Vibrating beam force sensor of improved ruggedness and mountability
At least one support tine, disposed generally in parallel to the force sensing tines of a DETF, is added to increase the stiffness of the structure for resisting various strains during assembly. Once the bonding operation is complete, the support tine(s) are cut or broken away from the structure to leave the remaining structure relatively strain free for operation.
1. A double-ended tuning fork vibrating beam assembly comprising:
first and second mount structures;
first and second generally parallel vibrating tines operatively coupled at respective longitudinal ends thereof to said first and second mount structures;
electrodes for stimulating said vibrating tines into vibration and for monitoring the frequency of vibration wherein the frequency of vibration is related to a direction and amount of force applied to said mount structures; and
first and second support tines extending between said mount structures outboard of said vibrating tines thereby increasing the stiffness of the assembly and resisting bending, twisting and bowing strains on said vibrator tines during manipulation and bonding/assembly, said support tines being adapted to be disabled following bonding/assembly to disable their strain resist function whereby the vibrating tines can operate as designed,
wherein the first and second support tines have a transverse dimension at every point along their length that is greater than the corresponding transverse dimension of the vibrating tines.
2. An assembly as in claim 1 , wherein each said support tine includes indicia for indicating a location for cutting or breaking the support tine to disable said strain resist function.
3. An assembly as in claim 2 , wherein said indicia comprises an area of weakness in each said support tine.
4. An assembly as in claim 3 , wherein said area of weakness includes at least one notch.
5. An assembly as in claim 4 , wherein said area of weakness comprises first and second diametrically opposite notches in said respective support tine.
6. An assembly as in claim 4 , wherein there is at least one notch at each longitudinal end of said support tine, adjacent said mount structures.
7. A double-ended tuning fork vibrating beam assembly comprising:
first and second mount structures;
first and second generally parallel vibrating tines operatively coupled at respective longitudinal ends thereof to said first and second mount structures;
electrodes for stimulating said vibrating tines into vibration and for monitoring the frequency of vibration wherein the frequency of vibration is related to a direction and amount of force applied to said mount structures; and
at least one support tine extending between said mount structures to rigidify the assembly, thereby to resist bending, twisting and/or bowing strains applied to the assembly, said at least one support tine including indicia for indicating a location for cutting or breaking the at least one support tine to disable said strain resist function,
wherein said indicia comprises an area of weakness in the at least one support tine,
wherein said area of weakness includes at least one notch, and
wherein each said area of weakness comprises first and second diametrically opposite notches in said support tine.
8. An assembly as in claim 7 , wherein there is first and second diametrically opposite notches at each longitudinal end of said support tine, adjacent said mount structures.
9. An assembly as in claim 7 , wherein each said mount structure includes a shoulder section between which said vibrating tines extend.
10. An assembly as in claim 7 , wherein said mount structures, vibrating tines, and at least one support tine are integrally formed in one piece.
11. A method of mounting a transducer comprising:
providing a transducer including:
first and second mount structures and first and second generally parallel vibrating tines operatively coupled at respective longitudinal ends thereof to said first and second mount structures,
electrodes for stimulating said vibrating tines into vibration and for monitoring the frequency of vibration wherein the frequency of vibration is related to a direction and amount of force applied to said mount structures, and
at least one support tine extending between said mount structures to rigidify the assembly, thereby to resist bending, twisting and/or bowing strains applied to the assembly;
bonding said mount structures to an assembly the forces on which are to be measured; and
disabling said strain resist function by at least one of cutting or breaking said at least one support tine.
12. A method as in claim 11 , wherein said disabling comprises removing the support tine.
13. A method as in claim 12 , wherein substantially the entire support tine is removed.
14. A method as in claim 11 , wherein the at least one support tine includes indicia for indicating a location for cutting or breaking the support tine.
15. A method as in claim 14 , wherein the indicia is an area of weakness.
16. A method as in claim 15 , wherein the indicia includes at least one notch.
17. A method as in claim 11 , wherein there are first and second support tines disposed outboard of the vibrating tines.