Claims
- 1. An ultrasonic inspection system for inspecting an aircraft stiffener comprising an immersion system including in combination:
- motor drive wheels;
- a fore and aft motor drive assembly;
- said fore and aft motor drive assemblies operating synchronously;
- a spring loaded platform;
- said fore and aft motor drive assemblies mounted on said spring-loaded platform for pushing said fore and aft motor drive assemblies against the aircraft stiffener;
- a non-movable fixed drive wheel disposed opposite said motor drive wheels; the interaction of said motor drive wheels providing translational movement of the stiffener through said immersion system;
- said immersion system including an immersion tank having an edge probe within said immersion tank for inspecting the edge of said aircraft stiffener;
- fore and aft position encoder assemblies operating synchronously;
- said fore position encoder assembly actuated as an aircraft stringer moves through said immersion system; and
- said aft position encoder assembly activated when said aircraft stringer disengages from said fore position encoder assembly until said aircraft stringer disengages from said aft position encoder assembly.
RELATED PATENT APPLICATIONS
This is divisional application to continuation-in-part U.S. patent application Ser. No. 08/829,968, filed Apr. 1, 1997, assigned to The Boeing Company, which is continuation-in-part of U.S. patent application Ser. No. 08/664,899, filed Jun. 17, 1996, now abandoned assigned to The Boeing Company, which is a continuation in part of U.S. patent application Ser. No. 08/086,283, filed Jul. 1, 1993, now U.S. Pat. No. 5,585,564, issued Dec. 17, 1996, assigned to the Boeing Company
US Referenced Citations (10)
Foreign Referenced Citations (1)
Number |
Date |
Country |
2064 773 |
Dec 1979 |
GBX |
Divisions (1)
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Number |
Date |
Country |
Parent |
829968 |
Apr 1997 |
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Continuation in Parts (2)
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Number |
Date |
Country |
Parent |
664899 |
Jun 1996 |
|
Parent |
086283 |
Jul 1993 |
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