Patent US4092293A successfully refreshed from Google Patents.
Patent US1936451A successfully refreshed from Google Patents.
Patent US4863798A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4863798A Expired / Lapsed US ⏱️ 0.0 years remaining

Refractory composite material and method of making such material

Assignee: 3M Co
•
Filing: 1988-07-21
•
Granted: 1989-09-05
•
Expires: 2008-07-21
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A porous substrate is formed from discrete elements preferably anisotropic and permeable to oxygen and preferably having a first coefficient of thermal expansion. A pyrolytic material permeable to oxygen may be deposited in a thin layer on the discrete elements. A barrier material (e.g. boron carbide or silicon carbide) may be deposited in a thin layer on the pyrolytic material to inhibit diffusion of elements into the pyrolytic material. A material impermeable to oxygen (e.g. boron nitride or silicon nitride) may be deposited in a thin layer on the barrier material. A refractory matrix permeable to oxygen may be deposited on the impermeable material. The matrix may include a metallic element (e.g. silicon, hafnium, tantalum or zirconium) and another element (e.g. oxygen, nitrogen, carbon or boron) chemically bonded to the metallic element. The matrix may have a second coefficient of thermal expansion different from the first coefficient and may have a minimal bond to the substrate. The matrix is accordingly able to move relative to the substrate with changes in temperature, partly because the pyrolytic material contributes to a shear between the matrix and substrate. A refractory material impermeable to oxygen may be deposited in a thin layer on the matrix and may include a metallic element (e.g. silicon, hafnium, tantalum or zirconium) and an element (e.g. oxygen, nitrogen and boron) chemically bonded to the metallic element. The different layers may be deposited on the substrate, each in a substantially uniform thickness, at an elevated temperature and at pressures pulsating at a particular rate, and in reverse directions, between first and second particular limits.

Inventors

  • 👤 David L. Arenz
  • 👤 Edward L. Paquette
  • 👤 Marc G. Simpson

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 05:51
CPC Classifications
C; C04; C04B; C04B41/00; C04B41/009; C04B30/00; C04B30/02; C04B35/00; C04B35/66; C04B35/71; C04B35/78; C04B35/80; C04B41/45; C04B41/4505; C04B41/4529; C04B41/4584; C04B41/52; C04B41/80; C04B41/81; C04B41/89; C23; C23C; C23C16/00; C23C16/04; C23C16/045; C23C16/44; C23C16/455; C04B2111/00; C04B2111/00241; Y; Y10; Y10S; Y10S427/00; Y10S427/10; Y10T; Y10T428/00; Y10T428/29; Y10T428/2913; Y10T428/2918; Y10T428/292; Y10T428/2933; Y10T428/2938; Y10T428/294; Y10T428/2942; Y10T428/2944; Y10T428/30

Claims Analysis

Total Claims: 44
Claim 1
Independent Claim 72 words
A refractory composite material, a porous permeable substrate defined by a plurality of discrete elements, a pyrolytic layer covering the discrete elements in the substrate, a layer of a material covering the pyrolytic layer and providing a barrier to inhibit diffusion into the pyrolytic layer, and a layer of a material covering the barrier layer and compatible with the material of the barrier layer and having properties of being impermeable to oxygen.
Claim 2
Dependent Claim 72 words
A refractory composite material, a porous permeable substrate defined by a plurality of discrete elements, a pyrolytic layer covering the discrete elements in the substrate, a layer of a material covering the pyrolytic layer and providing a barrier to inhibit diffusion into the pyrolytic layer, and a layer of a material covering the barrier layer and compatible with the material of the barrier layer and having properties of being impermeable to oxygen.
Claim 3
Dependent Claim 45 words
A refractory composite material as set forth in claim 1, including, a matrix disposed on the impermeable layer, the substrate having a first coefficient of thermal expansion and the matrix having a second coefficient of thermal expansion different from the first coefficient of thermal expansion.
Claim 4
Dependent Claim 38 words
A refractory composite material as set forth in claim 2, including, there being a minimal bond between the substrate and the matrix to provide for a movement of the matrix relative to the substrate with changes in temperature.
Claim 5
Dependent Claim 39 words
A refractory composite material as set forth in claim 3 wherein the discrete elements in the substrate are anisotropic and are permeable to oxygen and wherein the impermeable layer inhibits the oxidation of the discrete elements in the substrate.
Claim 6
Dependent Claim 43 words
A combination as set forth in claim 1 wherein the discrete elements in the substrate are carbonaceous and the pyrolytic layer is carbonaceous and the barrier layer and the impermeable layer include an element selected from the group consisting of boron and silicon.
Claim 7
Dependent Claim 73 words
A combination as set forth in claim 3 wherein the discrete elements in the substrate are carbonaceous and the pyrolytic layer is carbonaceous and the barrier layer and the impermeable layer include an element selected from the group consisting of boron and silicon and the matrix is formed from a refractory material defined by a refractory element chemically bonded to an element selected from the group consisting of oxygen, nitrogen, carbon and boron.
Claim 8
Dependent Claim 55 words
A refractory composite material, including, a porous substrate defined by a plurality of discrete elements, first means covering the discrete elements in the substrate and having properties of providing shear, second means covering the first means and providing a diffusion barrier, and third means covering the second means and defining a barrier impermeable to oxygen.
Claim 9
Dependent Claim 55 words
A refractory composite material, including, a porous substrate defined by a plurality of discrete elements, first means covering the discrete elements in the substrate and having properties of providing shear, second means covering the first means and providing a diffusion barrier, and third means covering the second means and defining a barrier impermeable to oxygen.
Claim 10
Dependent Claim 44 words
A refractory composite material as set forth in claim 7, including, the second means being formed from a material having properties of reacting with oxygen infiltrating into the second means to form a compound inhibiting any further infiltration of oxygen into the second means.
Claim 11
Dependent Claim 56 words
A refractory composite material as set forth in claim 8, including, the first means having a substantially uniform thickness at the different positions on the substrate and the second means having a substantially uniform thickness at the different positions on the first means and the third means having a substantially uniform thickness on the second means.
Claim 12
Dependent Claim 37 words
A refractory composite material as set forth in claim 7, including, a matrix disposed on the third means and having a minimal bond relative to the substrate for movement relative to the substrate with changes in temperature.
Claim 13
Dependent Claim 23 words
A refractory composite material as set forth in claim 10, including, means disposed on the matrix and defining a barrier impermeable to oxygen.
Claim 14
Dependent Claim 18 words
A refractory composite material as set forth in claim 8, wherein the second and third means include boron.
Claim 15
Dependent Claim 51 words
A refractory composite material, including, a porous, permeable substrate having a first coefficient of thermal expansion, a pyrolytic layer disposed on the substrate, means disposed on the pyrolytic layer and having impermeable properties and including a particular element providing a barrier against diffusion of the particular element into the pyrolytic layer.
Claim 16
Dependent Claim 51 words
A refractory composite material, including, a porous, permeable substrate having a first coefficient of thermal expansion, a pyrolytic layer disposed on the substrate, means disposed on the pyrolytic layer and having impermeable properties and including a particular element providing a barrier against diffusion of the particular element into the pyrolytic layer.
Claim 17
Dependent Claim 34 words
A refractory composite material as set forth in claim 13 wherein the porous, permeable substrate and the pyrolytic layer include carbon as an element and the particular element in the barrier means is boron.
Claim 18
Dependent Claim 68 words
A refractory composite material as set forth in claim 13, including, a matrix disposed on the barrier means, the substrate having a first coefficient of thermal expansion and the matrix having a second coefficient of thermal expansion, the pyrolytic layer having properties of providing a minimal bond between the substrate and the matrix to facilitate a displacement of the matrix relative to the substrate with changes in temperature.
Claim 19
Dependent Claim 33 words
A refractory composite material as set forth in claim 15 wherein the substrate and the pyrolytic layer are made from materials including carbon and the barrier means include boron as the particular element.
Claim 20
Dependent Claim 58 words
A refractory composite material, including, porous substrate means, barrier means disposed on the substrate means and including a particular element and having properties of preventing the diffusion of the particular element into the substrate means, and a matrix disposed on the barrier means and having properties of being movable relative to the substrate means with changes in temperature.
Claim 21
Dependent Claim 58 words
A refractory composite material, including, porous substrate means, barrier means disposed on the substrate means and including a particular element and having properties of preventing the diffusion of the particular element into the substrate means, and a matrix disposed on the barrier means and having properties of being movable relative to the substrate means with changes in temperature.
Claim 22
Dependent Claim 64 words
A refractory composite material as set forth in claim 17, including, the substrate means having a first coefficient of thermal expansion, and the matrix having a second coefficient of thermal expansion different from the first coefficient of thermal expansion and providing a minimal bond with the substrate means to facilitate a displacement of the matrix relative to the substrate means with changes in temperature.
Claim 23
Dependent Claim 23 words
A refractory composite material as set forth in claim 18 wherein the particular element is boron and the porous substrate means includes carbon.
Claim 24
Dependent Claim 23 words
A combination as set forth in claim 18, including, the substrate means being permeable to oxygen, the barrier means being impermeable to oxygen.
Claim 25
Dependent Claim 40 words
A combination as set forth in claim 20, including, the matrix being permeable to oxygen, and an impermeable layer disposed on the permeable layer and having refractory properties and including a metal and an element chemically bonded to the metal.
Claim 26
Dependent Claim 41 words
A combination as set forth in claim 22, the substrate means including carbon, the particular element constituting boron and the element chemically bonded to the metal in the matrix being selected from the group consisting of oxygen, carbon, nitrogen and boron.
Claim 27
Independent Claim 122 words
A method of producing a refractory composite material, including the steps of: forming a plurality of discrete elements into a porous substrate, the discrete elements being permeable to oxygen, depositing a layer of a pyrolytic material on the discrete elements by chemical vapor infiltration to cover the discrete elements in the substrate, the pyrolytic material being permeable to oxygen, depositing a layer of a barrier material on the pyrolytic layer by chemical vapor infiltration to cover the pyrolytic layer, and depositing by a chemical vapor infiltration a layer on the barrier layer of a material impermeable to oxygen to cover the material of the barrier layer, the barrier material having properties of inhibiting the diffusion of the impermeable material into the pyrolytic
Claim 28
Independent Claim 122 words
A method of producing a refractory composite material, including the steps of: forming a plurality of discrete elements into a porous substrate, the discrete elements being permeable to oxygen, depositing a layer of a pyrolytic material on the discrete elements by chemical vapor infiltration to cover the discrete elements in the substrate, the pyrolytic material being permeable to oxygen, depositing a layer of a barrier material on the pyrolytic layer by chemical vapor infiltration to cover the pyrolytic layer, and depositing by a chemical vapor infiltration a layer on the barrier layer of a material impermeable to oxygen to cover the material of the barrier layer, the barrier material having properties of inhibiting the diffusion of the impermeable material into the pyrolytic
Claim 29
Dependent Claim 58 words
A method as set forth in claim 23, wherein the discrete elements in the substrate are formed from a material including carbon, the pyrolytic material includes carbon, the barrier material includes an element selected from the group consisting of silicon and boron, and the impermeable material includes an element selected from the group consisting of silicon and boron.
Claim 30
Dependent Claim 47 words
A method as set forth in claim 23 wherein the barrier material includes a particular element and the impermeable material includes the particular element the barrier material has properties of inhibiting the diffusion of the particular element from the impermeable layer into the layer of pyrolytic material.
Claim 31
Dependent Claim 102 words
A method as set forth in claim 23, including the step of: depositing a matrix on the layer of permeable material, the matrix constituting a refractory material and being formed from a metallic element and another element chemically bonded to the metallic element, the substrate having a first coefficient of thermal expansion and the matrix having a second coefficient of thermal expansion different from the first coefficient of thermal expansion, the pyrolytic layer having properties of providing for a minimal bonding between the substrate and the matrix to obtain a displacement of the matrix relative to the substrate with changes in temperature.
Claim 32
Dependent Claim 43 words
A method as set forth in claim 26, including the step of: depositing a layer of an impermeable material on the matrix, the impermeable material constituting a refractory material formed from a metallic element and another element chemically bonded to the metallic element.
Claim 33
Dependent Claim 42 words
A method as set forth in claim 27 wherein the discrete elements in the substrate include carbon and the pyrolytic material includes carbon and the barrier material includes boron and the impermeable material on the layer of the barrier material includes boron.
Claim 34
Independent Claim 93 words
A method of forming a refractory composite material, including the following steps: forming a permeable, porous substrate, depositing a pyrolytic material on the substrate, depositing a barrier material on the pyrolytic material, depositing an impermeable material on the barrier material where the impermeable material is impermeable to oxygen, the barrier material having properties of inhibiting any diffusion of the impermeable material into the pyrolytic layer, and depositing a matrix of a refractory material on the impermeable material, the refractory material including a metallic element and an element chemically bonded to the refractory element.
Claim 35
Independent Claim 93 words
A method of forming a refractory composite material, including the following steps: forming a permeable, porous substrate, depositing a pyrolytic material on the substrate, depositing a barrier material on the pyrolytic material, depositing an impermeable material on the barrier material where the impermeable material is impermeable to oxygen, the barrier material having properties of inhibiting any diffusion of the impermeable material into the pyrolytic layer, and depositing a matrix of a refractory material on the impermeable material, the refractory material including a metallic element and an element chemically bonded to the refractory element.
Claim 36
Dependent Claim 64 words
A method as set forth in claim 29, wherein the substrate has a first coefficient of thermal expansion and the matrix has a second coefficient of thermal expansion different from the first coefficient of thermal expansion and there is a minimal bond between the substrate and the matrix to provide for a movement of the matrix relative to the substrate with changes in temperature.
Claim 37
Dependent Claim 27 words
A method as set forth in claim 30, including the step of: depositing an impermeable material on the matrix where the impermeable material is impermeable to oxygen.
Claim 38
Dependent Claim 72 words
A method as set forth in claim 29 wherein the barrier material, the impermeable material and the matrix are successively deposited on the pyrolytic material at an elevated temperature and alternately in opposite directions and with a pressure pulsating at a particular rate between first and second limits of pressure to obtain a uniform deposition of the barrier material, the impermeable material and the matrix in successive layers on the pyrolytic material.
Claim 39
Independent Claim 116 words
A method of making a refractory composite material, including the steps of: providing a porous substrate having a first coefficient of thermal expansion, passing gases through the substrate alternately in one direction and then in the opposite direction to deposit, by chemical vapor infiltration, an impermeable layer on the substrate, and passing gases through the substrate alternately in one direction and then in the other direction to deposit, by chemical vapor infiltration, on the substrate a matrix having a second coefficient of thermal expansion different from the first coefficient of thermal expansion and having a minimal bond to the substrate to provide for a displacement of the matrix relative to the substrate with changes in temperature.
Claim 40
Independent Claim 116 words
A method of making a refractory composite material, including the steps of: providing a porous substrate having a first coefficient of thermal expansion, passing gases through the substrate alternately in one direction and then in the opposite direction to deposit, by chemical vapor infiltration, an impermeable layer on the substrate, and passing gases through the substrate alternately in one direction and then in the other direction to deposit, by chemical vapor infiltration, on the substrate a matrix having a second coefficient of thermal expansion different from the first coefficient of thermal expansion and having a minimal bond to the substrate to provide for a displacement of the matrix relative to the substrate with changes in temperature.
Claim 41
Dependent Claim 60 words
A method as set forth in claim 33 wherein the pressure of the gases producing the impermeable layer is pulsated between first and second limits during the infiltration of the gases through the substrate and the pressure of the gases producing the matrix is pulsated between the first and second limits during the infiltration of the gases through the substrate.
Claim 42
Dependent Claim 46 words
A method as set forth in claim 34, including the step of: passing gases through the substrate alternately in one direction and then in the other direction to deposit, by chemical vapor infiltration, an impermeable layer on the substrate with the second coefficient of thermal expansion.
Claim 43
Dependent Claim 31 words
A method as set forth in claim 33 wherein the impermeable layer actually includes a barrier layer having properties of inhibiting diffusion of material from the impermeable layer into the substrate.
Claim 44
Dependent Claim 36 words
A method as set forth in claim 33 wherein the impermeable layer is deposited in a substantially uniform thickness on the substrate and the matrix is deposited in a substantially uniform thickness on the impermeable layer.

References Cited (Backward Citations)

US4596741A Cited
US4663230A Cited
US4772513A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1992-09-04 1993-03-06 1993-09-05 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1996-09-04 1997-03-06 1997-09-05 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2000-09-04 2001-03-06 2001-09-05 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag