FR2441730A1 - Systeme suppresseur de rayonnement infrarouge - Google Patents
Systeme suppresseur de rayonnement infrarougeInfo
- Publication number
- FR2441730A1 FR2441730A1 FR7927918A FR7927918A FR2441730A1 FR 2441730 A1 FR2441730 A1 FR 2441730A1 FR 7927918 A FR7927918 A FR 7927918A FR 7927918 A FR7927918 A FR 7927918A FR 2441730 A1 FR2441730 A1 FR 2441730A1
- Authority
- FR
- France
- Prior art keywords
- engine
- hot
- sight
- infrared radiation
- line
- 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.)
- Granted
Links
- 230000005855 radiation Effects 0.000 title 1
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 abstract 1
- 238000009434 installation Methods 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Exhaust Silencers (AREA)
- Exhaust Gas After Treatment (AREA)
- Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
Abstract
SYSTEME QUI OBSTRUE LA LIGNE DE VISEE DES ELEMENTS CHAUDS DE LA TURBINE DU MOTEUR, L'INSTALLATION DU SUPPRESSEUR NE CONDUISANT QU'A UNE PERTE DE PERFORMANCES REDUITE DU MOTEUR. IL COMPREND UN CONDUIT 70 DESTINE A RECEVOIR LE COURANT DE GAZ D'EJECTION CHAUD SORTANT DU MOTEUR 10, UN PREMIER MOYEN DE DIVISION 86 A DOUBLE PAROI DESTINE A DIVISER LE COURANT DE GAZ, ET D'AUTRE PART UN DEUXIEME MOYEN DE DIVISION 122, 124, DISPOSE EN AVAL DU PREMIER MOYEN, ET QUI DIVISE CHACUN DES DEUX COURANTS DE GAZ PARTIELS EN DEUX NOUVEAUX COURANTS DE GAZ, TOUT EN OBSTRUANT LA LIGNE DE VISEE VERS LES PIECES METALLIQUES CHAUDES QUAND ON REGARDE LE MOTEUR DE L'ARRIERE. APPLICATION AUX MOTEURS D'AVION.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/960,351 US4295332A (en) | 1978-11-13 | 1978-11-13 | Infrared suppressor system |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2441730A1 true FR2441730A1 (fr) | 1980-06-13 |
FR2441730B1 FR2441730B1 (fr) | 1985-03-01 |
Family
ID=25503080
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7927918A Granted FR2441730A1 (fr) | 1978-11-13 | 1979-11-13 | Systeme suppresseur de rayonnement infrarouge |
Country Status (7)
Country | Link |
---|---|
US (1) | US4295332A (fr) |
JP (1) | JPS5591729A (fr) |
DE (1) | DE2945439A1 (fr) |
FR (1) | FR2441730A1 (fr) |
GB (1) | GB2034414B (fr) |
IL (1) | IL58145A (fr) |
IT (1) | IT1125666B (fr) |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA1134627A (fr) * | 1979-08-09 | 1982-11-02 | Clayton G. Coffey | Systeme de repression des emissions dans l'infrarouge |
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 |
US4800715A (en) * | 1981-08-10 | 1989-01-31 | The United States Of America As Represented By The Secretary Of The Army | Apparatus for suppressing infrared radiation emitted from gas turbine engines |
GB2114229B (en) * | 1981-11-03 | 1984-11-21 | Rolls Royce | Gas turbine engine infra-red radiation suppressor |
US4537026A (en) * | 1982-04-07 | 1985-08-27 | Rolls-Royce Inc. | Variable area nozzles for turbomachines |
US5746047A (en) * | 1982-07-08 | 1998-05-05 | Gereral Electric Company | Infrared suppressor |
US6253540B1 (en) * | 1982-07-08 | 2001-07-03 | General Electric Company | Removable baffle infrared suppressor |
JPS59141753A (ja) * | 1983-01-31 | 1984-08-14 | Fuji Heavy Ind Ltd | V/stol機用推力増大偏向装置 |
US4864819A (en) * | 1985-06-03 | 1989-09-12 | General Electric Company | Exhaust system including protective arrangements |
IT1183880B (it) * | 1985-06-07 | 1987-10-22 | Agusta Aeronaut Costr | Elicottero con gruppo propulsore a turbina provvisto di dispositivo mascheratore di scarico |
DE3712328A1 (de) * | 1987-04-11 | 1988-10-27 | Messerschmitt Boelkow Blohm | Einrichtung zur infrarotstrahlungsabschirmung |
JPH0318632U (fr) * | 1990-03-07 | 1991-02-25 | ||
GB2249140B (en) * | 1990-08-30 | 1994-12-07 | S & C Thermofluids Ltd | Aircraft engine noise suppression |
US5699662A (en) * | 1996-05-28 | 1997-12-23 | Lockheed Martin Corporation | Infrared suppression exhaust duct system for a turboprop propulsion system for an aircraft |
US6055804A (en) * | 1997-07-23 | 2000-05-02 | Sikorsky Aircraft Corporation | Turning vane arrangement for IR suppressors |
FR2781254B1 (fr) * | 1998-07-17 | 2000-08-18 | Snecma | Tuyere d'ejection de turboreacteur a masquage du jet de gaz |
GB9915949D0 (en) | 1999-07-07 | 2000-06-21 | British Aerospace | Engine nozzle arrangement for an aircraft |
US7284364B2 (en) * | 2003-09-08 | 2007-10-23 | Northrop Grumman Ship Systems, Inc. | Passive exhaust suppressor and method |
US6988674B2 (en) * | 2004-06-08 | 2006-01-24 | General Electric Company | Method and apparatus for suppressing infrared signatures |
US7313909B2 (en) * | 2004-10-25 | 2008-01-01 | General Electric Company | High-emissivity infrared coating applications for use in HIRSS applications |
SE527789C2 (sv) * | 2004-11-05 | 2006-06-07 | Volvo Aero Corp | Utloppsanordning för styrning av ett gasflöde från en jetmotor |
US7823375B2 (en) * | 2005-08-01 | 2010-11-02 | Sikorsky Aircraft Corporation | Infrared suppression system |
US7607305B2 (en) * | 2005-08-03 | 2009-10-27 | General Electric Company | One-piece baffle infrared suppressor apparatus and method |
US7607306B2 (en) * | 2005-08-03 | 2009-10-27 | General Electric Company | Infrared suppressor apparatus and method |
US20100236244A1 (en) * | 2006-06-28 | 2010-09-23 | Longardner Robert L | Heat absorbing and reflecting shield for air breathing heat engine |
US8322126B2 (en) * | 2008-05-23 | 2012-12-04 | Rolls-Royce North American Technologies, Inc. | Gas turbine exhaust assembly |
US8776527B1 (en) | 2008-06-17 | 2014-07-15 | Rolls-Royce North American Technologies, Inc. | Techniques to reduce infrared detection of a gas turbine engine |
US20100162680A1 (en) * | 2008-12-31 | 2010-07-01 | Syed Jalaluddin Khalid | Gas turbine engine with ejector |
US8572947B2 (en) * | 2008-12-31 | 2013-11-05 | Rolls-Royce Corporation | Gas turbine engine with ejector |
US9353684B2 (en) * | 2009-12-11 | 2016-05-31 | Northrop Grumman Systems Corporation | Aircraft engine airflow modulation apparatus and method for engine bay cooling and cycle flow matching |
EP2598737B1 (fr) | 2010-07-26 | 2019-02-20 | Rolls-Royce Corporation | Turbine à gaz comprenant un éjecteur |
US9334060B2 (en) | 2012-09-21 | 2016-05-10 | Bell Helicopter Textron Inc. | Infrared suppressing exhaust system |
US9630706B2 (en) | 2013-02-22 | 2017-04-25 | Rolls-Royce Corporation | Positionable ejector member for ejector enhanced boundary layer alleviation |
WO2016140866A1 (fr) * | 2015-03-04 | 2016-09-09 | Sikorsky Aircraft Corporation | Ensemble échappement de turbine à gaz |
CN109611238B (zh) * | 2018-12-24 | 2020-04-24 | 南京航空航天大学 | 一种肋片强化换热红外抑制器及红外抑制方法 |
US11608189B2 (en) * | 2020-08-11 | 2023-03-21 | Textron Innovations Inc | Multistage infrared suppression exhaust system |
CN114151226B (zh) * | 2021-10-20 | 2023-05-05 | 中国航发四川燃气涡轮研究院 | 一种置于直二元收敛喷管流道内的多隔板综合隐身结构 |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3981143A (en) * | 1974-08-15 | 1976-09-21 | The United States Of America As Represented By The Secretary Of The Army | Infrared suppressor |
US4007587A (en) * | 1975-11-19 | 1977-02-15 | Avco Corporation | Apparatus for and method of suppressing infrared radiation emitted from gas turbine engine |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2087076A5 (fr) * | 1970-05-04 | 1971-12-31 | Bertin & Cie | |
US3815360A (en) * | 1971-04-16 | 1974-06-11 | Rohr Industries Inc | Combined infrared and sound suppressor for aircraft jet engine |
US4136518A (en) * | 1972-05-03 | 1979-01-30 | Avco Corporation | Infrared radiation suppressor for a gas turbine engine |
US3930627A (en) * | 1973-10-03 | 1976-01-06 | Summa Corporation | Radiation shielding and gas diffusion apparatus |
-
1978
- 1978-11-13 US US05/960,351 patent/US4295332A/en not_active Expired - Lifetime
-
1979
- 1979-08-30 IL IL58145A patent/IL58145A/xx unknown
- 1979-09-27 GB GB7933579A patent/GB2034414B/en not_active Expired
- 1979-11-10 DE DE19792945439 patent/DE2945439A1/de active Granted
- 1979-11-12 IT IT27209/79A patent/IT1125666B/it active
- 1979-11-13 FR FR7927918A patent/FR2441730A1/fr active Granted
- 1979-11-13 JP JP14609779A patent/JPS5591729A/ja active Granted
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3981143A (en) * | 1974-08-15 | 1976-09-21 | The United States Of America As Represented By The Secretary Of The Army | Infrared suppressor |
US4007587A (en) * | 1975-11-19 | 1977-02-15 | Avco Corporation | Apparatus for and method of suppressing infrared radiation emitted from gas turbine engine |
Also Published As
Publication number | Publication date |
---|---|
JPS5591729A (en) | 1980-07-11 |
US4295332A (en) | 1981-10-20 |
JPS6225853B2 (fr) | 1987-06-05 |
IT1125666B (it) | 1986-05-14 |
DE2945439C2 (fr) | 1988-12-29 |
GB2034414A (en) | 1980-06-04 |
GB2034414B (en) | 1982-08-11 |
DE2945439A1 (de) | 1980-05-22 |
FR2441730B1 (fr) | 1985-03-01 |
IT7927209A0 (it) | 1979-11-12 |
IL58145A (en) | 1982-12-31 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2441730A1 (fr) | Systeme suppresseur de rayonnement infrarouge | |
US5127222A (en) | Buffer region for the nacelle of a gas turbine engine | |
FR2440474A1 (fr) | Moteur a turbine a gaz dont les elements critiques du rotor sont proteges contre le contact direct des gaz chauds | |
FR2732947B1 (fr) | Montage pour coupler un moteur a turbine a gaz a turbosoufflante sur une structure d'avion | |
FR2400618A1 (fr) | Moteur a turbo soufflante refroidi par air et procede de refroidissement de ce moteur | |
FR2452599A1 (fr) | Systeme ameliore pour l'alimentation en air de refroidissement d'une turbomachine | |
FR2445438A1 (fr) | Moteur a turbosoufflante comportant un mecanisme perfectionne d'actionnment d'aubes d'obturation | |
FR2445439A1 (fr) | Moteur a turbosoufflante perfectionne | |
FR2398891A1 (fr) | Turbomachine a cycle de fonctionnement regule | |
FR2372965A1 (fr) | Diffuseur perfectionne pour moteur a turbine a gaz | |
GB1166140A (en) | Apparatus for silencing an engine | |
US2611238A (en) | Exhaust manifold for internalcombustion engines | |
FR2402771A1 (fr) | Moteur a turbine a gaz | |
GB2065863B (en) | Urbo supercharged diesel engine | |
BR9206852A (pt) | Aparelho e método para inflamar gás de baixo valor calórico | |
GB1166270A (en) | Interconnection for Flametubes. | |
GB1182687A (en) | Improvements in or relating to Multiflow Jet Propulsion Engines | |
FR2433106A1 (fr) | Dispositif de prise d'air sur compresseur de moteur a turbine a gaz | |
FR2457982A1 (fr) | Turboreacteur pour aeronef a decollage vertical | |
GB2018362A (en) | Gas turbine engine cooling | |
FR2396352A1 (fr) | Circuit d'attaque pour une servovalve | |
FR2379433A1 (fr) | Systeme de securite pour capotage de nacelle de turboreacteur | |
FR2384953A1 (fr) | Installation d'alimentation en combustible pour moteur a turbine a gaz | |
US2880574A (en) | By-pass turbo jet engine construction | |
EP0122475A3 (en) | Heating installation and method of operating it |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |