Method of measuring torsional stresses and/or axial stresses on a rotating shaft or on a comparable workpiece

• US 5,747,699 A
• Filed: 01/21/1997
• Issued: 05/05/1998
• Est. Priority Date: 07/20/1994
• Status: Expired due to Fees

• Current Assignee: Ebi, Gunter
• Original Assignee: Ebi, Gunter
• Inventors: Ebi, Gunter
• Primary Examiner(s): RAEVIS, ROBERT R
• Application Number:
  US08/776,895
• Time in Patent Office: 469 Days
• Field of Search: 73/800, 73/862.041, 73/862.324, 73/862.49, 73/862.624, 356/32, 356/35.5
• US Class Current: 73/800
• CPC Class Codes: G01L 3/12 involving photoelectric means

Abstract

A method for measuring torsional stress and axial stress of a rotating workpiece includes the step of arranging at a surface of the workpiece at least two reflector pairs such that connecting lines between reflectors of each reflector pair are slanted relative to one another. The workpiece is rotated about an axis of rotation. A coherent laser light is impinged onto the at least two reflector pairs to produce reflected and interfering light beam pairs for each one of the reflector pairs. The phase difference between the light beams of each light beam pair is determined and the torsional stress and axial stress are calculated from the phase difference.

Claims

1. A method for measuring torsional stress and axial stress of a rotating workpiece, said method comprising the steps of:

arranging at a surface of the workpiece at least two reflector pairs such that connecting lines between reflectors of each reflector pair are slanted relative to one another;

rotating the workpiece about an axis of rotation;

impinging a coherent laser light onto the at least two reflector pairs to produce reflected and interfering light beam pairs for each one of the reflector pairs;

determining a phase difference between the light beams of each light beam pair; and

calculating the torsional stress and axial stress from the phase difference.

2. A method according to claim 1, wherein in the step of arranging four reflectors are provided such that two reflectors define one of the reflector pairs and the other two reflectors define the other reflector pair.

3. A method according to claim 1, wherein in the step of arranging three reflectors are provided for defining two reflector pairs such that one of the three reflectors is common to both reflector pairs.

4. A method according to claim 1, wherein the step of arranging includes providing the reflectors in the form of impressions in the workpiece.

5. A method according to claim 4, wherein the step of arranging includes forming concave impressions.

6. A method according to claim 4, wherein the step of arranging includes forming equal-sided pyramid-shaped impressions with four facets.

7. A method according to claim 1, wherein the step of arranging includes connecting a carrier to the workpiece and providing the reflectors in the form of impressions in the carrier.

8. A method according to claim 7, wherein the step of arranging includes forming concave impressions.

9. A method according to claim 7, wherein the step of arranging includes forming equal-sided pyramid-shaped impressions with four facets.

10. A method according to claim 1, wherein a first one of the connecting lines extends at an angle of +45°

to the axis of rotation and a second one of the connecting lines extends at an angle of -45°

to the axis of rotation.

11. A method according to claim 1, wherein the step of arranging includes spacing the reflectors of each one of the reflector pairs at identical distance to one another.

12. A method according to claim 1, wherein the step of impinging includes supplying the coherent laser light in the form of individual laser beams.

13. A method according to claim 12, wherein the step of impinging includes focusing the individual laser beams onto the reflectors.

14. A method according to claim 1, wherein the step of impinging includes providing a laser beam of a diameter greater than a diameter of the reflectors.

15. A method according to claim 1, wherein the step of impinging includes providing a laser beam of a diameter greater than a diameter of an arrangement of the reflector pairs.

16. A method according to claim 1, wherein the step of impinging includes emitting the laser light continuously when the reflectors enter the area of the laser light impinging on the workpiece.

17. A method according to claim 1, wherein the step of impinging includes emitting the laser light in a pulsed mode when the reflectors enter the area of the laser light impinging on the workpiece.

18. A method according to claim 1, wherein the step of arranging includes distributing a plurality of the reflector pairs about a circumference of the workpiece.

19. A method according to claim 1, wherein the step of arranging includes distributing three reflector pairs on the workpiece surface.

20. A method according to claim 1, wherein in the step of arranging the reflector pairs are arranged such that two measuring planes are provided at the workpiece and wherein each measuring plane includes at least two reflector pairs.