IP Library Granted Patent US 7,153,543
Granted Patent B2
US 7,153,543 · App. 10/153,991 · Granted Dec 26, 2006

Refractory-carbon composite brake friction elements

Assignee: Dunlop Aerospace Limited
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Quick Facts
Patent No.
US 7,153,543
App. No.
10/153,991
Granted
Dec 26, 2006
Kind
B2
Abstract

Refractory carbide particles are located in a defined area of a matrix, specifically silicon carbide particles are encapsulated within a porous matrix or carbon precursor, by locating particles of refractory carbide-forming material or a precursor thereof in a defined area of the matrix followed by depositing carbon within the matrix at a temperature below that of the melting point of the carbide-forming material.

Claims (22)

1. A method of forming a rotor disc for a brake assembly, drive slots being present around the outer periphery thereof, the method comprising the sequential steps of:

a) providing a porous matrix of carbon or a carbon precursor material, the matrix comprising a laminate of two or more layers of the material, each layer having particles of a refractory carbide-forming material or a precursor thereof in an inner region only;

b) depositing carbon within the matrix at an elevated temperature which is kept below the melting point of the carbide-forming material to form a distribution of carbide encapsulated material only in the inner region, said inner region constituting a wear-resistant region of the rotor disc; and

c) machining the outer periphery to form the drive slots, said outer periphery that is machined being free of carbide to render said outer periphery readily machinable.

2. A method according to claim 1 , wherein the deposition in step b) is a chemical vapor infiltration (CVI) process.

3. A method according to claim 1 , wherein the matrix comprises carbon fibre or a precursor thereof.

4. A method according to claim 1 , wherein the refractory carbide forming material is boron or silicon or a precursor thereof.

5. A method of forming a stator disc for a brake assembly, drive slots being present around the inner periphery thereof, the method comprising the sequential steps of:

a) providing a porous matrix of carbon or a carbon precursor material, the matrix comprising a laminate of two or more layers of the material, each layer having particles of a refractory carbide-forming material or a precursor thereof in an outer region only;

b) depositing carbon within the matrix at an elevated temperature which is kept below the melting point of the carbide-forming material to form a distribution of carbide encapsulated material only in the outer region, said outer region constitution a wear-resistant region of the stator disc; and

c) machining the inner periphery to form the drive slots, said inner periphery that is machined being free of carbide to render said inner periphery readily machinable.

6. A method according to claim 5 , wherein the deposition in step b) is a chemical vapor infiltration (CVI) process.

7. A method according to claim 5 , wherein the matrix comprises carbon fibre or a precursor thereof.

8. A method according to claim 5 , wherein the refractory carbide forming material is boron or silicon or a precursor thereof.

9. A method of forming a rotor disc for a brake assembly, drive slots being present around the outer periphery thereof, the method comprising the sequential steps of:

a) providing a porous matrix of carbon or a carbon precursor material, the matrix comprising a laminate of two or more layers of the material, each layer having particles of a refractory carbide-forming material or a precursor thereof in an inner region only;

b) depositing carbon within the matrix at an elevated reaction temperature which is kept below the melting point of the carbide-forming material whereby the carbide-forming material is converted in the solid state to the carbide with the matrix only in the inner region, said inner region constituting a wear-resistant region of the rotor disc; and

c) machining the outer periphery to form the drive slots, said outer periphery that is machined being free of carbide, to render said outer periphery readily machinable.

10. A method of forming a stator disc for a brake assembly, drive slots being present around the inner periphery thereof, the method comprising the sequential steps of:

a) providing a porous matrix of carbon or a carbon precursor material, the matrix comprising a laminate of two or more layers of the material, each layer having particles of a refractory carbide-forming material or a precursor thereof in an outer region only;

b) depositing carbon within the matrix at an elevated reaction temperature which is kept below the melting point of the carbide-forming material whereby the carbide-forming material is converted in the solid state to the carbide with the matrix only in the outer region, said outer region constituting a wear-resistant region of the rotor disc; and

c) machining the inner periphery to form the drive slots, said inner periphery that is machined being free of carbide, to render said inner periphery readily machinable.

Assignments (3)
CORRECTIVE NAME CHANGE. THE NAME CHANGE (PREVIOUSLY RECORDED AT REEL/FRAME 020794/0906 ON APRIL 15, 2008) USED AN INCORRECT EXECUTION DATE OF DECEMBER 9, 1997. THE CORRECT EXECUTION DATE SHOULD BE JANUARY 4, 2008. Recorded Nov 24, 2008
From: DUNLOP AEROSPACE LIMITED
To: MEGGITT AEROSPACE LIMITED
Reel/Frame 021876/0456 →
CHANGE OF NAME Recorded Apr 15, 2008
From: DUNLOP AEROSPACE LIMITED
To: MEGGITT AEROSPACE LIMITED
Reel/Frame 020794/0906 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 16, 2002
From: JOHNSON, DAVID CALLUM
To: DUNLOP AEROSPACE LIMITED
Reel/Frame 013096/0382 →
Priority Claims (1)
GB 0112893.3 · May 25, 2001 · national
Continuity (1)
Related Publication 20020176990A1 · Nov 28, 2002