Vibrating beam force transducer with single isolator spring

• US 4,656,383 A
• Filed: 02/14/1986
• Issued: 04/07/1987
• Est. Priority Date: 02/14/1986
• 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 O.
• Application Number:
  US06/829,728
• Time in Patent Office: 417 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, 338/2, 338/47, 357/26
• US Class Current: 310/321
• CPC Class Codes: G01L 1/162 using piezoelectric resonators
• CPC Class Codes: G01P 15/097 by vibratory elements
• CPC Class Codes: Y10S 73/01 Vibration

Abstract

A force transducer having a vibratory member either a beam or a string and means for effectively isolating the vibratory member from its end mounts over the range of its operating frequencies to eliminate energy loss to the mounts. The axial stresses, either tension or compression, are directly transferred to the vibratory member to affect its natural resonant frequency. Isolation at vibration frequencies is effected by the cooperation of combined isolator masses and isolator springs with the vibratory member. The isolator masses comprise two bars extending from each end support of the vibratory member, each being coextensive with a portion of the support member. The pairs of masses are axially separated. The isolator springs comprise two single thin, spaced resilient members, each isolator spring connecting a single end support of the member and a single transducer end mount.

Claims

1. An apparatus comprising:

a single vibratory member having a longitudinal axis, said vibratory member being adapted to vibrate in a plane including said longitudinal axis;

means associated with said vibratory member to maintain vibration thereof at a characteristic frequency;

a supporting element secured to each end of said vibratory member and extending in both directions transversely of said longitudinal axis of said vibratory member;

a pair of end mounts;

two isolator springs each having a longitudinal axis, one of said isolator springs extending between one of said end mounts and one of said supporting elements, the other of said isolator springs extending between the other of said end mounts and the other of said supporting elements, said isolator springs transmitting axial forces from said end mounts to said vibratory member along the longitudinal axis thereof; and

a pair of isolator masses secured to each of said supporting elements, one at each end thereof respectively, said isolator masses being symmetrically disposed with respect to said vibratory member and one isolator mass of each pair of isolator masses being different in size and mass from the other isolator mass of the respective isolator mass pairs, said isolator springs and masses being effective to cancel the force and moment restraints produced at said end mounts whereby energy losses from said vibrating member may be prevented.

2. The apparatus of claim 1 wherein said isolator springs are attached to said supporting elements so that the longitudinal axes of said isolator springs are substantially coincident with the longitudinal axis of said vibratory member.

3. The apparatus of claim 1 wherein said vibratory member is a beam and said isolator masses generally extend along said longitudinal axis of said beam for coextensively straddling at least a portion of said beam, whereby the center of gravity corresponding to each of said pair of isolator masses is located in said plane including said longitudinal axis at a predetermined axial distance from said supporting elements.

4. The apparatus of claim 1 wherein said vibratory member is a string and the center of gravity corresponding to each of said pair of isolator masses is located in said plane including said longitudinal axis at the location where said string is secured to each of said supporting elements.

5. The apparatus of claim 1 wherein corresponding ones of said isolator masses are integrally connected to each other to form a single pair of isolator masses each one of which extending from one supporting element to the other, whereby said isolator masses prevent axial forces from being transmitted to said vibratory member.

6. The apparatus of claim 1 wherein each end mount has a pair of opposing recesses to form a pair of flexure hinges.

7. The apparatus of claim 1 wherein said apparatus is made of piezoelectric material.

8. The apparatus of claim 1 wherein said apparatus is made of quartz.

9. The apparatus of claim 1 wherein said apparatus is made of metal.

10. An apparatus comprising:

a single vibratory member having a longitudinal axis, said vibratory member being adapted to vibrate in plane including said longitudinal axis;

means associated with said vibratory member maintain vibration thereof at a characteristic frequency;

a supporting element secured to each end of said vibratory member and extending in both directions transversely of said longitudinal axis of said vibratory member;

a pair of end mounts;

two isolator springs each having a longitudinal axis, one of said isolator springs extending between one of said end mounts and one of said supporting elements, the other of said isolator springs extending between the other of said end mounts and the other of said supporting elements, said isolator springs transmitting axial forces from said end mounts to said vibratory member along the longitudinal axis thereof;

a pair of isolator means secured to each of said supporting elements, each pair being symmetrically disposed with respect to said vibratory member;

wherein one isolator means of each pair is asymmetric to the other isolator means of the pair;

wherein said isolator springs and means are effective to cancel the force and moment restraints produced at said end mounts to reduce or prevent energy losses from said vibrating member.

11. The apparatus of claim 10 wherein said isolator springs are attached to said supporting elements so that the longitudinal axes of said isolator springs are substantially coincident with the longitudinal axis of said vibratory member.

12. The apparatus of claim 10 wherein said vibratory member is a beam and said isolator means generally extends along said longitudinal axis of said beam for coextensively straddling at least a portion of said beam, whereby the center of gravity corresponding to each of said pair of isolator means is located in said plane including said longitudinal axis at a predetermined axial distance from said supporting elements.

13. The apparatus of claim 10 wherein said vibratory member is a string and the center of gravity corresponding to each of said pair of isolator means is located in said plane including said longitudinal axis at the location where said string is secured to each of said supporting elements.

14. The apparatus of claim 10 wherein corresponding ones of said isolator means are integrally connected to each other to form a single pair of isolator means each one of which extending from one supporting element to the other, whereby said isolator means prevent axial forces from being transmitted to said vibratory member.

15. The apparatus of claim 10 wherein each end mount has a pair of opposing recesses to form a pair of flexure hinges.

16. The apparatus of claim 10 wherein said apparatus is made of piezoelectric material.

17. The apparatus of claim 10 wherein said apparatus is made of quartz.

18. The apparatus of claim 10 wherein said apparatus is made of metal.