IT1141160B - Cappottatura di motore a turbina a gas - Google Patents
Cappottatura di motore a turbina a gasInfo
- Publication number
- IT1141160B IT1141160B IT19702/80A IT1970280A IT1141160B IT 1141160 B IT1141160 B IT 1141160B IT 19702/80 A IT19702/80 A IT 19702/80A IT 1970280 A IT1970280 A IT 1970280A IT 1141160 B IT1141160 B IT 1141160B
- Authority
- IT
- Italy
- Prior art keywords
- covering
- gas turbine
- turbine engine
- engine
- gas
- Prior art date
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
-
- 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
-
- 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
- F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
-
- 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
- F02K1/825—Infrared radiation suppressors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
- B64D2033/045—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes comprising infrared suppressors
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24149—Honeycomb-like
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
- Separating Particles In Gases By Inertia (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7909332A GB2044359B (en) | 1979-03-16 | 1979-03-16 | Gas turbine engine air intakes |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8019702A0 IT8019702A0 (it) | 1980-02-05 |
IT1141160B true IT1141160B (it) | 1986-10-01 |
Family
ID=10503928
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT19702/80A IT1141160B (it) | 1979-03-16 | 1980-02-05 | Cappottatura di motore a turbina a gas |
Country Status (6)
Country | Link |
---|---|
US (1) | US4291530A (it) |
JP (1) | JPS55128626A (it) |
DE (1) | DE3009510C2 (it) |
FR (1) | FR2451316A1 (it) |
GB (1) | GB2044359B (it) |
IT (1) | IT1141160B (it) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4265646A (en) * | 1979-10-01 | 1981-05-05 | General Electric Company | Foreign particle separator system |
GB2095335B (en) * | 1981-03-20 | 1984-05-31 | Rolls Royce | Gas turbine engine air intake system |
JPS588252A (ja) * | 1981-06-30 | 1983-01-18 | ヒューズ・ヘリコプターズ・インコーポレイテッド | 幅射線遮蔽およびガス拡散装置 |
GB2114229B (en) * | 1981-11-03 | 1984-11-21 | Rolls Royce | Gas turbine engine infra-red radiation suppressor |
GB2140090B (en) * | 1982-12-23 | 1986-10-01 | Rolls Royce | Air intakes of helicopter mounted gas turbine engines |
US4685942A (en) * | 1982-12-27 | 1987-08-11 | General Electric Company | Axial flow inlet particle separator |
IT1183880B (it) * | 1985-06-07 | 1987-10-22 | Agusta Aeronaut Costr | Elicottero con gruppo propulsore a turbina provvisto di dispositivo mascheratore di scarico |
GB2203801B (en) * | 1987-04-14 | 1991-11-27 | Rolls Royce Plc | A gas turbine engine |
US4767425A (en) * | 1987-07-06 | 1988-08-30 | The United States Of America As Represented By The Secretary Of The Army | Aspirator mechanism for turbine engine air cleaner |
GB8724537D0 (en) * | 1987-10-20 | 1987-11-25 | Rolls Royce Plc | Interturbine duct |
US4938021A (en) * | 1988-10-27 | 1990-07-03 | Sundstrand Corporation | Sustainer propulsion system |
US5694763A (en) * | 1990-04-11 | 1997-12-09 | United Technologies Corporation | Low observable engine inlet system |
US5265408A (en) * | 1992-02-13 | 1993-11-30 | Allied-Signal Inc. | Exhaust eductor cooling system |
GB2509886B (en) * | 1992-09-22 | 2015-03-18 | Rolls Royce Plc | Improvements in or relating to engine intake protection and supression of engine infra-red emissions |
US5697394A (en) * | 1993-03-02 | 1997-12-16 | United Technologies Corporation | Low observable engine air inlet system |
DE4321382C2 (de) * | 1993-06-26 | 1995-05-24 | Mtu Friedrichshafen Gmbh | Energieerzeugungssystem mit einer Gasturbine |
US6109562A (en) * | 1998-04-22 | 2000-08-29 | Pratt & Whitney Canada Corp. | Aircraft construction |
US6595742B2 (en) | 2000-10-02 | 2003-07-22 | Westar Corporation | Aircraft engine air filter and method |
US6651929B2 (en) | 2001-10-29 | 2003-11-25 | Pratt & Whitney Canada Corp. | Passive cooling system for auxiliary power unit installation |
JP4861407B2 (ja) * | 2005-04-13 | 2012-01-25 | シコルスキー エアクラフト コーポレイション | 一体型エンジン空気粒子フィルタアッセンブリ |
US7491253B2 (en) * | 2005-05-31 | 2009-02-17 | Aerospace Filtrations Systems, Inc. | Engine intake system with accessible, interchangeable air filters |
US7575014B2 (en) * | 2005-07-29 | 2009-08-18 | Aerospace Filtration Systems, Inc. | Control of engine intake door |
US7823375B2 (en) * | 2005-08-01 | 2010-11-02 | Sikorsky Aircraft Corporation | Infrared suppression system |
FR2900388B1 (fr) | 2006-04-28 | 2009-01-16 | Snecma Sa | Ensemble d'echappement des gaz de propulsion dans un aeronef formant un coude |
FR2905358B1 (fr) * | 2006-09-06 | 2008-10-17 | Eurocopter France | Cloison pare-feu d'aeronef. |
FR2905984B1 (fr) * | 2006-09-20 | 2011-12-30 | Turbomeca | Moteur d'helicoptere a turbine a gaz a emission sonore reduite par traitement acoustique d'un ejecteur |
FR2905983B1 (fr) * | 2006-09-20 | 2013-03-15 | Turbomeca | Dispositif d'insonorisation d'un moteur d'helicoptere a turbine a gaz, et moteur ainsi obtenu |
US8137424B2 (en) * | 2007-09-10 | 2012-03-20 | Honda Motor Co., Ltd. | Air cleaning device for internal combustion engine and internal combustion engine |
US7837753B2 (en) * | 2007-11-30 | 2010-11-23 | Honeywell International Inc. | Systems for filtering particles from an airflow |
EP2070454B1 (en) | 2007-12-12 | 2015-07-15 | Nestec S.A. | Beverage production machines comprising a plurality of core units |
US20090217643A1 (en) * | 2008-02-29 | 2009-09-03 | Sokhey Jagdish S | Gas discharge device for a vehicle engine |
KR101026190B1 (ko) * | 2009-01-23 | 2011-03-31 | 볼보 컨스트럭션 이큅먼트 에이비 | 엔진룸의 과열가스 온도 저감장치 |
EP2500269A1 (en) * | 2011-03-18 | 2012-09-19 | AGUSTAWESTLAND S.p.A. | Aircraft capable of hovering |
EP2964925B1 (en) | 2013-03-05 | 2020-08-05 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine heat exchanger system |
US9810079B2 (en) * | 2013-03-15 | 2017-11-07 | General Electric Company | Cyclonic dirt separating turbine accelerator |
EP3056423B1 (en) * | 2015-02-16 | 2017-12-13 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | An aircraft with a fuselage that defines at least an interior region and a drive system accommodating region |
US10899464B2 (en) * | 2018-03-14 | 2021-01-26 | Pratt & Whitney Canada Corp. | Moveable aircraft cowl and bypass section |
US11454171B1 (en) | 2019-06-27 | 2022-09-27 | United States Of America As Represented By The Secretary Of The Air Force | Turbine cooling system with energy separation |
CN110844091A (zh) * | 2019-10-11 | 2020-02-28 | 中国直升机设计研究所 | 一种引射式发动机防砂系统及方法 |
US11608189B2 (en) | 2020-08-11 | 2023-03-21 | Textron Innovations Inc | Multistage infrared suppression exhaust system |
CN113006973B (zh) * | 2021-04-13 | 2023-10-31 | 西安蓝坤工程科技有限公司 | 一种火箭发动机高空模拟试验的尾焰处理装置及方法 |
WO2023064215A1 (en) * | 2021-10-11 | 2023-04-20 | Boom Technology, Inc. | Dissimilarly shaped aircraft nozzles with tandem mixing devices, and associated systems and methods |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3421296A (en) * | 1966-11-15 | 1969-01-14 | United Aircraft Corp | Engine inlet air particle separator |
GB1201096A (en) * | 1966-11-15 | 1970-08-05 | United Aircraft Corp | Air particle separator |
FR2250671B1 (it) * | 1973-11-09 | 1980-01-04 | Aerospatiale | |
US4018046A (en) * | 1975-07-17 | 1977-04-19 | Avco Corporation | Infrared radiation suppressor for gas turbine engine |
-
1979
- 1979-03-16 GB GB7909332A patent/GB2044359B/en not_active Expired
-
1980
- 1980-01-29 US US06/116,653 patent/US4291530A/en not_active Expired - Lifetime
- 1980-02-05 IT IT19702/80A patent/IT1141160B/it active
- 1980-03-12 DE DE3009510A patent/DE3009510C2/de not_active Expired
- 1980-03-12 FR FR8005555A patent/FR2451316A1/fr active Granted
- 1980-03-14 JP JP3259280A patent/JPS55128626A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
DE3009510A1 (de) | 1980-09-18 |
IT8019702A0 (it) | 1980-02-05 |
FR2451316B1 (it) | 1983-03-18 |
FR2451316A1 (fr) | 1980-10-10 |
JPS577292B2 (it) | 1982-02-09 |
DE3009510C2 (de) | 1983-03-10 |
GB2044359A (en) | 1980-10-15 |
JPS55128626A (en) | 1980-10-04 |
US4291530A (en) | 1981-09-29 |
GB2044359B (en) | 1982-10-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19990129 |