Method and system for measuring torque in a tiltrotor aircraft

Patent metadata

Field	Value
Publication number	US-9841333-B2
Application number	US-201414526621-A
Country	US
Kind code	B2
Filing date	Oct 29, 2014
Priority date	Oct 29, 2014
Publication date	Dec 12, 2017
Grant date	Dec 12, 2017

Abstract

A method for calculating torque through a rotor mast of a propulsion system of a tiltrotor aircraft includes receiving the torque being applied through a quill shaft of the rotorcraft. The quill shaft is located between a fixed gearbox and a spindle gearbox, and the spindle gearbox is rotatable about a conversion access. The torque through the rotor mast is determined by using the torque through the quill shaft and the efficiency loss value between the quill shaft and the rotor mast.

First claim

The invention claimed is:

1. A propulsion system for a tiltrotor aircraft, the propulsion system comprising:
an engine disposed at a fixed location relative to a wing member;
a fixed gearbox;
a spindle gearbox that is rotatable about a conversion axis;
a rotor mast rotatably coupled to the spindle gearbox;
a quill shaft providing torque transfer between the fixed gearbox and the spindle gearbox; and
a torque measuring system associated with the quill shaft comprising:
a computer system configured to calculate the torque value through the quill shaft;
wherein the computer system is further configured to calculate the torque through the rotor mast.

2. The propulsion system according to claim 1 , wherein the conversion axis is perpendicular to a rotational axis of the rotor mast.

3. The propulsion system according to claim 1 , wherein the conversion axis is at an oblique angle to a rotational axis of the rotor mast.

4. A propulsion system for a tiltrotor aircraft, the propulsion system comprising:
an engine disposed at a fixed location relative to a wing member;
a fixed gearbox;
a spindle gearbox that is rotatable about a conversion axis;
a rotor mast rotatably coupled to the spindle gearbox;
a quill shaft providing torque transfer between the fixed gearbox and the spindle gearbox; and
a torque measuring system associated with the quill shaft comprising:
a computer system configured to calculate the torque value through the quill shaft;
wherein the computer system is further configured to calculate a torque efficiency loss between the rotor mast and the quill shaft.

5. The propulsion system according to claim 4 , wherein the conversion axis is perpendicular to a rotational axis of the rotor mast.

6. The propulsion system according to claim 4 , wherein the conversion axis is at an oblique angle to a rotational axis of the rotor mast.

7. The propulsion system according to claim 4 , wherein the torque measuring system further comprises:
an element associated with the quill shaft, wherein the element creates a magnetic field upon a torsional deflection of the quill shaft; and
a sensor configured for measuring the magnetic field.

8. The propulsion system according to claim 7 , wherein the sensor is a transducer.

9. The propulsion system according to claim 7 , wherein the element is located on an arcuate surface of the quill shaft.

10. The propulsion system according to claim 7 , wherein the element is a magnetoelastically active element.

11. The propulsion system according to claim 4 , wherein the torque measuring system comprises:
a stand pipe coupled to the quill shaft, such that the stand pipe rotates at the same velocity as the quill shaft;
a first magnet associated with the stand pipe, such that rotation of the stand pipe causes similar rotation of the first magnet;
a second magnet associated with the quill shaft, such that rotation of the quill shaft causes similar rotation of the second magnet; and
a sensor for detecting the magnetic field of the first magnet or the second magnet.

12. The propulsion system according to claim 11 , wherein the first magnet is coupled to the stand pipe and the second magnet is coupled to the quill shaft.

13. The propulsion system according to claim 11 , wherein the sensor is a transducer.

14. The propulsion system according to claim 1 , wherein the torque measuring system further comprises:
an element associated with the quill shaft, wherein the element creates a magnetic field upon a torsional deflection of the quill shaft; and
a sensor configured for measuring the magnetic field.

15. The propulsion system according to claim 14 , wherein the sensor is a transducer.

16. The propulsion system according to claim 14 , wherein the element is located on an arcuate surface of the quill shaft.

17. The propulsion system according to claim 14 , wherein the element is a magnetoelastically active element.

18. The propulsion system according to claim 1 , wherein the torque measuring system comprises:
a stand pipe coupled to the quill shaft, such that the stand pipe rotates at the same velocity as the quill shaft;
a first magnet associated with the stand pipe, such that rotation of the stand pipe causes similar rotation of the first magnet;
a second magnet associated with the quill shaft, such that rotation of the quill shaft causes similar rotation of the second magnet; and
a sensor for detecting the magnetic field of the first magnet or the second magnet.

19. The propulsion system according to claim 18 , wherein the first magnet is coupled to the stand pipe and the second magnet is coupled to the quill shaft.

20. The propulsion system according to claim 18 , wherein the sensor is a transducer.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Ehinger Ryan T
• Bockmiller David R

Classifications

• G01L3/101 Primary

  involving magnetic or electromagnetic means · CPC title

• G01L3/02 Primary

  Rotary-transmission dynamometers · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title

• B64C27/32

  Rotors · CPC title

• B64D35/00

  Transmitting power from power plants to propellers or rotors; Arrangements of transmissions · CPC title