CA2292821A1 - Dispositif d'echappement multicanal de turbomachine traite acoustiquement - Google Patents
Dispositif d'echappement multicanal de turbomachine traite acoustiquement Download PDFInfo
- Publication number
- CA2292821A1 CA2292821A1 CA002292821A CA2292821A CA2292821A1 CA 2292821 A1 CA2292821 A1 CA 2292821A1 CA 002292821 A CA002292821 A CA 002292821A CA 2292821 A CA2292821 A CA 2292821A CA 2292821 A1 CA2292821 A1 CA 2292821A1
- Authority
- CA
- Canada
- Prior art keywords
- flow
- exhaust device
- internal
- turbomachine
- turbine 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.)
- Granted
Links
- 230000002745 absorbent Effects 0.000 abstract 2
- 239000002250 absorbent Substances 0.000 abstract 2
- 239000011248 coating agent Substances 0.000 abstract 2
- 238000000576 coating method Methods 0.000 abstract 2
- 238000005192 partition Methods 0.000 abstract 2
- 238000009792 diffusion process Methods 0.000 abstract 1
- 230000000750 progressive effect Effects 0.000 abstract 1
- 238000000926 separation method Methods 0.000 abstract 1
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
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/827—Sound absorbing structures or liners
-
- 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
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
Abstract
L'invention concerne un dispositif d'échappement multicanal de turbomachine, du type multicanal à entré annulaire, comprenant une enveloppe extérieure de forme générale symétrique par rapport à un axe et au moins une séparation interne définissant plusieurs canaux sensiblement concentriques pour l'écoulement du flux d'échappement, un revêtement absorbant capable d'absorber une partie de l'énergie acoustique générée par l'écoulement est prévu sur au moins une surface de la séparation interne et/ou sur une surface interne de l'enveloppe extérieure. L'épaisseur du revêtement absorbant est adaptée sur la longueur du dispositif d'échappement pour optimiser l'écoulement dans les différents canaux en maintenant la diffusion progressive et en évitant les décollements au voisinage des surfaces immobiles. Grâce à cette disposition, la signature acoustique de la turbomachine est grandement réduite puisqu'il devient possible de bénéficier de l'augmentation de surface traitée acoustiquement due à la présence des séparations internes.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9815942 | 1998-12-17 | ||
FR9815942A FR2787513B1 (fr) | 1998-12-17 | 1998-12-17 | Dispositif d'echappement multicanal de turbomachine traite acoustiquement |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2292821A1 true CA2292821A1 (fr) | 2000-06-17 |
CA2292821C CA2292821C (fr) | 2008-03-18 |
Family
ID=9534084
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002292821A Expired - Fee Related CA2292821C (fr) | 1998-12-17 | 1999-12-17 | Dispositif d'echappement multicanal de turbomachine traite acoustiquement |
Country Status (10)
Country | Link |
---|---|
US (1) | US6672424B2 (fr) |
EP (1) | EP1010884B1 (fr) |
AT (1) | ATE333583T1 (fr) |
CA (1) | CA2292821C (fr) |
CY (1) | CY1105644T1 (fr) |
DE (1) | DE69932394T2 (fr) |
DK (1) | DK1010884T3 (fr) |
ES (1) | ES2268838T3 (fr) |
FR (1) | FR2787513B1 (fr) |
PT (1) | PT1010884E (fr) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6615576B2 (en) * | 2001-03-29 | 2003-09-09 | Honeywell International Inc. | Tortuous path quiet exhaust eductor system |
US7028416B1 (en) * | 2003-04-21 | 2006-04-18 | Darryl D Dobie | Noise attenuating drying apparatus for motor vehicles |
US7121814B2 (en) * | 2004-09-30 | 2006-10-17 | Carrier Corporation | Compressor sound suppression |
EP1805417A4 (fr) * | 2004-10-20 | 2010-10-06 | Carrier Corp | Suppression du bruit d"un compresseur |
US7367424B2 (en) * | 2005-02-14 | 2008-05-06 | Honeywell International, Inc. | Eccentric exhaust muffler for use with auxiliary power units |
EP1732062B1 (fr) * | 2005-06-07 | 2013-08-14 | Alstom Technology Ltd | Silencieux |
ES2317571T3 (es) * | 2005-08-08 | 2009-04-16 | Alstom Technology Ltd | Silenciador para instalaciones de turbinas de gas. |
US7472774B1 (en) * | 2006-01-27 | 2009-01-06 | Lockheed Martin Corporation | Versatile engine muffling system |
FR2905984B1 (fr) | 2006-09-20 | 2011-12-30 | Turbomeca | Moteur d'helicoptere a turbine a gaz a emission sonore reduite par traitement acoustique d'un ejecteur |
US7762374B2 (en) * | 2006-11-22 | 2010-07-27 | Honeywell International Inc. | Turbine engine diffusing exhaust muffler |
FR2941495B1 (fr) * | 2009-01-27 | 2017-09-29 | Turbomeca | Conduit d'echappement insonorise pour turbomoteur |
FR2946090B1 (fr) * | 2009-05-27 | 2016-01-22 | Turbomeca | Turbomoteur comportant un cone de guidage des gaz d'echappement avec un attenuateur sonore. |
US9200537B2 (en) | 2011-11-09 | 2015-12-01 | Pratt & Whitney Canada Corp. | Gas turbine exhaust case with acoustic panels |
US9416752B2 (en) | 2012-02-28 | 2016-08-16 | Pratt & Whitney Canada Corp. | Gas turbine exhaust having reduced jet noise |
US9309842B2 (en) * | 2013-02-07 | 2016-04-12 | General Electric Company | Air inlet silencer for turbomachines |
US9631542B2 (en) | 2013-06-28 | 2017-04-25 | General Electric Company | System and method for exhausting combustion gases from gas turbine engines |
US20150059312A1 (en) * | 2013-08-29 | 2015-03-05 | General Electric Company | Exhaust stack having a co-axial silencer |
US9969500B2 (en) | 2014-02-06 | 2018-05-15 | Honeywell International Inc. | Bifurcated ducts including plenums for stabilizing flow therethrough and exhaust systems including the same |
US11655816B2 (en) | 2015-05-08 | 2023-05-23 | Danfoss Power Solutions Gmbh & Co. Ohg | Fluid working systems |
US9587563B2 (en) * | 2015-07-21 | 2017-03-07 | The Boeing Company | Sound attenuation apparatus and method |
US9771868B2 (en) | 2015-07-21 | 2017-09-26 | The Boeing Company | Sound attenuation apparatus and method |
US10533452B2 (en) * | 2017-07-19 | 2020-01-14 | Garrett Transportation I Inc. | Acoustic damper with barrier member configured to dampen acoustic energy propogating upstream in gas flow |
DE102018212802A1 (de) * | 2018-08-01 | 2020-02-06 | Brose Fahrzeugteile GmbH & Co. Kommanditgesellschaft, Würzburg | Verdichtermodul und Kältemittelverdichter mit einem solchen Verdichtermodul |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2869671A (en) * | 1953-08-31 | 1959-01-20 | Karl E Schlachter | Gas turbine muffler |
US2886121A (en) * | 1956-10-25 | 1959-05-12 | John T Welbourn | Air-cooled silencer |
US3033307A (en) * | 1959-10-06 | 1962-05-08 | Industrial Acoustics Co | Noise attenuating apparatus |
FR1580553A (fr) * | 1968-07-26 | 1969-09-05 | ||
US3511336A (en) * | 1969-06-10 | 1970-05-12 | Rink Corp | Sound attenuator for air flow |
US3602333A (en) * | 1969-10-15 | 1971-08-31 | Chiyoda Chem Eng Construct Co | Silencer for suction or discharge of fluids under pressure |
US3721389A (en) * | 1971-06-10 | 1973-03-20 | Boeing Co | Exit nozzle assemblies for gas turbine power plants |
FR2191025B1 (fr) * | 1972-07-04 | 1975-03-07 | Aerospatiale | |
US3831376A (en) * | 1973-02-05 | 1974-08-27 | Boeing Co | Thrust reverser |
US3890060A (en) * | 1974-02-15 | 1975-06-17 | Gen Electric | Acoustic duct with asymmetric acoustical treatment |
GB1522558A (en) * | 1976-04-05 | 1978-08-23 | Rolls Royce | Duct linings |
US4109750A (en) * | 1977-05-24 | 1978-08-29 | Lockheed Aircraft Corporation | Zeno duct sound attenuating means |
US4244441A (en) * | 1979-07-31 | 1981-01-13 | The Garrett Corporation | Broad band acoustic attenuator |
DE3401210A1 (de) * | 1984-01-14 | 1985-07-25 | ASEA AB, Västerås | Schalldaempfer zum anschluss an einen stroemungskanal |
GB8910971D0 (en) * | 1989-05-12 | 1989-06-28 | Sound Attenuators Ltd | Improvements in attenuators |
JP2630652B2 (ja) * | 1989-08-09 | 1997-07-16 | 三菱電機ホーム機器株式会社 | 送風機 |
US4953659A (en) * | 1989-08-25 | 1990-09-04 | Norris Thomas R | Fluid blow-off muffler |
US5777947A (en) * | 1995-03-27 | 1998-07-07 | Georgia Tech Research Corporation | Apparatuses and methods for sound absorption using hollow beads loosely contained in an enclosure |
DE19803161C2 (de) * | 1998-01-28 | 2000-03-16 | Alstom Energy Syst Gmbh | Gasturbinenschalldämpfer mit Diffusor |
-
1998
- 1998-12-17 FR FR9815942A patent/FR2787513B1/fr not_active Expired - Fee Related
-
1999
- 1999-12-14 DE DE69932394T patent/DE69932394T2/de not_active Expired - Lifetime
- 1999-12-14 AT AT99403129T patent/ATE333583T1/de active
- 1999-12-14 EP EP99403129A patent/EP1010884B1/fr not_active Expired - Lifetime
- 1999-12-14 ES ES99403129T patent/ES2268838T3/es not_active Expired - Lifetime
- 1999-12-14 PT PT99403129T patent/PT1010884E/pt unknown
- 1999-12-14 DK DK99403129T patent/DK1010884T3/da active
- 1999-12-15 US US09/461,330 patent/US6672424B2/en not_active Expired - Fee Related
- 1999-12-17 CA CA002292821A patent/CA2292821C/fr not_active Expired - Fee Related
-
2006
- 2006-10-04 CY CY20061101427T patent/CY1105644T1/el unknown
Also Published As
Publication number | Publication date |
---|---|
EP1010884A1 (fr) | 2000-06-21 |
DE69932394T2 (de) | 2007-07-12 |
ES2268838T3 (es) | 2007-03-16 |
FR2787513B1 (fr) | 2001-01-19 |
CY1105644T1 (el) | 2010-12-22 |
ATE333583T1 (de) | 2006-08-15 |
PT1010884E (pt) | 2006-12-29 |
US20020166718A1 (en) | 2002-11-14 |
DK1010884T3 (da) | 2006-11-20 |
DE69932394D1 (de) | 2006-08-31 |
FR2787513A1 (fr) | 2000-06-23 |
US6672424B2 (en) | 2004-01-06 |
EP1010884B1 (fr) | 2006-07-19 |
CA2292821C (fr) | 2008-03-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |
Effective date: 20121217 |