US4530861A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method and apparatus for masking a surface of a blade member
Assignee: General Electric Co
•
Filing: 1983-12-19
•
Granted: 1985-07-23
•
Expires: 2003-12-19
Abstract
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.
Inventors
- 👤 David F. Sippel
- 👤 Robert L. Kearns
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 04:28
CPC Classifications
B; B24; B24C; B24C1/00; B24C1/08; B24C1/086; B05; B05B; B05B12/00; B05B12/16; B05B12/20; B05D; B05D1/00; B05D1/32; B24C1/04
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
208 words
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.
Claim 2
Independent Claim
208 words
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.
Claim 3
Dependent Claim
19 words
The method of claim 1 in which the holding means and the mask member are made of resilient material.
Claim 4
Dependent Claim
163 words
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.
Claim 5
Dependent Claim
163 words
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.
Claim 6
Dependent Claim
21 words
The apparatus of claim 3 in which the airfoil holding means and the mask member are of a non-metallic, resilient material.
Claim 7
Dependent Claim
21 words
The apparatus of claim 4 in which the mask member includes a rigidizing bar to provide rigidity to the mask member.
Claim 8
Dependent Claim
36 words
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.
References Cited (Backward Citations)
US2979024A
Cited
US3226245A
Cited
US3141794A
Cited
US3482423A
Cited
US3708936A
Cited
US3951701A
Cited
US4334495A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1988-07-22 | 1989-01-21 | 1989-07-23 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-07-22 | 1993-01-21 | 1993-07-23 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-07-22 | 1997-01-21 | 1997-07-23 | $7700.00 | Window Closed / Lapsed |