Contactless measurement of the stress of rotating parts

• US 7,043,999 B2
• Filed: 08/09/2002
• Issued: 05/16/2006
• Est. Priority Date: 08/11/2001
• Status: Expired due to Fees

• Current Assignee: Schaeffler KG (INA-Holding Schaeffler GmbH & Co. KG)
• Original Assignee: FAG Kugelfischer Georg Schã¤Fer AG (INA-Holding Schaeffler GmbH & Co. KG)
• Inventors: Bernhard, Josef, Hering, Joachim, Gempper, Sven, Wansch, Rainer, Strauss, Wolfram
• Primary Examiner(s): NOORI, MAX H
• Application Number:
  US10/486,590
• Publication Number:
  US 20040244496A1
• Time in Patent Office: 1,376 Days
• Field of Search: 738/01, 738/62, 738/623.81, 738/625.9
• US Class Current: 73/801
• CPC Class Codes: G01L 3/10 involving electric or magnetic means for indicating
• CPC Class Codes: G01L 5/0009 Force sensors associated with a bearing testing of bearings G01M13/04

Abstract

The invention relates to a method for measuring mechanical stresses of a rotating part (1) in an essentially closed metal housing. The rotating part comprises a sensor (2) which reflects electromagnetic waves and which can be measurably deformed as a result of a mechanical stress exerted on said rotating part (1) The two antennas (A1, A2) receiving the reflected signals of the sensor (2) are arranged in the bearing housing (10) in such a way that they cannot rotate in relation to the sensor and are distanced (α). Said antennas emit receiving signals (a1,a2) which are sent to an electronic evaluation system (20,21) which measures the mechanical stresses of the rotating part (1) on the basis of both receiving signals (a1,a2).

Claims

1. A method for measurement of mechanical loads or stresses of a rotating part in an essentially closed metal housing for a bearing;

wherein the rotating part carries a sensor, which reflects electromagnetic waves and changes property in measurable fashion based on the strain or load of the rotating part;

wherein two antennas, receiving reflected signals of the sensor, are arranged such that they cannot turn relative to the sensor and are spaced in the housing, and these antennas put out two electrical reception signals, which are taken to an electronic evaluation system, in order to utilize both reception signals for determining the load or strain of the rotating part.

2. The method of claim 1, wherein the sensor is firmly applied to the rotating part and is deformed along with it in a measurable fashion.

3. The method of claim 1, wherein the rotating part is mounted in the housing such that it can rotate, as a shaft on a roller bearing in the bearing housing.

4. The method of claim 1, wherein the load or strain of the rotating part

(i) is determined through the mechanical deformation of the sensor either from the one reception signal or the other reception signal;

or

(ii) it is determined from a combination of the two reception signals.

5. The method of claim 1, wherein the two antennas are arranged at a distance, in particular, a circumferential spacing (α

), so that due to reflected signals of the sensor a first reception signal from the one antenna is rising when a second reception signal from the second antenna is falling.

6. The method of claim 5, wherein a minimum of the first reception signal in the first antenna occurs essentially at a maximum of the second reception signal of the second antenna, for the same angular position (φ

) of the rotating part, in particular, the sensor on the rotating part.

7. The method of claim 1, wherein the electronic evaluation system switches between the two reception signals in order to evaluate the first signal at a first time range and the second signal at a later time range in order to measure the strain.

8. The method of claim 7, wherein the switching occurs essentially when the currently measured (active) reception signal falls below a threshold value, in particular, below a signal strength which is possessed by the second, not yet evaluated (heretofore passive) reception signal of the second antenna.

9. The method of claim 1, wherein the sensor is a passive sensor, which picks up electromagnetic waves, delays them by a travel time and reflects them, in particular, an SAW sensor for reflection of surface acoustic waves that are beamed in by an antenna, especially as a pulse of high-frequency components.

10. The method of claim 9, wherein the sensor has several reflector sites, which are arranged at a spacing on the sensor and which successively reflect an incident high-frequency pulse, in order to obtain a reflected signal which is load-dependent or temperature-dependent by at least one travel time of the shaft between one of the reflection sites and the conversion site, making it possible to measure the phase and obtain information as to the strain on the rotating part.

11. The method of claim 1, wherein the measurement occurs during a rotation (ω

) of the rotating part.

14. The method of claim 7, wherein a threshold value is determined for the switching from at least one of the measured reception signals, in particular, it is automatically tracked.

17. The method of claim 1, wherein a mechanical load or stress on the rotating part is measured, as a consequence of a mechanical change, such as stretching or compression of the sensor.

18. The method of claim 1, wherein the electromagnetic signal is a pulsed high-frequency signal.

19. The method of claim 18, wherein at least one of the two antennas is used as a transmission antenna for the electromagnetic waves, in particular, the high frequency pulse, to be reflected by the transmitter or sensor for both antennas as the reflection signal in forming several reception signals.

12. A device for determination of loads on a rotating part in an essentially closed metal bearing housing, wherein the rotating part carries a transmitter, which reflects electromagnetic waves and which can be deformed in measurable fashion by virtue of a load on the rotating part;

and wherein two antennas—

receiving reflected signals of the transmitter—

are arranged such that they cannot turn relative to the transmitter and are at a spacing (α

) in the bearing housing, in order to put out at least two reception signals to an electronic evaluation system, in which both reception signals can be evaluated—

jointly or alternatively—

in order to determine the load on the part.

13. The device of claim 12, wherein the mechanical deformation of the transmitter or sensor which is determined is its extension or contraction in terms of the reception signals formed from the reflected signals of the two antennas, by evaluating an in-phase and a quadrature value of the reception signals.

15. The device of claim 12, wherein only one electronic evaluation system is provided for both reception signals of the two antennas.

16. The device of claim 12, wherein a thermal influence on the transmitter is measured, which represents a uniform thermal load or stress on the rotating part.

20. The device of claim 12, wherein more than two nonrotating antennas are provided for reception of the reflected signal of the passive transmitter, which send their several reception signals formed from the at least one reflected signal to an electronic evaluation system for evaluation.

21. The device of claim 12, wherein a working signal is formed from the minimum of two reception signals of a maximum-value circuit as the particular maximum value for the two individual reception signals and this is sent on to an evaluation circuit.