DE602005009232D1 - Akoustische Isolierung des Stators eines Niederdruckverdichters - Google Patents
Akoustische Isolierung des Stators eines NiederdruckverdichtersInfo
- Publication number
- DE602005009232D1 DE602005009232D1 DE602005009232T DE602005009232T DE602005009232D1 DE 602005009232 D1 DE602005009232 D1 DE 602005009232D1 DE 602005009232 T DE602005009232 T DE 602005009232T DE 602005009232 T DE602005009232 T DE 602005009232T DE 602005009232 D1 DE602005009232 D1 DE 602005009232D1
- Authority
- DE
- Germany
- Prior art keywords
- low
- pressure compressor
- stator
- acoustic insulation
- shoulder
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/24—Heat or noise insulation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
-
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
-
- 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
- F05D2260/30—Retaining components in desired mutual position
-
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP05292778A EP1801389B1 (de) | 2005-12-23 | 2005-12-23 | Akoustische Isolierung des Stators eines Niederdruckverdichters |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602005009232D1 true DE602005009232D1 (de) | 2008-10-02 |
Family
ID=36941962
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602005009232T Active DE602005009232D1 (de) | 2005-12-23 | 2005-12-23 | Akoustische Isolierung des Stators eines Niederdruckverdichters |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1801389B1 (de) |
AT (1) | ATE405735T1 (de) |
DE (1) | DE602005009232D1 (de) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3005107B1 (fr) * | 2013-04-25 | 2016-10-07 | Snecma | Turbomachine a double flux |
FR3005692B1 (fr) * | 2013-05-14 | 2015-05-22 | Snecma | Bague de support destinee au montage d'un bec de separation et d'une virole d'un turboreacteur, ensemble de maintien, procedes de montage |
FR3005693B1 (fr) * | 2013-05-16 | 2017-12-22 | Snecma | Turbomachine d'aeronef a double flux comprenant une virole inter-veine a maintien aval simplifie |
RU2549398C1 (ru) * | 2014-03-25 | 2015-04-27 | Открытое акционерное общество "Авиадвигатель" | Двухконтурный двигатель |
US10156243B2 (en) | 2015-05-04 | 2018-12-18 | Safran Aero Boosters Sa | Composite splitter lip for axial turbomachine compressor |
GB201705734D0 (en) | 2017-04-10 | 2017-05-24 | Rolls Royce Plc | Flow splitter |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9828812D0 (en) * | 1998-12-29 | 1999-02-17 | Rolls Royce Plc | Gas turbine nose cone assembly |
GB2364748A (en) * | 2000-07-15 | 2002-02-06 | Rolls Royce Plc | Gas turbine engine nose cone with tool access hole plug/cover |
US6561760B2 (en) | 2001-08-17 | 2003-05-13 | General Electric Company | Booster compressor deicer |
US6725645B1 (en) | 2002-10-03 | 2004-04-27 | General Electric Company | Turbofan engine internal anti-ice device |
-
2005
- 2005-12-23 EP EP05292778A patent/EP1801389B1/de active Active
- 2005-12-23 DE DE602005009232T patent/DE602005009232D1/de active Active
- 2005-12-23 AT AT05292778T patent/ATE405735T1/de not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
ATE405735T1 (de) | 2008-09-15 |
EP1801389A1 (de) | 2007-06-27 |
EP1801389B1 (de) | 2008-08-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |