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US5094527A Expired / Lapsed US ⏱️ 0.0 years remaining

Temperature compensated strain sensor for composite structures

Assignee: Lockheed Martin Corp
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Filing: 1990-05-14
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Granted: 1992-03-10
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Expires: 2010-05-14
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Abstract

Abstract A temperature compensated strain sensor for measuring the strain at specific locations within a molded composite structure and the like, is disclosed. In detail, the invention comprises a hollow tubular member mounted within the structure which has first and second ends extending out thereof and passing in proximity to each specific location at with strain is to be measured. A first optical fiber is mounted within the hollow tubular member and has first and second ends exiting the first and second ends, respectively, of the hollow tubular member. A plurality of second optical fibers, equal to the number of specific locations at which strain is to be measured, are mounted within the hollow tubular member and have first and second ends exiting the first and second ends, respectively, thereof. One each of the second optical fibers exits the hollow tubular member and extends across and is bonded to the resin of the structure at the specific location and thereafter re-enters the hollow tubular member.

Inventors

  • 👤 David A. Martin

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 19:47
CPC Classifications
G; G01; G01M; G01M11/00; G01M11/08; G01M11/083; G01M11/086; G01B; G01B11/00; G01B11/16

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 169 words
A temperature compensated strain sensor for measuring the strain at specific locations within a molded composite structure, comprising: a hollow tubular member mounted within the structure and having first and second ends extending out thereof and passing in proximity to each specific location at which strain is to be measured; a temperature sensitive optical fiber mounted within said hollow tubular member and having first and second ends exiting said first and second ends, respectively, of said hollow tubular member; and strain and temperature sensitive optical fibers equal to the number of specific locations at which strain is to be measured, said strain and temperature sensitive optical fibers mounted within said hollow tubular member and having first and second ends exiting said first and second ends of said hollow tubular member, respectively, thereof, one each of said strain and temperature measuring optical fibers exiting said hollow tubular member and extending across and bonded to the resin of the structure at the specific location and thereafter re-entering said hollow tubular member.
Claim 2
Dependent Claim 169 words
A temperature compensated strain sensor for measuring the strain at specific locations within a molded composite structure, comprising: a hollow tubular member mounted within the structure and having first and second ends extending out thereof and passing in proximity to each specific location at which strain is to be measured; a temperature sensitive optical fiber mounted within said hollow tubular member and having first and second ends exiting said first and second ends, respectively, of said hollow tubular member; and strain and temperature sensitive optical fibers equal to the number of specific locations at which strain is to be measured, said strain and temperature sensitive optical fibers mounted within said hollow tubular member and having first and second ends exiting said first and second ends of said hollow tubular member, respectively, thereof, one each of said strain and temperature measuring optical fibers exiting said hollow tubular member and extending across and bonded to the resin of the structure at the specific location and thereafter re-entering said hollow tubular member.
Claim 3
Dependent Claim 110 words
The sensor as set for in claim 1 wherein: said hollow tubular member comprises alternating first and second hollow tubular sections joined together, said second sections located in the proximity to the specific locations, said second sections having a diameter less than the diameter of said first sections and further having ends in an overlapping relationship with adjacent ends of said first sections; said one each of said strain and temperature sensitive fibers exiting and returning to said hollow tubular member between the overlapping portions of first and second hollow tubular sections; and said overlapping portions of said first and second tubular sections sealed to each other by an adhesive.
Claim 4
Dependent Claim 32 words
The sensor as set forth in claim 2 wherein said sensor further comprises means to sense the change in length in said temperature measuring and said strain and temperature sensitive optical fibers.

References Cited (Backward Citations)

US3910105A Cited
US4163397A Cited
US4697876A Cited
US4836030A Cited
US4932262A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1995-03-10 1995-09-09 1996-03-10 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1999-03-10 1999-09-09 2000-03-10 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2003-03-10 2003-09-09 2004-03-10 $7700.00 Window Closed / Lapsed

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