IP Library Granted Patent US 6,939,104
Granted Patent B2
US 6,939,104 · App. 10/479,180 · Granted Sep 6, 2005

Turbine blade with sealing element

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Quick Facts
Patent No.
US 6,939,104
App. No.
10/479,180
Granted
Sep 6, 2005
Kind
B2
Abstract

A turbine blade including a head at its peripherally outer end, and on the outside face thereof at least one wiper is formed having a first end portion and a second end portion, with a wiper tip extending between the two end portions. The first portion situated on the suction side of the blade is taller than the second end portion to form a sawtooth effect between the wipers of two adjacent blades mounted on a turbine rotor. The tip of each wiper presents a convex surface between the first portion and the second portion.

Claims (28)

1. A blade for a turbine, the blade having a pressure side and a suction side disposed on either side of an axis of the blade, the blade comprising:

a head situated at a peripherally outer end of the blade; and

at least one sealing wiper formed on the head, said sealing wiper disposed transversely to the pressure and suction sides and presenting a first end portion at the suction side and a second end portion at the pressure side, said first end portion being taller than said second end portion, said sealing wiper presenting a wiper tip between said first and second end portions,

wherein the wiper tip presents a convex surface that extends between said first and second end portions.

2. A blade according to claim 1 , wherein said convex surface presents a circular cross-section having a middle axis, a center, and a radius.

3. A blade according to claim 2 , wherein said middle axis is offset from the blade axis by an angle oriented from the pressure side towards the suction side, and wherein the center is offset by a distance measured perpendicularly to the blade axis.

4. A blade according to claim 3 , wherein the distance is not less than half of one pitch step corresponding to half a spacing between said first end portion and said second end portion.

5. A blade according to claim 1 , wherein a difference in height between said first end portion and said second end portion is at least 0.2 mm.

6. A blade according to claim 1 , wherein the blade carries two wipers.

7. A blade according to claim 6 , wherein the two wipers are substantially parallel.

8. A blade according to claim 6 , wherein said two wipers are disposed in parallel planes perpendicular to an axis of rotation of the blade.

9. A blade according to claim 1 , wherein said convex surface extends continuously from said first end portion to said second end portion.

10. A blade for a turbine, said blade having a pressure side and a suction side, said blade comprising:

at least one wiper with a first end portion at the suction side and a second end portion at the pressure side, said first end portion being higher than said second end portion, said wiper having a wiper tip between said first and second end portions,

wherein the wiper tip has a convex surface that extends between said first and second end portions.

11. A blade according to claim 10 , wherein said wiper is disposed transversely relative to the pressure and suction sides.

12. A turbine comprising:

a stator;

a rotor in said stator, said rotor comprising a plurality of blades, each blade being configured according to claim 11 .

13. A blade according to claim 11 , wherein said convex surface presents a circular cross-section having a middle axis, a center, and a radius.

14. A blade according to claim 13 , wherein said middle axis is offset from a blade axis by an angle oriented from the pressure side towards the suction side, and wherein the center is offset by a distance measured perpendicularly to the blade axis.

15. A blade according to claim 14 , wherein the distance is not less than half of one pitch step corresponding to half a spacing between said first end portion and said second end portion.

16. A blade according to claim 11 , wherein a difference in height between said first end portion and said second end portion is at least 0.2 mm.

17. A turbine according to claim 12 , wherein each blade carries two wipers.

18. A turbine according to claim 17 , wherein the two wipers are substantially parallel.

19. A turbine according to claim 18 , wherein said two wipers are disposed in parallel planes perpendicular to an axis of rotation of the rotor.

20. A turbine according to claim 17 , wherein said two wipers are disposed to form a baffle with an inside wall of said stator.

21. A blade according to claim 11 , wherein said convex surface extends continuously from said first end portion to said second end portion.

Assignments (4)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
CHANGE OF NAME Recorded Feb 20, 2008
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 020609/0569 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 29, 2004
From: GIOT, CHANTAL; SOUPIZON, JEAN-LUC
To: SNECMA MOTEURS
Reel/Frame 015150/0161 →