Hollow titanium airfoil with titanium coating

Patent metadata

Field	Value
Publication number	US-10830064-B2
Application number	US-201715620059-A
Country	US
Kind code	B2
Filing date	Jun 12, 2017
Priority date	Jun 12, 2017
Publication date	Nov 10, 2020
Grant date	Nov 10, 2020

Abstract

An airfoil surface includes a first titanium portion, a second titanium portion, an aluminum alloy braze disposed there between, and a titanium coating covering the aluminum alloy braze, at least part of the first titanium portion and at least part of the second titanium portion.

First claim

What is claimed is:

1. An airfoil surface comprising a first titanium portion, a second titanium portion, an aluminum alloy braze disposed there between, and a titanium coating disposed on and covering the aluminum alloy braze, at least part of the first titanium portion and at least part of the second titanium portion.

2. The airfoil surface of claim 1 , wherein the first and second titanium portions are secured to one another with the aluminum alloy braze.

3. The airfoil surface of claim 1 , wherein the first titanium portion includes machined ribs.

4. The airfoil surface of claim 1 , wherein the machined ribs include undercuts that have an arcuate shape.

5. The airfoil surface of claim 1 , wherein the second titanium portion is a hot-formed sheet that provides a cover and the cover provides one side of the airfoil.

6. The airfoil surface of claim 1 , wherein the airfoil has a root and a tip defined by the first titanium portion.

7. The airfoil surface of claim 1 , wherein the titanium coating has a thickness of 0.0005 inches to 0.0015 inches (0.0127 millimeters to 0.0381 millimeters).

8. The airfoil surface of claim 1 , wherein the titanium coating comprises titanium, a titanium alloy, or a combination thereof.

9. The airfoil surface of claim 1 , wherein the titanium coating covers substantially all of the surface of the second titanium portion and at least part of the surface of the first titanium portion.

10. A method of manufacturing an airfoil comprising providing first and second titanium portions, applying an aluminum alloy braze to at least one of the first and second titanium portions, heating the airfoil to melt the aluminum alloy braze and join the first and second portions to one another to provide an airfoil surface with an aluminum alloy braze joint; and providing a titanium coating to the airfoil surface, wherein the titanium coating is disposed on and covers the aluminum alloy braze joint, at least part of the first titanium portion, and at least part of the second titanium portion.

11. The method of claim 10 , wherein the method further comprises machining the first titanium portion.

12. The method of claim 10 , wherein the method further comprises applying the aluminum alloy braze before the machining step.

13. The method of claim 10 , wherein the method further comprises pressing the second titanium portion to produce a cover that provides a side of the airfoil.

14. The method of claim 10 , wherein the method further comprises pickling or laser cleaning the first titanium portion, the second titanium portion or both.

15. The method of claim 14 , wherein the method comprises applying the aluminum alloy braze after pickling or laser cleaning.

16. The method of claim 10 , wherein the method further comprises bagging the first and second titanium portions prior to performing the heating step.

17. The method of claim 10 , wherein the method further comprises providing the titanium coating by cathodic arc deposition.

18. The method of claim 10 , wherein the titanium coating has a thickness of 0.0005 inches to 0.007 inches (0.0127 millimeters to 0.1778 millimeters).

19. The method of claim 10 , wherein the titanium coating comprises titanium, titanium alloy, or a combination thereof.

20. The airfoil surface of claim 1 , wherein the aluminum alloy braze is an Al—Cu—Mn alloy.

Assignees

• United Technologies Corp
• Raytheon Tech Corp

Inventors

• Dolan Robert C

Classifications

• F01D5/147

  Construction, i.e. structural features, e.g. of weight-saving hollow blades (F01D5/148, F01D5/16 and F01D5/20 take precedence; blade shape F01D5/141; blades with cooling or heating channels or cavities F01D5/18; heating, heat-insulating or cooling means on blades F01D5/18) · CPC title

• F05D2300/121

  Aluminium · CPC title

• C22C14/00

  Alloys based on titanium · CPC title

• B32B15/013

  one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium · CPC title

• B23P15/04

  turbine or like blades from several pieces · CPC title