IP Library Granted Patent US 10,605,089
Granted Patent B2
US 10,605,089 · App. 15/853,380 · Granted Mar 31, 2020

Blades and blade dampers for gas turbine engines

Inventor: Tracy A. Propheter-Hinckley (Manchester, CT)
Assignee: UNITED TECHNOLOGIES CORPORATION
F01D5/16F01D5/22F01D11/006F05D2250/75
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Quick Facts
Patent No.
US 10,605,089
App. No.
15/853,380
Granted
Mar 31, 2020
Kind
B2
Abstract

A blade damper for a gas turbine blade includes a blade damper body with a first damping surface and a second damping surface. The first damping surface is on a first side of the damper body and the second damping surface is on a second side of the damper body opposite the first damping surface for providing full functionality in both flipped and unflipped orientations.

Claims (26)

1. A blade damper, comprising:

a damper body having a first leg, a second leg disposed adjacent to the first leg, a third leg, and a fourth leg disposed adjacent to the third leg, and the first leg and the second leg are parallel with a longitudinal axis of the damper body and the third leg and the fourth leg are parallel with a lateral axis that is disposed transverse to the longitudinal axis,

wherein the damper body defines a first damping surface and a second damping surface on an opposite side of the damper body from the first damping surface,

wherein the first damping surface is identical to the second damping surface for providing full functionality when rotated 180 degrees about one of its longitudinal axis and latitudinal axis and rotated about its radial axis.

2. A damper as recited in claim 1 , wherein the second damping surface is identical to the first damping surface when the damper body is rotated 180 degrees about its lateral axis and rotated about its radial axis.

3. A damper as recited in claim 1 , wherein the second damping surface is identical to the first damping surface when the damper body is rotated 180 degrees about its longitudinal axis and rotated about its radial axis.

4. A damper as recited in claim 1 , wherein the damper body has two-fold rotational symmetry about a symmetry axis of the damper body.

5. A damper as recited in claim 4 , wherein the symmetry axis is a radial axis of the damper body.

6. A damper as recited in claim 4 , wherein the symmetry axis is a longitudinal axis of the damper body.

7. A damper as recited in claim 1 , wherein the damper body has a first and a second bearing lobe which define the first damping surface.

8. A damper as recited in claim 7 , wherein the damper body has a third and a fourth bearing lobe which define the second damping surface.

9. A damper as recited in claim 7 , wherein the first and second bearing lobes define a seal receptacle extending between adjacent sides of the bearing lobes.

10. A damper as recited in claim 9 , wherein the seal receptacle is a first seal receptacle, wherein the third and fourth bearing lobes define a second seal receptacle extending between adjacent sides of bearing lobes, and wherein the second seal receptacle is disposed transverse to the first seal receptacle.

11. A blade damper, comprising:

a damper body having a first lobe, a second lobe disposed adjacent to the first lobe, a third lobe, and a fourth lobe disposed adjacent to the third lobe, the first lobe and the second lobe are parallel with a longitudinal axis of the damper body and the third lobe and the fourth lobe are parallel with a lateral axis that is disposed transverse to the longitudinal axis,

wherein the first lobe and the second lobe define a first damping surface on the damper body and the third lobe and the fourth lobe define a second damping surface on an opposite side of the damper body from the first damping surface;

wherein the first damping surface is identical to the second damping surface for providing full functionality when rotated 180 degrees about one of its longitudinal axis and latitudinal axis and rotated about its radial axis.

12. A damper as recited in claim 11 , wherein the second damping surface is identical to the first damping surface when the damper body is rotated 180 degrees about its lateral axis and rotated about its radial axis.

13. A damper as recited in claim 11 , wherein the second damping surface is identical to the first damping surface when the damper body is rotated 180 degrees about its longitudinal axis and rotated about its radial axis.

14. A damper as recited in claim 11 , wherein the damper body has two-fold rotational symmetry about a symmetry axis of the damper body.

15. A damper as recited in claim 14 , wherein the symmetry axis is a radial axis of the damper body.

16. A damper as recited in claim 14 , wherein the symmetry axis is the longitudinal axis of the damper body.

17. A damper as recited in claim 11 , wherein the damper body has a first leg and a second leg that are parallel one another and parallel the longitudinal axis.

18. A damper as recited in claim 11 , wherein the damper body has a third and a fourth leg that are parallel one another and parallel the latitude axis.

19. A damper as recited in claim 11 , wherein the first and second bearing lobes define a seal receptacle extending between adjacent sides of the bearing lobes.

20. A damper as recited in claim 19 , wherein the seal receptacle is a first seal receptacle, wherein the third and fourth bearing lobes define a second seal receptacle extending between adjacent sides of bearing lobes, and wherein the second seal receptacle is disposed transverse to the first seal receptacle.

Assignments (5)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
SECURITY AGREEMENT Recorded Nov 21, 2022
From: MEVOTECH LP
To: NATIONAL BANK OF CANADA
Reel/Frame 061973/0256 →
CORRECTIVE ASSIGNMENT TO CORRECT THE AND REMOVE PATENT APPLICATION NUMBER 11886281 AND ADD PATENT APPLICATION NUMBER 14846874. TO CORRECT THE RECEIVING PARTY ADDRESS PREVIOUSLY RECORDED AT REEL: 054062 FRAME: 0001. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF ADDRESS. Recorded Mar 4, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 055659/0001 →
CHANGE OF NAME Recorded Sep 4, 2020
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 054062/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 22, 2017
From: PROPHETER-HINCKLEY, TRACY A.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 044474/0264 →