IN2012DE00783A - - Google Patents

Info

Publication number
IN2012DE00783A
IN2012DE00783A IN783DE2012A IN2012DE00783A IN 2012DE00783 A IN2012DE00783 A IN 2012DE00783A IN 783DE2012 A IN783DE2012 A IN 783DE2012A IN 2012DE00783 A IN2012DE00783 A IN 2012DE00783A
Authority
IN
India
Prior art keywords
exhaust duct
aircraft
drive means
exhaust gas
exhaust
Prior art date
Application number
Other languages
English (en)
Inventor
Massimo Brunetti
Andrea Cogliati
Dario Iannucci
Alessandro Scandroglio
Original Assignee
Agustawestland Spa
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 Agustawestland Spa filed Critical Agustawestland Spa
Publication of IN2012DE00783A publication Critical patent/IN2012DE00783A/en

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
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust heads, chambers, or the like
    • 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
    • H—ELECTRICITY
    • H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N10/00—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects
    • H10N10/10—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects operating with only the Peltier or Seebeck effects
    • H10N10/13—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects operating with only the Peltier or Seebeck effects characterised by the heat-exchanging means at the junction
    • H—ELECTRICITY
    • H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N10/00—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects
    • H10N10/10—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects operating with only the Peltier or Seebeck effects
    • H10N10/17—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects operating with only the Peltier or Seebeck effects characterised by the structure or configuration of the cell or thermocouple forming the device
    • 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
    • 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
    • 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
    • F05D2220/60—Application making use of surplus or waste energy
    • 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
    • Y02T50/50—On board measures aiming to increase energy efficiency
    • 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)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Exhaust Silencers (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Hybrid Cells (AREA)
  • Electric Suction Cleaners (AREA)
IN783DE2012 2011-03-18 2012-03-16 IN2012DE00783A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP11425066A EP2500269A1 (de) 2011-03-18 2011-03-18 Zum Schwebeflug fähiges Luftfahrzeug

Publications (1)

Publication Number Publication Date
IN2012DE00783A true IN2012DE00783A (de) 2015-08-21

Family

ID=45814428

Family Applications (1)

Application Number Title Priority Date Filing Date
IN783DE2012 IN2012DE00783A (de) 2011-03-18 2012-03-16

Country Status (7)

Country Link
US (1) US8939397B2 (de)
EP (2) EP2500269A1 (de)
JP (1) JP2012197073A (de)
KR (1) KR101872867B1 (de)
CN (1) CN102689691B (de)
IN (1) IN2012DE00783A (de)
RU (1) RU2595735C2 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
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US9666781B2 (en) * 2013-08-19 2017-05-30 The Boeing Company Methods for recovering waste energy from bleed air ducts
JP2015039925A (ja) * 2013-08-21 2015-03-02 株式会社Ｉｈｉエアロスペース スラスタ用熱エネルギ回収装置
EP2868896A1 (de) * 2013-11-05 2015-05-06 Rolls-Royce Deutschland Ltd & Co KG Turbomaschine mit Energiegewinnungsvorrichtung, Energiegewinnungsvorrichtung und Verfahren zur Energiegewinnung
CN105217046B (zh) * 2015-09-28 2017-08-29 易瓦特科技股份公司 具有柔性排气管的排气通道
FR3042539B1 (fr) * 2015-10-16 2017-11-24 Labinal Power Systems Systeme anti-flexion pour turbomachine d'aeronef
US10291156B2 (en) * 2015-10-30 2019-05-14 Ge Aviation Systems Llc Combined hybrid thermionic and thermoelectric generator
GB2559956B (en) * 2017-02-15 2020-09-16 Ge Aviat Systems Ltd Power distribution node for a power architecture
US10366909B2 (en) * 2017-07-27 2019-07-30 Taiwan Semiconductor Manufacturing Company, Ltd. Thermal chamber exhaust structure and method
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
KR102407759B1 (ko) * 2020-10-13 2022-06-13 현대오토에버 주식회사 비행체용 전력 분배 시스템 및 방법
WO2022095008A1 (zh) * 2020-11-09 2022-05-12 常州机电职业技术学院 一种汽车排气系统余热回收利用装置及回收利用方法

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US4018046A (en) * 1975-07-17 1977-04-19 Avco Corporation Infrared radiation suppressor for gas turbine engine
GB2044359B (en) * 1979-03-16 1982-10-27 Rolls Royce Gas turbine engine air intakes
GB2114229B (en) * 1981-11-03 1984-11-21 Rolls Royce Gas turbine engine infra-red radiation suppressor
SU1285168A1 (ru) * 1985-08-01 1987-01-23 Институт технической теплофизики АН УССР Глушитель шума выхлопа двигател внутреннего сгорани
US5699965A (en) * 1989-06-30 1997-12-23 Sikorsky Aircraft Corporation Infrared suppressor for a gas turbine engine
US6134879A (en) * 1989-12-21 2000-10-24 United Technologies Corporation Suppression system for a gas turbine engine
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Also Published As

Publication number Publication date
CN102689691A (zh) 2012-09-26
EP2500270A2 (de) 2012-09-19
RU2595735C2 (ru) 2016-08-27
EP2500270A8 (de) 2012-12-12
US20120233988A1 (en) 2012-09-20
RU2012110189A (ru) 2013-09-27
EP2500270A3 (de) 2013-10-23
EP2500269A1 (de) 2012-09-19
CN102689691B (zh) 2016-02-17
EP2500270B1 (de) 2015-08-26
KR20120106660A (ko) 2012-09-26
US8939397B2 (en) 2015-01-27
KR101872867B1 (ko) 2018-07-02
JP2012197073A (ja) 2012-10-18

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