Hollow component manufacture

Patent metadata

Field	Value
Publication number	US-9694438-B2
Application number	US-201414509338-A
Country	US
Kind code	B2
Filing date	Oct 8, 2014
Priority date	Oct 21, 2013
Publication date	Jul 4, 2017
Grant date	Jul 4, 2017

Abstract

A method of manufacturing a hollow component, such as a fan blade for a gas turbine engine, includes the steps of: (a) providing first and second panels and a membrane; (b) providing a stop-off material on at least one of the first and second panels and the membrane to define regions where no diffusion bonding is to take place; (c) assembling the panels and the membrane together so the membrane is between the panels; (d) diffusion bonding the panels and the membrane together. The method is such that when assembled in step (c) the membrane does not extend to at least one edge of the first and second panels, so that in that region the first and second panels are diffusion bonded directly to each other.

First claim

The invention claimed is:

1. A method of manufacturing a hollow component comprising the steps of:
(a) providing first and second panels and a membrane;
(b) providing a stop-off material on at least one surface to define regions where no diffusion bonding is to take place;
(c) assembling the panels and the membrane together so the membrane is between the panels and extends beyond a boundary of an internal cavity so that a portion of the membrane is bonded between the panels, but the membrane does not extend to an edge of the panels; and
(d) diffusion bonding the panels and the membrane together;
wherein in a region of the edge of the panels, the first and second panels are diffusion bonded directly to each other.

2. The method of claim 1 , in which the component is a fan blade for a gas turbine engine.

3. The method of claim 1 , in which the first and second panels each have a leading edge, a trailing edge, a tip and a root, and the membrane does not extend to at least one of the leading edge, the trailing edge, the tip and the root.

4. The method of claim 1 , in which at least one of the first and second panels and the membrane has a locating feature so that in step (d) the position of the membrane is correct with respect to the first and second panels.

5. The method of claim 4 , in which the locating feature is a recess.

6. The method of claim 4 , in which the locating feature is configured to ensure that the orientation of the membrane is correct with respect to the first and second panels.

7. A hollow component formed by the method of claim 1 .

8. A hollow component formed by a diffusion bonding process, the component formed from first and second panels with a membrane between them, at least one of the first and second panels and the membrane having a stop-off material applied to it to define regions where no diffusion bonding is to take place, wherein the membrane extends beyond a boundary of an internal cavity so that a portion of the membrane is bonded between the panels, but the membrane does not extend to an edge of the panels, and in the diffusion bonding process the first and second panels are diffusion bonded directly to each other in the region of the edge of the panels.

9. The component of claim 8 , the component being a fan blade for a gas turbine engine.

10. The component of claim 8 , in which the first and second panels each have a leading edge, a trailing edge, a tip and a root, and the membrane does not extend to at least one of the leading edge, the trailing edge, the tip and the root.

11. The component of claim 8 , in which at least one of the first and second panels and the membrane has a locating feature so that the position of the membrane is correct with respect to the first and second panels.

12. The component of claim 11 , in which the locating feature is a recess.

13. The component of claim 11 , in which the locating feature is configured to ensure that the orientation of the membrane is correct with respect to the first and second panels.

Assignees

• Rolls Royce Plc

Inventors

• Andrews Ian John
• Wallis Michael James
• Fearn Ian

Classifications

• B21D26/055 Primary

  Blanks having super-plastic properties · CPC title

• Y10T428/12486

  Laterally noncoextensive components [e.g., embedded, etc.] · CPC title

• B21D53/78

  propeller blades; turbine blades · CPC title

• F05D2230/236

  Diffusion bonding · CPC title

• Y10T428/12389

  having variation in thickness · CPC title