IN163828B - - Google Patents
Info
- Publication number
- IN163828B IN163828B IN435/DEL/85A IN435DE1985A IN163828B IN 163828 B IN163828 B IN 163828B IN 435DE1985 A IN435DE1985 A IN 435DE1985A IN 163828 B IN163828 B IN 163828B
- Authority
- IN
- India
Links
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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
-
- 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
- B64D2033/045—Arrangement 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)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Exhaust Silencers (AREA)
- Toys (AREA)
- Supercharger (AREA)
- Exhaust Gas After Treatment (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR8408709A FR2565293B1 (fr) | 1984-06-04 | 1984-06-04 | Ensemble dilueur-deviateur de jet pour turbomoteur d'aerodyne |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IN163828B true IN163828B (enExample) | 1988-11-19 |
Family
ID=9304662
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IN435/DEL/85A IN163828B (enExample) | 1984-06-04 | 1985-05-30 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US4662174A (enExample) |
| EP (1) | EP0165167B1 (enExample) |
| JP (1) | JPS61247857A (enExample) |
| DE (1) | DE3560391D1 (enExample) |
| FR (1) | FR2565293B1 (enExample) |
| IN (1) | IN163828B (enExample) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5699662A (en) * | 1996-05-28 | 1997-12-23 | Lockheed Martin Corporation | Infrared suppression exhaust duct system for a turboprop propulsion system for an aircraft |
| US6122980A (en) * | 1998-06-26 | 2000-09-26 | Horiba Instruments, Inc. | Mixing system |
| US6971240B2 (en) | 2004-03-30 | 2005-12-06 | General Electric Company | Methods and apparatus for exhausting gases from gas turbine engines |
| US7484494B2 (en) * | 2006-01-27 | 2009-02-03 | Gm Global Technology Operations, Inc. | Method and apparatus for a spark-ignited direct injection engine |
| US20090217643A1 (en) * | 2008-02-29 | 2009-09-03 | Sokhey Jagdish S | Gas discharge device for a vehicle engine |
| US20140060004A1 (en) * | 2011-09-20 | 2014-03-06 | Bell Helicopter Textron Inc. | Tiltrotor vectored exhaust system |
| US10407177B2 (en) | 2014-05-30 | 2019-09-10 | Sikorsky Aircraft Corporation | Convertible engine exhaust for rotocraft |
| WO2016043943A2 (en) | 2014-08-28 | 2016-03-24 | Sikorsky Aircraft Corporation | Pitch control system |
| US20220154613A1 (en) * | 2020-11-17 | 2022-05-19 | Pacific Crown Helicopters | Deflector exhaust nozzle for as350/ec130 and for other single engine helicopters |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1144879A (fr) * | 1955-03-30 | 1957-10-18 | Napier & Son Ltd | Tubulure d'échappement pour groupe propulseur d'avion du type à turbine à gaz |
| US3053477A (en) * | 1958-08-27 | 1962-09-11 | Daimler Benz Ag | Aircraft, especially vertical take-off aircraft |
| DE1066428B (enExample) * | 1959-01-17 | |||
| US3279192A (en) * | 1963-12-30 | 1966-10-18 | Gen Electric | Variable area exhaust nozzle |
| US3989193A (en) * | 1974-03-02 | 1976-11-02 | Motoren- Und Turbinen-Union Munchen Gmbh M.A.N. Maybach Mercedes-Benz | Device for varying the gas exit area of an exhaust nozzle for a jet deflecting device |
| US3979065A (en) * | 1974-10-31 | 1976-09-07 | United Technologies Corporation | Cooling liner for an exhaust nozzle |
| US3921906A (en) * | 1974-12-02 | 1975-11-25 | Gen Electric | Infrared suppression system for a gas turbine engine |
| US4018046A (en) * | 1975-07-17 | 1977-04-19 | Avco Corporation | Infrared radiation suppressor for gas turbine engine |
| US4007587A (en) * | 1975-11-19 | 1977-02-15 | Avco Corporation | Apparatus for and method of suppressing infrared radiation emitted from gas turbine engine |
| FI782193A7 (fi) * | 1977-07-16 | 1979-01-17 | Jastram Werke | Foerfarande foer aostadkommande av skjutkraft vid styrdrivanordningar foer fartyg och en haerfoer avsedd styrdrivanordning |
| US4215537A (en) * | 1978-07-27 | 1980-08-05 | Avco Corporation | Apparatus for and method of suppressing infrared radiation emitted from gas turbine engine |
| US4312480A (en) * | 1979-11-26 | 1982-01-26 | Hughes Helicopters, Inc. | Radiation shielding and gas diffusion apparatus |
| US4369937A (en) * | 1981-05-18 | 1983-01-25 | The United States Of America As Represented By The Secretary Of The Army | Hinging and latching apparatus |
| FR2508412A1 (en) * | 1981-06-25 | 1982-12-31 | Hughes Helicopters Inc | IR radiation shield for military aircraft - has air-cooled gas conductor to block outlet line-of-sight and cool heated gases |
| DE3129305A1 (de) * | 1981-07-24 | 1983-02-10 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Einrichtung zur infrarotunterdrueckung fuer fluggeraete, insbesondere hubschrauber |
| GB2114229B (en) * | 1981-11-03 | 1984-11-21 | Rolls Royce | Gas turbine engine infra-red radiation suppressor |
| US4544098A (en) * | 1982-12-27 | 1985-10-01 | United Technologies Corporation | Cooled exhaust nozzle flaps |
-
1984
- 1984-06-04 FR FR8408709A patent/FR2565293B1/fr not_active Expired
-
1985
- 1985-05-30 IN IN435/DEL/85A patent/IN163828B/en unknown
- 1985-06-03 US US06/740,783 patent/US4662174A/en not_active Expired - Lifetime
- 1985-06-03 DE DE8585401085T patent/DE3560391D1/de not_active Expired
- 1985-06-03 EP EP85401085A patent/EP0165167B1/fr not_active Expired
- 1985-06-04 JP JP60121378A patent/JPS61247857A/ja active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0262696B2 (enExample) | 1990-12-26 |
| EP0165167A1 (fr) | 1985-12-18 |
| FR2565293B1 (fr) | 1986-10-17 |
| US4662174A (en) | 1987-05-05 |
| EP0165167B1 (fr) | 1987-07-29 |
| DE3560391D1 (en) | 1987-09-03 |
| JPS61247857A (ja) | 1986-11-05 |
| FR2565293A1 (fr) | 1985-12-06 |