Method and apparatus for masking a surface of a blade member

• US 4,530,861 A
• Filed: 12/19/1983
• Issued: 07/23/1985
• Est. Priority Date: 12/19/1983
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Kearns, Robert L., Sippel, David F.
• Primary Examiner(s): Lawrence, Evan K.
• Application Number:
  US06/562,940
• Time in Patent Office: 582 Days
• Field of Search: 118/504, 118/505, 118/213, 118/301, 118/406, 118/503, 427/282, 427/444, 427/300, 51/310-312, 51/274, 29/156.8 B, 29/23.5
• US Class Current: 427/444
• CPC Class Codes: B05B 12/20 Masking elements, i.e. elements defining uncoated areas on an object to be coated
• CPC Class Codes: B05D 1/32 using means for protecting parts of a surface not to be coated, e.g. using stencils, resists
• CPC Class Codes: B24C 1/04 for treating only selected parts of a surface, e.g. for carving stone or glass
• CPC Class Codes: B24C 1/086 Descaling; Removing coating films

Abstract

A method and apparatus for masking from treatment selected surfaces of a turbine blade. The blade is positioned in an apparatus which includes a holder enclosing the airfoil section of the blade and a distinct spaced apart mask member elastically secured to the holder and having a deformable surface covering a surface of the blade spaced from the airfoil.

Claims

1. A method for masking portions of a member, wherein said member is a metallic blade comprising a first portion having a base, a platform first surface facing the base, and a shank therebetween, and a second portion having an airfoil connected to a platform second surface facing the airfoil, the base having a surface selected to be masked from treatment and including a port therein, the selected surface being spaced from the second portion, the method for masking the selected surface of the base, the airfoil and the second platform surface comprising the steps of:

disposing the airfoil in a holding means through an opening in the holding means shaped to releasably enclose the periphery of the airfoil;

providing a substantially rigid mask member which is distinct from the holding means and which includes an elastically deformable mask surface having a positioning protrusion for insertion into the port, the mask surface being contoured substantially to the selected base surface;

covering the base surface with the mask surface, with the protrusion within the port; and

then,

securing the mask member at the base surface elastically with an elastic means between the mask member and the holding means, the elastic means pressing the platform second surface against the holding means.

2. The method of claim 1 in which the holding means and the mask member are made of resilient material.

3. Masking apparatus for use with a turbine engine blade member which includes a first portion to be treated comprised of a base having a base surface selected to be masked from treatment and including a port therein, a platform having a first surface facing the base, and a shank therebetween, the blade member also including a second portion comprising an airfoil extending from the platform at a second platform surface facing the airfoil, the selected surface being spaced from the second portion, the masking apparatus comprising:

an airfoil holding means including an opening therein shaped to the contour of the air foil of the blade member to releasably hold and enclose the airfoil portion;

a substantially rigid mask member distinct from the airfoil holding means and including an elastically deformable mask surface having a positioning protrusion for insertion into the port and contoured substantially to the selected base surface; and

elastic strap means secured between the mask member and the airfoil holding means.

4. The apparatus of claim 3 in which the airfoil holding means and the mask member are of a non-metallic, resilient material.

5. The apparatus of claim 4 in which the mask member includes a rigidizing bar to provide rigidity to the mask member.

6. The apparatus of claim 3 in which the airfoil holding means includes a locating surface adapted to cooperate with the second platform surface to control relative positioning of the blading member and the airfoil holding means.