IP Library Granted Patent US 12,460,979
Granted Patent B2
US 12,460,979 · App. 18/270,287 · Granted Nov 4, 2025

Torque transmission and measurement assembly for a turbomachine

Inventors: Benjamin Nicolas Fulleringer (Moissy-Cramayel, FR); Rémi Joseph Lanquetin (Moissy-Cramayel, FR); Arnaud Georges Nifenecker (Moissy-Cramayel, FR)
Assignee: SAFRAN HELICOPTER ENGINES
G01L3/08
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Quick Facts
Patent No.
US 12,460,979
App. No.
18/270,287
Granted
Nov 4, 2025
Kind
B2
Abstract

An assembly for measuring a torque transmitted between a first member and a second member of a turbomachine includes a pinion having a first annular portion and a second annular portion joining together at a connecting portion carrying a gearing of the pinion, said first and second annular portions extending axially in opposite directions, from the connecting portion. The pinion also includes an axial power shaft with a first area coupled to the first annular portion, and a second area for coupling to the second member, and a device for measuring the torsion between the first and second areas. The device includes a first phonic wheel on the power shaft, a second phonic wheel equipping the second annular portion of the pinion and axially aligned with the first phonic wheel, and an acquisition means axially aligned with and opposite to the first phonic wheel and the second phonic wheel and outputting a signal representative of an angular variation.

Claims (15)

1 . An assembly ( 1 ) for transmitting and measuring a torque transmitted between a first member and a second member ( 16 ) of a turbomachine, comprising:

a pinion ( 2 ) which includes a first annular portion ( 5 ) and a second annular portion ( 6 ) joining together at a connecting portion ( 7 ) carrying a gearing ( 4 ) of the pinion ( 2 ), said first and second annular portions ( 5 , 6 ) extending axially according to an axis of rotation (X) of the pinion ( 2 ) in opposite directions (D 1 , D 2 ), from the connecting portion ( 7 ), at least one of said annular portions ( 5 , 6 ) being guided in rotation by a guide bearing ( 8 , 9 ) of the pinion ( 2 ), the pinion further including a power shaft ( 10 ) extending axially, said power shaft ( 10 ) including a first area ( 11 ) coupled in rotation to the first annular portion ( 5 ) of the pinion ( 2 ), and a second area ( 12 ) for coupling in rotation to the second member ( 16 ) of the turbomachine, the first area being spaced axially apart from the second area, and

means for measuring the torsion of the power shaft ( 10 ) disposed at a third area of the power shaft ( 10 ) located between the first and second areas ( 11 , 12 ), said means for measuring including

a first phonic wheel ( 20 ) equipping the third area of the power shaft ( 10 ),

a second phonic wheel ( 25 ) equipping the second annular portion ( 6 ) of the pinion ( 2 ) and axially aligned with the first phonic wheel ( 20 ), and

an acquisition means ( 27 ) axially aligned with and opposite the first phonic wheel ( 20 ) and the second phonic wheel ( 25 ) and being configured to output a signal representative of an angular variation between the first phonic wheel ( 20 ) and the second phonic wheel ( 25 ).

2 . The assembly ( 1 ) according to claim 1 , characterised in that the pinion ( 2 ) and the power shaft ( 10 ) are made in one piece.

3 . The assembly ( 1 ) according to claim 2 , characterised in that the pinion ( 2 ) and the power shaft ( 10 ) are made in one piece by additive manufacturing or by permanent assembly.

4 . The assembly ( 1 ) according to claim 1 , characterised in that the second phonic wheel ( 25 ) is formed at one end of a cylindrical portion ( 6 b ) of the second annular portion ( 6 ) of the pinion ( 2 ), said end being located opposite the junction between the second annular portion ( 6 ) and the first annular portion ( 5 ) of the pinion ( 2 ).

5 . The assembly ( 1 ) according to claim 4 , characterised in that a guide bearing ( 9 ) of the pinion ( 2 ) is mounted around said cylindrical portion ( 6 b ) to guide it in rotation.

6 . The assembly ( 1 ) according to claim 1 , characterised in that the signal originating from the acquisition means ( 27 ) is transmitted to a calculation member configured to determine the torque transmitted by the power shaft ( 10 ) from said signal.

7 . The assembly ( 1 ) according to claim 1 , characterised in that the first area and the second area of the power shaft ( 10 ) are formed by a first axial end ( 11 ) and a second axial end ( 12 ) opposite said power shaft ( 10 ).

8 . The assembly ( 1 ) according to claim 7 , characterised in that the second area ( 12 ) includes splines ( 14 ) intended to cooperate with complementary splines ( 15 ) of the second member ( 16 ) of the turbomachine.

9 . The assembly ( 1 ) according to claim 1 , characterised in that the first annular portion ( 5 ) comprises a cylindrical portion ( 5 b ) guided in rotation by a guide bearing ( 8 ) of the pinion ( 2 ).

10 . A turbomachine comprising the assembly ( 1 ) according to claim 1 .

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 14, 2023
From: FULLERINGER, BENJAMIN NICOLAS; LANQUETIN, RÉMI JOSEPH; NIFENECKER, ARNAUD GEORGES
To: SAFRAN HELICOPTER ENGINES
Reel/Frame 065555/0144 →
Priority Claims (1)
FR 2014235 · Dec 30, 2020 · national
Continuity (1)
Related Publication 20240053213A1 · Feb 15, 2024
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