Diaphragm deflection sensor for fused silica diaphragm module

• US 4,600,836 A
• Filed: 04/03/1984
• Issued: 07/15/1986
• Est. Priority Date: 04/03/1984
• Status: Expired due to Fees

• Current Assignee: Babcock & Wilcox Company (Babcock International Group PLC)
• Original Assignee: Babcock & Wilcox Company (Babcock International Group PLC)
• Inventors: Jeffers, Larry A., Berthold, John W. III, Thompson, Larry B.
• Primary Examiner(s): LaRoche, Eugene R.
• Assistant Examiner(s): Mottola, Steven J.
• Application Number:
  US06/596,481
• Time in Patent Office: 833 Days
• Field of Search: 73/705, 73/717, 73/800, 73/862.39, 250/227, 250/231 P, 250/231 R, 250/237 G, 250/237 R, 356/358
• US Class Current: 250/231.19
• CPC Class Codes: G01L 9/0077 for measuring reflected light

Abstract

A high temperature pressure transducer and sensing apparatus to determine the deflection of the transducer diaphragm is disclosed. The pressure transducer utilizes a fused silica diaphragm (12) which is illuminated at selected locations by a coherent laser source (52) via optical fibers (38, 46). The light reflected by the diaphragm (12) forms interference fringe patterns which are focused by gradient index rod lenses (36) on the ends of optical fibers (40, 48) for transmission to a fringe counting circuit (54). By digital techniques, the fringe count is converted into a determination of diaphragm deflection.

Claims

1. A system for determining the deflection of a pressure transducer diaphragm, comprising:

a light source;

first means for transmitting the light produced by said light source to the diaphragm at a first location thereon, located at the approximate center of the diaphragm;

second means for transmitting the light produced by said light source to the diaphragm at a second location thereon, said first and second locations being radially offset from one another and located on one side of said diaphragm;

first means for intercepting the light reflected from said first location on the diaphragm;

second means for intercepting the light reflected from said second location on the diaphragm, said light reflected from said first and second locations forming interference fringe patterns at their respective intercepting means;

first means for detecting said interference fringe patterns formed by the intercepted reflected light at said first intercepting means, and establishing output signals indicative thereof;

second means for detecting said interference fringe patterns formed by the intercepted reflected light at said second intercepting means, and establishing output signals indicative thereof;

third means for transmitting said intercepted reflected light forming interference fringe patterns from said first and second intercepting means to said first and second detecting means; and

a fringe counting circuit, connected to said first and second detecting means, for;

counting said output signals indicative of the interference fringe patterns formed at said first and second light intercepting means;

comparing the output signals from said first detecting means with the output signals from said second detecting means to determine whether said output signals from both detecting means are simultaneously increasing or decreasing; and

producing a determination as to the deflection of the pressure transducer diaphragm.

2. The system as defined in claim 1 wherein said first and second light transmitting means comprise:

first optical fiber means;

means for optically coupling said light source to said first optical fiber means;

light collimating means; and

means for optically coupling said light collimating means to said first optical fiber means.

3. The system as defined in claim 1 wherein said third light transmitting means comprise second optical fiber means.

4. The system as defined in claim 1 wherein said first and second light intercepting means comprise gradient index rod lenses, optically coupled to said third light transmitting means, for focusing said interference fringe patterns onto the ends of said second optical fiber means.

5. The system as defined in claim 1 wherein said first and second means for detecting said interference fringe patterns comprise photodetectors.

6. The system as defined in claim 1 wherein said pressure transducer diaphragm is comprised of fused silica material.

7. The system as defined in claim 1 wherein said light source is a coherent laser source.

8. The system as defined in claim 2 wherein said first optical fiber means comprise single mode optical fibers.

9. The system as defined in claim 3 wherein said second optical fiber means comprise multi-mode optical fibers.

10. The system as defined in claim 2 further including a 3 dB coupler optically coupled to and lying between said light source and said first optical fiber means of said first and second light transmitting means.