Selectively tuning frequency modes of a structure

1. A method comprising:

by program instructions on a computing device,

identifying, by a finite element analysis module, a plurality of frequency modes of a structure; and

selectively altering a target frequency mode a greater amount than the other frequency modes of the structure, including modifying a local physical attribute of a portion of the structure associated with the target frequency mode without modifying the physical attribute over the entire structure comprising:

receiving, by the finite element analysis module, an identification of the target frequency mode;

identifying, by the finite element analysis module, a current frequency of the target frequency mode;

receiving, by the finite element analysis module, an identification of a preferred frequency of the target frequency mode;

calculating, by the finite element analysis module, a modal ratio as the quotient of the preferred frequency divided by the current frequency;

calculating, by the finite element analysis module, an amount of mass to change in dependence upon the modal ratio;

providing, by the finite element analysis module, to a geometry modification module, the calculated amount of mass to change;

identifying, by the finite element analysis module, one or more locations of the structure to change mass by the calculated amount, including identifying locations at which deflection is greater than a predefined threshold when operating at the target frequency mode;

providing, by the finite element analysis module, to the geometry modification module, the identified locations of the structure to change the mass by the calculated amount;

changing, by the geometry modification module, mass by the calculated amount at the identified locations;

identifying, by the finite element analysis module, again the frequency modes of the structure, including identifying a shifted frequency of the target frequency mode; and

recalculating, by the finite element analysis module, the modal ratio as the quotient of the target frequency divided by the shifted frequency.

2. The method of claim 1 wherein modifying the local attribute of the portion of the structure associated with the target frequency mode without modifying the physical attribute over the entire structure is preformed, iteratively, until the modal ratio falls within a predefined range of values.

3. The method of claim 1 wherein modifying the local physical attribute of the portion of the structure associated with the target frequency mode without modifying the physical attribute over the entire structure further comprises:

iteratively, until the modal ratio falls within the predefined range of values:

calculating an amount of stiffness to change in dependence upon the modal ratio;

providing, to the geometry modification module, the calculated amount of stiffness to change;

identifying one or more locations of the structure to change the stiffness by the calculated amount, including identifying locations at which strain is greater than a predefined threshold when operating at the target frequency mode;

providing, to the geometry modification module, the identified locations of the structure to change the stiffness by the calculated amount;

changing, by the geometry modification module, stiffness by the calculated amount at the identified locations;

identifying again the frequency modes of the structure, including identifying the shifted frequency of the target frequency mode; and

recalculating the modal ratio as the quotient of the target frequency divided by the shifted frequency.

4. The method of claim 1 wherein:

the structure comprises one part of an apparatus comprising at least a second structure; and

selectively altering a target frequency mode a greater amount than the other frequency modes of the structure further comprises selectively altering the target frequency mode a greater amount than any frequency mode of the second structure.

5. The method of claim 1 wherein the finite element analysis module comprising a plug-in to a finite element analysis application.

6. An apparatus comprising a computer processor and a computer memory operatively coupled to the computer processor, the computer memory having disposed within it computer program instructions that, when executed by the computer processor, cause the apparatus to carry out the steps of:

identifying, by a finite element analysis module, a plurality of frequency modes of a structure; and

selectively altering a target frequency mode a greater amount than the other frequency modes of the structure, including modifying a local physical attribute of a portion of the structure associated with the target frequency mode without modifying the physical attribute over the entire structure comprising:

receiving, by the finite element analysis module, an identification of the target frequency mode;

identifying, by the finite element analysis module, a current frequency of the target frequency mode;

receiving, by the finite element analysis module, an identification of a preferred frequency of the target frequency mode;

calculating, by the finite element analysis module, a modal ratio as the quotient of the preferred frequency divided by the current frequency;

calculating, by the finite element analysis module, an amount of mass to change in dependence upon the modal ratio;

providing, by the finite element analysis module, to a geometry modification module, the calculated amount of mass to change;

identifying, by the finite element analysis module, one or more locations of the structure to change mass by the calculated amount, including identifying locations at which deflection is greater than a predefined threshold when operating at the target frequency mode;

providing, by the finite element analysis module, to the geometry modification module, the identified locations of the structure to change the mass by the calculated amount;

changing, by the geometry modification module, mass by the calculated amount at the identified locations;

identifying, by the finite element analysis module, again the frequency modes of the structure, including identifying a shifted frequency of the target frequency mode; and

recalculating, by the finite element analysis module, the modal ratio as the quotient of the target frequency divided by the shifted frequency.

7. The apparatus of claim 6 wherein modifying the local attribute of the portion of the structure associated with the target frequency mode without modifying the attribute over the entire structure is preformed, iteratively, until the modal ratio falls within a predefined range of values.

8. The apparatus of claim 6 wherein modifying the local physical attribute of the portion of the structure associated with the target frequency mode without modifying the physical attribute over the entire structure further comprises:

iteratively, until the modal ratio falls within the predefined range of values:

calculating an amount of stiffness to change in dependence upon the modal ratio;

providing, to the geometry modification module, the calculated amount of stiffness to change;

identifying one or more locations of the structure to change the stiffness by the calculated amount, including identifying locations at which strain is greater than a predefined threshold when operating at the target frequency mode;

providing, to the geometry modification module, the identified locations of the structure to change the stiffness by the calculated amount;

changing, by the geometry modification module, stiffness by the calculated amount at the identified locations;

identifying again the frequency modes of the structure, including identifying the shifted frequency of the target frequency mode; and

recalculating the modal ratio as the quotient of the target frequency divided by the shifted frequency.

9. The apparatus of claim 6 wherein:

the structure comprises one part of an apparatus comprising at least a second structure; and

selectively altering a target frequency mode a greater amount than the other frequency modes of the structure further comprises selectively altering the target frequency mode a greater amount than any frequency mode of the second structure.

10. The apparatus of claim 6 wherein the finite element analysis module comprising a plug-in to a finite element analysis application.

11. A computer program product including a non-transitory computer readable medium, the computer program product comprising computer program instructions that, when executed, cause a computer to carry out the steps of:

identifying, by a finite element analysis module, a plurality of frequency modes of a structure; and

selectively altering a target frequency mode a greater amount than the other frequency modes of the structure, including modifying a local physical attribute of a portion of the structure associated with the target frequency mode without modifying the physical attribute over the entire structure comprising:

receiving, by the finite element analysis module, an identification of the target frequency mode;

identifying, by the finite element analysis module, a current frequency of the target frequency mode;

receiving, by the finite element analysis module, an identification of a preferred frequency of the target frequency mode;

calculating, by the finite element analysis module, a modal ratio as the quotient of the preferred frequency divided by the current frequency;

calculating, by the finite element analysis module, an amount of mass to change in dependence upon the modal ratio;

providing, by the finite element analysis module, to a geometry modification module, the calculated amount of mass to change;

identifying, by the finite element analysis module, one or more locations of the structure to change mass by the calculated amount, including identifying locations at which deflection is greater than a predefined threshold when operating at the target frequency mode;

providing, by the finite element analysis module, to the geometry modification module, the identified locations of the structure to change the mass by the calculated amount;

changing, by the geometry modification module, mass by the calculated amount at the identified locations;

identifying, by the finite element analysis module, again the frequency modes of the structure, including identifying a shifted frequency of the target frequency mode; and

recalculating, by the finite element analysis module, the modal ratio as the quotient of the target frequency divided by the shifted frequency.

12. The computer program product of claim 11 wherein modifying the local attribute of the portion of the structure associated with the target frequency mode without modifying the physical attribute over the entire structure is preformed, iteratively, until the modal ratio falls within a predefined range of values.

13. The computer program product of claim 11 wherein modifying the local physical attribute of the portion of the structure associated with the target frequency mode without modifying the physical attribute over the entire structure further comprises:

iteratively, until the modal ratio falls within the predefined range of values:

calculating an amount of stiffness to change in dependence upon the modal ratio;

providing, to the geometry modification module, the calculated amount of stiffness to change;

identifying one or more locations of the structure to change the stiffness by the calculated amount, including identifying locations at which strain is greater than a predefined threshold when operating at the target frequency mode;

providing, to the geometry modification module, the identified locations of the structure to change the stiffness by the calculated amount;

changing, by the geometry modification module, stiffness by the calculated amount at the identified locations;

identifying again the frequency modes of the structure, including identifying the shifted frequency of the target frequency mode; and

recalculating the modal ratio as the quotient of the target frequency divided by the shifted frequency.

14. The computer program product of claim 11 wherein:

the structure comprises one part of an apparatus comprising at least a second structure; and

selectively altering a target frequency mode a greater amount than the other frequency modes of the structure further comprises selectively altering the target frequency mode a greater amount than any frequency mode of the second structure.

15. The computer program product of claim 11 wherein a finite element analysis module comprising a plug-in to the finite element analysis application.