JPS6469761A - Bypass-gas turbine engine - Google Patents
Bypass-gas turbine engineInfo
- Publication number
- JPS6469761A JPS6469761A JP63205648A JP20564888A JPS6469761A JP S6469761 A JPS6469761 A JP S6469761A JP 63205648 A JP63205648 A JP 63205648A JP 20564888 A JP20564888 A JP 20564888A JP S6469761 A JPS6469761 A JP S6469761A
- Authority
- JP
- Japan
- Prior art keywords
- nozzle body
- connecting member
- bypass
- turbine
- lobe
- 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.)
- Pending
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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49231—I.C. [internal combustion] engine making
- Y10T29/49234—Rotary or radial engine making
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49428—Gas and water specific plumbing component making
- Y10T29/49432—Nozzle making
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8720113A GB2209054B (en) | 1987-08-26 | 1987-08-26 | Gas turbine nozzles |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6469761A true JPS6469761A (en) | 1989-03-15 |
Family
ID=10622828
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP63205648A Pending JPS6469761A (en) | 1987-08-26 | 1988-08-18 | Bypass-gas turbine engine |
Country Status (5)
Country | Link |
---|---|
US (1) | US4813230A (ja) |
JP (1) | JPS6469761A (ja) |
DE (1) | DE3826438A1 (ja) |
FR (1) | FR2619858B1 (ja) |
GB (1) | GB2209054B (ja) |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5638675A (en) * | 1995-09-08 | 1997-06-17 | United Technologies Corporation | Double lobed mixer with major and minor lobes |
US5761900A (en) * | 1995-10-11 | 1998-06-09 | Stage Iii Technologies, L.C. | Two-stage mixer ejector suppressor |
FR2740175B1 (fr) * | 1995-10-18 | 1997-11-21 | Snecma | Dispositif de pylone associe au melangeur d'une tuyere d'ejection de turboreacteur a flux melangeur |
DE19909792A1 (de) * | 1999-03-05 | 2000-09-07 | Rolls Royce Deutschland | Blütenmischer für ein Zweikreis-Strahltriebwerk |
US6578355B1 (en) | 1999-03-05 | 2003-06-17 | Rolls-Royce Deutschland Ltd & Co Kg | Bloom mixer for a turbofan engine |
DE19909793A1 (de) * | 1999-03-05 | 2000-09-07 | Rolls Royce Deutschland | Blütenmischer für ein Zweikreis-Strahltriebwerk |
DE19952797A1 (de) * | 1999-11-03 | 2001-05-10 | Rolls Royce Deutschland | Blütenmischer für ein Zweikreis-Strahltriebwerk |
JP4743465B2 (ja) * | 2001-04-19 | 2011-08-10 | 株式会社Ihi | ジェットエンジン用ローブミキサー |
ATE358772T1 (de) * | 2001-12-07 | 2007-04-15 | Jack H Anderson | Blütenmischer für strahltriebwerke |
US7017331B2 (en) * | 2002-12-07 | 2006-03-28 | Anderson Jack H | Jet nozzle mixer |
US7043898B2 (en) * | 2003-06-23 | 2006-05-16 | Pratt & Whitney Canada Corp. | Combined exhaust duct and mixer for a gas turbine engine |
US7114323B2 (en) * | 2004-03-05 | 2006-10-03 | United Technologies Corporation | Jet exhaust noise reduction system and method |
FR2875854B1 (fr) * | 2004-09-29 | 2009-04-24 | Snecma Propulsion Solide Sa | Melangeur pour tuyere a flux separes |
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 |
US7418813B2 (en) * | 2004-12-27 | 2008-09-02 | General Electric Company | Gas turbine engine exhaust nozzle including an infrared suppression system having a plurality of U-shaped blocking fins and method of assembling said exhaut nozzle |
FR2912469B1 (fr) * | 2007-02-12 | 2009-05-08 | Snecma Propulsion Solide Sa | Procede de fabrication d'une structure a lobes de melangeur de flux en cmc pour moteur aeronautique a turbine de gaz. |
US7882696B2 (en) * | 2007-06-28 | 2011-02-08 | Honeywell International Inc. | Integrated support and mixer for turbo machinery |
US8015820B2 (en) * | 2008-06-03 | 2011-09-13 | United Technologies Corporation | Gas turbine engine exhaust component and manufacturing method of same |
US20100199626A1 (en) * | 2008-12-31 | 2010-08-12 | Benjamin Roland Harding | Turbine engine exhaust gas tube mixer |
US8739513B2 (en) * | 2009-08-17 | 2014-06-03 | Pratt & Whitney Canada Corp. | Gas turbine engine exhaust mixer |
EP2841750B1 (en) * | 2012-04-27 | 2018-06-13 | General Electric Company | Variable immersion lobe mixer and method of fabricating the same |
US10190536B2 (en) | 2012-09-17 | 2019-01-29 | Pratt & Whitney Canada Corp. | Turbine exhaust case mixer of gas turbine with variable thickness |
DE102012220358A1 (de) * | 2012-11-08 | 2014-06-12 | Rolls-Royce Deutschland Ltd & Co Kg | Düse mit Leitvorrichtungen |
DE102012220360A1 (de) * | 2012-11-08 | 2014-05-08 | Rolls-Royce Deutschland Ltd & Co Kg | Düse mit Leitvorrichtungen |
US9188024B2 (en) | 2013-02-22 | 2015-11-17 | Pratt & Whitney Canada Corp. | Exhaust section for bypass gas turbine engines |
US9970386B2 (en) * | 2013-06-07 | 2018-05-15 | United Technologies Corporation | Exhaust stream mixer |
US10197010B2 (en) * | 2013-08-12 | 2019-02-05 | The Boeing Company | Long-duct, mixed-flow nozzle system for a turbofan engine |
FR3028294B1 (fr) * | 2014-11-06 | 2020-06-12 | Safran Aircraft Engines | Carenage pour melangeur de tuyere de turbomachine a double flux |
EP3091288B1 (en) * | 2015-05-08 | 2019-04-03 | Ansaldo Energia Switzerland AG | Mixing system |
US20180100468A1 (en) * | 2016-10-07 | 2018-04-12 | Rolls-Royce North American Technologies Inc. | System and method for reduction of turbine exhaust gas impingement on adjacent aircraft structure |
US11118481B2 (en) | 2017-02-06 | 2021-09-14 | Raytheon Technologies Corporation | Ceramic matrix composite turbine exhaust assembly for a gas turbine engine |
US11028778B2 (en) | 2018-09-27 | 2021-06-08 | Pratt & Whitney Canada Corp. | Engine with start assist |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB766986A (en) * | 1952-07-25 | 1957-01-30 | Geoffrey Michael Lilley | Noise suppressing nozzles for aircraft jet propulsion engines |
GB874496A (en) * | 1957-08-30 | 1961-08-10 | Robert Westley | Jet propulsion nozzle noise suppression means and thrust reverser |
GB996461A (en) * | 1962-09-03 | 1965-06-30 | Bristol Siddeley Engines Ltd | Improvements relating to jet propulsion power plants |
US3415337A (en) * | 1966-04-20 | 1968-12-10 | Gen Electric | Air injector device for air-cooled noise suppressors |
US3508403A (en) * | 1968-03-28 | 1970-04-28 | Gen Electric | Turbofan engines |
US3982696A (en) * | 1975-07-01 | 1976-09-28 | Grumman American Aviation Corporation | Jet noise suppressor nozzle |
US4117671A (en) * | 1976-12-30 | 1978-10-03 | The Boeing Company | Noise suppressing exhaust mixer assembly for ducted-fan, turbojet engine |
US4254620A (en) * | 1978-02-27 | 1981-03-10 | The Boeing Company | Jet engine multiduct noise suppressor |
GB2031070B (en) * | 1978-10-02 | 1982-11-17 | Boeing Co | Suppression of noise from a ducted-fan turbojet engine |
US4302934A (en) * | 1979-11-01 | 1981-12-01 | United Technologies Corporation | Lobed mixer/inverter |
US4401269A (en) * | 1980-09-26 | 1983-08-30 | United Technologies Corporation | Lobe mixer for gas turbine engine |
US4335801A (en) * | 1980-12-15 | 1982-06-22 | The Boeing Company | Noise suppressing nozzle |
-
1987
- 1987-08-26 GB GB8720113A patent/GB2209054B/en not_active Expired - Lifetime
- 1987-09-22 US US07/099,873 patent/US4813230A/en not_active Expired - Lifetime
-
1988
- 1988-08-03 DE DE3826438A patent/DE3826438A1/de not_active Withdrawn
- 1988-08-18 JP JP63205648A patent/JPS6469761A/ja active Pending
- 1988-08-24 FR FR8811158A patent/FR2619858B1/fr not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
GB8720113D0 (en) | 1987-12-16 |
US4813230A (en) | 1989-03-21 |
GB2209054A (en) | 1989-04-26 |
GB2209054B (en) | 1992-04-15 |
DE3826438A1 (de) | 1989-03-09 |
FR2619858B1 (fr) | 1993-05-14 |
FR2619858A1 (fr) | 1989-03-03 |
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