BRPI0911399A2 - dispositivo de resfriamento de uma parede, e, turbomotor para aeronave. - Google Patents

dispositivo de resfriamento de uma parede, e, turbomotor para aeronave.

Info

Publication number
BRPI0911399A2
BRPI0911399A2 BRPI0911399A BRPI0911399A BRPI0911399A2 BR PI0911399 A2 BRPI0911399 A2 BR PI0911399A2 BR PI0911399 A BRPI0911399 A BR PI0911399A BR PI0911399 A BRPI0911399 A BR PI0911399A BR PI0911399 A2 BRPI0911399 A2 BR PI0911399A2
Authority
BR
Brazil
Prior art keywords
cooling device
wall cooling
turbomotor
aircraft
aircraft turbomotor
Prior art date
Application number
BRPI0911399A
Other languages
English (en)
Inventor
Claude Mons
Original Assignee
Snecma
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 Snecma filed Critical Snecma
Publication of BRPI0911399A2 publication Critical patent/BRPI0911399A2/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00—Tubular elements; Assemblies of tubular elements
    • F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • 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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/077—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type the plant being of the multiple flow type, i.e. having three or more flows
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L2201/00—Properties
    • C08L2201/12—Shape memory
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/505—Shape memory behaviour
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
    • F28F2013/005—Thermal joints
    • F28F2013/008—Variable conductance materials; Thermal switches
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2255/00—Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes
    • F28F2255/04—Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes comprising shape memory alloys or bimetallic elements
    • 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)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Thermal Sciences (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
BRPI0911399A 2008-04-17 2009-04-15 dispositivo de resfriamento de uma parede, e, turbomotor para aeronave. BRPI0911399A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0852609A FR2930324B1 (fr) 2008-04-17 2008-04-17 Dispositif de refroidissement d'une paroi
PCT/FR2009/050688 WO2009138613A1 (fr) 2008-04-17 2009-04-15 Dispositif de refroidissement d'une paroi

Publications (1)

Publication Number Publication Date
BRPI0911399A2 true BRPI0911399A2 (pt) 2016-01-05

Family

ID=40149747

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0911399A BRPI0911399A2 (pt) 2008-04-17 2009-04-15 dispositivo de resfriamento de uma parede, e, turbomotor para aeronave.

Country Status (10)

Country Link
US (1) US8561386B2 (pt)
EP (1) EP2288862B1 (pt)
CN (1) CN102007363A (pt)
AT (1) ATE533022T1 (pt)
BR (1) BRPI0911399A2 (pt)
CA (1) CA2721381A1 (pt)
ES (1) ES2377049T3 (pt)
FR (1) FR2930324B1 (pt)
RU (1) RU2010146634A (pt)
WO (1) WO2009138613A1 (pt)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10119059B2 (en) 2011-04-11 2018-11-06 Jun Cui Thermoelastic cooling
US9429071B2 (en) * 2011-06-23 2016-08-30 Continuum Dynamics, Inc. Supersonic engine inlet diffuser with deployable vortex generators
US10018385B2 (en) 2012-03-27 2018-07-10 University Of Maryland, College Park Solid-state heating or cooling systems, devices, and methods
US9671030B2 (en) * 2012-03-30 2017-06-06 General Electric Company Metallic seal assembly, turbine component, and method of regulating airflow in turbo-machinery
US9316152B2 (en) * 2012-06-13 2016-04-19 General Electric Company Active control of bucket cooling supply for turbine
EP2937510A1 (en) * 2014-04-25 2015-10-28 Siemens Aktiengesellschaft Turbine with improved cooling means
FR3028021B1 (fr) * 2014-10-30 2019-03-22 Safran Aircraft Engines Echangeur de chaleur turbomoteur comportant un tel echangeur
US9903274B2 (en) * 2014-11-07 2018-02-27 General Electric Company Variable geometry heat exchanger apparatus
JP2017040446A (ja) * 2015-08-20 2017-02-23 いすゞ自動車株式会社 熱交換器
CN105066530B (zh) * 2015-08-31 2018-04-03 天津商业大学 一种固体压缩制冷方法及装置
US10113818B2 (en) * 2016-01-27 2018-10-30 Garrett Transportation I Inc. Bimetallic fin with themo-adjusting turbulation feature
US11008943B2 (en) 2016-08-31 2021-05-18 Unison Industries, Llc Fan casing assembly with cooler and method of moving
US20180058472A1 (en) * 2016-08-31 2018-03-01 Unison Industries, Llc Fan casing assembly with cooler and method of moving
CA3035518A1 (en) * 2016-09-08 2018-03-15 Unison Industries, Llc Fan casing assembly with cooler
BR102017027998A2 (pt) * 2017-01-13 2018-12-04 Unison Industries, Llc refrigerante de revestimento de ventilador
FR3064735B1 (fr) * 2017-04-03 2021-01-01 Valeo Systemes Thermiques Dispositif d’echange thermique pour vehicule automobile
CN108344323A (zh) * 2018-02-22 2018-07-31 上海理工大学 一种换热装置
US11492972B2 (en) 2019-12-30 2022-11-08 General Electric Company Differential alpha variable area metering
US11674396B2 (en) 2021-07-30 2023-06-13 General Electric Company Cooling air delivery assembly
US11920500B2 (en) 2021-08-30 2024-03-05 General Electric Company Passive flow modulation device
US11692448B1 (en) 2022-03-04 2023-07-04 General Electric Company Passive valve assembly for a nozzle of a gas turbine engine
US11834993B1 (en) * 2023-03-29 2023-12-05 Pratt & Whitney Canada Corp. Engine exhaust reverse flow prevention
US12221927B2 (en) 2023-04-21 2025-02-11 Pratt & Whitney Canada Corp. Flammable fluid reservoir
US12044173B1 (en) 2023-04-28 2024-07-23 Pratt & Whitney Canada Corp. Engine exhaust reverse flow prevention
US12326092B2 (en) 2023-05-16 2025-06-10 Pratt & Whitney Canada Corp. Engine exhaust reverse flow prevention
US12203415B2 (en) 2023-06-20 2025-01-21 Pratt & Whitney Canada Corp. Engine exhaust reverse flow prevention
US12291997B1 (en) 2024-04-30 2025-05-06 General Electric Company Variable area turbine nozzle assembly

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4807433A (en) * 1983-05-05 1989-02-28 General Electric Company Turbine cooling air modulation
JPS60164192A (ja) * 1984-02-06 1985-08-27 Toshiba Corp 排熱回収用熱交換器
JPS61186785A (ja) 1985-02-15 1986-08-20 Matsushita Electric Works Ltd 熱搬送器
DE3542762A1 (de) * 1985-12-04 1987-06-11 Mtu Muenchen Gmbh Einrichtung zur steuerung oder regelung von gasturbinentriebwerken bzw. gasturbinenstrahltriebwerken
US5171024A (en) * 1988-05-23 1992-12-15 Westinghouse Electric Corp. Reactor coolant pump shaft seal utilizing shape memory metal
DE19919835A1 (de) * 1999-04-30 2000-11-09 Schott Rohrglas Gmbh Sonnenkollektor mit formvariablem Abstandshalter
US7204472B2 (en) * 2004-03-12 2007-04-17 Gm Global Technology Operations, Inc. Active pressure relief valves and methods of use
FR2873167B1 (fr) 2004-07-15 2007-11-02 Hurel Hispano Sa Dispositif de refroidissement de la tuyere primaire d'un turboreacteur a double flux
US7340883B2 (en) * 2004-11-12 2008-03-11 The Boeing Company Morphing structure
US8038389B2 (en) * 2006-01-04 2011-10-18 General Electric Company Method and apparatus for assembling turbine nozzle assembly
US8201413B2 (en) * 2006-07-24 2012-06-19 United Technologies Corporation Seal land with air injection for cavity purging
GB0700238D0 (en) * 2007-01-06 2007-02-14 Rolls Royce Plc Nozzle arrangement
FR2924168B1 (fr) * 2007-11-23 2015-09-04 Snecma Tuyere de soufflante a section reglable

Also Published As

Publication number Publication date
EP2288862A1 (fr) 2011-03-02
WO2009138613A1 (fr) 2009-11-19
ES2377049T3 (es) 2012-03-22
FR2930324B1 (fr) 2011-06-17
ATE533022T1 (de) 2011-11-15
US20110030337A1 (en) 2011-02-10
EP2288862B1 (fr) 2011-11-09
RU2010146634A (ru) 2012-05-27
US8561386B2 (en) 2013-10-22
FR2930324A1 (fr) 2009-10-23
CA2721381A1 (fr) 2009-11-19
CN102007363A (zh) 2011-04-06

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE AS 5A, 6A E 7A ANUIDADES.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2384 DE 13-09-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.