Magnetostrictive type strain sensing means and methods

• US 7,913,569 B2
• Filed: 12/11/2007
• Issued: 03/29/2011
• Est. Priority Date: 12/11/2007
• Status: Expired due to Fees

• Current Assignee: Israel Aerospace Industries Limited (Government of Israel)
• Original Assignee: Israel Aerospace Industries Limited (Government of Israel)
• Inventors: Shammass, Saeid, Sol, Uri, Girshovich, Simon
• Primary Examiner(s): Caputo; Lisa M
• Assistant Examiner(s): ROY, PUNAM P
• Application Number:
  US12/001,622
• Publication Number:
  US 20090145239A1
• Time in Patent Office: 1,204 Days
• Field of Search: 737/79, 324/209
• US Class Current: 73/779
• CPC Class Codes: G01B 7/16 for measuring the deformation in a solid, e.g. by resistance strain gauge

Abstract

A strain gauge including: a system including a transmission coil, a magnetostrictive material layer and a receiver coil wherein an alternating transmission signal is applied across the transmission coil and an induced signal is induced in the receiver coil, the intensity of the detected signal across the receiver coil being a measurement of strain, wherein frequency of transmission signal is near to a resonance frequency of the system.

Claims

1. A method of monitoring strain at a designated location in a composite substructure comprising a solid dielectric material, comprising the steps of:

fixing a magnetostrictive material layer to the composite substructure;

bringing a transmission coil into proximity with the magnetostrictive material;

bringing a receiver coil into proximity with the magnetostrictive material;

applying an electrical signal across the transmission coil over a range of frequencies; and

monitoring a frequency near a resonant frequency and having a near minimum detected signal strength across the receiver coil to determine changes in strain of the composite substructure.

2. The method of claim 1, wherein the magnetostrictive material is sandwiched between the transmission coil and the receiver coil.

3. The method of claim 1, wherein said composite substructure comprises said solid dielectric at said location, and at least one of a group consisting of the transmission coil, receiver coil and magnetostrictive material layer are embedded in the composite substructure for measuring the strain of the structural component.