Method and apparatus for ultrasonic inspection

• US 4,945,766 A
• Filed: 09/08/1989
• Issued: 08/07/1990
• Est. Priority Date: 09/08/1989
• Status: Expired due to Fees

• Current Assignee: General Motors Corporation (Motors Liquidation Co. GUC Trust)
• Original Assignee: General Motors Corporation (Motors Liquidation Co. GUC Trust)
• Inventors: Hickling, Robert, Pirrallo, Karen M., Dahlmann, Virgil R., Talaki, Kelly A., Zielesch, Kenneth J.
• Primary Examiner(s): MYRACLE, JERRY
• Application Number:
  US07/404,469
• Time in Patent Office: 333 Days
• Field of Search: 73/119 R, 73/597, 73/598, 73/865.8, 73/629, 73/620, 73/598, 382/8, 367/104, 358/96
• US Class Current: 73/598
• CPC Class Codes: G01B 17/00 Measuring arrangements characterised by the use of infrasonic, sonic or ultrasonic vibrations
• CPC Class Codes: G01N 29/30 Arrangements for calibrating or comparing, e.g. with standard objects
• CPC Class Codes: G01S 15/89 for mapping or imaging

Abstract

Valve spring assemblies are checked for proper assembly of keys by ultrasonically scanning a plurality of assemblies along a path crossing the stem, keys and cap to acquire profile data; compensating for temperature effects by determining the average time of flight to the stems, which are nominally the same distance from the ultrasonic sensor, and searching for each individual stem in a window centered on the average time of flight; then defining windows for the keys and cap offset from the measured surface of each stem; and searching the data for points within the respective windows to determine proper positioning of each element. The apparatus includes ultrasonic equipment, a scanning manipulator to move the ultrasonic sensor over the part, and a computer interfaced to the ultrasonic equipment and manipulator for control and data analysis.

Claims

1. In an ultrasonic sensing system having a sensor for inspecting a series of objects each having a plurality of surfaces facing the sensor including a reference surface at a known nominal distance from the sensor, the method comprising the steps of:

scanning the sensor over the surfaces of the objects and recording the time of flight of the ultrasonic signals;

determining the average time of flight to the reference surfaces in the course of inspecting a series of objects;

for each object, establishing parameters on the desired distance of each surface from the reference surface, extracting features from the recorded time of flight data, locating the feature corresponding to the reference surface based on the average time of flight, and determining the reference time of flight;

setting a window in which each acceptable surface other than the reference surface is to be found; and

determining whether each feature for a respective surface is in a corresponding window.

2. The invention as defined in claim 1 including setting each window location based on the desired distance of each surface from the plane of reference surface and the reference time of flight.

3. The invention as defined in claim 2 including setting a window width corresponding to the allowable tolerance of the feature position and setting lateral window depending on feature size and position as measured from the reference surface feature.

4. The invention as defined in claim 1 including the steps of setting a reference time window around the average time of flight in which an acceptable reference surface is to be found, and determining for each object whether its reference surface is within the reference window.

5. The invention as defined in claim 1 wherein the step of establishing parameters comprises:

scanning a model object with the sensor and determining an offset and a window width for each feature surface.

6. The invention as defined in claim 1 wherein the step of scanning with the sensor comprises sweeping paths along the surfaces at a repeatable rate and with ultrasonic pulses emitted at a constant frequency.

7. The invention as defined in claim 1 wherein the step of extracting features from the time of flight data comprises grouping the time of flight data for each feature distinguished from adjacent features by gaps in received data and by substantial differences in time of flight.

8. In an ultrasonic sensing system having a sensor for inspecting a series of valve spring assemblies each having a plurality of surfaces facing the sensor including keys and caps and including a stem surface at a known nominal distance from the sensor, the method comprising the steps of:

establishing desired parameters including the desired offset of each key and cap surface from the stem surface and the size of each key and cap surface;

scanning the sensor over the valve spring assemblies including the stem surfaces and recording the time of flight of each ultrasonic signal;

averaging the time of flight of the signals for a plurality of stem surfaces;

setting a time window in which a stem is to be found, the stem window being based on the allowable tolerance of the stem surface and the averaged time of flight;

for each particular stem, measuring the average time of flight for the surface and determining whether the stem surface is within the stem window;

setting time windows in which each acceptable key and cap is to be found, each window being based on the desired offset of each key and cap, respectively, and the averaged time of flight for the respective stem surface; and

determining whether the resulting time of flight for each key and cap surface is in a corresponding time window.

9. The invention as defined in claim 8 wherein an established desired parameter is that the cap be parallel to the stem surface and including the step of determining whether the cap is parallel to the stem surface by calculating the slope of cap time of flight data.

10. The invention as defined in claim 8 wherein the step of determining whether the resulting time of flight for each key and cap surface is in a corresponding time window comprises the steps of:

determining the size of each surface from the number of signal pulses at a given position; and

identifying the cap and the keys from the position and size data.

11. The invention as defined in claim 10 wherein a stream of data is generated during each scan across the assembly, and wherein the step of identifying the stem, cap and the keys comprises:

searching for stem data in the center of the stream data produced during the scan across the valve assembly, verifying the position of the stem, searching adjacent the stem data for key data, and searching adjacent the key data for the cap data.

12. The invention as defined in claim 8 wherein time windows for the keys and caps are two dimensional having lateral boundaries, and the step of setting time windows further comprises:

setting boundaries spaced laterally from the stem position based on the sizes and the expected distances from the stem of keys and caps respectively.

13. Apparatus for ultrasonic inspection of object configurations where each object has a reference surface and feature surfaces to be measured, comprising:

ultrasonic sensor means for emitting a series of pulses toward a surface to be measured, receiving reflected pulses and measuring the time of flight of the pulses,

means for scanning the sensor means across the object in a predetermined path along the surfaces to be measured,

memory means for storing the size of each surface along the scan path and the desired offset distance of each feature surface from the reference surface, and

computer means including the memory means for

(a) determining a reference time of flight based on a running average of pulses to the reference surfaces,

(b) setting a time window based on the reference time of flight for an acceptable reference surface,

(c) locating the reference surface within the said time window,

(d) setting a time window for each feature surface referenced to the time of flight for the located reference, and

(e) comparing the time of flight for each measured object surface to the corresponding feature time window to determine acceptability.

14. Apparatus for ultrasonic inspection of a valve spring assembly where each assembly has a reference stem surface and key surfaces to be measured, comprising:

ultrasonic sensor means for emitting a series of pulses toward the assembly to be measured, receiving reflected pulses and measuring the time of flight of the pulses,

manipulator means for scanning the sensor means across the valve spring assemblies in a predetermined path along the surfaces to be measured,

memory means for storing the size of each stem and key surface along the scan path and the desired offset distance of each key surface from the stem surface, and

computer means including the memory means for

(a) determining a reference time of flight based on a running average of pulses to a plurality of the stem surfaces,

(b) setting a time window based on the reference time of flight for an acceptable stem height,

(c) locating the stem surface within the said time window,

(d) setting a key time window for key surfaces referenced to the time of flight for the located stem surface, and

(e) comparing the time of flight for each measured key surface to the corresponding key time window to determine acceptability.

15. Apparatus for ultrasonic inspection of a valve spring assembly where each assembly has a reference stem surface and key and cap surfaces to be measured, comprising:

ultrasonic sensor means for emitting a series of pulses toward the assembly to be measured, receiving reflected pulses and measuring the time of flight of the pulses,

manipulator means for scanning the sensor means across the valve spring assemblies in a predetermined path along the surfaces to be measured,

memory means for storing the size of each stem, key and cap surface along the scan path and the desired offset distance of each key surface from the stem surface, and

computer means including the memory means for

(a) determining a reference time of flight based on a running average of pulses to a plurality of the stem surfaces,

(b) setting a time window based on the reference time of flight for an acceptable stem height,

(c) locating the stem surface within the said time window,

(d) setting cap and key time window for cap and key surfaces referenced to the time of flight for the located stem surface,

(e) comparing the time of flight for each measured key surface to the corresponding key time window,

(f) determining cap tilt from the measured cap surfaces, and

(g) determining acceptability from the presence of key surfaces within the key windows and from the cap tilt.