Components resistant to traveling wave vibration and methods for manufacturing the same

Patent metadata

Field	Value
Publication number	US-9683447-B2
Application number	US-201414250681-A
Country	US
Kind code	B2
Filing date	Apr 11, 2014
Priority date	Apr 11, 2014
Publication date	Jun 20, 2017
Grant date	Jun 20, 2017

Abstract

Components resistant to traveling wave vibration and methods for manufacturing the same are provided. The component comprises a component body and a plurality of features disposed thereabout according to an asymmetry pattern that separates a pair of repeated eigenvalues associated with a targeted mode that deflects in excess of a threshold deflection limit in response to traveling wave excitation. The method comprises identifying, in a model of a rotationally periodic component, one or more modes thereof that deflect in excess of a threshold deflection limit in response to a traveling wave excitation. Each of the modes has a pair of repeated eigenvalues associated therewith. An asymmetry pattern is determined that separates each pair of repeated eigenvalues by a desired frequency split. A plurality of features are formed and disposed according to the asymmetry pattern about the component body defining an asymmetrical component comprising the component resistant to traveling wave vibration.

First claim

What is claimed is:

1. A method for manufacturing a component resistant to traveling wave vibration, the component comprising a component body having a front side and a back side and the method comprising the steps of:
identifying, in a model of a rotationally periodic component, one or more modes thereof that deflect in excess of a threshold deflection limit in response to a traveling wave excitation, each of the one or more modes having a pair of repeated eigenvalues associated therewith;
determining an asymmetry pattern that separates each pair of repeated eigenvalues by a desired frequency split; and
forming and disposing a plurality of features according to the asymmetry pattern about a circumference of the front side of the component body and about a circumference of the back side of the component body, the asymmetry pattern on the front side shifted circumferentially from the asymmetry pattern on the back side by an offset angle to define an asymmetrical component comprising the component resistant to traveling wave vibration.

2. The method of claim 1 , wherein the identifying step comprises vibration testing of the rotationally periodic component.

3. The method of claim 1 , wherein the determining step comprises analytically modeling the one or more modes.

4. The method of claim 1 , wherein the step of forming and disposing a plurality of features results in the asymmetry pattern about the front side being the same or different from the asymmetry pattern about the back side.

5. The method of claim 1 , wherein the forming and disposing step comprises at least one of adding or removing material from discrete regions of the component body.

6. The method of claim 5 , wherein the component comprises a disc for a turbomachine, the disc comprising:
the component body comprising a rotatable body having a rim disposed about a periphery thereof, wherein the disc comprises a bladed disc or an unbladed disc and the step of forming and disposing a plurality of features comprises at least one of adding or removing disc material from discrete regions of the disc.

7. A method for manufacturing a component resistant to traveling wave vibration, the component comprising a component body having a front side and a back side and the method comprising the steps of:
obtaining data relating to a vibration response of a model of a rotationally periodic component;
selecting one or more modes of the rotationally periodic component that exceed a threshold deflection limit;
analytically modeling the one or more modes with an analytical model, each of the one or more modes having a pair of repeated eigenvalues associated therewith;
determining an asymmetry pattern that separates each pair of repeated eigenvalues by a desired frequency split, wherein the step of determining the asymmetry pattern comprises:
applying a proposed asymmetry pattern to the analytical model;
analyzing the analytical model to determine if the proposed asymmetry pattern results in the desired frequency split for each pair of repeated eigenvalues associated with each of the one or more modes;
if the proposed asymmetry pattern does not result in the desired frequency split, repeating the applying and analyzing steps until the proposed asymmetry pattern results in the desired frequency split, the proposed asymmetry pattern resulting in the desired frequency split comprising the asymmetry pattern; and

at least one of adding or removing material according to the asymmetry pattern from a circumference of the front side of the component body and a circumference of the back side of the component body, the asymmetry pattern on the front side shifted circumferentially from the asymmetry pattern on the back side by an offset angle to define an asymmetrical component comprising the component resistant to traveling wave vibration.

8. The method of claim 7 , wherein the obtaining data step comprises obtaining data from vibration testing of the model of the rotationally periodic component.

9. The method of claim 7 , wherein the step of at least one of adding or removing material from the front side, the back side, or both the front and back sides of the component body result in the asymmetry pattern about the front side being the same or different from the asymmetry pattern about the back side.

10. The method of claim 7 , wherein the component comprises a disc for a turbomachine, the disc comprising:
the component body comprising a rotatable body having a rim disposed about a periphery thereof, wherein the disc comprises a bladed disc or an unbladed disc and the forming and disposing a plurality of features comprises at least one of adding or removing disc material from discrete regions of the disc.

11. A component resistant to traveling wave vibration, the component comprising:
a component body having a front side and a back side; and
a plurality of features arranged in a first asymmetric pattern about a circumference of the front side of the component body and arranged in a second asymmetric pattern about a circumference of the back side of the component body, the first asymmetric pattern shifted circumferentially from the second asymmetric pattern by an offset angle, with each of the plurality of features defined to separate each pair of repeated eigenvalues associated with a targeted mode, which deflects in excess of a threshold deflection limit in response to a traveling wave excitation.

12. The component of claim 11 , wherein the first asymmetry pattern on the front side is the same or different from the second asymmetry pattern on the back side.

13. The component of claim 11 , wherein a disc for a turbomachine comprises the component, the disc comprising:
the component body comprising a rotatable body having a rim disposed about a periphery of the rotatable body, wherein the disc comprises a bladed disc or an unbladed disc and the targeted mode comprises a nodal diameter mode.

14. The component of claim 13 , wherein the plurality of features are formed from disc material that is at least one of added to or removed from discrete regions of the disc.

15. The component of claim 13 , wherein the first asymmetry pattern comprises an asymmetric pattern of cuts or protrusions on the rim that define interrupted rim projections.

Assignees

• Honeywell Int Inc

Inventors

• Gentile David P
• Lentz Jeff
• Schroeder Gerhard

Classifications

• F05D2250/294

  grooved · CPC title

• F01D5/34

  Rotor-blade aggregates of unitary construction {, e.g. formed of sheet laminae; (discs formed of sheet laminae F01D5/028; ceramic materials F01D5/284, composite materials F01D5/282)} · CPC title

• F05D2260/961

  by mistuning rotor blades or stator vanes with irregular interblade spacing, airfoil shape · CPC title

• Y02T50/671

  Cross-Sectional Technologies · mapped topic

• F05D2230/10

  by removing material · CPC title