Turbomachine rotor blade

Patent metadata

Field	Value
Publication number	US-10196907-B2
Application number	US-201314372841-A
Country	US
Kind code	B2
Filing date	Jan 16, 2013
Priority date	Jan 17, 2012
Publication date	Feb 5, 2019
Grant date	Feb 5, 2019

Abstract

A turbomachine rotor blade includes an outer part at its distal end. The outer part includes a platform defining an outside surface of a passage for gas passing through a turbomachine and presenting first and second opposite side edges; and upstream and downstream sealing wipers extending outwards from the platform, each wiper extending between two lateral faces situated respectively at the first and second side edges. The two lateral faces of the upstream or the downstream wiper are covered at least in part in an anti-wear material.

First claim

The invention claimed is:

1. A turbomachine rotor blade comprising:
an outer part at its distal end, the outer part including:
a platform defining an outside surface of a passage for gas passing through a turbomachine and presenting first and second opposite side edges; and
upstream and downstream sealing wipers extending outwards from said platform, each wiper extending between two lateral faces situated respectively at the first and second side edges, wherein

the two lateral faces of the upstream or the downstream wiper are covered, at least in part, in an anti-wear material, and wherein
at least one of the two lateral faces is covered in part in the anti-wear material, such that only an inner zone, in a radial direction, of said at least one of the two lateral faces is covered.

2. A blade according to claim 1 , wherein each of the first and second side edges presents a profile between the upstream and downstream wipers, which profile has a first portion close to the upstream wiper, a second portion that is an intermediate portion, and a third portion that is close to the downstream wiper, the first and third portions being substantially parallel to each other and the second portion extending obliquely between the first and third portions from upstream to downstream and from a suction side towards a pressure side of the blade.

3. A blade according to claim 2 , wherein each of the first and second side edges presents an upstream end portion in line with the first portion and a downstream end portion in line with the third portion.

4. A blade according to claim 2 , wherein the first and third portions extend substantially perpendicularly to the wipers.

5. A blade according to claim 2 , wherein the upstream wiper slopes upstream at a non-zero angle relative to the radial direction, each of the two lateral faces of the upstream wiper joining the side edge of the platform in the intermediate portion, and wherein the anti-wear material covers each of the two lateral faces of the upstream wiper, at least in part, and covers the intermediate portion of each side edge at least in part, such that the anti-wear material situated on the suction side of the blade is exposed downstream whereas the anti-wear material situated on the pressure side of the blade is exposed upstream.

6. A blade according to claim 1 , wherein one of the two lateral faces is completely covered in the anti-wear material.

7. A blade according to claim 1 , wherein the two lateral faces of the upstream wiper are covered in the anti-wear material.

8. A blade according to claim 1 , wherein the upstream and/or downstream wiper slopes upstream in an axial section plane at a non-zero angle relative to the radial direction.

9. A blade according to claim 1 , in which the upstream and/or downstream wiper extends substantially in the radial direction.

10. A blade according to claim 1 , wherein the anti-wear material extends heightwise from an inner face of the platform.

11. A blade according to claim 1 , wherein the two lateral faces of the upstream or the downstream wiper that are covered, at least in part, in the anti-wear material are inter-blade contact surfaces.

12. A blade according to claim 1 , wherein each of the first and second side edges presents a profile between the upstream and downstream wipers, which profile is generally U-shaped with a first portion close to the upstream wiper and forming a first branch of the U-shape, a second portion that is an intermediate portion and forming a base of the U-shape, and a third portion close to the downstream wiper and forming a second branch of the U-shape, the first and third portions diverging.

13. A blade according to claim 12 , wherein the second portion extends substantially perpendicularly to the wipers.

14. A blade according to claim 12 , wherein the third portion is at least twice as long as the first portion.

15. A turbomachine including a blade according to claim 1 .

16. A blade according to claim 1 , wherein each of the first and second side edges presents a profile between the upstream and downstream wipers, which profile has a first portion close to the upstream wiper, a second portion that is an intermediate portion, and a third portion that is close to the downstream wiper, the first and third portions being substantially parallel to each other and the second portion extending obliquely between the first and third portions from upstream to downstream and from a suction side towards a pressure side of the blade.

17. A blade according to claim 16 , wherein
the upstream wiper slopes upstream at a non-zero angle relative to the radial direction, each of the two lateral faces of the upstream wiper joining the side edge of the platform in the its intermediate portion, and wherein the anti-wear material covers the intermediate portion of each side edge at least in part, such that the anti-wear material situated on the suction side of the blade is exposed downstream whereas the anti-wear material situated on the pressure side of the blade is exposed upstream.

Assignees

• Safran Aircraft Engines

Inventors

• Bensalah Slim
• Negri Arnaud
• Digard Brou De Cuissart Sebastien
• Klein Guillaume
• Tang Ba-Phuc
• Mathieu David
• Doremus Sibylle

Classifications

• F01D5/288

  Protective coatings for blades · CPC title

• F01D5/225 Primary

  by shrouding · CPC title

• F01D5/30

  Fixing blades to rotors; Blade roots {; Blade spacers} · CPC title

• F01D5/28

  Selecting particular materials; {Particular measures relating thereto;} Measures against erosion or corrosion · CPC title

• Y02T50/673

  Cross-Sectional Technologies · mapped topic