Device and method for detecting workpiece fractures

• US 5,952,836 A
• Filed: 04/28/1997
• Issued: 09/14/1999
• Est. Priority Date: 04/28/1997
• Status: Expired due to Fees

• Current Assignee: Mcdonnell Douglas Corporation (The Boeing Co.)
• Original Assignee: Mcdonnell Douglas Corporation (The Boeing Co.)
• Inventors: Haake, John M.
• Primary Examiner(s): Ballato, Josie
• Assistant Examiner(s): VALONE, THOMAS F
• Application Number:
  US08/846,180
• Time in Patent Office: 869 Days
• Field of Search: 324/718, 73/799, 73/776, 73/789, 73/783, 416/61, 416/134
• US Class Current: 324/718
• CPC Class Codes: G01R 27/08 Measuring resistance by measuring both voltage and current
• CPC Class Codes: G01R 31/52 Testing for short-circuits, leakage current or ground faults
• CPC Class Codes: G01R 31/54 Testing for continuity
• CPC Class Codes: G01R 31/58 Testing of lines, cables or conductors testing of electric windings G01R31/72
• CPC Class Codes: H05K 1/053 the metal substrate being covered by an inorganic insulating layer
• CPC Class Codes: H05K 1/167 incorporating printed resistors
• CPC Class Codes: H05K 3/048 using a lift-off resist pattern or a release layer pattern

Abstract

A device for detecting fractures or corrosion in a workpiece having a non-conductive outer surface. A thin film layer of metallic material comprising a plurality of separate crack detection wires is bonded to the non-conductive surface of the workpiece. A top coating of protective material is applied to the thin film layer to protect the detection wires from abrasion and corrosion. When an electrical current is transmitted through the detection wires, a predictable resistivity pattern is viewable on a monitor. As a fracture propagates through the workpiece causing the crack detection wires to break one-by-one, the change in resistivity of the wires can be monitored and the existence and extent of any fracture or corrosion to the wires determined.

Claims

1. A device for detecting fractures in a rotor strap of a helicopter, the rotor strap including first and second legs that form an acute angle having an apex, an inboard lug that joins the first and second legs inboard of the apex, and first and second outboard lugs disposed at distal ends of the first and second legs, repectively, wherein the device includes:

an electrically conductive wiring pattern formed on a major surface of the rotor strap, the wiring pattern including a first portion disposed about the inboard lug, a second portion adjacent the apex, a third portion extending along the first leg, a fourth portion extending along the second leg, a fifth portion disposed about the first outboard lug, and a sixth portion disposed about the second outboard lug; and

,

wherein the wiring pattern is formed in such a manner that a fracture in the rotor strap that intersects the wiring pattern will cause the wiring pattern to fracture, whereby the existence of a fracture in the rotor strap can be detected by monitoring one or more electrical characteristics of the wiring pattern.

2. The device as set forth in claim 1, further including a protective top coating formed on the wiring pattern to protect the wiring pattern from abrasion and corrosion.

3. The device as set forth in claim 1, wherein the major surface of the rotor strap is electrically non-conductive.

4. The device as set forth in claim 1, further including means for coupling the wiring pattern to a test instrument that is capable of monitoring at least one electrical characteristic of the wiring pattern.

5. The device as set forth in claim 1, wherein the rotor strap comprises an aluminum substrate and the major surface comprises an anodized surface of the aluminum substrate.

6. The device as set forth in claim 1, wherein the wiring pattern is comprised of a plurality of separate, spaced-apart wires.

7. The device as set forth in claim 1, wherein the second portion of the wiring pattern has a serpentine shape.

8. The device as set forth in claim 1, wherein each of the first, second, third, fourth, and fifth portions of the wiring pattern has a serpentine shape.

9. The device as set forth in claim 1, wherein the rotor strap comprises an aluminum substrate and the major surface comprises an electrically insulating layer formed on the aluminum substrate.

10. The device as set forth in claim 7, wherein the wiring pattern is comprised of a plurality of separate, spaced-apart wires.

11. The device as set forth in claim 8, wherein the wiring pattern is comprised of a plurality of separate, spaced-apart wires.