← Back to Patent Explorer
US5026604A Expired / Lapsed US ⏱️ 0.0 years remaining

Composite material with refractory fibrous reinforcement and ceramic matrix

Assignee: Safran Aircraft Engines SAS
•
Filing: 1988-04-06
•
Granted: 1991-06-25
•
Expires: 2008-04-06
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A composite structure having a fibrous reinforcing body formed from fibers of a refractory material, a ceramic matrix surrounding the fibers of the reinforcing body and an intermediate layer of a refractory material having a laminar structure disposed between the fibers of the refractory material having a laminar structure disposed between the fibers of the refractory material and the ceramic matrix and adherent to both. The intermediate layer has a thickness sufficient to reduce the susceptibility of the structure to crack propagation and to increase impact strength but not exceeding 3.0 microns. The intermediate layer is also elastically deformable in shear and has an elongation at break greater than the matrix.

Inventors

  • 👤 Jacques Thebault

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-07 12:11
CPC Classifications
C; C04; C04B; C04B35/00; C04B35/71; C04B35/78; C04B35/80; C04B35/01; C04B35/10; C04B35/111; C04B35/117; C04B35/515; C04B35/56; C04B35/565; C04B35/571; C04B35/622; C04B35/624; C04B35/626; C04B35/628; C04B35/62844; C04B35/62857; C04B35/6286; C04B35/62863; C04B35/62865; C04B35/62868; C04B35/62884; C04B35/62897; C04B2235/00; C04B2235/02; C04B2235/30; C04B2235/32; C04B2235/3217; C04B2235/44; C04B2235/441; C04B2235/50; C04B2235/52; C04B2235/5208; C04B2235/5216; C04B2235/524; C04B2235/5244; C04B2235/5248; C04B2235/60; C04B2235/614; C04B2235/616; C04B2235/70; C04B2235/95; C04B2235/96; C04B2235/9669; C04B2235/9684; Y; Y10; Y10S; Y10S428/00; Y10S428/902; Y10S428/903; Y10T; Y10T428/00; Y10T428/29; Y10T428/2913; Y10T428/2918; Y10T428/292; Y10T428/2933; Y10T428/2938; Y10T428/294; Y10T428/2956

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 98 words
A composite structure comprising (a) a fibrous reinforcing body formed from fibers of a refractory material; (b) a ceramic matrix surrounding the fibers of the reinforcing body; and (c) an intermediate layer of a refractory material having a laminar structure disposed between the fibers of the refractory material and the ceramic matrix and adherent to both, wherein said intermediate layer has a thickness sufficient to reduce the susceptibility of the structure to crack propagation and to increase impact strength not exceeding 3.0 microns is elastically deformable in shear and has an elongation at break greater than the matrix.
Claim 2
Dependent Claim 98 words
A composite structure comprising (a) a fibrous reinforcing body formed from fibers of a refractory material; (b) a ceramic matrix surrounding the fibers of the reinforcing body; and (c) an intermediate layer of a refractory material having a laminar structure disposed between the fibers of the refractory material and the ceramic matrix and adherent to both, wherein said intermediate layer has a thickness sufficient to reduce the susceptibility of the structure to crack propagation and to increase impact strength not exceeding 3.0 microns is elastically deformable in shear and has an elongation at break greater than the matrix.
Claim 3
Dependent Claim 19 words
A structure according to claim 1, wherein the intermediate layer has a thickness of from 0.2 to 3 microns.
Claim 4
Dependent Claim 16 words
A structure according to claim 1, wherein the intermediate layer consists essentially of laminar pyrolytic carbon.
Claim 5
Dependent Claim 15 words
A structure according to claim 1, wherein the intermediate layer consists essentially of boron nitride.
Claim 6
Dependent Claim 15 words
A structure according to claim 1, wherein the reinforcing body is formed from carbon fibers.
Claim 7
Dependent Claim 16 words
A structure according to claim 1, wherein the reinforcing body is formed from silicon carbide fibers.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1994-06-24 1994-12-24 1995-06-25 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1998-06-24 1998-12-24 1999-06-25 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2002-06-24 2002-12-24 2003-06-25 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag