JPS61247857A - 重航空機のタ−ビンエンジンの排煙希釈偏向装置 - Google Patents

重航空機のタ−ビンエンジンの排煙希釈偏向装置

Info

Publication number
JPS61247857A
JPS61247857A JP60121378A JP12137885A JPS61247857A JP S61247857 A JPS61247857 A JP S61247857A JP 60121378 A JP60121378 A JP 60121378A JP 12137885 A JP12137885 A JP 12137885A JP S61247857 A JPS61247857 A JP S61247857A
Authority
JP
Japan
Prior art keywords
nozzle
deflection device
dilution
exhaust gas
mixer
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
Application number
JP60121378A
Other languages
English (en)
Japanese (ja)
Other versions
JPH0262696B2 (enExample
Inventor
フランソワ、バランタン、トウルメ
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Publication of JPS61247857A publication Critical patent/JPS61247857A/ja
Publication of JPH0262696B2 publication Critical patent/JPH0262696B2/ja
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • B64D2033/045Arrangement 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)
JP60121378A 1984-06-04 1985-06-04 重航空機のタ−ビンエンジンの排煙希釈偏向装置 Granted JPS61247857A (ja)

Applications Claiming Priority (2)

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
FR8408709 1984-06-04

Publications (2)

Publication Number Publication Date
JPS61247857A true JPS61247857A (ja) 1986-11-05
JPH0262696B2 JPH0262696B2 (enExample) 1990-12-26

Family

ID=9304662

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60121378A Granted JPS61247857A (ja) 1984-06-04 1985-06-04 重航空機のタ−ビンエンジンの排煙希釈偏向装置

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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
IN163828B (enExample) 1988-11-19
EP0165167B1 (fr) 1987-07-29
DE3560391D1 (en) 1987-09-03
FR2565293A1 (fr) 1985-12-06

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