FR3120907B1 - Ensemble rotorique de soufflante - Google Patents

Ensemble rotorique de soufflante Download PDF

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Publication number
FR3120907B1
FR3120907B1 FR2102690A FR2102690A FR3120907B1 FR 3120907 B1 FR3120907 B1 FR 3120907B1 FR 2102690 A FR2102690 A FR 2102690A FR 2102690 A FR2102690 A FR 2102690A FR 3120907 B1 FR3120907 B1 FR 3120907B1
Authority
FR
France
Prior art keywords
rotor
annular element
rotor assembly
unbalance
fan rotor
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
FR2102690A
Other languages
English (en)
Other versions
FR3120907A1 (fr
Inventor
Grégory Benevent
Thomas Robert Paul Falaise
Stéphane Xavier Gérard Rousselin
Etienne Romain Pascal Grenier
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 FR2102690A priority Critical patent/FR3120907B1/fr
Publication of FR3120907A1 publication Critical patent/FR3120907A1/fr
Application granted granted Critical
Publication of FR3120907B1 publication Critical patent/FR3120907B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/027—Arrangements for balancing
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/025—Fixing blade carrying members on shafts
    • 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
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/14—Two-dimensional elliptical
    • F05D2250/141—Two-dimensional elliptical circular
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/23—Three-dimensional prismatic
    • F05D2250/232—Three-dimensional prismatic conical
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/28—Three-dimensional patterned
    • F05D2250/281—Three-dimensional patterned threaded
    • 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
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/35—Arrangement of components rotated
    • 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
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/37—Retaining components in desired mutual position by a press fit connection

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Ensemble rotorique de soufflante d’une turbomachine d’axe longitudinal comprenant un rotor configuré pour être mobile en rotation autour de l’axe longitudinal, le rotor comportant une virole de support ; un cône amont agencé en amont du rotor, le cône amont présentant une face radialement externe délimitant, radialement vers l’intérieur, une surface d’écoulement d’air ; un dispositif d’équilibrage comportant au moins un premier élément annulaire qui est solidaire en rotation avec la virole de support du rotor, ledit élément annulaire présentant un premier balourd apte à réduire un balourd du rotor, dans lequel ledit premier élément annulaire présente une face radialement externe délimitant, radialement vers l’intérieur, une surface d’écoulement d’air. Figure de l’abrégé : Figure 2
FR2102690A 2021-03-17 2021-03-17 Ensemble rotorique de soufflante Active FR3120907B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2102690A FR3120907B1 (fr) 2021-03-17 2021-03-17 Ensemble rotorique de soufflante

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2102690A FR3120907B1 (fr) 2021-03-17 2021-03-17 Ensemble rotorique de soufflante
FR2102690 2021-03-17

Publications (2)

Publication Number Publication Date
FR3120907A1 FR3120907A1 (fr) 2022-09-23
FR3120907B1 true FR3120907B1 (fr) 2023-12-22

Family

ID=75690550

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2102690A Active FR3120907B1 (fr) 2021-03-17 2021-03-17 Ensemble rotorique de soufflante

Country Status (1)

Country Link
FR (1) FR3120907B1 (fr)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9511457B2 (en) * 2012-02-09 2016-12-06 Pratt & Whitney Canada Corp. Gas turbine engine rotor balancing
FR3053430B1 (fr) * 2016-06-30 2019-01-25 Snecma Ensemble de turbomachine permettant un assemblage etanche d'un cone avant sur une virole avant
FR3087481B1 (fr) * 2018-10-19 2022-12-02 Safran Aircraft Engines Ensemble d’equilibrage modulaire pour turbomachine

Also Published As

Publication number Publication date
FR3120907A1 (fr) 2022-09-23

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