FR3015573B1 - Turbomachine d'aeronef comportant un echangeur de chaleur du type pre-refroidisseur - Google Patents
Turbomachine d'aeronef comportant un echangeur de chaleur du type pre-refroidisseurInfo
- Publication number
- FR3015573B1 FR3015573B1 FR1362956A FR1362956A FR3015573B1 FR 3015573 B1 FR3015573 B1 FR 3015573B1 FR 1362956 A FR1362956 A FR 1362956A FR 1362956 A FR1362956 A FR 1362956A FR 3015573 B1 FR3015573 B1 FR 3015573B1
- Authority
- FR
- France
- Prior art keywords
- heat exchanger
- cooling type
- aircraft turbomachine
- turbomachine
- aircraft
- 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
Links
- 238000001816 cooling Methods 0.000 title 1
Classifications
-
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
- F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/10—Aircraft characterised by the type or position of power plant of gas-turbine type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
-
- 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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- 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
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
- F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
-
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
- B64D15/04—Hot gas application
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0618—Environmental Control Systems with arrangements for reducing or managing bleed air, using another air source, e.g. ram air
-
- 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
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
-
- 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
- F05D2260/213—Heat transfer, e.g. cooling by the provision of a heat exchanger within the cooling circuit
-
- 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
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1362956A FR3015573B1 (fr) | 2013-12-19 | 2013-12-19 | Turbomachine d'aeronef comportant un echangeur de chaleur du type pre-refroidisseur |
US15/104,445 US11060462B2 (en) | 2013-12-19 | 2014-12-15 | Aircraft turbomachine comprising a heat exchanger of the precooler type |
PCT/FR2014/053349 WO2015092251A1 (fr) | 2013-12-19 | 2014-12-15 | Turbomachine d'aéronef comportant un échangeur de chaleur du type pré-refroidisseur |
CA2933353A CA2933353C (fr) | 2013-12-19 | 2014-12-15 | Turbomachine d'aeronef comportant un echangeur de chaleur du type pre-refroidisseur |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1362956A FR3015573B1 (fr) | 2013-12-19 | 2013-12-19 | Turbomachine d'aeronef comportant un echangeur de chaleur du type pre-refroidisseur |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3015573A1 FR3015573A1 (fr) | 2015-06-26 |
FR3015573B1 true FR3015573B1 (fr) | 2015-12-11 |
Family
ID=50289974
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1362956A Active FR3015573B1 (fr) | 2013-12-19 | 2013-12-19 | Turbomachine d'aeronef comportant un echangeur de chaleur du type pre-refroidisseur |
Country Status (4)
Country | Link |
---|---|
US (1) | US11060462B2 (fr) |
CA (1) | CA2933353C (fr) |
FR (1) | FR3015573B1 (fr) |
WO (1) | WO2015092251A1 (fr) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USD791301S1 (en) * | 2014-11-27 | 2017-07-04 | Ubbink B.V. | Wall duct |
USD791300S1 (en) * | 2014-11-27 | 2017-07-04 | Ubbink B.V. | Wall duct |
US9879591B2 (en) | 2015-02-20 | 2018-01-30 | Pratt & Whitney Canada Corp. | Engine intake assembly with selector valve |
US20170074167A1 (en) * | 2015-09-10 | 2017-03-16 | Honeywell International Inc. | Turbofan engine mounted precooler system |
US10563585B2 (en) | 2016-03-02 | 2020-02-18 | United Technologies Corporation | Heat exchanger for gas turbine engine |
EP3478581B1 (fr) | 2016-06-30 | 2021-04-28 | Bombardier Inc. | Ensemble et procédé de conditionnement d'air chauffé par moteur à bord d'un aéronef |
US20180162537A1 (en) | 2016-12-09 | 2018-06-14 | United Technologies Corporation | Environmental control system air circuit |
EP3413001B1 (fr) * | 2017-06-06 | 2020-01-08 | Ge Avio S.r.l. | Échangeur de chaleur fabriqué par production additive |
US10807722B2 (en) * | 2017-07-11 | 2020-10-20 | Hamilton Sunstrand Corporation | Cabin air compressor motor cooling flow enhancement cowl |
FR3075865B1 (fr) * | 2017-12-21 | 2020-07-17 | Safran Nacelles | Ensemble propulsif pour aeronef et procede de ventilation d’une enceinte moteur |
FR3078947B1 (fr) * | 2018-03-13 | 2020-03-13 | Airbus Operations | Systeme de propulsion d'un aeronef comportant un turboreacteur double flux et un systeme de prelevement d'air a encombrement reduit |
FR3087840B1 (fr) | 2018-10-29 | 2021-01-08 | Safran Aircraft Engines | Capot de nacelle pour ensemble propulsif d'aeronef |
FR3108944B1 (fr) | 2020-04-02 | 2022-03-25 | Safran Aircraft Engines | Element a paroi composite pour une turbomachine d’aeronef |
US11834993B1 (en) | 2023-03-29 | 2023-12-05 | Pratt & Whitney Canada Corp. | Engine exhaust reverse flow prevention |
US11976595B1 (en) * | 2023-06-13 | 2024-05-07 | Pratt & Whitney Canada Corp. | Gas turbine engine with air/oil cooler having an airflow control baffle |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5123242A (en) * | 1990-07-30 | 1992-06-23 | General Electric Company | Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine |
FR2839948B1 (fr) * | 2002-05-22 | 2004-12-17 | Airbus France | Echangeur pour circuit de conditionnement d'air d'aeronef et ensemble de propulsion integrant un tel echangeur |
FR2891313A1 (fr) * | 2005-09-26 | 2007-03-30 | Airbus France Sas | Turbomoteur a double flux pourvu d'un prerefroidisseur |
US7607308B2 (en) * | 2005-12-08 | 2009-10-27 | General Electric Company | Shrouded turbofan bleed duct |
GB0607771D0 (en) * | 2006-04-20 | 2006-05-31 | Rolls Royce Plc | A heat exchanger arrangement |
US7861512B2 (en) * | 2006-08-29 | 2011-01-04 | Pratt & Whitney Canada Corp. | Turbofan bypass duct air cooled fluid cooler installation |
FR2905975B1 (fr) * | 2006-09-20 | 2008-12-05 | Snecma Sa | Conduite de soufflante pour une turbomachine. |
US8397487B2 (en) * | 2011-02-28 | 2013-03-19 | General Electric Company | Environmental control system supply precooler bypass |
US9206912B2 (en) * | 2013-01-23 | 2015-12-08 | The Boeing Company | Dual door fan air modulating valve |
EP3084183B1 (fr) * | 2013-12-18 | 2019-07-10 | United Technologies Corporation | Ensemble de commande d'écoulement d'échangeur de chaleur et procédé correspondant |
-
2013
- 2013-12-19 FR FR1362956A patent/FR3015573B1/fr active Active
-
2014
- 2014-12-15 US US15/104,445 patent/US11060462B2/en active Active
- 2014-12-15 WO PCT/FR2014/053349 patent/WO2015092251A1/fr active Application Filing
- 2014-12-15 CA CA2933353A patent/CA2933353C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
CA2933353C (fr) | 2022-03-01 |
CA2933353A1 (fr) | 2015-06-25 |
US20170002747A1 (en) | 2017-01-05 |
US11060462B2 (en) | 2021-07-13 |
WO2015092251A1 (fr) | 2015-06-25 |
FR3015573A1 (fr) | 2015-06-26 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR3015573B1 (fr) | Turbomachine d'aeronef comportant un echangeur de chaleur du type pre-refroidisseur | |
EP2951419A4 (fr) | Moteur de turbine à gaz comportant un échangeur de chaleur à bifurcation inférieure | |
FR3001253B1 (fr) | Systeme regule de refroidissement d'huile d'un turboreacteur avec degivrage de la nacelle | |
EP2843213A4 (fr) | Échangeur de chaleur pour moteur d'aéronef | |
EP2971667A4 (fr) | Trou de refroidissement de film formé de turbine à gaz | |
EP3066389A4 (fr) | Bouclier thermique pour chambre de combustion de moteur à turbine doté d'un ou de plusieurs éléments de refroidissement | |
GB201521937D0 (en) | Gas turbine engine turbine cooling system | |
GB201305432D0 (en) | A gas turbine engine cooling arrangement | |
EP3071885A4 (fr) | Structure à parois multiples pour moteur à turbine dotée d'un(d') élément(s) de refroidissement interne(s) | |
FR2995397B1 (fr) | Intercalaire d'echangeur de chaleur. | |
GB2536803B (en) | Gas turbine engine fluid heat management system | |
GB2510654B (en) | Method and system for monitoring the performance of a heat exchanger | |
FR3005453B1 (fr) | Nacelle de turboreacteur d'aeronef | |
FR3006992B1 (fr) | Systeme de chauffage de l habitacle d un aeronef muni d un echangeur thermique annulaire autour de la tuyere d echappement | |
EP3090145A4 (fr) | Turbulateur de passage de refroidissement de composant de turbine à gaz | |
EP3071887A4 (fr) | Structure à parois multiples d'un moteur à turbine avec élément(s) de refroidissement | |
EP2997231A4 (fr) | Socle de turbulateur à passage de refroidissement de profil aérodynamique de moteur à turbine à gaz | |
GB201410801D0 (en) | Fuel oil exchanger utilizing heat pipes | |
FR3008485B1 (fr) | Echangeur de chaleur | |
EP2971671A4 (fr) | Canaux de refroidissement de composant de moteur à turbine à gaz | |
FR3015654B1 (fr) | Echangeur de chaleur d'une turbomachine | |
DK3047223T3 (da) | Varmeveksler med forbedret konfiguration | |
EP2971683A4 (fr) | Collecteur d'échangeur de chaleur de moteur à turbine à gaz | |
GB2565506B (en) | Cooling structure for gas turbine engine | |
FR3040478B1 (fr) | Echangeur de chaleur |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 3 |
|
RM | Correction of a material error |
Effective date: 20160404 |
|
PLFP | Fee payment |
Year of fee payment: 4 |
|
PLFP | Fee payment |
Year of fee payment: 5 |
|
CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
|
PLFP | Fee payment |
Year of fee payment: 6 |
|
PLFP | Fee payment |
Year of fee payment: 7 |
|
PLFP | Fee payment |
Year of fee payment: 8 |
|
PLFP | Fee payment |
Year of fee payment: 9 |
|
PLFP | Fee payment |
Year of fee payment: 10 |
|
PLFP | Fee payment |
Year of fee payment: 11 |