Device and method for detecting workpiece fractures
First Claim
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.
1 Assignment
0 Petitions
Accused Products
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.
63 Citations
11 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. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
-
Specification