BRPI0814492A2 - Denteado disposto na periferia do orifício de saída do jato de tubeira de motor a jato, tubeira de motor a jato e motor a jato de fluxo duplo - Google Patents
Denteado disposto na periferia do orifício de saída do jato de tubeira de motor a jato, tubeira de motor a jato e motor a jato de fluxo duploInfo
- Publication number
- BRPI0814492A2 BRPI0814492A2 BRPI0814492-3A2A BRPI0814492A BRPI0814492A2 BR PI0814492 A2 BRPI0814492 A2 BR PI0814492A2 BR PI0814492 A BRPI0814492 A BR PI0814492A BR PI0814492 A2 BRPI0814492 A2 BR PI0814492A2
- Authority
- BR
- Brazil
- Prior art keywords
- jet engine
- jet
- tube
- experience
- outlet
- Prior art date
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
- F02K1/46—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
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/11—Two-dimensional triangular
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient 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)
- Nozzles (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Escalators And Moving Walkways (AREA)
- Fuel-Injection Apparatus (AREA)
- Jet Pumps And Other Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0705847A FR2920036B1 (fr) | 2007-08-14 | 2007-08-14 | Chevrons anti-bruit pour tuyere |
PCT/FR2008/001165 WO2009053554A1 (fr) | 2007-08-14 | 2008-08-04 | Chevron anti-bruit pour tuyère, tuyère et turbomoteur pourvus d'un tel chevron |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0814492A2 true BRPI0814492A2 (pt) | 2015-02-03 |
Family
ID=38896759
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0814492-3A2A BRPI0814492A2 (pt) | 2007-08-14 | 2008-08-04 | Denteado disposto na periferia do orifício de saída do jato de tubeira de motor a jato, tubeira de motor a jato e motor a jato de fluxo duplo |
Country Status (9)
Country | Link |
---|---|
US (1) | US8887489B2 (pt) |
EP (1) | EP2179163B1 (pt) |
JP (1) | JP5066610B2 (pt) |
CN (1) | CN101809272B (pt) |
BR (1) | BRPI0814492A2 (pt) |
CA (1) | CA2694996C (pt) |
FR (1) | FR2920036B1 (pt) |
RU (1) | RU2466290C2 (pt) |
WO (1) | WO2009053554A1 (pt) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2930972B1 (fr) * | 2008-05-07 | 2012-11-30 | Airbus France | Turbomachine a double flux pour aeronef a emission de bruit reduite |
FR2945838B1 (fr) * | 2009-05-20 | 2014-06-13 | Snecma | Capot pour tuyere de turbomachine muni de motifs a ailettes laterales pour reduire le bruit de jet. |
FR2960028B1 (fr) * | 2010-05-12 | 2016-07-15 | Snecma | Dispositif pour attenuer le bruit emis par le jet d'un moteur de propulsion d'un aeronef. |
JP5842211B2 (ja) * | 2011-01-21 | 2016-01-13 | 国立研究開発法人宇宙航空研究開発機構 | 空力騒音低減装置 |
FR2988014A1 (fr) | 2012-03-16 | 2013-09-20 | Centre Nat Rech Scient | Dispositif de pulsation d'un fluide |
FR3070186B1 (fr) * | 2017-08-21 | 2021-06-11 | Safran Aircraft Engines | Tuyere secondaire modifiee acoustique |
CN109372653A (zh) * | 2018-12-13 | 2019-02-22 | 中国航发沈阳发动机研究所 | 一种涡扇发动机降噪排气组件 |
US10992103B1 (en) * | 2019-12-02 | 2021-04-27 | Sharp Fukuyama Laser Co., Ltd. | Laser device |
CN112502853B (zh) * | 2020-11-27 | 2021-11-02 | 中国商用飞机有限责任公司 | 喷管、配备该喷管的喷气发动机和喷气式飞机 |
US20220195960A1 (en) * | 2020-12-21 | 2022-06-23 | Rohr, Inc. | Gas turbine engine exhaust chevrons |
US20230167783A1 (en) * | 2021-12-01 | 2023-06-01 | General Electric Company | Propulsion system for a gas turbine engine |
US11959438B2 (en) * | 2021-12-30 | 2024-04-16 | Medhat Osman | Ultra quiet split flow thrust reverser |
US11920539B1 (en) | 2022-10-12 | 2024-03-05 | General Electric Company | Gas turbine exhaust nozzle noise abatement |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL98695C (pt) * | 1952-07-25 | |||
CA1100463A (en) * | 1978-11-22 | 1981-05-05 | Frederick L. Gilbertson | Nozzle structure with notches |
GB2104967B (en) * | 1981-09-03 | 1985-07-17 | Rolls Royce | Exhaust mixer for turbofan aeroengine |
GB2160265A (en) * | 1984-06-12 | 1985-12-18 | Rolls Royce | Turbofan exhaust mixers |
GB2289921A (en) * | 1994-06-03 | 1995-12-06 | A E Harris Limited | Nozzle for turbofan aeroengines |
US6360528B1 (en) * | 1997-10-31 | 2002-03-26 | General Electric Company | Chevron exhaust nozzle for a gas turbine engine |
US6532729B2 (en) * | 2001-05-31 | 2003-03-18 | General Electric Company | Shelf truncated chevron exhaust nozzle for reduction of exhaust noise and infrared (IR) signature |
US6505706B2 (en) * | 2001-06-14 | 2003-01-14 | Pratt & Whitney Canada Corp. | Exhaust flow guide for jet noise reduction |
FR2855558B1 (fr) * | 2003-05-28 | 2005-07-15 | Snecma Moteurs | Tuyere de turbomachine a reduction de bruit |
FR2857416B1 (fr) * | 2003-07-09 | 2007-05-25 | Snecma Moteurs | Dispositif de reduction du bruit de jet d'une turbomachine |
US7093423B2 (en) * | 2004-01-20 | 2006-08-22 | General Electric Company | Methods and apparatus for operating gas turbine engines |
US7305817B2 (en) * | 2004-02-09 | 2007-12-11 | General Electric Company | Sinuous chevron exhaust nozzle |
FR2868131B1 (fr) | 2004-03-25 | 2006-06-09 | Airbus France Sas | Tuyere primaire a chevrons pour turboreacteur a double flux d'aeronef et aeronef comportant une telle tuyere |
RU2265130C1 (ru) * | 2004-04-20 | 2005-11-27 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" | Смеситель двухконтурного турбореактивного двигателя (трдд) |
FR2873166B1 (fr) * | 2004-07-13 | 2008-10-31 | Snecma Moteurs Sa | Tuyere de turbomachine a motifs a reduction de bruit de jet |
US7434384B2 (en) * | 2004-10-25 | 2008-10-14 | United Technologies Corporation | Fluid mixer with an integral fluid capture ducts forming auxiliary secondary chutes at the discharge end of said ducts |
FR2902758B1 (fr) * | 2006-06-21 | 2009-04-10 | Airbus France Sas | Ensemble propulsif d'aeronef comportant un conduit d'ejection avec un bord de fuite echancre |
FR2902837B1 (fr) * | 2006-06-26 | 2008-10-24 | Snecma Sa | Capot pour tuyere de turbomachine muni de motifs triangulaires a doubles sommets pour reduire le bruit de jet |
FR2902836B1 (fr) * | 2006-06-26 | 2008-10-24 | Snecma Sa | Capot pour tuyere de turbomachine muni de motifs triangulaires a point d'inflexion pour reduire le bruit de jet |
US7966824B2 (en) * | 2006-08-09 | 2011-06-28 | The Boeing Company | Jet engine nozzle exit configurations and associated systems and methods |
-
2007
- 2007-08-14 FR FR0705847A patent/FR2920036B1/fr not_active Expired - Fee Related
-
2008
- 2008-08-04 JP JP2010520606A patent/JP5066610B2/ja not_active Expired - Fee Related
- 2008-08-04 US US12/672,796 patent/US8887489B2/en not_active Expired - Fee Related
- 2008-08-04 WO PCT/FR2008/001165 patent/WO2009053554A1/fr active Application Filing
- 2008-08-04 RU RU2010109411/06A patent/RU2466290C2/ru not_active IP Right Cessation
- 2008-08-04 BR BRPI0814492-3A2A patent/BRPI0814492A2/pt not_active IP Right Cessation
- 2008-08-04 CA CA2694996A patent/CA2694996C/fr not_active Expired - Fee Related
- 2008-08-04 CN CN2008801033043A patent/CN101809272B/zh not_active Expired - Fee Related
- 2008-08-04 EP EP08841996.5A patent/EP2179163B1/fr not_active Not-in-force
Also Published As
Publication number | Publication date |
---|---|
CN101809272B (zh) | 2013-09-04 |
US20110192167A1 (en) | 2011-08-11 |
RU2466290C2 (ru) | 2012-11-10 |
CA2694996A1 (fr) | 2009-04-30 |
WO2009053554A1 (fr) | 2009-04-30 |
JP5066610B2 (ja) | 2012-11-07 |
EP2179163A1 (fr) | 2010-04-28 |
EP2179163B1 (fr) | 2016-09-28 |
FR2920036B1 (fr) | 2013-11-15 |
JP2010535985A (ja) | 2010-11-25 |
US8887489B2 (en) | 2014-11-18 |
RU2010109411A (ru) | 2011-09-20 |
CN101809272A (zh) | 2010-08-18 |
CA2694996C (fr) | 2015-10-06 |
FR2920036A1 (fr) | 2009-02-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application fees: dismissal - article 86 of industrial property law | ||
B08K | Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87) |