US2006078730A1PendingUtilityA1
Carbon fibrous structure
Assignee: BUSSAN NANOTECH RES INST INCPriority: Aug 31, 2004Filed: Jun 8, 2005Published: Apr 13, 2006
Est. expiryAug 31, 2024(expired)· nominal 20-yr term from priority
Y10T428/2918C01B 2202/36C01B 32/162Y10S977/752C01B 32/05B82Y 30/00Y10T428/2913D01F 9/127B82Y 40/00Y10S977/843
40
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Claims
Abstract
The present invention provides a carbon fibrous structure comprising a three dimensional network of carbon fibers, said carbon fibers each having an outside diameter of 15-100 nm, and said fibrous structure comprising a granular part with which said carbon fibers are bound in a state that said carbon fibers extend outwardly from the granular part, the granular part being produced in a growth process of the carbon fibers, and a method for making the same.
Claims
exact text as granted — not AI-modified1 . A carbon fibrous structure comprising a three dimensional network of carbon fibers, said carbon fibers each having an outside diameter of 15-100 nm, and said fibrous structure comprising a granular part with which said carbon fibers are bound in a state that said carbon fibers extend outwardly from the granular part, the granular part being produced in a growth process of the carbon fibers.
2 . The carbon fibrous structure according to claim 1 , wherein said carbon fibrous structure has an area based circle-equivalent mean diameter of 50-100 μm.
3 . The carbon fibrous structure according to claim 2 , wherein said carbon fibrous structure has a bulk density of 0.0001-0.05 g/cm 3 .
4 . The carbon fibrous structure according to claim 3 , wherein said carbon fibrous structure has a bulk density of 0.001-0.02 g/cm 3 .
5 . The carbon fibrous structure according to claim 4 , wherein I D /I G of said carbon fibrous structure determined by Raman spectroscopy is not more than 0.2, wherein I D is peak intensity at 1360 cm −1 and I G is peak intensity at 1580 cm −1 .
6 . The carbon fibrous structure according to claim 5 , wherein I D /I G of said carbon fibrous structure determined by Raman spectroscopy is not more than 0.1.
7 . The carbon fibrous structure according to claim 6 , wherein said carbon fibrous structure has a combustion initiation temperature in air of not less than 750° C.
8 . The carbon fibrous structure according to claim 7 , wherein a diameter of the granular particle part is larger than individual outside diameters of the carbon fibers.
9 . The carbon fibrous structure according to claim 8 , wherein the carbon fibers are produced using as carbon sources at least two carbon compounds which have different decomposition temperatures.
10 . The carbon fibrous structure according to claim 2 , wherein I D /I G of said carbon fibrous structure determined by Raman spectroscopy is not more than 0.2, wherein I D is peak intensity at 1360 cm −1 and I G is peak intensity at 1580 cm −1 .
11 . The carbon fibrous structure according to claim 10 , wherein I D /I G of said carbon fibrous structure determined by Raman spectroscopy is not more than 0.1.
12 . The carbon fibrous structure according to claim 11 , wherein said carbon fibrous structure has a combustion initiation temperature in air of not less than 750° C.
13 . The carbon fibrous structure according to claim 12 , wherein a diameter of the granular particle part is larger than individual outside diameters of the carbon fibers.
14 . The carbon fibrous structure according to claim 13 , wherein the carbon fibers are produced using as carbon sources at least two carbon compounds which have different decomposition temperatures.
15 . The carbon fibrous structure according to claim 1 , wherein said carbon fibrous structure has a bulk density of 0.0001-0.05 g/cm 3 .
16 . The carbon fibrous structure according to claim 15 , wherein said carbon fibrous structure has a bulk density of 0.001-0.02 g/cm 3 .
17 . The carbon fibrous structure according to claim 16 , wherein I D /I G of said carbon fibrous structure determined by Raman spectroscopy is not more than 0.2, wherein I D is peak intensity at 1360 cm −1 and I G is peak intensity at 1580 cm −1 .
18 . The carbon fibrous structure according to claim 17 , wherein I D /I G of said carbon fibrous structure determined by Raman spectroscopy is not more than 0.1.
19 . The carbon fibrous structure according to claim 18 , wherein said carbon fibrous structure has a combustion initiation temperature in air of not less than 750° C.
20 . The carbon fibrous structure according to claim 19 , wherein a diameter of the granular particle part is larger than individual outside diameters of the carbon fibers.
21 . The carbon fibrous structure according to claim 20 , wherein the carbon fibers are produced using as carbon sources at least two carbon compounds which have different decomposition temperatures.
22 . The carbon fibrous structure according to claim 15 , wherein I D /I G of said carbon fibrous structure determined by Raman spectroscopy is not more than 0.2, wherein I D is peak intensity at 1360 cm −1 and I G is peak intensity at 1580 cm −1 .
23 . The carbon fibrous structure according to claim 22 , wherein I D /I G of said carbon fibrous structure determined by Raman spectroscopy is not more than 0.1.
24 . The carbon fibrous structure according to claim 23 , wherein said carbon fibrous structure has a combustion initiation temperature in air of not less than 750° C.
25 . The carbon fibrous structure according to claim 24 , wherein a diameter of the granular particle part is larger than individual outside diameters of the carbon fibers.
26 . The carbon fibrous structure according to claim 25 , wherein the carbon fibers are produced using as carbon sources at least two carbon compounds which have different decomposition temperatures.
27 . The carbon fibrous structure according to claim 1 , wherein I D /I G of said carbon fibrous structure determined by Raman spectroscopy is not more than 0.2, wherein I D is peak intensity at 1360 cm −1 and I G is peak intensity at 1580 cm −1 .
28 . The carbon fibrous structure according to claim 27 , wherein I D /I G of said carbon fibrous structure determined by Raman spectroscopy is not more than 0.1.
29 . The carbon fibrous structure according to claim 28 , wherein said carbon fibrous structure has a combustion initiation temperature in air of not less than 750° C.
30 . The carbon fibrous structure according to claim 29 , wherein a diameter of the granular particle part is larger than individual outside diameters of the carbon fibers.
31 . The carbon fibrous structure according to claim 30 , wherein the carbon fibers are produced using as carbon sources at least two carbon compounds which have different decomposition temperatures.
32 . The carbon fibrous structure according to claim 1 , wherein said carbon fibrous structure has a combustion initiation temperature in air of not less than 750° C.
33 . The carbon fibrous structure according to claim 32 , wherein a diameter of the granular particle part is larger than individual outside diameters of the carbon fibers.
34 . The carbon fibrous structure according to claim 33 , wherein the carbon fibers are produced using as carbon sources at least two carbon compounds which have different decomposition temperatures.
35 . The carbon fibrous structure according to claim 1 , wherein a diameter of the granular particle part is larger than individual outside diameters of the carbon fibers.
36 . The carbon fibrous structure according to claim 35 , wherein the carbon fibers are produced using as carbon sources at least two carbon compounds which have different decomposition temperature.
37 . The carbon fibrous structure according to claim 1 , wherein the carbon fibers are produced using as carbon sources at least two carbon compounds which have different decomposition temperature.
38 . A method for forming a carbon fibrous structure having a granular core to which a plurality of carbon fibers are attached, the method comprising:
heating a mixture of a carbon source and a catalyst at a constant temperature in a range of 800-1300° C. to produce a first intermediate, wherein the carbon source comprises at least two carbon compounds having different decomposition temperatures or the carbon source comprises a carbon compound that can produce, in the heating, at least two carbon components having different decompositions temperatures; heating the first intermediate at a constant temperature in a range of 800-1200° C. to produce a second intermediate; and heating the second intermediate at a constant temperature in a range of 2400-3000° C. to produce the carbon fibrous structure.Cited by (0)
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