DE69909276D1 - Schubdüse einer gasturbine - Google Patents

Schubdüse einer gasturbine

Info

Publication number
DE69909276D1
DE69909276D1 DE69909276T DE69909276T DE69909276D1 DE 69909276 D1 DE69909276 D1 DE 69909276D1 DE 69909276 T DE69909276 T DE 69909276T DE 69909276 T DE69909276 T DE 69909276T DE 69909276 D1 DE69909276 D1 DE 69909276D1
Authority
DE
Germany
Prior art keywords
gas turbine
throttle nozzle
throttle
nozzle
turbine
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.)
Expired - Fee Related
Application number
DE69909276T
Other languages
English (en)
Other versions
DE69909276T2 (de
Inventor
James Crone
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.)
Pratt and Whitney Canada Corp
Original Assignee
Pratt and Whitney Canada Corp
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 Pratt and Whitney Canada Corp filed Critical Pratt and Whitney Canada Corp
Publication of DE69909276D1 publication Critical patent/DE69909276D1/de
Application granted granted Critical
Publication of DE69909276T2 publication Critical patent/DE69909276T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/08Other arrangements or adaptations of exhaust conduits
    • F01N13/082Other arrangements or adaptations of exhaust conduits of tailpipe, e.g. with means for mixing air with exhaust for exhaust cooling, dilution or evacuation
    • 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
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30Exhaust heads, chambers, or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/60Fluid transfer
    • F05D2260/601Fluid transfer using an ejector or a jet pump

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Exhaust Silencers (AREA)
  • Jet Pumps And Other Pumps (AREA)
DE69909276T 1998-04-22 1999-04-21 Schubdüse einer gasturbine Expired - Fee Related DE69909276T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09/063,926 US6109562A (en) 1998-04-22 1998-04-22 Aircraft construction
US63926 1998-04-22
PCT/CA1999/000353 WO1999054204A1 (en) 1998-04-22 1999-04-21 Jet engine exhaust nozzle

Publications (2)

Publication Number Publication Date
DE69909276D1 true DE69909276D1 (de) 2003-08-07
DE69909276T2 DE69909276T2 (de) 2004-02-05

Family

ID=22052409

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69909276T Expired - Fee Related DE69909276T2 (de) 1998-04-22 1999-04-21 Schubdüse einer gasturbine

Country Status (6)

Country Link
US (1) US6109562A (de)
EP (1) EP1071609B1 (de)
JP (1) JP2002512151A (de)
CA (1) CA2329343C (de)
DE (1) DE69909276T2 (de)
WO (1) WO1999054204A1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1497490B1 (de) * 2002-04-10 2012-08-22 Fisher & Paykel Appliances Limited Wäschetrockner
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
CA2830938C (en) 2011-04-28 2015-03-24 Bell Helicopter Textron Inc. Self-aligning inlet plenum system for rotorcraft
US20140060004A1 (en) * 2011-09-20 2014-03-06 Bell Helicopter Textron Inc. Tiltrotor vectored exhaust system
US9969500B2 (en) * 2014-02-06 2018-05-15 Honeywell International Inc. Bifurcated ducts including plenums for stabilizing flow therethrough and exhaust systems including the same
US10279924B2 (en) * 2017-05-12 2019-05-07 Bell Helicopter Textron Inc. Engine exhaust duct mounting assembly
CN109606709A (zh) * 2018-11-14 2019-04-12 中国直升机设计研究所 一种用于直升机的排气管安装结构
CN114178790B (zh) * 2021-12-08 2023-03-17 中国航发南方工业有限公司 发动机排气段制作工艺
US11732633B2 (en) * 2022-01-04 2023-08-22 Caterpillar Inc. Exhaust discharge system
FR3140117A1 (fr) * 2022-09-27 2024-03-29 Airbus Helicopters Aéronef muni d’un moteur et d’un conduit d’échappement drainé autour d’une tuyère d’éjection du moteur
FR3141681A1 (fr) 2022-11-09 2024-05-10 Airbus Helicopters Aéronef muni d’un conduit d’échappement couplé à un système de stabilisation

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2231239A (en) * 1939-05-16 1941-02-11 Curtiss Wright Corp Cowling exhaust outlet
US2650666A (en) * 1946-07-25 1953-09-01 Dorand Rene Rotary-wing aircraft with jet-driven rotor
US2605851A (en) * 1946-11-30 1952-08-05 Chrysler Corp Air intake for aircraft turbopropeller power plant
US2653585A (en) * 1949-12-22 1953-09-29 United Aircraft Corp Engine cooling and exhaust arrangement
FR1512579A (fr) * 1966-12-30 1968-02-09 Sud Aviation Dispositif sustentateur et propulseur pour appareil à réaction du type combiné hélicoptère-autogire
GB2044359B (en) * 1979-03-16 1982-10-27 Rolls Royce Gas turbine engine air intakes
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
US4388804A (en) * 1981-08-17 1983-06-21 J. I. Case Company Exhaust assembly for tractors
US4519543A (en) * 1982-04-07 1985-05-28 Rolls-Royce Inc. Vectorable nozzles for turbomachines
US4552309A (en) * 1982-04-07 1985-11-12 Rolls-Royce Inc. Variable geometry nozzles for turbomachines
GB2266080A (en) * 1992-04-16 1993-10-20 Rolls Royce Plc Mounting arrangement for a gas turbine engine.
DE19524731A1 (de) * 1995-07-07 1997-01-09 Bmw Rolls Royce Gmbh Turboprop-Triebwerk mit einem Luft-Ölkühler
CA2226441C (en) * 1995-07-07 2007-01-23 Kurt Steiner Turboprop engine with an air-oil cooler

Also Published As

Publication number Publication date
JP2002512151A (ja) 2002-04-23
EP1071609B1 (de) 2003-07-02
EP1071609A1 (de) 2001-01-31
CA2329343C (en) 2007-05-15
US6109562A (en) 2000-08-29
CA2329343A1 (en) 1999-10-28
DE69909276T2 (de) 2004-02-05
WO1999054204A1 (en) 1999-10-28

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee