DE602005022687D1 - Vorrichtung und Methode zur Reduktion des Luftstrahlaustrittslärms - Google Patents
Vorrichtung und Methode zur Reduktion des LuftstrahlaustrittslärmsInfo
- Publication number
- DE602005022687D1 DE602005022687D1 DE200560022687 DE602005022687T DE602005022687D1 DE 602005022687 D1 DE602005022687 D1 DE 602005022687D1 DE 200560022687 DE200560022687 DE 200560022687 DE 602005022687 T DE602005022687 T DE 602005022687T DE 602005022687 D1 DE602005022687 D1 DE 602005022687D1
- Authority
- DE
- Germany
- Prior art keywords
- reducing
- air jet
- jet exit
- exit noise
- noise
- 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
- 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
- F02K1/38—Introducing air inside the jet
- F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
-
- 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
- F02K1/44—Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction
-
- 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
- F02K1/46—Nozzles 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
- F02K1/48—Corrugated nozzles
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP20050253603 EP1731747B1 (de) | 2005-06-10 | 2005-06-10 | Vorrichtung und Methode zur Reduktion des Luftstrahlaustrittslärms |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602005022687D1 true DE602005022687D1 (de) | 2010-09-16 |
Family
ID=35427658
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE200560022687 Active DE602005022687D1 (de) | 2005-06-10 | 2005-06-10 | Vorrichtung und Methode zur Reduktion des Luftstrahlaustrittslärms |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP1731747B1 (de) |
DE (1) | DE602005022687D1 (de) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8635875B2 (en) | 2010-04-29 | 2014-01-28 | Pratt & Whitney Canada Corp. | Gas turbine engine exhaust mixer including circumferentially spaced-apart radial rows of tabs extending downstream on the radial walls, crests and troughs |
FR2979673B1 (fr) * | 2011-09-01 | 2013-08-23 | Snecma | Procede de melange de flux dans un turboreacteur double flux et sortie moteur de mise en oeuvre |
US10197010B2 (en) | 2013-08-12 | 2019-02-05 | The Boeing Company | Long-duct, mixed-flow nozzle system for a turbofan engine |
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 |
DE102016110018A1 (de) * | 2016-05-31 | 2017-11-30 | Jk-Holding Gmbh | Verwendung einer Fluiddüse in einem Fluid |
CN111288491B (zh) * | 2020-03-20 | 2021-07-16 | 中国科学院工程热物理研究所 | 一种燃烧室结构 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3568792A (en) | 1969-06-18 | 1971-03-09 | Rohr Corp | Sound-suppressing and thrust-reversing apparatus |
US6612106B2 (en) * | 2000-05-05 | 2003-09-02 | The Boeing Company | Segmented mixing device having chevrons for exhaust noise reduction in jet engines |
US6640537B2 (en) * | 2000-12-18 | 2003-11-04 | Pratt & Whitney Canada Corp. | Aero-engine exhaust jet noise reduction assembly |
GB2372780A (en) | 2001-03-03 | 2002-09-04 | Rolls Royce Plc | Gas turbine engine nozzle with noise-reducing tabs |
-
2005
- 2005-06-10 EP EP20050253603 patent/EP1731747B1/de active Active
- 2005-06-10 DE DE200560022687 patent/DE602005022687D1/de active Active
Also Published As
Publication number | Publication date |
---|---|
EP1731747B1 (de) | 2010-08-04 |
EP1731747A1 (de) | 2006-12-13 |
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