Vibrating beam force transducer with angled isolator springs

• US 4,658,174 A
• Filed: 03/20/1986
• Issued: 04/14/1987
• Est. Priority Date: 03/20/1986
• Status: Expired due to Term

• Current Assignee: Kearfott Corp. (Astronautics Corporation of America)
• Original Assignee: The Singer Company - Patent Department
• Inventors: Albert, William C.
• Primary Examiner(s): BUDD, MARK OSBORNE
• Application Number:
  US06/841,982
• Time in Patent Office: 390 Days
• Field of Search: 310/321, 310/323, 310/324, 310/338, 310/367, 310/368, 310/361, 310/25, 310/330-332, 310/329, 73/778, 73/777, 73/781, 73/141 R, 73/DIG. 1, 73/DIG. 4, 73/517 R, 73/517 AV, 29/25.35, 338/2, 338/47, 357/26
• US Class Current: 310/323.21
• CPC Class Codes: G01L 1/106 Constructional details
• CPC Class Codes: G01P 15/097 by vibratory elements
• CPC Class Codes: Y10S 73/01 Vibration

Abstract

An isolation system which prevents energy from being transferred by the vibrating member of a resonator to its end mounts is formed by having isolator springs coupled to respective isolation masses. Each of the isolation masses is connected to a corresponding end mount. Each pair of isolator springs is angled in such a way that the axes of the isolator springs would intersect at a node located somewhere along the longitudinal axes of the vibrating member. Consequently, the axes of the isolator springs are positioned perpendicularly to loci of motions representing the direction of force and moment reactions produced at the roots of the vibrating member.

Claims

1. An apparatus comprising:

a member adapted to vibrate in a plane along the longitudinal axis;

means connected to the member for maintaining the vibration of the member at a characteristic frequency;

an isolation mass secured to each end of the member, each isolation mass including a base extending transversely from the longitudinal axis in both directions;

an end mount positioned in parallel spaced relation to the base of each isolation mass;

a pair of non-parallel spaced isolator springs coupling each isolation mass to the corresponding end mount, each isolator spring being positioned perpendicularly to a locus of motion located proximately at the base of the isolation mass, the locus of motion intersecting the junction of the base where the isolation spring is coupled to the isolation mass, the locus of motion being representative of the direction of motion of the force and moment reactions produced at the root of the vibrating member;

whereby energy losses from the vibrating member are substantially eliminated.

2. The apparatus according to claim 1, wherein each non-parallel spaced isolator spring is angled obliquely toward the longitudinal axis from the base of the isolation mass to the corresponding end mount, respective axes of the isolator springs intersecting at a node located in the direction away from the vibrating member and the junction where the springs are coupled to the base.

3. The apparatus according to claim 1, wherein each non-parallel spaced isolator spring is angled obliquely toward the longitudinal axis from the corresponding end mount to the base of the isolation mass, the axes of the isolator springs intersecting at a node located away from the junction of the isolator mass where the springs are coupled.

4. The apparatus according to claim 2, wherein the member is a beam.

5. The apparatus according to claim 3, wherein the member is a beam.

6. The apparatus according to claim 1, wherein the apparatus is made of piezoelectric material.

7. The apparatus according to claim 1, wherein the apparatus is made of quartz.

8. The apparatus according to claim 1, wherein the apparatus is made of metal.

9. In an apparatus including a vibrating member, an isolation mass secured to each end of the vibrating member and an end mount positioned in spaced relation to each isolation mass, a method of preventing energy losses from the vibrating member, comprising:

interposing between each isolation mass and the corresponding end mount a pair of non-parallel spaced isolator springs for coupling the isolation mass to the corresponding end mount;

positioning each isolator spring perpendicularly to a locus of motion located in the isolation mass, the locus of motion intersecting the junction where the isolator spring is coupled to the isolation mass, the location of motion being representative of the direction of motion of the force and moment reactions produced at the root of the vibrating member;

thereby preventing energy losses from the vibrating member.

10. The method according to claim 9, wherein the positioning step further comprises:

angling each isolator spring obliquely from the base of the isolation mass to the corresponding end mount; and

projecting the axes of the isolator springs toward the longitudinal axis of the vibrating member;

thereby intersecting the node located in the direction away from the vibrating member and the junctions of the isolation mass where the isolator springs are coupled.

11. The method according to claim 9, wherein the positioning step further comprises:

angling each isolator spring obliquely from the corresponding end mount to the isolation mass;

projecting the axes of the isolator springs toward the longitudinal axis of the vibrating member;

thereby intersecting a node located away from the junctions of the isolator mass where the springs are coupled.