Mistuned rotor blade array for passive flutter control

• US 6,428,278 B1
• Filed: 12/04/2000
• Issued: 08/06/2002
• Est. Priority Date: 12/04/2000
• Status: Expired due to Term

• Current Assignee: Raytheon Technologies Corporation d/b/a RTX
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Srinivasan, Sriram, Byrne, W. Kerry, Block, Rachel J., Silkowski, Peter D., Montgomery, Matthew
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): NGUYEN, NINH H
• Application Number:
  US09/729,046
• Publication Number:
  US 20020067991A1
• Time in Patent Office: 610 Days
• Field of Search: 416/228, 416/234, 416/500, 416/203, 415/119
• US Class Current: 416/203
• CPC Class Codes: F01D 5/10 Anti- vibration means specially adapted for radial flow machines or engines F01D5/04
• CPC Class Codes: F01D 5/16 for counteracting blade vibration
• CPC Class Codes: F05D 2260/961 by mistuning rotor blades or stator vanes with irregular interblade spacing, airfoil shape
• CPC Class Codes: Y10S 416/50 Vibration damping features

Abstract

The present invention relates to an improved array of flow directing elements for incorporation in turbomachinery. In accordance with the present invention, an array of flow directing elements comprises a plurality of flow directing elements mounted to a rotor disk. The plurality of flow directing elements includes a first set of first flow directing elements whose natural vibration frequency has been modified by having material removed from a leading edge tip region and a second set of second flow directing elements whose natural vibration frequency has been modified by having material removed from a midspan leading edge region. The array may further comprise unmodified flow directing elements arranged with the modified flow directing elements.

Claims

1. An array of flow directing elements for use in turbomachinery comprising:

a plurality of flow directing elements mounted to a rotor disk;

said plurality of flow directing elements comprising a first set of first flow directing elements whose natural vibration frequency has been modified by having material removed from a leading edge tip region; and

said plurality of flow directing elements further comprising a second set of second flow directing elements whose natural vibration frequency has been modified by having material removed from a leading edge region substantially at a midspan point of the flow directing surface.

2. An array according to claim 1, wherein each of said first flow directing elements and each of said second flow directing elements are identical except for said regions where said materials has been removed.

3. An array of flow directing elements for use in turbomachinery comprising:

a plurality of flow directing elements mounted to a rotor disk;

said plurality of flow directing elements comprising a first set of first flow directing elements whose natural vibration frequency has been modified by having material removed from a leading edge tip region;

said plurality of flow directing elements further comprising a second set of second flow directing elements whose natural vibration frequency has been modified by having material removed from a midspan leading edge region; and

said first set of flow directing elements having frequencies of first bending, first torsion, and second bending vibration modes different from the first bending, first torsion, and second bending vibration mode frequencies of said second flow directing elements.

4. An array according to claim 3, further comprising said first and second sets of flow directing elements being arranged in an alternating pattern so that adjacent flow directing elements do not have the same vibration frequency.

5. An array according to claim 3, wherein said first and second flow directing elements are aligned in a row.

6. An array according to claim 3, wherein said array comprises a rotor blade assembly for an engine.

7. An array of flow directing elements for use in turbomachinery comprising:

a plurality of flow directing elements mounted to a rotor disk;

said plurality of flow directing elements comprising a first set of first flow directing elements whose natural vibration frequency has been modified by having material removed from a leading edge tip region;

said plurality of flow directing elements further comprising a second set of second flow directing elements whose natural vibration frequency has been modified by having material removed from a midspan leading edge region; and

third unmodified flow directing elements.

8. An array according to claim 7, wherein said flow directing elements are arranged in an alternating pattern of one of said first flow directing elements, one of said unmodified flow directing elements, and one of said second flow directing elements so that no adjacent flow directing elements have the same vibration frequency.

9. An array according to claim 7, wherein said flow directing elements are arranged in sequences of one of said first flow directing elements, one of said unmodified flow directing elements, one of said second flow directing elements, and one of said unmodified flow directing elements.

10. An array according to claim 7, wherein sufficient material is removed from each said first flow directing element so that the difference in first torsion frequency between an unmodified flow directing element and said first flow directing element exceeds 1.0% of the average first torsion frequency for the unmodified flow directing element.

11. An array according to claim 7, wherein sufficient material is removed from said second flow directing elements such that the difference in first torsion frequency between said unmodified flow directing element and said second flow directing element exceeds 1.0% of the average first torsion frequency of an unmodified flow directing element.

12. An array according to claim 7, wherein said first, second, and third flow directing elements are aligned in a row.