GB2141418A - A process for the production of carbon-containing materials having ultrafine grains - Google Patents
A process for the production of carbon-containing materials having ultrafine grains Download PDFInfo
- Publication number
- GB2141418A GB2141418A GB08414925A GB8414925A GB2141418A GB 2141418 A GB2141418 A GB 2141418A GB 08414925 A GB08414925 A GB 08414925A GB 8414925 A GB8414925 A GB 8414925A GB 2141418 A GB2141418 A GB 2141418A
- Authority
- GB
- United Kingdom
- Prior art keywords
- carbon
- process according
- aerogel
- containing materials
- production
- 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.)
- Granted
Links
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title claims abstract description 52
- 229910052799 carbon Inorganic materials 0.000 title claims abstract description 45
- 239000000463 material Substances 0.000 title claims abstract description 30
- 238000000034 method Methods 0.000 title claims abstract description 24
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 10
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 30
- 239000011148 porous material Substances 0.000 claims abstract description 24
- 239000000758 substrate Substances 0.000 claims abstract description 16
- 239000004965 Silica aerogel Substances 0.000 claims abstract description 12
- 239000000835 fiber Substances 0.000 claims abstract description 8
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract description 8
- 238000005234 chemical deposition Methods 0.000 claims abstract description 5
- 229910002804 graphite Inorganic materials 0.000 claims abstract description 4
- 239000010439 graphite Substances 0.000 claims abstract description 4
- 239000004964 aerogel Substances 0.000 claims description 15
- 239000000741 silica gel Substances 0.000 claims description 12
- 229910002027 silica gel Inorganic materials 0.000 claims description 12
- 239000006229 carbon black Substances 0.000 claims description 9
- 239000007788 liquid Substances 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 7
- 238000000280 densification Methods 0.000 abstract description 7
- 238000003889 chemical engineering Methods 0.000 abstract description 2
- OKKJLVBELUTLKV-UHFFFAOYSA-N Methanol Chemical compound OC OKKJLVBELUTLKV-UHFFFAOYSA-N 0.000 description 24
- 238000005470 impregnation Methods 0.000 description 14
- 239000002904 solvent Substances 0.000 description 9
- 239000006230 acetylene black Substances 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 239000000499 gel Substances 0.000 description 3
- 230000003301 hydrolyzing effect Effects 0.000 description 3
- 239000000377 silicon dioxide Substances 0.000 description 3
- LFQCEHFDDXELDD-UHFFFAOYSA-N tetramethyl orthosilicate Chemical compound CO[Si](OC)(OC)OC LFQCEHFDDXELDD-UHFFFAOYSA-N 0.000 description 3
- 238000002679 ablation Methods 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000001000 micrograph Methods 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 238000011282 treatment Methods 0.000 description 2
- 238000004078 waterproofing Methods 0.000 description 2
- ZAMOUSCENKQFHK-UHFFFAOYSA-N Chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- CREMABGTGYGIQB-UHFFFAOYSA-N carbon carbon Chemical compound C.C CREMABGTGYGIQB-UHFFFAOYSA-N 0.000 description 1
- 239000011203 carbon fibre reinforced carbon Substances 0.000 description 1
- 229910052801 chlorine Inorganic materials 0.000 description 1
- 239000000460 chlorine Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 210000003739 neck Anatomy 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/009—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/52—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbon, e.g. graphite
- C04B35/521—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbon, e.g. graphite obtained by impregnation of carbon products with a carbonisable material
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
- C04B35/80—Fibres, filaments, whiskers, platelets, or the like
- C04B35/83—Carbon fibres in a carbon matrix
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/50—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials
- C04B41/5001—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials with carbon or carbonisable materials
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/52—Multiple coating or impregnating multiple coating or impregnating with the same composition or with compositions only differing in the concentration of the constituents, is classified as single coating or impregnation
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/85—Coating or impregnation with inorganic materials
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/89—Coating or impregnation for obtaining at least two superposed coatings having different compositions
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
- F16D69/02—Compositions of linings; Methods of manufacturing
- F16D69/023—Composite materials containing carbon and carbon fibres or fibres made of carbonizable material
Abstract
The present invention relates to a process for the production of carbon-containing materials having ultrafine grains. This process is characterised in that a chemical deposition in the vapour phase is effected on all or part of a silica aerogel. The latter may be a self-supported block or may fill the pores of a porous material eg carbon foam, polycrystalline graphite or carbon fibre based substrate. Uses: the densification and improvement of the ablation-and oxidation-resistance of carbon-containing materials, intended in particular for the production of nozzles, brakes, and elements for chemical engineering.
Description
SPECIFICATION
A process for the production of carbon-containing materials having ultrafine grains
It is well established in the art that industrial carbons and graphites and carbon fibre/carbon matrix compounds are porous materials having a pore size in the range of from several tenths of a micron to one hundred microns or more.
This porosity creates disadvantages for certain uses of these materials. These include its use for nozzles, oxidation resistant materials, materials for fused-salt reactors, and heat exchangers etc.
The waterproofing or densifying of these porous materials is limited either by the closure of the narrow necks of pores if the process is a chemical deposition in the vapour phase (henceforth abbreviated to CDVP) or by the number of operations if the process is a liquid impregnation.
It is, moreover, known that before commercialisation compressed carbon black is generally in the form of aggregates. These aggregates may be agglomerated by a binder, such as pitch, or densified by a CDVP, but they produce a porous material similar two industrial carbons.
In contrast, if acetylene black drawn from the outlet of the reactor which has not been compacted is used as a starting material, a homogenous material may be obtained by isostatic or mono directional compression, the pores of which are submicronic, not only when the openings of the pores are measured, but also in the pores themselves (this is essentially due to the three dimensional texture of the particles of this black). This homogeneous material having ultrafine dimensions is densified well by carbon CDVP and produces a dense carbon which, even though it has good resistance to ablation, is not sufficiently resistant to thermal shock.
In his French patent application filed on 10th September 1981, Publication No. 2512441 for a "Process for the production of low-density carbon having ultrafine homogeneous porosit", the Applicant claims to be able to produce a so-called "aerocarbon" material.
Aerocarbon is obtained by producing a suspension of carbon black particles in a liquid which is subsequently removed under hypercritical conditions.
If the aerocarbon is densified well by CDVP, producing a material having ultrafine grains, it is not always easy to produce it having a homogeneous density, especially when a fibrous substrate is to be impregnated with black.
The main object of the present invention is to produce carbon-containing materials having untrafine grains and a homogeneous density which do not suffer from the disadvantages of this type of material and/or are easier to use.
Accordingly the present invention, provides a process for producing carbon-containing materials having ultrafine grains consisting of the CDVP of carbon, characterised in that the carbon is completely or partially deposited on a silica aerogel.
The silica aerogels are generally obtained by producing a silica gel impregnated with solvent, and removing the solvent under hypercritical conditions.
A silica aerogel may, for example, be obtained in the following manner: a silica gel impregnated with solvent is produced by hydrolysing a methyl orthosilicate diluted in methanol; the methanol is removed under hypercricitcal conditions: at a pressure of more than 78 bars and at a temperature of more than 240"C (these values are the critical parameters of the methanol).
Figure 1 shows the cycle (indicated by the arrow) for producing this aerogel using gel impregnated with methanol.
As the silica particles are reticulated among themselves when the gel is formed, the gel remains in place when the solvent is removed and as the solvent is removed under hypercricital conditions, a silica aerogel is obtained which has neither contracted not fissured.
This aerogel has a homogeneous density and an ultrafine microporosity (from 10 to 1000 Â ) which is favourable to a carbon CDVP.
Nevertheless, the conditions of this CDVP should be adapted so that densification takes place in the mass of the entire aerogel. In general, the process is carried out at a more elevated pressure and at a lower temperature than those used under conventional CDVP conditions for coarser substrates (such as polycrystalline graphite, fibrous substrates).
Figure 2 shows the densification of a silica aerogel by carbon CDVP using methane under different conditions, as a function of time: curve (1)
conventional conditions: pressure (P) ; 10 mbtemperature (T) = 1000"C curve (2)
P = 100 mb; T = 800"C
curve (3) P = 1 bar ; T = 700"C.
According to the present invention, the aerogel may be a self-supported block or be formed in the pores of porous materials, such as polycrystalline graphites, foams, fibrous substrates (felts, carbon fibre/carbon matrix composites etc.) for example.
In this latter case, the porous material is impregnated with the liquid mixture which forms the silica gel and the solvent of the mixture subsequently removed under hypercritical conditions: the pores of the material are then filled with aerogel. The resulting material is densified well by carbon CDVP.
According to another variant of the present invention, the composition of the porous material may be created in the liquid mixture which forms the silica gel, the solvent being subsequently removed under hypercritical conditions.
This is, for example, the case with certain fibrous substrates which may be formed in the liquid mixture which produces the silica gel by placing loose fibres therein or stacking deposits of fibres or fabrics therein, filtering the excess of liquid to densify in fibres and subsequently removing the solvent under hypercritical conditions. A fibrous substrate impregnated with aerogel is thus obtained.
Like the preceding material, this substrate is densified well by carbon CDVP.
A last variant according to the present invention consists of carrying out the carbon CDVP on a silica aerogel containing carbon black. The carbon black is obtained by dispersing particles of carbon black in the liquid mixture which forms the silica gel and forming the silica gel by removing the solvent under hypercritical conditions.
During this latter operation, the particles of carbon black are maintained in place by the silica gel thereby producing a homogeneous distribution of carbon black.
As in the preceding case, this silica gel which contains the carbon black may be a self-supported block or may be formed in the pores of the porous materials.
In all cases it can be seen that the silica does not react during the CDVP and that the pores are completely filled.
The materials which are ultimately obtained are highly densified, enable load and calories to be transferred in an excellent manner, have very good oxidation-resistance and good waterproofing.
In many cases they may be used as such, nevertheless, for certain uses, the presence of silica may be disadvantageous. Should this be the case, it may be removed by heat treatment at 2.700 C or even better by heat treatment at 2,8000C under chlorine. These treatments do not substantially modify the texture and structure of the carbon.
Moreover it should be noted that after these treatments, the pores created by removing the silica may be filled, by carrying out a CDVP of the final carbon.
The following Examples illustrate the present invention but do not limit the scope thereof.
Example 1
A self-supported silica aerogel tube, 100/80 mm in diameter and 100 mm in height, is obtained by hydrolysing a methyl orthosilicate diluted in an aqueous solution of methanol and removing the methanol under hypercritical conditions at a (temperature of more than 240"C and at a pressure of more than 78 bars).
The density of this block is 0.2.
A carbon CDVP is carried out by cracking the methane at a pressure of 1 bar, at 700"C.
After about 1100 hours, a carbon-containing material is obtained which has a density of 1.6, the oxidation-resistance properties of which are similar to those of vitrious carbon.
Example 2 Atridirectional carbon fibre substrate having a density of 0.7 is impregnated with a silica aerogel by placing it in an aqueous methanol solution containing a methyl orthosilicate, hydrolysing the latter to form the silica gel and removing the methanol under hypercritical conditions.
This substrate which has been impregnated with aerogel then undergoes a carbon CDVP under the following conditions;
gas used: methane
temperature: 700"C pressure: 1 bar
After 400 hours, a material is obtained which has a density of 1.7.
By way of comparison, Figure 3 shows, as a function of time, the densification of this same substrate:
- without any preliminary impregnation before the CDVP (curve 1) under conventional conditions,
-with preliminary impregnation with acetylene black which has been simply dried (curve 2),
- with preliminary impregnation with aerocarbon (curve 3) and
- with preliminary impregnation with aerogel according to the present invention (curve 4).
It can be seen that, without preliminary impregnation or with impregnation with acetylene black, the densification is limited to 1.5 after about 1000 hours, whereas a density of 1.7 is obtained after a relatively short period of time (400 hours) with preliminary impregnation with aerogel, this showing the great interest in the process according to the present invention.
Figure 4 shows a micrograph of the material obtained according to this Example. It can be seen that the empty octets of the 3D are all completely filled with aerogel and pyrocarbon.
If a carbon CDVP is used:
- without preliminary impregnation these octets are empty,
- with preliminary impregnation with acetylene black which has been simply dried, there are small piles of densified black,
- with preliminary impregnation with aerocarbon, the octets are to a greater or lesser extent.
It can also be seen in Figure 4 that there is virtually no discontinuity between the fibres and the aerogel and that the load and calories can be transferred equally well from one strand to another when used under stress at elevated temperature.
The materials which are obtained according to this Example may have numerous uses and particularly for the production of nozzles.
Example 3
A carbon felt having a density of 0.3 is impregnated with aerogel in the same manner as the fibrous 3D substrate of the preceding Example, and then undergoes a carbon CDVP under the same conditions as those specified in the preceding Example.
After a period of 350 hours, the density of the felt is 1.7 whereas 600 hours are necessary to obtain this same density without preliminary impregnation with aerogel (the CDVP is effected at 1,000 C under a pressure of 10 mbars).
Figures 5 and 6 are micrographs of carbon felt which has been densified by CDVP under the above-specified conditions, with and without preliminary impregnation with aerogel respectively. Figure 5 shows a submicronic carbon isotrope without any particular deposit on the fibres. Figure 6 shows the usual aspect of a carbon-carbon composite.
The material which is obtained according to this Example has many uses and, particularly in the production of brakes and nozzles.
Example 4
Polycrystalline graphite is impregnated with a silica aerogel in the same manner as the materials in
Examples 2 and 3, and then undergoes a carbon CDVP under the same conditions as those used in these
Examples.
The material which is finally obtained has improved oxidation-resistance and tightness.
This material also has numerous uses, particularly in the production of elements for chemical engineering.
In general the process according to the present invention enables materials having markedly improved resistance to ablation and oxidation and elevated density to be obtained which are unobtainable by conventional densification methods. High pressure-high temperature impregnation (1000 bars; 1000"C) alone enables elevated densities to be attained, at the price of a very substantial investment and even then only for pieces with restricted limited dimensions.
It should be noted that the process according to the present invention
1) may be repeated several times on a porous material to correct possible defects,
2) may be used to perfect the densification of porous materials which have already been partially densified to a greater or lesser extent by other processes, such as the formation of aerocarbon and/or CDVP.
Claims (11)
1. A process for the production of carbon-containing materials having ultrafine grains consisting of a chemical deposition in the vapour phase of carbon, characterised in that the chemical deposition in the vapour phase of carbon is completely or partially carried out on a silica aerogel.
2. A process according to claim 1, characterised in that the silica aerogel contains carbon black.
3. A process according to claim 1 or claim 2, characterised in that the silica gel is a self-supported block.
4. A process according to claim 1 or claim 2, characterised in that the silica gel is formed in the pores of porous materials.
5. A process according to claim 4, characterised in that the porous material is a carbon foam, a polycrystalline graphite or a carbon fibre-based substrate.
6. A process according to claim 5, characterised in that the carbon fibre-based substrate is a 3D.
7. A process according to claim 5, characterised in that the carbon fibre-based substrate is a felt.
8. A process according to claim 1 or claim 2, characterised in that a carbon fibre substrate is formed in the liquid mixture which forms the aerogel and which subsequently produces it.
9. A process according to any one of the preceding claims, characterised in that the chemical deposition in the vapour phase of carbon is carried out at a more elevated pressure and at a lower temperature than those conventionally used.
10. Carbon-containing materials having ultrafine grains characterised in that they are produced according to any one of the preceding claims.
11. A process for the production of carbon-containing materials substantially as herein described with reference to any one of the specific examples.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8309864A FR2548174B1 (en) | 1983-06-15 | 1983-06-15 | PROCESS FOR OBTAINING CARBON MATERIALS COMPRISING ULTRA-FINE GRAINS |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8414925D0 GB8414925D0 (en) | 1984-07-18 |
GB2141418A true GB2141418A (en) | 1984-12-19 |
GB2141418B GB2141418B (en) | 1986-11-12 |
Family
ID=9289791
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08414925A Expired GB2141418B (en) | 1983-06-15 | 1984-06-12 | A process for the production of carbon-containing materials having ultrafine grains |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE3422388A1 (en) |
FR (1) | FR2548174B1 (en) |
GB (1) | GB2141418B (en) |
IT (1) | IT1180180B (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5306555A (en) * | 1991-09-18 | 1994-04-26 | Battelle Memorial Institute | Aerogel matrix composites |
US5855953A (en) * | 1994-03-31 | 1999-01-05 | The Regents, University Of California | Aerogel composites and method of manufacture |
US6004436A (en) * | 1996-08-16 | 1999-12-21 | The Regents Of The University Of California | Processes for the chemical modification of inorganic aerogels |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115448747A (en) * | 2022-08-30 | 2022-12-09 | 易高环保能源科技(张家港)有限公司 | Graphite fiber composite foam carbon and preparation method thereof |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB692303A (en) * | 1949-03-30 | 1953-06-03 | Theodore Raphael Palumbo | Improvements in or relating to electric resistors and method of manufacturing same |
US2859139A (en) * | 1954-12-07 | 1958-11-04 | Union Carbide Corp | Method of making a silica containing carbon brush and resulting article |
FR1148280A (en) * | 1955-04-30 | 1957-12-05 | Kuehnle Ag | Process for sealing the pores of sintered graphite objects and objects conforming to those obtained |
FR1286599A (en) * | 1960-04-26 | 1962-03-02 | Atomic Energy Authority Uk | Manufacturing process of carbon-impregnated shaped articles |
FR2512441B1 (en) * | 1981-09-10 | 1985-10-25 | Lorraine Carbone | PROCESS FOR THE MANUFACTURE OF LOW DENSITY CARBON WITH HOMOGENEOUS ULTRAFINE POROSITY |
-
1983
- 1983-06-15 FR FR8309864A patent/FR2548174B1/en not_active Expired
-
1984
- 1984-06-08 IT IT21311/84A patent/IT1180180B/en active
- 1984-06-12 GB GB08414925A patent/GB2141418B/en not_active Expired
- 1984-06-15 DE DE19843422388 patent/DE3422388A1/en active Granted
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5306555A (en) * | 1991-09-18 | 1994-04-26 | Battelle Memorial Institute | Aerogel matrix composites |
US5855953A (en) * | 1994-03-31 | 1999-01-05 | The Regents, University Of California | Aerogel composites and method of manufacture |
US5879744A (en) * | 1994-03-31 | 1999-03-09 | The Regents Of The University Of California | Method of manufacturing aerogel composites |
US6004436A (en) * | 1996-08-16 | 1999-12-21 | The Regents Of The University Of California | Processes for the chemical modification of inorganic aerogels |
Also Published As
Publication number | Publication date |
---|---|
IT8421311A0 (en) | 1984-06-08 |
FR2548174B1 (en) | 1985-10-25 |
GB2141418B (en) | 1986-11-12 |
IT1180180B (en) | 1987-09-23 |
DE3422388C2 (en) | 1987-09-10 |
FR2548174A1 (en) | 1985-01-04 |
GB8414925D0 (en) | 1984-07-18 |
DE3422388A1 (en) | 1984-12-20 |
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