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DE602008001141D1 - Verbesserung an Drehflügelflugzeugen, die mit Turbotriebwerken ausgestattet sind - Google Patents

Verbesserung an Drehflügelflugzeugen, die mit Turbotriebwerken ausgestattet sind

Info

Publication number
DE602008001141D1
DE602008001141D1 DE602008001141T DE602008001141T DE602008001141D1 DE 602008001141 D1 DE602008001141 D1 DE 602008001141D1 DE 602008001141 T DE602008001141 T DE 602008001141T DE 602008001141 T DE602008001141 T DE 602008001141T DE 602008001141 D1 DE602008001141 D1 DE 602008001141D1
Authority
DE
Germany
Prior art keywords
rotary
improvement
wing aircraft
aircraft equipped
turbocharged engines
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.)
Active
Application number
DE602008001141T
Other languages
English (en)
Inventor
Bernard Certain
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 Helicopters SAS
Original Assignee
Eurocopter France SA
Eurocopter SA
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 Eurocopter France SA, Eurocopter SA filed Critical Eurocopter France SA
Publication of DE602008001141D1 publication Critical patent/DE602008001141D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B64C27/16—Drive of rotors by means, e.g. propellers, mounted on rotor blades
    • B64C27/18—Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • 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
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • B64D35/02—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • F02C3/103—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor the compressor being of the centrifugal type
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
    • 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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/329—Application in turbines in gas turbines in helicopters
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE602008001141T 2007-10-26 2008-10-13 Verbesserung an Drehflügelflugzeugen, die mit Turbotriebwerken ausgestattet sind Active DE602008001141D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0707547A FR2922860B1 (fr) 2007-10-26 2007-10-26 Amelioration aux giravions equipes de turbomoteurs

Publications (1)

Publication Number Publication Date
DE602008001141D1 true DE602008001141D1 (de) 2010-06-17

Family

ID=39363991

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602008001141T Active DE602008001141D1 (de) 2007-10-26 2008-10-13 Verbesserung an Drehflügelflugzeugen, die mit Turbotriebwerken ausgestattet sind

Country Status (8)

Country Link
US (1) US20090113871A1 (de)
EP (1) EP2052967B1 (de)
KR (1) KR20090042718A (de)
CN (1) CN101417592B (de)
CA (1) CA2641962C (de)
DE (1) DE602008001141D1 (de)
FR (1) FR2922860B1 (de)
RU (1) RU2458826C2 (de)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2899640B1 (fr) * 2006-04-05 2011-11-25 Eurocopter France Procede et dispositif pour realiser un controle de l'etat de sante d'un turbomoteur d'un giravion bimoteur
FR2961260B1 (fr) * 2010-06-15 2014-05-02 Turbomeca Architecture de turbomoteur non lubrifie
US9267438B2 (en) 2011-10-11 2016-02-23 Pratt & Whitney Canada Corp. Starting of aircraft engine
US9429077B2 (en) 2011-12-06 2016-08-30 Pratt & Whitney Canada Corp. Multiple turboshaft engine control method and system for helicopters
US9180964B2 (en) 2013-03-15 2015-11-10 Bell Helicopter Textron Inc. Autorotative enhancement system
FR3008679B1 (fr) * 2013-07-16 2015-08-14 Eurocopter France Installation motrice modulaire et aeronef muni d'un rotor de sustentation
FR3019222B1 (fr) * 2014-03-27 2018-07-13 Safran Helicopter Engines Turbomoteur, helicoptere bimoteur equipe d'un tel turbomoteur et procede d'optimisation du regime de super-ralenti a puissance nulle d'un tel helicoptere bimoteur
FR3019588B1 (fr) * 2014-04-08 2019-06-14 Safran Helicopter Engines Dispositif d'assistance d'un systeme propulsif a propergol solide d'un helicoptere monomoteur, helicoptere monomoteur comprenant un tel dispositif et procede correspondant
US10066547B2 (en) * 2014-07-01 2018-09-04 United Technologies Corporation Combined two engine cycle with at least one recuperated cycle engine for rotor drive
FR3024180B1 (fr) * 2014-07-28 2016-07-22 Turbomeca Dispositif pneumatique de reactivation rapide d'un turbomoteur, architecture d'un systeme propulsif d'un helicoptere multi-moteur equipe d'un tel dispositif et helicoptere correspondant
FR3024707B1 (fr) * 2014-08-07 2018-03-23 Turbomeca Dispositif d'assistance rapide pour une turbomachine a turbine libre d'un aeronef
EP4538181A3 (de) * 2015-09-15 2025-06-18 Sikorsky Aircraft Corporation Antriebssystemanordnung für drehflügler
CN107757929A (zh) * 2016-08-23 2018-03-06 吴茂盛 空气动力直升机
US10753225B2 (en) * 2017-03-31 2020-08-25 The Boeing Company Engine turning motor via pneumatic or hydraulic motor
US11186185B2 (en) * 2017-05-31 2021-11-30 Textron Innovations Inc. Rotor brake effect by using electric distributed anti-torque generators and opposing electric motor thrust to slow a main rotor
US11519434B2 (en) 2017-08-10 2022-12-06 Paul NEISER Apparatus and method for fluid manipulation
US12270301B2 (en) 2017-08-10 2025-04-08 Paul NEISER System and method for fluid manipulation
CN109720586A (zh) * 2017-10-30 2019-05-07 成都飞机工业（集团）有限责任公司 一种附面层隔道
US11267563B2 (en) 2018-10-29 2022-03-08 Pratt & Whitney Canada Corp. Aircraft engine with clutch and mechanical lock
JP7049234B2 (ja) * 2018-11-15 2022-04-06 本田技研工業株式会社 ハイブリッド飛行体
CN112173137B (zh) * 2020-09-25 2022-09-30 中国直升机设计研究所 一种直升机降温进气道

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2923128A (en) * 1955-08-17 1960-02-02 United Aircraft Corp Fuel control for a split turbine type power plant
US3002710A (en) * 1956-05-15 1961-10-03 Sud Aviation Helicopters
FR1325704A (fr) * 1962-03-14 1963-05-03 Sud Aviation Perfectionnement apporté aux boîtes de transmission pour hélicoptères monorotor à plusieurs turbines
US3195349A (en) * 1963-01-07 1965-07-20 Boeing Co Method and apparatus for determining the available power output of an engine
US3548597A (en) * 1968-09-16 1970-12-22 Alexander Hossen Etessam Turbine engine for aircraft having a supplementary compressor driven by a supplementary turbine
US3922852A (en) * 1973-10-17 1975-12-02 Gen Electric Variable pitch fan for gas turbine engine
FR2568541B1 (fr) * 1984-08-06 1987-03-20 Aerospatiale Boite de transmission principale pour helicoptere bimoteur
DE3708596A1 (de) * 1987-03-17 1988-09-29 Mtu Muenchen Gmbh Gasturbinenanlage fuer hubschrauber
US6308512B1 (en) * 1999-06-10 2001-10-30 Enhanced Turbine Output Holding, Llc Supercharging system for gas turbines
EP1362984B1 (de) * 2002-05-16 2007-04-25 ROLLS-ROYCE plc Gasturbine
RU2236991C1 (ru) * 2002-12-30 2004-09-27 Открытое Акционерное Общество "Московский Вертолетный Завод Им. М.Л. Миля" Вентиляторная установка вертолета
US20050151001A1 (en) * 2003-07-02 2005-07-14 Loper Arthur W. Compound helicopter
US7111462B2 (en) * 2004-07-21 2006-09-26 Steward-Davis International, Inc. Onboard supplemental power system at varying high altitudes
RU2282564C2 (ru) * 2004-10-21 2006-08-27 Валентин Алексеевич Малкин Вертолет
US7513120B2 (en) * 2005-04-08 2009-04-07 United Technologies Corporation Electrically coupled supercharger for a gas turbine engine

Also Published As

Publication number Publication date
RU2008141617A (ru) 2010-04-27
CN101417592B (zh) 2012-05-23
RU2458826C2 (ru) 2012-08-20
EP2052967B1 (de) 2010-05-05
FR2922860A1 (fr) 2009-05-01
US20090113871A1 (en) 2009-05-07
CA2641962C (fr) 2011-12-13
CN101417592A (zh) 2009-04-29
FR2922860B1 (fr) 2010-01-22
CA2641962A1 (fr) 2009-04-26
KR20090042718A (ko) 2009-04-30
EP2052967A1 (de) 2009-04-29

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Legal Events

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