CA3073405A1 - Methode de chauffage d`une pale de soufflante au moyen de l`effet coanda - Google Patents

Methode de chauffage d`une pale de soufflante au moyen de l`effet coanda Download PDF

Info

Publication number
CA3073405A1
CA3073405A1 CA3073405A CA3073405A CA3073405A1 CA 3073405 A1 CA3073405 A1 CA 3073405A1 CA 3073405 A CA3073405 A CA 3073405A CA 3073405 A CA3073405 A CA 3073405A CA 3073405 A1 CA3073405 A1 CA 3073405A1
Authority
CA
Canada
Prior art keywords
blade
heated air
airfoil
fan
fan blade
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.)
Pending
Application number
CA3073405A
Other languages
English (en)
Inventor
Richard Ivakitch
David Menheere
Paul Stone
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.)
Pratt and Whitney Canada Corp
Original Assignee
Pratt and Whitney Canada Corp
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 Pratt and Whitney Canada Corp filed Critical Pratt and Whitney Canada Corp
Priority to CA3073405A priority Critical patent/CA3073405A1/fr
Publication of CA3073405A1 publication Critical patent/CA3073405A1/fr
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047Heating to prevent icing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/02De-icing means for engines having icing phenomena
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/36Application in turbines specially adapted for the fan of turbofan engines
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CA3073405A 2020-02-21 2020-02-21 Methode de chauffage d`une pale de soufflante au moyen de l`effet coanda Pending CA3073405A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA3073405A CA3073405A1 (fr) 2020-02-21 2020-02-21 Methode de chauffage d`une pale de soufflante au moyen de l`effet coanda

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA3073405A CA3073405A1 (fr) 2020-02-21 2020-02-21 Methode de chauffage d`une pale de soufflante au moyen de l`effet coanda

Publications (1)

Publication Number Publication Date
CA3073405A1 true CA3073405A1 (fr) 2021-08-21

Family

ID=77369513

Family Applications (1)

Application Number Title Priority Date Filing Date
CA3073405A Pending CA3073405A1 (fr) 2020-02-21 2020-02-21 Methode de chauffage d`une pale de soufflante au moyen de l`effet coanda

Country Status (1)

Country Link
CA (1) CA3073405A1 (fr)

Similar Documents

Publication Publication Date Title
CA2528049C (fr) Refroidissement par impact de jet de plate-forme de profil aerodynamique
US5252026A (en) Gas turbine engine nozzle
US10196982B2 (en) Gas turbine engine having a flow control surface with a cooling conduit
CA2844552C (fr) Trous de purge inverses menages dans l'enveloppe de protection d'un compresseur
CN111335973A (zh) 用于燃气涡轮发动机的护罩密封
US11391208B2 (en) Fan blade anti-icing concept
GB2224779A (en) Aircraft engine inlet cowl anti-icing system
US8371814B2 (en) Turbine engine components
CN110454236B (zh) 一种用于燃气涡轮发动机进口可调导叶的防冰装置
US8206079B2 (en) Temperature controlling apparatus
US11306658B2 (en) Cooling system for a turbine engine
US11156093B2 (en) Fan blade ice protection using hot air
JP2006200530A (ja) ロータアセンブリ先端隙間を維持する方法および装置
CA2923297A1 (fr) Systeme de refroidissement d'une enveloppe de turbine
US20050163609A1 (en) Gas turbine engine including airfoils having an improved airfoil film cooling configuration and method therefor
EP3590846A1 (fr) Section d'entrée d'air de carter moteur
CN111263847B (zh) 涡轮排气壳体的冷却
US11807379B2 (en) Turbofan engine, nacelle thereof, and associated method of operation
US11118457B2 (en) Method for fan blade heating using coanda effect
CA3073405A1 (fr) Methode de chauffage d`une pale de soufflante au moyen de l`effet coanda
US20160312654A1 (en) Turbine airfoil cooling
US20230358170A1 (en) Diffuser with passlets
US20230417150A1 (en) Augmented cooling for tip clearance optimization
CA3105434A1 (fr) Reacteur a double flux, nacelle de celui-ci et methode de fonctionnement associee

Legal Events

Date Code Title Description
EEER Examination request

Effective date: 20231130