SYSTEM AND METHOD FOR INSPECTING PARTS USING FREQUENCY RESPONSE FUNCTION

• US 20170138906A1
• Filed: 11/13/2015
• Published: 05/18/2017
• Est. Priority Date: 11/13/2015
• Status: Active Grant

• Current Assignee: Honeywell Federal Manufacturing & Technologies, LLC (Honeywell International Inc.)
• Original Assignee: Honeywell Federal Manufacturing & Technologies, LLC (Honeywell International Inc.)
• Inventors: HARTWIG, TROY, BROWN, BEN
• Granted Patent: US 10,444,110 B2
• Time in Patent Office: Days
• CPC Class Codes: G01M 7/022 Vibration control arrangements, e.g. for generating random vibrations
• CPC Class Codes: G01M 7/025 Measuring arrangements
• CPC Class Codes: G01N 2291/012 Phase angle
• CPC Class Codes: G01N 2291/014 Resonance or resonant frequency
• CPC Class Codes: G01N 2291/015 Attenuation, scattering
• CPC Class Codes: G01N 2291/2698 Other discrete objects, e.g. bricks
• CPC Class Codes: G01N 29/043 in the interior, e.g. by shear waves
• CPC Class Codes: G01N 29/045 by imparting shocks to the workpiece and detecting the vibrations or the acoustic waves caused by the shocks measuring resonant frequency G01H13/00; measuring strength properties by application of mechanical stress G01N3/00
• CPC Class Codes: G01N 29/11 by measuring attenuation of acoustic waves
• CPC Class Codes: G01N 29/12 by measuring frequency or resonance of acoustic waves measuring frequency or resonant frequency of mechanical vibrations or acoustic waves in general G01H1/06, G01H3/04, G01H13/00; acoustic resonators G10K11/04; vibration or shock testing of structures G01M7/00
• CPC Class Codes: G01N 29/4427 with stored values, e.g. threshold values

Abstract

A system and method for the non-destructive testing of additively manufactured parts. An input mechanism excites with an excitation force (e.g., a vibration) an additive manufacturing build platform on which the part is located to induce a dynamic response in the part. An output mechanism (e.g., a non-contact transducer) senses the induced dynamic response in the part. A processor determines and examines the relationship between the response and excitation to identify an indication of a defect in the part, and communicates an alert if the indication is identified. The processor may compare the phase, magnitude, coherence, or time delay of the relationship to a reference relationship and/or may compare the modal frequency or the modal damping to a reference to identify a deviation greater than a pre-established threshold.

Claims

1. A system for the non-destructive testing of one or more parts manufactured using an additive manufacturing process, the system comprising:

an input mechanism configured to excite with an excitation force an additive manufacturing build platform on which the one or more parts are located to induce a dynamic response in the one or more parts;

an output mechanism configured to sense the induced dynamic response in the one or more parts; and

a processing element configured to determine a relationship between the excitation force and the dynamic response and to examine the determined relationship to identify an indication of a defect in the one or more parts, and to communicate an alert if the indication of the defect is identified.

2. The system as set forth in claim 1, wherein a plurality of parts located on the additive manufacturing build platform are tested simultaneously.

3. The system as set forth in claim 1, wherein the defect in the one or more parts is selected from the group consisting of:

porosities, voids, unfused powders, dimensional variations, non-homogenous powders, improper microstructure, improper microstructure, and cracks.

4. The system as set forth in claim 1, wherein the excitation force is selected from the group consisting of:

impulsive vibrations, swept sinusoid vibrations, and random input vibrations.

5. The system as set forth in claim 1, wherein the excitation force excites the additive manufacturing build platform by introducing the excitation force directly to the additive manufacturing build platform so as to introduce the excitation force indirectly to the one or more parts located on the additive manufacturing build platform.

6. The system as set forth in claim 1, wherein the system is further configured to minimize external damping imparted to the one or more parts, including minimizing one or more forms of friction.

7. The system as set forth in claim 1, wherein the relationship between the excitation force and the dynamic response may include one or more of a frequency response function, a coherence function, a cross-correlation function, and a cross-power spectrum.

8. The system as set forth in claim 1, wherein the processing element is configured to compare a phase of the determined relationship to a reference to identify the indication of the defect.

9. The system as set forth in claim 1, wherein the processing element is configured to compare a magnitude of the determined relationship to a reference to identify the indication of the defect.

10. The system as set forth in claim 1, wherein the processing element is configured to compare a coherence function between the excitation force and the dynamic response to a reference to identify the indication of the defect.

11. The system as set forth in claim 1, wherein the processing element is configured to determine one or more modal parameters, and compare the one or modal parameters to a reference to identify the indication of the defect.

12. The system as set forth in claim 1, wherein the processing element is configured to determine a characteristic time delay, and compare the characteristic time delay to a reference to identify the indication of the defect.

13. A system for the non-destructive testing of one or more parts manufactured using an additive manufacturing process, the system comprising:

an input mechanism configured to excite with vibrational excitation force an additive manufacturing build platform on which the one or more parts are located to induce a dynamic response in each of the parts, wherein the input mechanism directly excites the additive manufacturing build platform so as to indirectly excite the one or more parts located on the additive manufacturing build platform;

a non-contact transducer configured to sense the induced dynamic response in the one or more parts; and

an electronic processing element configured to determine a relationship between the vibrational excitation and the dynamic response, and to examine the relationship to identify an indication of a defect in the one or more parts, and to electronically communicate an alert if the indication of the defect is identified.

14. A method for the non-destructive testing of one or more parts manufactured using an additive manufacturing process, the method comprising:

exciting with an input mechanism an additive manufacturing build platform on which the one or more parts are located by using an excitation force to induce a dynamic response in the one or more parts;

sensing with an output mechanism the dynamic response in the one or more parts; and

determining with an electronic processing element a relationship between the excitation force and the dynamic response, and examining with the electronic processing element the determined relationship to identify an indication of a defect in the one or more parts, and electronically communicating an alert if the indication of the defect is identified.

15. The method as set forth in claim 14, wherein a plurality of parts located on the additive manufacturing build platform are tested simultaneously.

16. The method as set forth in claim 14, wherein the defect in the one or more parts is selected from the group consisting of:

porosities, voids, unfused powders, dimensional variations, non-homogenous powders, improper microstructure, and cracks.

17. The method as set forth in claim 14, wherein the excitation force is selected from the group consisting of:

impulsive vibrations, swept sinusoid vibrations, and random input vibrations.

18. The method as set forth in claim 14, wherein the excitation force excites the additive manufacturing build platform by introducing the excitation force directly to the additive manufacturing build platform so as to introduce the excitation force indirectly to the one or more parts located on the additive manufacturing build platform.

19. The method as set forth in claim 14, further including the step of minimizing external damping imparted to the one or more parts, including minimizing one or more forms of friction.

20. The method as set forth in claim 14, wherein the relationship between the excitation force and the dynamic response may include one or more of a frequency response function, a coherence function, a cross-correlation function, and a cross-power spectrum.

21. The method as set forth in claim 14, wherein the processing element is configured to compare a phase of the determined relationship to a reference to identify the indication of the defect.

22. The method as set forth in claim 14, wherein the processing element is configured to compare a magnitude of the determined relationship to a reference to identify the indication of the defect.

23. The method as set forth in claim 14, wherein the processing element is configured to compare a coherence function between the excitation force and the dynamic response to a reference to identify the indication of the defect.

24. The method as set forth in claim 14, wherein the processing element is configured to determine one or more modal parameters, and compare the one or modal parameters to a reference to identify the indication of the defect.

25. The method as set forth in claim 14, wherein the processing element is configured to determine a characteristic time delay, and compare the characteristic time delay to a reference to identify the indication of the defect.