USH200H - High temperature structural insulating material - Google Patents

High temperature structural insulating material Download PDF

Info

Publication number
USH200H
USH200H US06/625,324 US62532484A USH200H US H200 H USH200 H US H200H US 62532484 A US62532484 A US 62532484A US H200 H USH200 H US H200H
Authority
US
United States
Prior art keywords
beads
binder
binder composition
temperature
structural insulating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US06/625,324
Inventor
Wayne Y. Chen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
United States, AS REPRESENTED BY US DEPARTMENT OF ENERGY
US Department of Energy
Original Assignee
US Department of Energy
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by US Department of Energy filed Critical US Department of Energy
Priority to US06/625,324 priority Critical patent/USH200H/en
Assigned to UNITED STATES OF AMERICA AS REPRESENTED BY THE US DEPARTMENT OF ENERGY reassignment UNITED STATES OF AMERICA AS REPRESENTED BY THE US DEPARTMENT OF ENERGY ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: CHEN, WAYNE Y.
Application granted granted Critical
Publication of USH200H publication Critical patent/USH200H/en
Abandoned legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/622Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/64Burning or sintering processes
    • C04B35/645Pressure sintering
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03CCHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
    • C03C14/00Glass compositions containing a non-glass component, e.g. compositions containing fibres, filaments, whiskers, platelets, or the like, dispersed in a glass matrix
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/622Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/626Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
    • C04B35/63Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B using additives specially adapted for forming the products, e.g.. binder binders
    • C04B35/6303Inorganic additives
    • C04B35/6316Binders based on silicon compounds
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F7/00Casings, e.g. crankcases or frames
    • F02F7/0085Materials for constructing engines or their parts
    • F02F7/0087Ceramic materials
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03CCHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
    • C03C2214/00Nature of the non-vitreous component
    • C03C2214/32Nature of the non-vitreous component comprising a sol-gel process

Definitions

  • This invention relates to a high-temperature, low-density structural insulating composite having a favorable combination of low thermal conductivity, high compressive strength and elevated service temperature.
  • Composites of the invention have properties useful as insulating structures at high temperatures and particularly as liners within cylinders of high temperature engines.
  • thermo conductivity of amorphous glass is in the order of 1.2 Watts/meter/°C.(W/m°C.).
  • a commercial glass ceramic with voids has a thermal conductivity in the order of 0.6 W/m°C. At this value (0.6 W/m°C.) of conductivity, calculations indicate that the radial heat conduction through the ceramic is roughly equal to the axial heat conduction through the metal wall which the ceramic is intended to replace for thermal purposes. Calculations further indicate that efficiency of a heat engine and particularly a Stirling engine would be improved if the thermal conductivity of the insulation could be lowered to about 0.2 W/m°C.
  • thermal conductivity While some materials have the lower thermal conductivity, they usually have a useful service temperature below 800° C. and/or insufficient compressive strength. In many instances, low thermal conductivity is combined with low strength or high thermal conductivity is combined with high strength. A material having a combination of a thermal conductivity below about 0.20 W/m°C. and a strength above about 250 psi and particularly above about 400 psi would be desirable.
  • one object of the invention is a high temperature insulating material.
  • Another object is a high temperature insulating material capable of being formed into a structural member.
  • An additional object is a high temperature insulating material having a thermal conductivity below about 0.2 W/m°C., a compressive strength above about 250 psi and a useful service temperature of above about 800° C.
  • the invention is directed to a high temperature structural insulating material characterized by a closed-cell, compact array of hollow ceramic beads bonded together under pressure and sintering conditions, and to a method of producing the structural materials.
  • ceramic refers to a material having crystalline properties.
  • the material or composite is produced by forming a mixture of hollow ceramic beads and a binder composition wherein the beads and binder composition (coating the beads) are compacted under sintering conditions (below the softening temperature of the ceramic beads) and under pressure to provide a compact, tightly packed array of the beads with closed cells with the adjacent surface areas of the beads being bonded together by the binder.
  • the ceramic beads preferably have a softening temperature above about 800° C., a size within the range of 20-200 ⁇ m diameter and a wall thickness in the range of about 2-4 ⁇ m.
  • the binder composition preferably includes a wetting agent and is used in an amount sufficient to coat the external surface areas of the beads.
  • hollow ceramic beads are selected which are small in size, typically 20-200 microns in diameter with wall thicknesses above about 2.0 microns. They are further characterized by a bulk density in the order of about 0.3-0.5 gm/cc. They also are of closed cell, have low thermal conductivity and have a fine finish and low friction.
  • a mixture is formed of the beads and a compatible binder composition.
  • the binder composition includes a wetting agent such as an alcohol ethoxylate to improve compatibility.
  • Mixing is carried out by a stirrer controlled by a low speed motor to remove air.
  • Suitable weight ratios of beads:binder composition are in the order of 1:1-2 and preferably about 1:1.2-1.6.
  • the ratios of beads: wetting agent:binder are in the order of 1:0.01-0.02:1-2 and preferably 1:0.012-0.016:1.2-1.6.
  • the binder is selected to form a strong adhesive bond between adjacent surface areas of the beads.
  • a wetting agent is preferably used to increase contact between the beads and binder.
  • the binder is a commercial colloidal silica solution marketed by DuPont Corporation as Ludox HS30.
  • the combination of beads, wetting agent and binder after mixing are inserted into a suitably shaped form and compacted under sintering conditions and pressure to provide a compact, tightly packed composite.
  • the sintering conditions include a temperature of above about 700° C. and preferably above about 800° C. With ceramics having a softening temperature above about 1200° C., the sintering temperature preferably is above about 900° C.
  • the pressure is applied incremently to reduce the initial volume by 10-20% and provide some slight physical distortion of the beads to increase the adjacent surface areas of the beads and provide a compact composite.
  • the mixture was then placed in a hollow form to provide a wall-like shape and heated to about 950° C. for sintering for about 8.5 hours. Pressure (estimated to be at least 50-100 psi) on the mixture was applied by a compactor and reduced the volume by about 20%.
  • the beads are retained in compact, tightly packed structures without cracks in adjacent portions of the beads. Most of the beads are bonded to adjacent beads to form structural-strong arrays of bonded beads. The information from enlarged photos further reveals a slight distortion of many beads which increases the surface area of bonding between adjacent beads.
  • the thermal conductivity was below about 0.2 W/m°C. with a compressive strength above about 400 psi. These materials also exhibited low thermal stress and low gas permeability.
  • Beads having lower softening temperatures of 700° C. and identified as D32/4500 from Minnesota Mining and Manufacturing Company were made into composites by sintering at about 600° C. without any bonding agent. While they exhibited good properties of thermal conductivity and strength, their low softening temperature would limit their usefulness at temperatures above 800° C.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Inorganic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Structural Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Dispersion Chemistry (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Compositions Of Oxide Ceramics (AREA)
  • Ceramic Products (AREA)

Abstract

A high temperature structural insulating material useful as a liner for cylinders of high temperature engines through the favorable combination of high service temperature (above about 800° C.), low thermal conductivity (below about 0.2 W/m° C.), and high compressive strength (above about 250 psi). The insulating material is produced by selecting hollow ceramic beads with a softening temperature above about 800° C., a diameter within the range of 20-200 μm, and a wall thickness in the range of about 2-4 μm; compacting the beads and a compatible silicate binder composition under pressure and sintering conditions to provide the desired structural form with the structure having a closed-cell, compact array of bonded beads.

Description

CONTRACTUAL ORIGIN OF THE INVENTION
The United States Government has rights in this invention pursuant to Contract No. W-31-109-ENG-38 between the U.S. Department of Energy and The University of Chicago representing Argonne National Laboratory.
BACKGROUND OF THE INVENTION
This invention relates to a high-temperature, low-density structural insulating composite having a favorable combination of low thermal conductivity, high compressive strength and elevated service temperature. Composites of the invention have properties useful as insulating structures at high temperatures and particularly as liners within cylinders of high temperature engines.
In the development of high temperature liners, available materials have in general not exhibited the desired combination of thermal conductivity and compressive strengths at operating temperatures of 800° C. and above. The thermal conductivity of amorphous glass is in the order of 1.2 Watts/meter/°C.(W/m°C.). A commercial glass ceramic with voids has a thermal conductivity in the order of 0.6 W/m°C. At this value (0.6 W/m°C.) of conductivity, calculations indicate that the radial heat conduction through the ceramic is roughly equal to the axial heat conduction through the metal wall which the ceramic is intended to replace for thermal purposes. Calculations further indicate that efficiency of a heat engine and particularly a Stirling engine would be improved if the thermal conductivity of the insulation could be lowered to about 0.2 W/m°C.
While some materials have the lower thermal conductivity, they usually have a useful service temperature below 800° C. and/or insufficient compressive strength. In many instances, low thermal conductivity is combined with low strength or high thermal conductivity is combined with high strength. A material having a combination of a thermal conductivity below about 0.20 W/m°C. and a strength above about 250 psi and particularly above about 400 psi would be desirable.
Accordingly, one object of the invention is a high temperature insulating material. Another object is a high temperature insulating material capable of being formed into a structural member. An additional object is a high temperature insulating material having a thermal conductivity below about 0.2 W/m°C., a compressive strength above about 250 psi and a useful service temperature of above about 800° C. These and other objects will become apparent from the following description.
SUMMARY OF THE INVENTION
Briefly, the invention is directed to a high temperature structural insulating material characterized by a closed-cell, compact array of hollow ceramic beads bonded together under pressure and sintering conditions, and to a method of producing the structural materials. For purposes of this invention, "ceramic" refers to a material having crystalline properties. The material or composite is produced by forming a mixture of hollow ceramic beads and a binder composition wherein the beads and binder composition (coating the beads) are compacted under sintering conditions (below the softening temperature of the ceramic beads) and under pressure to provide a compact, tightly packed array of the beads with closed cells with the adjacent surface areas of the beads being bonded together by the binder. The ceramic beads preferably have a softening temperature above about 800° C., a size within the range of 20-200 μm diameter and a wall thickness in the range of about 2-4 μm. The binder composition preferably includes a wetting agent and is used in an amount sufficient to coat the external surface areas of the beads.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
In the method for producing the inventive composite, hollow ceramic beads are selected which are small in size, typically 20-200 microns in diameter with wall thicknesses above about 2.0 microns. They are further characterized by a bulk density in the order of about 0.3-0.5 gm/cc. They also are of closed cell, have low thermal conductivity and have a fine finish and low friction.
A mixture is formed of the beads and a compatible binder composition. Preferably, the binder composition includes a wetting agent such as an alcohol ethoxylate to improve compatibility. Mixing is carried out by a stirrer controlled by a low speed motor to remove air. Suitable weight ratios of beads:binder composition are in the order of 1:1-2 and preferably about 1:1.2-1.6. With the wetting agent, the ratios of beads: wetting agent:binder are in the order of 1:0.01-0.02:1-2 and preferably 1:0.012-0.016:1.2-1.6.
The binder is selected to form a strong adhesive bond between adjacent surface areas of the beads. With colloidial silica gel binder, a wetting agent is preferably used to increase contact between the beads and binder. Preferably, the binder is a commercial colloidal silica solution marketed by DuPont Corporation as Ludox HS30.
The combination of beads, wetting agent and binder after mixing are inserted into a suitably shaped form and compacted under sintering conditions and pressure to provide a compact, tightly packed composite. The sintering conditions include a temperature of above about 700° C. and preferably above about 800° C. With ceramics having a softening temperature above about 1200° C., the sintering temperature preferably is above about 900° C. Preferably, the pressure is applied incremently to reduce the initial volume by 10-20% and provide some slight physical distortion of the beads to increase the adjacent surface areas of the beads and provide a compact composite.
The following examples are provided for illustrative purposes and are not intended to be restrictive as to the scope of the invention:
EXAMPLES I-IV
In tests to produce an insulating composite, two different beads were selected having useful temperatures above about 800° C. and other properties as set forth in Table I. Both were obtained from Emerson Cummins Company of Canton, Massachusetts and are identified as "SI" (a borosilicate glass) and "FA-A" (a ceramic) being crystalline and reportedly having a metal content predominantly of Si and Al with Fe, Mg, Na, K and Ti being present by weight in the respective amounts of 2%, 1%, 0.5% 0,5% and 1%. Properties of these beads plus a sample of glass beads (D32/4500) from Minnesota Mining and Manufacturing Company are provided in Table I.
              TABLE I                                                     
______________________________________                                    
Physical Properties of Three Microsphere Brands                           
______________________________________                                    
Commercial Designation                                                    
                SI       FA-A     D32/4500                                
Composition     glass    ceramic  glass                                   
Bulk Density,                                                             
lb./cu.ft.      9.5      25.0                                             
g./cc.          0.155    0.4      0.32                                    
True Particle Density                                                     
lb./cu./ft.     15.8     46.5                                             
g./cc.          0.254    0.65                                             
Particle Size Range                                                       
(by weight)                                                               
>175μ        0        5                                                
149-175μ     14       11                                               
125-145μ     10       19                                               
100-125μ     12       24                                               
 62-100μ     40       35                                               
 44-62μ      15       4                                                
<44μ         9        2                                                
Packing Factor  0.559    0.620                                            
Average Wall Thickness, μm                                             
                1.5      3.5      0.8-2.2                                 
Softening Temperature                                                     
                985      1200     715                                     
Strength under hydro-                                                     
                55.0     83.0      10                                     
static Pressure                                                           
[Volume % savings at                                                      
1500 psi (100 kg./cm.sup.2)]                                              
Thermal Conductivity                                                      
                0.10     0.13     0.029-0.12                              
(W/m °C.)                                                          
______________________________________                                    
Six samples of the FA-A beads having bulk densities varying between 0.422-0.474 gm/cc were made into composites. Previously, it had been determined that FA-A beads could not be sintered in air at 950° C. without any binder. In the process, the beads of each sample were mixed with a wetting agent (GAF's Antarox BL240) and a binder (DuPont's Ludox HS30) in a ratio of 1:0.015:1.4. The mixing was carried out by stirrer connected to a slow motor. The wetting agent is further identified as an alcohol ethoxylate with the binder being identified as a colloidal silica solution (aluminum modified silicate, pH values 8.6-9.3).
The mixture was then placed in a hollow form to provide a wall-like shape and heated to about 950° C. for sintering for about 8.5 hours. Pressure (estimated to be at least 50-100 psi) on the mixture was applied by a compactor and reduced the volume by about 20%.
As revealed by scanning electron photomicrographs, the beads are retained in compact, tightly packed structures without cracks in adjacent portions of the beads. Most of the beads are bonded to adjacent beads to form structural-strong arrays of bonded beads. The information from enlarged photos further reveals a slight distortion of many beads which increases the surface area of bonding between adjacent beads.
Performance tests were run on the four samples and provided the data in Table II.
              TABLE II                                                    
______________________________________                                    
     Bulk                                                                 
     Den-                           Thermal                               
     sity   Compressive             Conductivity                          
Sam- gm/    Strength   Young's      Strength                              
ple  cc     psi        Modulus      W/m °C.                        
______________________________________                                    
330  0.446  968        27.30 ×                                      
                                10.sup.4 psi                              
                                      0.122                               
412  0.440  1208       8.88 ×                                       
                                10.sup.4 psi                              
                                      0.110                               
419  0.474  627        5.89 ×                                       
                                10.sup.4 psi                              
                                      0.117                               
615  0.423  (488-573)  (7.08-7.48) ×                                
                                10.sup.4 psi                              
                                      0.104                               
______________________________________                                    
As indicated above, the thermal conductivity was below about 0.2 W/m°C. with a compressive strength above about 400 psi. These materials also exhibited low thermal stress and low gas permeability.
In contrast, other tests with the "SI" beads were carried out and revealed that collapse of the beads occurred at about one atmosphere pressure and 830° C. Sintering of the beads at 950° C. with sodium silicate solution was unsuccessful as only partial sintering was obtained. Bonding agents were used including Dupont's Ludox HS30 without success. Inspection of the samples revealed that the walls of some beads become broken and the beads tended to soften and deform.
Beads having lower softening temperatures of 700° C. and identified as D32/4500 from Minnesota Mining and Manufacturing Company were made into composites by sintering at about 600° C. without any bonding agent. While they exhibited good properties of thermal conductivity and strength, their low softening temperature would limit their usefulness at temperatures above 800° C.
The foregoing description of embodiments of the invention has been presented for purposes of illustration and description. It is not intended to be exhaustive or to limit the invention to the precise form disclosed, and obviously many modifications and variations are possible in light of the above teaching.

Claims (6)

The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:
1. A method of producing a structural insulating composite having a useful temperature above about 800° C. a thermal conductivity of below about 0.2 Watts/meter/°C. as measured at temperatures in the range of 25°-200° C. and a compressive strength above about 400 psi, the method comprising the steps of
selecting hollow ceramic beads having a metal content predominantly of Si and Al, an outer diameter in the range of about 20-200 microns, a wall thickness of above about 2 microns, a softening temperature above about 800° C., and a bulk density above about 0.3 gm/cc,
forming a mixture of the ceramic beads with a compatible binder composition in amounts sufficient to coat the beads and in a beads-to-binder ratio of about 1:1-2 by weight,
removing entrained gas bubbles in said mixture, and
compacting the mixture under sintering conditions and pressure to provide the structural insulating composition, the sintering conditions including a temperature below the softening temperature but above 700° C., and a sintering time sufficient to produce said composite with said temperature, thermal conductivity and compressive strength, the pressure being applied to increase the surface area of contact between the bead surface areas being joined by the binder composition.
2. The method of claim 1 wherein the selection of ceramic beads results in said beads having a thickness of about 2-4 μm.
3. The method of claim 2 wherein the binder composition includes a wetting agent in a ratio of beads:wetting agent:binder of about 1:0.012-0.016:1.2-1.6.
4. The method of claim 3 wherein the binder composition includes colloidal silica suspension having ceramic bonding properties as a binder and the ratio is about 1:1.4, and said beads have a minor content of Fe, Mg, Na, K and Ti.
5. A shaped, structural insulating composite being the product of the method of claim 1 and characterized by a closely packed, bonded array of said beads with closed cells.
6. The shaped, structural insulating composite of claim 5 wherein the weight ratio of beads to binder composition is about 1:1.4.
US06/625,324 1984-06-27 1984-06-27 High temperature structural insulating material Abandoned USH200H (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US06/625,324 USH200H (en) 1984-06-27 1984-06-27 High temperature structural insulating material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/625,324 USH200H (en) 1984-06-27 1984-06-27 High temperature structural insulating material

Publications (1)

Publication Number Publication Date
USH200H true USH200H (en) 1987-01-06

Family

ID=24505539

Family Applications (1)

Application Number Title Priority Date Filing Date
US06/625,324 Abandoned USH200H (en) 1984-06-27 1984-06-27 High temperature structural insulating material

Country Status (1)

Country Link
US (1) USH200H (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002026487A1 (en) * 2000-09-28 2002-04-04 Court Caroline B Decorative vitreous beads and products and methods of making same
US6444162B1 (en) 2000-11-27 2002-09-03 The United States Of America As Represented By The United States Department Of Energy Open-cell glass crystalline porous material
US6472579B1 (en) 2000-11-27 2002-10-29 The United States Of America As Represented By The Department Of Energy Method for solidification of radioactive and other hazardous waste

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2634563A (en) 1946-02-12 1953-04-14 American Can Co Method of producing bulged containers
US2691598A (en) 1950-03-30 1954-10-12 Lab Annexes A L I Meurice Chim Porous materials suitable for use as thermal and acoustic insulators and process for their manufacture
US2806509A (en) 1956-06-11 1957-09-17 Goodyear Aircraft Corp Sandwich structures
US2811457A (en) 1952-12-18 1957-10-29 Johns Manville Inorganic bonded thermal insulating bodies and method of manufacture
US3298842A (en) 1963-03-22 1967-01-17 Du Pont Process for preparing hollow refractory particles
US3632385A (en) 1970-03-17 1972-01-04 Atomic Energy Commission Carbon composite structures and method for making same
US3888691A (en) 1972-10-06 1975-06-10 Lockheed Aircraft Corp Porous ceramic
US3974315A (en) 1973-08-15 1976-08-10 The Carborundum Company Closed cellular fused silica bodies
US4078028A (en) 1975-12-27 1978-03-07 Showa Vermiculite Kabushiki Kaisha Method for manufacture of noncombustible, smokeless building composite material

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2634563A (en) 1946-02-12 1953-04-14 American Can Co Method of producing bulged containers
US2691598A (en) 1950-03-30 1954-10-12 Lab Annexes A L I Meurice Chim Porous materials suitable for use as thermal and acoustic insulators and process for their manufacture
US2811457A (en) 1952-12-18 1957-10-29 Johns Manville Inorganic bonded thermal insulating bodies and method of manufacture
US2806509A (en) 1956-06-11 1957-09-17 Goodyear Aircraft Corp Sandwich structures
US3298842A (en) 1963-03-22 1967-01-17 Du Pont Process for preparing hollow refractory particles
US3632385A (en) 1970-03-17 1972-01-04 Atomic Energy Commission Carbon composite structures and method for making same
US3888691A (en) 1972-10-06 1975-06-10 Lockheed Aircraft Corp Porous ceramic
US3974315A (en) 1973-08-15 1976-08-10 The Carborundum Company Closed cellular fused silica bodies
US4078028A (en) 1975-12-27 1978-03-07 Showa Vermiculite Kabushiki Kaisha Method for manufacture of noncombustible, smokeless building composite material

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
"A Closed Cell Structural Material Having High Temperature Thermal Insulating Properties" by W. Y. C. Chen and J. G. Daley, Argonne National Laboratory Report, ANL-82-54, 1982.
"Proc. of the First Conf. on Advanced Materials for Alternative Fuel Capable Directly Fired Heat Engines" edited by John W. Fairbanks and John Stringer, Jul. 31-Aug. 3, 1979, pp. 527-541, pp. 582-605.
Chen, Wayne Y. C., High Temperature Structural Insulating Material with Closed Cell Structure, Particulate Science and Technology, 1983, pp. 335-356.
Large Cost Reduction and Efficiency Enhancement of Stirling Engines by Deployment of Porous Ceramic Insulation" (Feasibility Study), Stirling Technology, Inc., 1980.

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002026487A1 (en) * 2000-09-28 2002-04-04 Court Caroline B Decorative vitreous beads and products and methods of making same
US6444162B1 (en) 2000-11-27 2002-09-03 The United States Of America As Represented By The United States Department Of Energy Open-cell glass crystalline porous material
US6472579B1 (en) 2000-11-27 2002-10-29 The United States Of America As Represented By The Department Of Energy Method for solidification of radioactive and other hazardous waste
US6667261B1 (en) 2000-11-27 2003-12-23 The United States Of America As Represented By The United States Department Of Energy Open-cell glass crystalline porous material

Similar Documents

Publication Publication Date Title
US6667261B1 (en) Open-cell glass crystalline porous material
US4657810A (en) Fired hollow ceramic spheroids
EP0244109B1 (en) Thermally bonded fibrous products
US4595662A (en) Ceramic material for a honeycomb structure
CA1087593A (en) Macroporous microspheroids and a process for their manufacture
US4598054A (en) Ceramic material for a honeycomb structure
JPS6340779A (en) Heat insulator comprising sedimented silica and fly ash
JPS58135181A (en) Manufacture of porous ceramic seal
US5897943A (en) Metal matrix composite including homogeneously distributed fly ash, binder, and metal
US5569423A (en) Process for the manufacture of a silica fiber based heat insulating material
Abe et al. Formation of porous fumed silica coating on the surface of glass fibers by a dry mechanical processing technique
USH200H (en) High temperature structural insulating material
EP0639164B1 (en) Ceramic products
US4769189A (en) Process for making hollow, ceramic spheroids
CA1227624A (en) Making hot pressed silicon nitride by use of low density reaction bonded body
US5506179A (en) Ceramics binder mixture and binding method
CN112521058A (en) Honeycomb structure ceramic thermal insulation composite material and manufacturing method thereof
GB2170515A (en) Making sintered porous metal articles by centrifuging
JP3359429B2 (en) Ceramic bonding composition and bonding method
US5556586A (en) Process for manufacturing a heat insulating material
JPH045721B2 (en)
JP2819351B2 (en) Insulation structure
JPH03193336A (en) Heat-resistant honeycomb structural body
JPS5842142B2 (en) Inorganic porous body and its manufacturing method
JP3186993B2 (en) Insulation

Legal Events

Date Code Title Description
AS Assignment

Owner name: UNITED STATES OF AMERICA AS REPRESENTED BY THE US

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:CHEN, WAYNE Y.;REEL/FRAME:004333/0677

Effective date: 19840625

STCF Information on status: patent grant

Free format text: PATENTED CASE