Multifunction sensor using thin film transistor transducers

• US 4,457,173 A
• Filed: 05/03/1982
• Issued: 07/03/1984
• Est. Priority Date: 05/03/1982
• Status: Expired due to Fees

• Current Assignee: United States Of America As Represented By The Secretary Of The Army (Government of the United States of America)
• Original Assignee: The United States Of America As Represented By The Secretary Of The Army
• Inventors: Hunter, Joe S.
• Primary Examiner(s): Gill, Jr., James J.
• Assistant Examiner(s): Chapman, Jr., John E.
• Application Number:
  US06/373,922
• Time in Patent Office: 792 Days
• Field of Search: 73/504, 73/505, 73/510, 73/511, 73/516 R, 73/517 R, 73/517 A, 74/5 F, 74/5.6 D
• US Class Current: 73/510
• CPC Class Codes: G01C 19/02 Rotary gyroscopes
• CPC Class Codes: G01P 15/14 by making use of gyroscopes gyroscopes per se G01C19/00

Abstract

A multifunction sensor provides two axes of angular rate and two axes of ear acceleration information from a single instrument. The multifunction sensor utilizes an air bearing rotor to support the spinning transducers. Angular rate measurements are made by utilizing two thin film transistors mounted on the rotor and oriented to sense strain about axes in a first plane orthogonal to the rotor spin axis. The two transducers output signals are summed to provide common mode rejection. A second set of thin film transistors are mounted on the rotor in a second plane orthogonal to that of the first set of transistors and oriented to sense strain along the axes orthogonal to the rotor spin axis. Two axes of acceleration can be measured by integrating this output signal at the proper time using a clock frequency. Angular rate and linear acceleration signals may be extracted from the rotating member via slip ring contacts or inductive pickoffs. These AC signals are amplified and demodulated to provide voltages which are proportional to angular rate and linear acceleration.

Claims

1. A rotating body which rotates at a high speed about a first axis, the improvement comprising a first flexible joint mounted on said body in a first plane orthogonal to said first axis whereby acceleration of said body will cause said flexible joint to flex;

a first transducer mounted in said flexible joint so as to detect at its output the amount of strain in said flexible joint caused by said acceleration;

first measurement means connected to said first transducer for measuring said acceleration;

a second flexible joint mounted on said body in a second plane which is orthogonal to said first plane;

a second transducer connected to said second joint so as to detect at its output the amount of strain in said second joint caused by acceleration of said body; and

second measurement means connected to said second transducer for measuring the output of said second transducer.

2. A device as set forth in claim 1 wherein said first flexible joint is mounted in a horizontal plane relative to said first axis;

and said second flexible joint is mounted in a vertical plane relative to said first axis.

3. A device as set forth in claim 1 or 2 wherein said transducers are thin film transistors which vary their outputs in accordance to strain exerted on the transistors.

4. A device as set forth in claim 2 further comprising a third flexible joint mounted in the plane of said first flexible joint on the other side of said axis;

a fourth flexible joint mounted in the plane of said second flexible joint on the other side of said axis;

third and fourth transducers mounted in said third and fourth flexible joints respectively for measuring the strain on these joints; and

said measurement means summing outputs of said first and third transducers and said second and fourth transducers respectively so to provide common mode rejection.

5. A device as set forth in claim 1 or 4 wherein said body is rotated in an air bearing suspension system.