FR3116081B1 - Turbomachine blade comprising an electrical connector placed at the level of a pivot - Google Patents

Turbomachine blade comprising an electrical connector placed at the level of a pivot Download PDF

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Publication number
FR3116081B1
FR3116081B1 FR2011399A FR2011399A FR3116081B1 FR 3116081 B1 FR3116081 B1 FR 3116081B1 FR 2011399 A FR2011399 A FR 2011399A FR 2011399 A FR2011399 A FR 2011399A FR 3116081 B1 FR3116081 B1 FR 3116081B1
Authority
FR
France
Prior art keywords
blade
pivot
level
cable part
electrical connector
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
FR2011399A
Other languages
French (fr)
Other versions
FR3116081A1 (en
Inventor
Clément Raphaël Laroche
Ulrich Vincent Max Dubois
Kévin Emilien André Minjot
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 FR2011399A priority Critical patent/FR3116081B1/en
Priority to PCT/FR2021/051893 priority patent/WO2022096805A1/en
Publication of FR3116081A1 publication Critical patent/FR3116081A1/en
Application granted granted Critical
Publication of FR3116081B1 publication Critical patent/FR3116081B1/en
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
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • F01D7/02—Rotors with blades adjustable in operation; Control thereof having adjustment responsive to speed
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B64C11/04—Blade mountings
    • B64C11/06—Blade mountings for variable-pitch blades
    • 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
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)

Abstract

La présente invention concerne une aube (1) de turbomachine à calage ajustable, comprenant :un pivot (2) configuré pour être monté en rotation à l’intérieur d’une cavité d’un disque (10a, 10b) de turbomachine de sorte que le pivot (2) soit mobile en rotation par rapport au disque (10a, 10b) autour d’un axe d’empilement (A) de l’aube (1) ;une pale (3) comprenant un pied de pale (30) et fixée au pivot (2) au niveau du pied de pale (30), la pale (3) comprenant une pluralité de sections de pale empilées à partir du pied de pale (30) le long de l’axe d’empilement (A) ;un câble (4a) de connexion électrique comprenant une première partie (4a-1) de câble fixée à la pale (3) et une deuxième partie (4a-2) de câble fixée au pivot (2) et s’étendant entre la première partie (4a-1) de câble et la deuxième partie (4a-2) de câble. Figure pour l’abrégé : Figure 2The present invention relates to a turbine engine blade (1) with adjustable pitch, comprising:a pivot (2) configured to be rotatably mounted inside a cavity of a turbine engine disc (10a, 10b) so that the pivot (2) is rotatable relative to the disk (10a, 10b) around a stacking axis (A) of the blade (1);a blade (3) comprising a blade root (30) and attached to the pivot (2) at the blade root (30), the blade (3) comprising a plurality of blade sections stacked from the blade root (30) along the stacking axis (A );an electrical connection cable (4a) comprising a first cable part (4a-1) fixed to the blade (3) and a second cable part (4a-2) fixed to the pivot (2) and extending between the first cable part (4a-1) and the second cable part (4a-2). Figure for abstract: Figure 2

FR2011399A 2020-11-06 2020-11-06 Turbomachine blade comprising an electrical connector placed at the level of a pivot Active FR3116081B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR2011399A FR3116081B1 (en) 2020-11-06 2020-11-06 Turbomachine blade comprising an electrical connector placed at the level of a pivot
PCT/FR2021/051893 WO2022096805A1 (en) 2020-11-06 2021-10-27 Turbomachine vane comprising an electrical connector placed at a pivot

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2011399A FR3116081B1 (en) 2020-11-06 2020-11-06 Turbomachine blade comprising an electrical connector placed at the level of a pivot
FR2011399 2020-11-06

Publications (2)

Publication Number Publication Date
FR3116081A1 FR3116081A1 (en) 2022-05-13
FR3116081B1 true FR3116081B1 (en) 2023-06-02

Family

ID=74125467

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2011399A Active FR3116081B1 (en) 2020-11-06 2020-11-06 Turbomachine blade comprising an electrical connector placed at the level of a pivot

Country Status (2)

Country Link
FR (1) FR3116081B1 (en)
WO (1) WO2022096805A1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2942454B1 (en) * 2009-02-23 2012-09-14 Airbus France BLADE RETENTION DEVICE FOR TURBOMACHINE PROPELLER.
FR2996588A1 (en) * 2012-10-10 2014-04-11 Snecma Propeller for e.g. aeronautical turboengines, has pivots with counterweight system that includes pair of inner channels for airflow ventilation discharge to capture and guide airflow directly in contact with blade foot borne by pivots
FR2996590B1 (en) * 2012-10-10 2014-12-19 Snecma PROPELLER COMPRISING A PIVOT HAVING A PELTIER CELL
FR2996875A1 (en) * 2012-10-12 2014-04-18 Snecma INSTALLATION OF MEASUREMENTS FOR BREAKING TESTS ON A TURBOMACHINE

Also Published As

Publication number Publication date
WO2022096805A1 (en) 2022-05-12
FR3116081A1 (en) 2022-05-13

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