FR3119641B1 - HOLLOW BLADE, PROVIDED WITH HEAT EXCHANGE BRIDGES PASSING THROUGH A COOLING CAVITY - Google Patents

HOLLOW BLADE, PROVIDED WITH HEAT EXCHANGE BRIDGES PASSING THROUGH A COOLING CAVITY Download PDF

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Publication number
FR3119641B1
FR3119641B1 FR2101208A FR2101208A FR3119641B1 FR 3119641 B1 FR3119641 B1 FR 3119641B1 FR 2101208 A FR2101208 A FR 2101208A FR 2101208 A FR2101208 A FR 2101208A FR 3119641 B1 FR3119641 B1 FR 3119641B1
Authority
FR
France
Prior art keywords
heat exchange
cooling cavity
hollow blade
bridges passing
exchange bridges
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
FR2101208A
Other languages
French (fr)
Other versions
FR3119641A1 (en
Inventor
Michel Slusarz
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.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR2101208A priority Critical patent/FR3119641B1/en
Publication of FR3119641A1 publication Critical patent/FR3119641A1/en
Application granted granted Critical
Publication of FR3119641B1 publication Critical patent/FR3119641B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • 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
    • F05D2240/00Components
    • F05D2240/10Stators
    • F05D2240/12Fluid guiding means, e.g. vanes
    • F05D2240/127Vortex generators, turbulators, or the like, for mixing
    • 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
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/18Two-dimensional patterned
    • 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
    • F05D2250/00Geometry
    • F05D2250/20Three-dimensional
    • F05D2250/23Three-dimensional prismatic
    • F05D2250/231Three-dimensional prismatic cylindrical
    • 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
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/221Improvement of heat transfer
    • F05D2260/2214Improvement of heat transfer by increasing the heat transfer surface

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

L’aube refroidie et renfermant une cavité (4) parcourue par un fluide de refroidissement circulant entre deux parois principales (2, 3) est pourvue de pontets (11) joignant les parois (2, 3) afin de promouvoir des turbulences dans l’écoulement. Ces pontets sont munis de reliefs (13) à leur surface extérieure, qui augmentent leur efficacité en accroissant les échanges de chaleur entre le fluide et la matière de l’aube de diverses manières. Figure pour l’abrégé : Figure 2C.The cooled blade and containing a cavity (4) through which a cooling fluid circulates between two main walls (2, 3) is provided with bridges (11) joining the walls (2, 3) in order to promote turbulence in the flow. These bridges are provided with reliefs (13) on their outer surface, which increase their efficiency by increasing the exchanges of heat between the fluid and the material of the blade in various ways. Figure for abstract: Figure 2C.

FR2101208A 2021-02-09 2021-02-09 HOLLOW BLADE, PROVIDED WITH HEAT EXCHANGE BRIDGES PASSING THROUGH A COOLING CAVITY Active FR3119641B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2101208A FR3119641B1 (en) 2021-02-09 2021-02-09 HOLLOW BLADE, PROVIDED WITH HEAT EXCHANGE BRIDGES PASSING THROUGH A COOLING CAVITY

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2101208A FR3119641B1 (en) 2021-02-09 2021-02-09 HOLLOW BLADE, PROVIDED WITH HEAT EXCHANGE BRIDGES PASSING THROUGH A COOLING CAVITY
FR2101208 2021-02-09

Publications (2)

Publication Number Publication Date
FR3119641A1 FR3119641A1 (en) 2022-08-12
FR3119641B1 true FR3119641B1 (en) 2023-05-12

Family

ID=75746814

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2101208A Active FR3119641B1 (en) 2021-02-09 2021-02-09 HOLLOW BLADE, PROVIDED WITH HEAT EXCHANGE BRIDGES PASSING THROUGH A COOLING CAVITY

Country Status (1)

Country Link
FR (1) FR3119641B1 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015065717A1 (en) * 2013-10-29 2015-05-07 United Technologies Corporation Pedestals with heat transfer augmenter
US10196900B2 (en) * 2014-12-15 2019-02-05 United Technologies Corporation Heat transfer pedestals with flow guide features
US10907480B2 (en) * 2018-09-28 2021-02-02 Raytheon Technologies Corporation Ribbed pin fins

Also Published As

Publication number Publication date
FR3119641A1 (en) 2022-08-12

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