Method for manufacturing a blading member assembly, and blading member assembly

Patent metadata

Field	Value
Publication number	US-2016362984-A1
Application number	US-201615178645-A
Country	US
Kind code	A1
Filing date	Jun 10, 2016
Priority date	Jun 12, 2015
Publication date	Dec 15, 2016
Grant date	—

Abstract

Disclosed is a method for manufacturing a blading member assembly for a fluid flow machine, wherein the blading member assembly includes at least one airfoil member and one platform member. The method includes manufacturing a platform member blank, manufacturing an airfoil member blank, and processing at least one of said blanks thus obtaining the at least one airfoil member and at least one platform member, and subsequently joining the at least one platform member and the at least one airfoil member, thus providing the blading member assembly. The method, for instance, provides larger flexibility in arranging cooling openings.

First claim

1 . A method for manufacturing a blading member assembly for a fluid flow machine, wherein the blading member assembly includes at least one airfoil member and one platform member, the method comprising:
manufacturing a platform member blank, manufacturing an airfoil member blank, processing at least one of said blanks thus obtaining the at least one airfoil member and at least one platform member, and subsequently joining the at least one platform member and the at least one airfoil member, thus providing the blading member assembly.

2 . The method according to claim 1 , wherein processing a blank comprises:
applying at least one machining step.

3 . The method according to claim 1 , wherein machining comprises:
drilling.

4 . The method according to claim 1 , wherein drilling comprises:
drilling coolant ducts for a cooling opening.

5 . The method according to claim 2 , wherein machining comprises:
machining an outlet aperture of at least one cooling opening.

6 . The method according to claim 2 , wherein the blank includes an interface section which is configured to mate with an interface section of a further member when assembled, the method comprising:
machining the interface section.

7 . The method according to claim 1 , wherein the method comprises:
applying at least one of a milling or eroding step to the interface section.

8 . The method according to claim 1 , wherein processing a blank comprises:
applying at least one coating step to the blank.

9 . The method according to claim 8 , wherein the coating step comprises:
applying at least one of a protective coating and/or a thermal barrier coating.

10 . The method according to claim 8 , wherein the method comprises:
coating an airfoil member blank, wherein at least an airfoil member aerodynamic section is coated.

11 . The method according to claim 8 , wherein the method comprises:
coating a platform member blank, wherein at least a hot gas side surface of the platform member blank is coated.

12 . The method according to claim 8 , wherein applying the coating step comprises:
partially coating the blank while some sections of the blank are left uncoated.

13 . The method according to claim 1 , wherein the blank includes an interface section which is configured and adapted to mate with an interface section of a further member when assembled, and wherein the interface section is left uncoated.

14 . A blading member assembly for a fluid flow machine, the blading member assembly comprising:
at least one airfoil member and at least one platform member, at least one cooling opening being provided on one of the members, an outlet aperture of said cooling opening on the hot gas side defining an envelope, wherein said envelope when extrapolated on the hot gas side will interfere with at least one other member of the blading member assembly.

15 . A blading member assembly for a fluid flow machine, the blading member assembly comprising:
at least one airfoil member and at least one platform member, at least one cooling opening being provided in one of the members, said cooling opening including a coolant duct section having a straight axial extent, wherein an axis of said straight axial extent when extrapolated on the hot gas side interferes with at least one other member of the blading member assembly.

Assignees

• Ansaldo Energia Ip Uk Ltd

Inventors

• Brandl Herbert
• Benz Eribert
• Koehnke Rene
• Paralikas Ioannis

Classifications

• F05D2230/90

  Coating; Surface treatment · CPC title

• F01D5/288

  Protective coatings for blades · CPC title

• F05D2230/10

  by removing material · CPC title

• F01D5/186 Primary

  Film cooling (F01D5/187 takes precedence) · CPC title

• F05D2220/32

  in gas turbines · CPC title