IT8019702A0 - Cappottatura di motore a turbina agas. - Google Patents

Cappottatura di motore a turbina agas.

Info

Publication number
IT8019702A0
IT8019702A0 IT8019702A IT1970280A IT8019702A0 IT 8019702 A0 IT8019702 A0 IT 8019702A0 IT 8019702 A IT8019702 A IT 8019702A IT 1970280 A IT1970280 A IT 1970280A IT 8019702 A0 IT8019702 A0 IT 8019702A0
Authority
IT
Italy
Prior art keywords
turbine engine
engine cowl
agas
agas turbine
cowl
Prior art date
Application number
IT8019702A
Other languages
English (en)
Other versions
IT1141160B (it
Inventor
John Robert Ballard
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of IT8019702A0 publication Critical patent/IT8019702A0/it
Application granted granted Critical
Publication of IT1141160B publication Critical patent/IT1141160B/it

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—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)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Separating Particles In Gases By Inertia (AREA)
IT19702/80A 1979-03-16 1980-02-05 Cappottatura di motore a turbina a gas IT1141160B (it)

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 true IT8019702A0 (it) 1980-02-05
IT1141160B 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)

* Cited by examiner, † Cited by third party
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
US7866600B2 (en) * 2005-04-13 2011-01-11 Sikorsky Aircraft Corporation Integrated engine air particle filter assembly
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
PL3056423T3 (pl) 2015-02-16 2018-04-30 Airbus Helicopters Deutschland GmbH Statek powietrzny z kadłubem, który wyznacza co najmniej obszar wewnętrzny i obszar mieszczący układ napędowy
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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1201096A (en) * 1966-11-15 1970-08-05 United Aircraft Corp Air particle separator
US3421296A (en) * 1966-11-15 1969-01-14 United Aircraft Corp Engine inlet 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

Also Published As

Publication number Publication date
FR2451316A1 (fr) 1980-10-10
GB2044359B (en) 1982-10-27
FR2451316B1 (it) 1983-03-18
DE3009510A1 (de) 1980-09-18
US4291530A (en) 1981-09-29
DE3009510C2 (de) 1983-03-10
JPS577292B2 (it) 1982-02-09
GB2044359A (en) 1980-10-15
JPS55128626A (en) 1980-10-04
IT1141160B (it) 1986-10-01

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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