Technologies Corporation Eductor exhaust silencer assembly with bypass gasflow
CN203585530U (zh) * 2012-09-28 2014-05-07 费希尔控制国际公司 模态衰减器
US20140174094A1 (en) * 2012-12-21 2014-06-26 United Technologies Corporation APU Exhaust Housing Perforated Ring
AT513955A1 (de) * 2013-01-16 2014-08-15 Henn Gmbh & Co Kg Schalldämpfer und Verfahren zu seiner Herstellung
US9611050B2 (en) 2013-07-26 2017-04-04 The Boeing Company Auxiliary power unit inlet apparatus and methods
US9789747B2 (en) * 2014-07-31 2017-10-17 The Boeing Company Systems and methods for duct protection of a vehicle
US10352210B2 (en) * 2014-09-09 2019-07-16 3M Innovative Properties Company Acoustic device
US9376946B1 (en) * 2015-04-02 2016-06-28 Fisher Controls International Llc Modal attenuator
US9771868B2 (en) 2015-07-21 2017-09-26 The Boeing Company Sound attenuation apparatus and method
US9587563B2 (en) 2015-07-21 2017-03-07 The Boeing Company Sound attenuation apparatus and method
DE102015214709A1 (de) * 2015-07-31 2017-02-02 Mahle International Gmbh Strömungskanal und Belüftungs-, Heizungs- oder Klimaanlage
WO2019005858A1 (en) * 2017-06-28 2019-01-03 3M Innovative Properties Company MICROPERFORATED CONDUIT
FR3109179B1 (fr) 2020-04-10 2023-05-12 Safran Aircraft Engines Grille de conduit de décharge optimisée et vanne de décharge optimisée
CN114704703B (zh) * 2022-03-15 2023-10-13 中国船舶集团有限公司第七一一研究所 水管道消声装置、消声方法及船

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1975861A (en) * 1931-07-02 1934-10-09 Oldberg Mfg Company Muffler
US2251880A (en) * 1936-04-24 1941-08-05 Hayes Ind Inc Muffler and silencer construction
US2988302A (en) * 1959-01-14 1961-06-13 Gen Sound Control Inc Silencing means for aircraft
US3286786A (en) * 1964-12-23 1966-11-22 Garrett Corp Gas turbine exhaust silencer and acoustical material therefor
US3463402A (en) * 1966-12-28 1969-08-26 United Aircraft Corp Jet sound suppressing means
US3572464A (en) * 1969-10-06 1971-03-30 Rohr Corp Method and apparatus for suppressing the noise of a fan-jet engine
RO53910A2 (de) * 1970-10-26 1973-09-20
US3726091A (en) * 1971-02-16 1973-04-10 Rohr Corp Sound suppressing apparatus
US3711013A (en) * 1971-04-26 1973-01-16 Rohr Corp Thrust control and sound apparatus
US3739984A (en) * 1971-08-25 1973-06-19 Rohr Industries Inc Thrust augmenting and south suppressing apparatus and method
US3749316A (en) * 1972-06-26 1973-07-31 Rohr Industries Inc Sound suppressing thrust augmenting apparatus
US4128769A (en) * 1976-09-27 1978-12-05 The Garrett Corporation Eductor muffler
US4240252A (en) * 1978-01-19 1980-12-23 General Electric Company Acoustically-treated mixer for a mixed flow gas turbine engine
US4433751A (en) * 1981-12-09 1984-02-28 Pratt & Whitney Aircraft Of Canada Limited Sound suppressor liner
US4747467A (en) * 1986-04-01 1988-05-31 Allied-Signal Inc. Turbine engine noise suppression apparatus and methods

Also Published As

Publication number Publication date
JPH0814244B2 (ja) 1996-02-14
CA2072118C (en) 2001-03-27
CA2072118A1 (en) 1991-05-29
JPH05501743A (ja) 1993-04-02
EP0502924B1 (de) 1995-02-15
EP0502924A1 (de) 1992-09-16
WO1991008379A1 (en) 1991-06-13
US5162620A (en) 1992-11-10
DE69017042T2 (de) 1995-08-10

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee