Method of manufacturing a fibre reinforced metal matrix composite article

• US 8,647,453 B2
• Filed: 08/02/2011
• Issued: 02/11/2014
• Est. Priority Date: 08/11/2010
• Status: Active Grant

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Doorbar, Philip J
• Primary Examiner(s): Heinrich, Samuel M
• Application Number:
  US13/196,397
• Publication Number:
  US 20120037602A1
• Time in Patent Office: 924 Days
• Field of Search: 298/892, 298/897, 298/897.1, 156/73.1, 228/110.1, 228/111, 228/175, 228/176, 228/193, 228/903, 219/121.12, 219/121.13, 219/121.14, 219/121.63, 219/121.64, 264/442
• US Class Current: 156/73.1
• CPC Class Codes: B22F 2201/01 Reducing atmosphere
• CPC Class Codes: B22F 2999/00 Aspects linked to processes or compositions used in powder metallurgy
• CPC Class Codes: B22F 5/009 of turbine components other than turbine blades of turbine blades B22F5/04
• CPC Class Codes: B23K 20/021 Isostatic pressure welding
• CPC Class Codes: B23K 20/10 making use of vibrations, e.g. ultrasonic welding
• CPC Class Codes: B23K 2101/001 Turbines
• CPC Class Codes: C22C 47/04 by coating, e.g. with a protective or activated covering
• CPC Class Codes: C22C 47/06 by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element
• CPC Class Codes: C22C 47/064 Winding wires
• CPC Class Codes: Y10T 29/49337 Composite blade

Abstract

A method of manufacturing a fiber reinforced metal matrix composite article, the method comprises forming a first metal component, forming a second metal component and forming at least one fiber preform comprising at least one metal coated fiber. The metal at least one first portion of the at least one metal coated fiber of the at least one fiber preform is bonded to the metal at least one second portion of the at least one metal coated fiber of the at least one fiber preform to hold the at least one fiber in position. The at least one fiber preform is placed between the first metal component and the second metal component. The second metal component is sealed to the first metal component, and heat and pressure is applied such as to consolidate the at least one fiber preform and to diffusion bond the metal on the fiber of the at least one fiber preform, the first metal component and the second metal component to form a unitary composite article. The bonding comprises ultrasonic welding.

Claims

1. A method of manufacturing a fibre reinforced metal matrix composite article, the method comprising the steps of:

(a) forming a first metal component,

(b) forming a second metal component,

(c) forming at least one fibre preform, the at least one fibre preform comprising at least one metal coated fibre,

(d) bonding the metal at least one first portion of the at least one metal coated fibre of the at least one fibre preform to the metal at least one second portion of the at least one metal coated fibre of the at least one fibre preform to hold the at least one fibre in position, wherein the bonding comprises ultrasonic welding,

(e) placing the at least one fibre preform between the first metal component and the second metal component,

(f) sealing the second metal component to the first metal component, and

(g) applying heat and pressure such as to consolidate the at least one fibre preform and to diffusion bond the metal on the fibre of the at least one fibre preform, the first metal component and the second metal component to form a unitary composite article.

2. A method as claimed in claim 1 wherein step (d) comprises bonding the metal at a plurality of first portions of the at least one metal coated fibre of the at least one fibre preform to the metal at a plurality of second portions of the at least one metal coated fibre of the at least one fibre preform to hold the at least one fibre in position.

3. A method as claimed in claim 1 wherein step (d) comprises local ultrasonic welding to directly bond the metal at the least one first portion to the metal at the at least one second portion.

4. A method as claimed in claim 1 wherein step (d) comprises providing a metal member and bonding the metal at least one first portion of the at least one metal coated fibre of the at least one fibre preform to the metal member and bonding the metal at least one second portion of the at least one metal coated fibre of the at least one fibre preform to the metal member to hold the at least one fibre in position.

5. A method as claimed in claim 4 wherein the metal member is selected from a group comprising a metal wire and a metal foil.

6. A method as claimed in claim 4 wherein step (d) comprises wrapping the metal member around the at least one metal coated fibre.

7. A method as claimed in claim 1 wherein (d) comprises ultrasonic welding the metal of the at least one metal coated fibre of the least one fibre preform to the metal coated fibre of the at least one fibre preform in a line weld.

8. A method as claimed in claim 1 wherein step (c) comprises winding the at least one metal coated fibre in a spiral.

9. A method as claimed in claim 8 wherein step (c) comprises winding the at least one metal coated fibre such that the metal on adjacent turns of the metal coated fibre abut each other.

10. A method as claimed in claim 8 wherein step (c) comprises winding the at least one metal coated fibre such that there is a space between the metal on is adjacent turns of the metal coated fibre.

11. A method as claimed in claim 8 wherein step (c) comprises winding at least one metal wire with the at least one metal coated fibre in a spiral.

12. A method as claimed in claim 1 wherein step (c) comprises arranging a plurality of metal coated fibres in a plane with the metal coated fibres extending in a single direction.

13. A method as claimed in claim 1 wherein the at least one fibre is selected from a group comprising a silicon carbide fibre, a silicon nitride fibre, a boron fibre, a carbon fibre, a tungsten fibre and an alumina fibre.

14. A method as claimed in claim 1 wherein the at least one metal coated fibre is selected from a group comprising a titanium coated fibre, a titanium alloy coated fibre and a titanium aluminide coated fibre.

15. A method as claimed in claim 1 wherein the first metal component is selected from a group comprising titanium, titanium alloy and titanium aluminide.

16. A method as claimed in claim 1 wherein step (a) comprises forming a groove in the first metal component, step (e) comprises placing the at least one fibre preform in the groove of the first metal component and placing the second metal component in the groove of the metal component.

17. A method as claimed in claim 16 wherein step (b) comprises forming a projection on the second metal component and step (e) comprises placing the projection of the second metal component in the groove of the first metal component.

18. A method as claimed in claim 17 wherein step (a) comprises forming a circumferentially and axially extending groove in an end face of the first metal component, step (b) comprises forming a circumferentially and axially extending projection on an end face of the second metal component, step (c) comprises winding at least one metal coated fibre on a former to form the fibre preform, step (e) comprises placing the fibre preform in the circumferentially extending groove of the first metal component and placing the second metal component in the groove of the first metal component.

19. A method as claimed in claim 1 wherein the fibre reinforced metal matrix composite article is selected from a group comprising a rotor, a shaft and a stator.

20. A method as claimed in claim 19 wherein the fibre reinforced metal matrix composite article comprises a rotor with integral rotor blades.

21. A method as claimed in claim 19 wherein the fibre reinforced metal matrix composite article is selected from a group comprising a gas turbine engine rotor, a gas turbine engine shaft and a gas turbine engine stator.

22. A method as claimed in 19 wherein the fibre reinforced metal matrix composite article is selected from a group comprising an electrical machine rotor, an electrical machine shaft and an electrical machine stator.

23. A method of manufacturing a fibre reinforced metal matrix composite article, the method comprising the steps of:

(a) forming a first metal component,

(b) forming a second metal component,

(c) forming at least one fibre preform, the at least one fibre preform comprising at least one metal coated fibre,

(d) bonding the metal at least one first portion of the at least one metal coated fibre of the at least one fibre preform to the metal at least one second portion of the at least one metal coated fibre of the at least one fibre preform to hold the at least one fibre in position, wherein the bonding comprises electron beam welding,

(e) placing the at least one fibre preform between the first metal component and the second metal component,

(f) sealing the second metal component to the first metal component, and

(g) applying heat and pressure such as to consolidate the at least one fibre preform and to diffusion bond the metal on the fibre of the at least one fibre preform, the first metal component and the second metal component to form a unitary composite article.

24. A method as claimed in claim 23 wherein step (d) comprises local electron beam welding to directly bond the metal at the least one first portion to the metal at the at least one second portion.

25. A method as claimed in claim 23 wherein step (d) comprises providing a metal member and bonding the metal at least one first portion of the at least one metal coated fibre of the at least one fibre preform to the metal member and bonding the metal at least one second portion of the at least one metal coated fibre of the at least one fibre preform to the metal member to hold the at least one fibre in position.