UA84403C2 - Устройство для подачи охлаждающего воздуха к створке регулируемого реактивного сопла турбореактивного двигателя и турбореактивный двигатель - Google Patents
Устройство для подачи охлаждающего воздуха к створке регулируемого реактивного сопла турбореактивного двигателя и турбореактивный двигательInfo
- Publication number
- UA84403C2 UA84403C2 UAA200500225A UAA200500225A UA84403C2 UA 84403 C2 UA84403 C2 UA 84403C2 UA A200500225 A UAA200500225 A UA A200500225A UA A200500225 A UAA200500225 A UA A200500225A UA 84403 C2 UA84403 C2 UA 84403C2
- Authority
- UA
- Ukraine
- Prior art keywords
- turbo
- jet engine
- cooling air
- exhaust nozzle
- supplying cooling
- Prior art date
Links
- 238000001816 cooling Methods 0.000 title abstract 3
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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
- F02K1/1223—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series
-
- 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
- F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
-
- 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
- F05D2260/20—Heat transfer, e.g. cooling
-
- 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)
- Jet Pumps And Other Pumps (AREA)
- Exhaust Gas After Treatment (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Exhaust Silencers (AREA)
- Supercharger (AREA)
- Lift Valve (AREA)
Abstract
Устройство, согласно изобретению, для подачи охлаждающего воздуха к створке (21) регулируемого реактивного сопла (1) в газовой турбине, которое содержит трубку (30), которая соединяет створку (21) с источником (31) охлаждающего воздуха. Трубка (30) содержит по крайней мере одну выдвижную часть (32) и одно шаровое соединение (33, 34).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0400219A FR2865000B1 (fr) | 2004-01-12 | 2004-01-12 | Dispositif d'alimentation en air de refroidissement de volets de tuyere |
Publications (1)
Publication Number | Publication Date |
---|---|
UA84403C2 true UA84403C2 (ru) | 2008-10-27 |
Family
ID=34586485
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAA200500225A UA84403C2 (ru) | 2004-01-12 | 2005-01-10 | Устройство для подачи охлаждающего воздуха к створке регулируемого реактивного сопла турбореактивного двигателя и турбореактивный двигатель |
Country Status (9)
Country | Link |
---|---|
US (1) | US7213393B2 (ru) |
EP (1) | EP1553282B1 (ru) |
JP (1) | JP4057014B2 (ru) |
CA (1) | CA2492149C (ru) |
DE (1) | DE602005002660T2 (ru) |
ES (1) | ES2293507T3 (ru) |
FR (1) | FR2865000B1 (ru) |
RU (1) | RU2386049C2 (ru) |
UA (1) | UA84403C2 (ru) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2860045B1 (fr) * | 2003-09-24 | 2006-01-06 | Snecma Moteurs | Systeme de ventilation pour une tuyere d'ejection convergente divergente |
US7458221B1 (en) * | 2003-10-23 | 2008-12-02 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Variable area nozzle including a plurality of convexly vanes with a crowned contour, in a vane to vane sealing arrangement and with nonuniform lengths |
US20080006641A1 (en) * | 2005-02-22 | 2008-01-10 | Pratt & Whitney Canada Corp. | Positioning arrangement for components of a pressure vessel and method |
FR2901321B1 (fr) * | 2006-05-18 | 2011-08-12 | Aircelle Sa | Procede d'homogeneisation de l'air en sortie de turboreacteur pour abaisser le bruit genere |
FR2920195B1 (fr) | 2007-08-23 | 2009-11-20 | Snecma | Turbomachine a double flux a reduction de bruit de jet |
US7861535B2 (en) * | 2007-09-24 | 2011-01-04 | United Technologies Corporation | Self-aligning liner support hanger |
FR2933127B1 (fr) * | 2008-06-25 | 2015-04-24 | Snecma | Dispositif de prelevement d'air de refroidissement dans une turbomachine |
FR2933128B1 (fr) * | 2008-06-25 | 2010-09-17 | Snecma | Dispositif de prelevement d'air de refroidissement dans une turbomachine |
FR2937679B1 (fr) * | 2008-10-24 | 2010-12-03 | Snecma | Dispositif de prelevement d'air de refroidissement dans une turbomachine |
US8991191B2 (en) * | 2009-11-24 | 2015-03-31 | General Electric Company | Thermally actuated passive gas turbine engine compartment venting |
RU2456468C1 (ru) * | 2011-02-04 | 2012-07-20 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") | Система переброса рабочего тела для поворотного сопла турбореактивного двигателя |
US9249732B2 (en) | 2012-09-28 | 2016-02-02 | United Technologies Corporation | Panel support hanger for a turbine engine |
US9243515B2 (en) | 2012-09-28 | 2016-01-26 | United Technologies Corporation | Support hanger for flexibly connecting a plurality of panels |
WO2014160486A1 (en) | 2013-03-13 | 2014-10-02 | Rolls-Royce North American Technologies, Inc. | Compact actuation system for a gas turbine engine exhaust nozzle |
WO2015112554A1 (en) * | 2014-01-24 | 2015-07-30 | United Technologies Corporation | Divergent flap |
RU2578944C1 (ru) * | 2014-12-11 | 2016-03-27 | Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО УМПО | Регулируемое сверхзвуковое сопло турбореактивного двигателя |
RU2678235C1 (ru) * | 2017-12-22 | 2019-01-24 | Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Поворотное осесимметричное сопло турбореактивного двигателя |
CN114151228B (zh) * | 2022-02-09 | 2022-04-22 | 中国航发四川燃气涡轮研究院 | 二元矢量喷管调节片离散式冷气分区的方法 |
CN115614176B (zh) * | 2022-08-29 | 2024-04-19 | 中国航发四川燃气涡轮研究院 | 基于内外涵结构一体化的红外与雷达综合隐身装置 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE337119C (de) * | 1921-05-26 | Friedrich Wilhelm Koehler | Rohrkupplung mit halbkugelfoermigen Endflanschen | |
US5101624A (en) * | 1989-09-07 | 1992-04-07 | General Electric Company | Exhaust nozzle hinge |
US5255849A (en) * | 1991-11-05 | 1993-10-26 | General Electric Company | Cooling air transfer apparatus for aircraft gas turbine engine exhaust nozzles |
US5720434A (en) * | 1991-11-05 | 1998-02-24 | General Electric Company | Cooling apparatus for aircraft gas turbine engine exhaust nozzles |
US5603531A (en) * | 1994-12-06 | 1997-02-18 | United Technologies Corporation | Blind assembly-swivel crossover tube |
US5680755A (en) * | 1995-09-25 | 1997-10-28 | General Electric Company | Convertible ejector selectively cooled thrust vectoring exhaust nozzle |
US6301877B1 (en) * | 1995-11-13 | 2001-10-16 | United Technologies Corporation | Ejector extension cooling for exhaust nozzle |
-
2004
- 2004-01-12 FR FR0400219A patent/FR2865000B1/fr not_active Expired - Fee Related
-
2005
- 2005-01-03 US US11/025,910 patent/US7213393B2/en active Active
- 2005-01-06 CA CA2492149A patent/CA2492149C/fr active Active
- 2005-01-10 UA UAA200500225A patent/UA84403C2/ru unknown
- 2005-01-11 RU RU2005100177/06A patent/RU2386049C2/ru active
- 2005-01-11 JP JP2005003399A patent/JP4057014B2/ja active Active
- 2005-01-11 ES ES05300019T patent/ES2293507T3/es active Active
- 2005-01-11 EP EP05300019A patent/EP1553282B1/fr active Active
- 2005-01-11 DE DE602005002660T patent/DE602005002660T2/de active Active
Also Published As
Publication number | Publication date |
---|---|
RU2386049C2 (ru) | 2010-04-10 |
DE602005002660T2 (de) | 2008-06-19 |
CA2492149C (fr) | 2011-11-15 |
FR2865000A1 (fr) | 2005-07-15 |
DE602005002660D1 (de) | 2007-11-15 |
US20050210864A1 (en) | 2005-09-29 |
RU2005100177A (ru) | 2006-06-20 |
US7213393B2 (en) | 2007-05-08 |
EP1553282B1 (fr) | 2007-10-03 |
CA2492149A1 (fr) | 2005-07-12 |
JP4057014B2 (ja) | 2008-03-05 |
EP1553282A1 (fr) | 2005-07-13 |
FR2865000B1 (fr) | 2006-06-09 |
JP2005201265A (ja) | 2005-07-28 |
ES2293507T3 (es) | 2008-03-16 |
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