Resonance test system

• US 7,953,561 B2
• Filed: 07/03/2002
• Issued: 05/31/2011
• Est. Priority Date: 07/03/2002
• Status: Active Grant

• Current Assignee: Alliance For Sustainable Energy LLC
• Original Assignee: Alliance For Sustainable Energy LLC
• Inventors: White, Darris, Musial, Walter
• Primary Examiner(s): Schechter; Andrew
• Assistant Examiner(s): Huynh; Phuong
• Application Number:
  US10/520,011
• Publication Number:
  US 20060037402A1
• Time in Patent Office: 3,254 Days
• Field of Search: 702/42, 702/56, 702/141, 702179-190, 702/43, 702/44, 702 58- 62, 702116-122, 738/08, 737/89, 737/98, 735/79, 738/49, 737/88, 737/94, 737/95, 738/06
• US Class Current: 702/42
• CPC Class Codes: G01M 7/00 Vibration-testing of structures; Shock-testing of structures G01M9/00 takes precedence
• CPC Class Codes: G01N 2203/0005 Repeated or cyclic
• CPC Class Codes: G01N 2203/0023 Bending
• CPC Class Codes: G01N 2203/0039 Hammer or pendulum
• CPC Class Codes: G01N 2203/0073 Fatigue
• CPC Class Codes: G01N 3/34 generated by mechanical means, e.g. hammer blows

Abstract

An apparatus (10) for applying at least one load to a specimen (12) according to one embodiment of the invention may comprise a mass (18). An actuator (20) mounted to the specimen (12) and operatively associated with the mass (18) moves the mass (18) along a linear displacement path (22) that is perpendicular to a longitudinal axis of the specimen (12). A control system (26) operatively associated with the actuator (20) operates the actuator (20) to reciprocate the mass (18) along the linear displacement path (22) at a reciprocating frequency, the reciprocating frequency being about equal to a resonance frequency of the specimen (12) in a test configuration.

Claims

1. An apparatus for applying at least one cyclical load to a specimen, the specimen extending at least along a longitudinal axis, comprising:

a mass;

an actuator mounted to the specimen and operatively associated with said mass, said actuator moving said mass along a linear displacement path that is perpendicular to the longitudinal axis of the specimen, wherein the specimen comprises a wind turbine blade that is rigidly mounted at a root end and unsupported at a tip end and wherein the actuator is mounted at a location between the root end and the tip end of the specimen such that the moving of the mass relative to the wind turbine blade applies a bending load to the specimen; and

a control system operatively associated with said actuator, said control system operating said actuator to reciprocate said mass along the linear displacement path at a reciprocating frequency, said reciprocating frequency being about equal to a resonance frequency of the specimen in a test configuration causing displacement of the tip relative to the longitudinal axis of the specimen.

2. The apparatus of claim 1, further comprising a feedback sensor operatively associated with said control system, said feedback sensor producing a feedback signal, said control system being responsive to the feedback signal produced by said feedback sensor, said control system operating said actuator to change a displacement of said mass in response to said feedback signal.

3. The apparatus of claim 2, wherein said feedback sensor comprises a strain gauge and wherein the feedback signal produced by said feedback sensor is related to a strain in the specimen.

4. The apparatus of claim 2, wherein said feedback sensor comprises an accelerometer and wherein the feedback signal produced by said feedback sensor is related to an acceleration of the specimen.

5. The apparatus of claim 1, further comprising a load frame mounted directly to the specimen, said actuator being mounted to said load frame.

6. The apparatus of claim 5, wherein said actuator comprises a linear hydraulic actuator having a proximal end and a distal end, the proximal end of said linear hydraulic actuator being mounted to said load frame, the distal end of said linear hydraulic actuator being mounted to said mass so that the mass moves independently of the specimen.

7. The apparatus of claim 1, further comprising a transverse load actuator operatively associated with the specimen, said transverse load actuator applying to the specimen a load in a transverse direction, said transverse direction being substantially orthogonal to the longitudinal axis of the specimen and to the linear displacement path and wherein the transverse load actuator is attached to the specimen at a location between the tip end and the root end of the specimen.

8. The apparatus of claim 7, wherein the load applied to the specimen by said transverse load actuator is varied at the reciprocating frequency.

9. The apparatus of claim 1, further comprising a static mass mounted to the specimen.

10. A system for vibrating a specimen, the specimen extending at least along a longitudinal axis from a first to a second end, comprising:

reciprocating mass means operatively associated with the specimen for sinusoidally vibrating the specimen along the longitudinal axis at about a resonance frequency of the specimen in a test configuration, wherein the specimen is rigidly supported at the first end and unsupported at the second end and wherein the reciprocating mass means is mounted to the specimen at a location between the first and second ends; and

displacement control means operatively associated with said reciprocating mass means for varying a vibrational displacement of the specimen,

wherein said reciprocating mass means comprises;

a mass; and

actuator means operatively associated with said mass for reciprocating said mass along a displacement path that is perpendicular to the longitudinal axis of the specimen such that the mass does not contact the specimen during the reciprocating.

11. A method for vibrating a wind turbine blade specimen, the specimen extending at least along a longitudinal axis from a root to a tip, comprising:

mounting a mass to the specimen nearer to the tip than to the root so that said mass can be reciprocated along a linear displacement path that is perpendicular to the longitudinal axis of the specimen to apply a flap load to the specimen; and

reciprocating the mass along the linear displacement path at a reciprocation frequency that is about equal to a resonance frequency of the specimen in a test configuration, wherein the mass remains spaced apart from the specimen during reciprocating along the linear displacement path.

12. The method of claim 11, further comprising:

detecting a strain in the specimen; and

controlling a displacement of the mass to place a desired load on the specimen based on the detected strain.

13. The method of claim 11, further comprising:

detecting an acceleration of the specimen; and

controlling a displacement of the mass to place a desired load on the specimen based on the detected acceleration.

14. The method of claim 11, further comprising applying to the specimen a load in a transverse direction, the transverse direction being substantially orthogonal to the longitudinal axis of the specimen and to the linear displacement path.

15. The method of claim 14, further comprising varying the load applied to the specimen in the transverse direction at about the reciprocation frequency.

16. An apparatus for applying at least one cyclical load to a specimen, the specimen extending at least along a longitudinal axis, comprising:

a mass;

an actuator mounted to the specimen and operatively associated with said mass, said actuator moving said mass along a linear displacement path that is substantially perpendicular to the longitudinal axis of the specimen;

a transverse load actuator operatively associated with the specimen, said transverse load actuator applying to the specimen a cyclical load in a transverse direction, said transverse direction being substantially perpendicular to the longitudinal axis of the specimen and to the linear displacement path; and

a control system operatively associated with said actuator and said transverse load actuator, said control system operating said actuator to reciprocate said mass along the linear displacement path at a reciprocating frequency, said reciprocating frequency being about equal to a resonance frequency of the specimen in a test configuration, said control system operating said transverse load actuator to vary the cyclical load at about the reciprocating frequency.

17. The apparatus of claim 16, further comprising a feedback sensor operatively associated with said control system, said feedback sensor producing a feedback signal, said control system being responsive to the feedback signal produced by said feedback sensor, said control system operating said actuator to change a displacement of said mass in response to said feedback signal.

18. The apparatus of claim 17, wherein said feedback sensor comprises at least one accelerometer.

19. The apparatus of claim 17, wherein said feedback sensor comprises at least one strain gauge.

20. The apparatus of claim 16, wherein said control system comprises a PID controller.