IP Library › Granted Patent US 10,677,670
Granted Patent B2
US 10,677,670 · App. 16/068,347 · Granted Jun 9, 2020

Twisting torque sensor

Inventor: Lionel Renault (Bosdarros, FR)
Assignee: SAFRAN HELICOPTER ENGINES
G01L3/04F01D5/085F01D17/04F01D21/003G01L3/101G01L3/109G01L3/12G01L3/08G01L3/10Y02T50/676
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Quick Facts
Patent No.
US 10,677,670
App. No.
16/068,347
Granted
Jun 9, 2020
Kind
B2
Abstract

The invention relates to a twisting torque sensor, comprising a transmission shaft ( 12 ) subjected to the torque to be measured, a reference shaft ( 14 ), and a device for measuring an angular deformation representing the torque to be measured between the two shafts. The torque sensor is characterised in that the transmission shaft ( 12 ) comprises a bore ( 24 ) extending from one end of the transmission shaft ( 12 ), referred to as input ( 28 ) of the shaft, to an opposite end, and in that the torque sensor comprises an enclosure ( 22 ) for confining the temperature of the two shafts, and a fluid circulation circuit including a portion made up of said bore ( 24 ), an injector ( 32 ) for injecting the fluid into the bore ( 24 ) at said input ( 28 ) of the shaft, and a fluid temperature sensor ( 34 ) in the fluid circulation circuit, the measured temperature being intended for correcting the torque measurement.

Claims (15)

1. Twisting-torque sensor, comprising a first shaft, referred to as the transmission shaft, subjected to the torque to be measured, a second shaft, referred to as the reference shaft, and a device for measuring an angular deformation between the transmission shaft and the reference shaft, said angular deformation representing the torque to be measured,

wherein the transmission shaft comprises a bore forming an internal wall and extending from one end of the transmission shaft, referred to as the input of the shaft, to an opposite end, referred to as the output of the shaft, and in that the torque sensor comprises:

a temperature-confinement enclosure of the first and second shafts, and

a fluid-circulation circuit, comprising:

a portion constituted by said bore of the transmission shaft,

a fluid injector to inject fluid into the bore at said input of the shaft, and

a temperature sensor, referred to as the main temperature sensor, suitable for measuring the temperature of the fluid in the fluid-circulation circuit, the measured temperature of the fluid being intended for a correction of the torque measurement.

2. Torque sensor according to claim 1 , wherein the transmission shaft and the reference shaft are coaxial, the transmission shaft being arranged inside the reference shaft.

3. Torque sensor according to claim 1 , wherein the transmission shaft and the reference shaft are coaxial, the reference shaft being arranged inside the transmission shaft and the fluid circulating between the internal wall of the transmission shaft and an external wall of the reference shaft.

4. Torque sensor according to claim 1 , wherein the fluid is oil and the fluid-circulation circuit is a hydraulic circuit.

5. Torque sensor according to claim 1 , wherein the main temperature sensor is suitable for measuring the temperature of the fluid at the input of the shaft.

6. Torque sensor according to claim 5 , wherein the twisting-torque sensor comprises an auxiliary temperature sensor, suitable for measuring the temperature of the fluid at the output of the shaft.

7. Torque sensor according to claim 1 , wherein the bore comprises two bore subsections connected by a transition zone, a first subsection on the same side as the shaft input, and a second subsection on the same side as the shaft output, the second subsection having a diameter smaller than the diameter of the first subsection.

8. Torque sensor according to claim 7 , wherein the second subsection is offset with respect to the first subsection and to the bore.

9. Turbine engine, comprising a rotating shaft, wherein the turbine engine comprises a twisting-torque sensor according to claim 1 , suitable for measuring the torque of the rotating shaft.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 14, 2018
From: RENAULT, LIONEL
To: SAFRAN HELICOPTER ENGINES
Reel/Frame 046833/0851 →
Priority Claims (1)
FR 16 50431 · Jan 20, 2016 · national
Continuity (1)
Related Publication 20190025142A1 · Jan 24, 2019
Cited By (2)
US 12,276,558 US 12,704,424