US2021115597A1PendingUtilityA1
Carbon fiber and method of producing same
Est. expiryJun 18, 2038(~11.9 yrs left)· nominal 20-yr term from priority
D01F 6/18D01F 9/22D01F 6/38D01F 9/225
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Claims
Abstract
A carbon fiber having a strand elastic modulus of 360 GPa or more, a strand strength of 3.5 GPa or more, and a single-fiber diameter of 6.0 μm or more, and having a residual twist count of 2 turns/m or more in a test in which one end is fixed end and another end is free end which is capable of rotation about the axis of a fiber bundle.
Claims
exact text as granted — not AI-modified1 - 22 . (canceled)
23 . A carbon fiber having a strand elastic modulus of 360 GPa or more, a strand strength of 3.5 GPa or more, and a single-fiber diameter of 6.0 μm or more, and having a residual twist count of 2 turns/m or more in a test in which one end is fixed end and another end is free end which is capable of rotation about the axis of a fiber bundle.
24 . The carbon fiber as set forth in claim 23 , meeting the relationship represented by formula (1), wherein Es (GPa) is the single-fiber elastic modulus and A (N) is the loop fracture load:
A≥− 0.0017× Es+ 1.02 (1).
25 . The carbon fiber as set forth in claim 23 , having a single-fiber diameter of 6.0 μm or more, satisfying the relationship represented by formula (2) wherein E (GPa) is the strand elastic modulus and B (MPa) is the knot strength determined under conditions where the heat loss rate is 0.15% or less at 450° C., and having a twist count of 20 to 80 turns/m:
B≥ 6.7×10 9 ×E −2.85 (2).
26 . The carbon fiber as set forth in claim 23 , wherein the total fineness is 850 g/km.
27 . The carbon fiber as set forth in claim 23 , wherein the strand elastic modulus is 440 GPa or more.
28 . The carbon fiber as set forth in claim 23 , wherein the twist angle of the carbon fiber bundle surface layer is 2.0° to 30.5°.
29 . The carbon fiber as set forth in claim 28 , wherein the twist angle of the carbon fiber bundle surface layer is 4.8° to 10.0°.
30 . The carbon fiber as set forth in claim 23 , wherein the single-fiber diameter is 6.5 μm or more.
31 . The carbon fiber as set forth in claim 23 , wherein single-fiber diameter is 7.4 μm or less.
32 . The carbon fiber as set forth in claim 23 , wherein the crystallite size Lc (nm) and the orientation parameter of crystallites π 002 (%) satisfy the relationship represented by formula (3):
π 002 ≥4.0× Lc+ 73.2 (3).
33 . The carbon fiber as set forth in claim 23 , wherein the crystallite size Lc is 2.2 to 3.5 nm.
34 . The carbon fiber as set forth in claim 23 , wherein the strand elastic modulus E (GPa) and the crystallite size Lc (nm) satisfy the relationship represented by formula (4):
E×Lc −0.5 ≥200 (GPa/nm 0.5 ) (4).
35 . The carbon fiber as set forth in claim 23 , wherein the surface oxygen concentration O/C is 0.05 to 0.50.
36 . The carbon fiber bundle as set forth in claim 23 , wherein the filament number is 10,000 or more.
37 . A carbon fiber meeting the relationship represented by formula (1) wherein Es (GPa) is the single-fiber elastic modulus and A (N) is the loop fracture load:
A≥− 0.0017× Es+ 1.02 (1).
38 . A carbon fiber having a single-fiber diameter of 6.0 μm or more, satisfying the relationship represented by formula (2) wherein E (GPa) is the strand elastic modulus and B (MPa) is the knot strength determined under conditions where the heat loss rate is 0.15% or less at 450° C., and having a twist count of 5 to 80 turns/m:
B≥ 6.7×10 9 ×E −2.81 (2).
39 . The carbon fiber as set forth in claim 37 , wherein either the single-fiber elastic modulus or the strand elastic modulus is 360 GPa or more.
40 . A method of producing a carbon fiber comprising:
a step in which a precursor fiber bundle for carbon fiber is subjected to stabilization (oxidation) treatment in an air atmosphere in the temperature range of 200° C. to 300° C.; a step of pre-carbonization in which the resulting stabilized fiber (oxidized fiber) bundle is heat-treated in an inert atmosphere at or below a maximum temperature of 500° C. to 1,000° C. until the density reaches 1.5 to 1.8 g/cm 3 ; and a step of carbonization in which the resulting pre-carbonized fiber bundle is heat-treated in an inert atmosphere, the precursor fiber bundle for carbon fiber having a single-fiber fineness of 0.9 dtex or more, having a tension controlled at 5 mN/dtex or more during the carbonization treatment, meeting either (c) or (d), and having a strand elastic modulus of 360 GPa or more:
(c) the fiber bundle to be subjected to the carbonization treatment has a twist count of 2 turns/m or more, and
(d) the total fineness, which is the product of the single fiber fineness (g/km) and the filament number (number), of the resulting carbon fiber is 740 g/km or more.
41 . The method as set forth in claim 40 , wherein the fiber bundle to be subjected to carbonization treatment has a twist count of 16 turns/m or more.
42 . The method as set forth in claim 40 , wherein the maximum temperature in the carbonization treatment step is 1,500° C. or more.
43 . The method as set forth in claim 42 , wherein the maximum temperature in the carbonization treatment step is 2,300° C. or more.
44 . The method as set forth in claim 40 , wherein electrolytic surface treatment with an amount of current of 2 to 100 c/g is performed after the carbonization treatment step.
45 . A carbon fiber having a strand elastic modulus of 360 GPa or more, a strand strength of 3.5 GPa or more, a single-fiber diameter of 6.0 μm or more, and a total fineness, which is a product of the single-fiber fineness (g/km) and the filament number (number) of the carbon fiber, of 740 g/km or more, and meeting the relationship represented by formula (1), wherein Es (Gpa) is the single-fiber elastic modulus and A (N) is the loop fracture load:
A≥− 0.0017× Es+ 1.02 (1).
46 . A carbon fiber having a strand elastic modulus of 360 GPa or more, a strand strength of 3.5 GPa or more, a single-fiber diameter of 6.0 μm or more, and a total fineness, which is a product of the single-fiber fineness (g/km) and the filament number (number) of the carbon fiber, of 740 g/km or more, satisfying the relationship represented by formula (2) wherein E (GPa) is the strand elastic modulus and B (MPa) is the knot strength determined under conditions where the heat loss rate is 0.15% or less at 450° C., and having a twist count of 20 to 80 turns/m:
B≥ 6.7×10 9 ×E −2.85 (2).
47 . A carbon fiber having a strand elastic modulus of 360 GPa or more, a strand strength of 3.5 GPa or more, a single-fiber diameter of 6.0 μm or more, and a total fineness, which is a product of the single-fiber fineness (g/km) and the filament number (number) of the carbon fiber, of 740 g/km or more, wherein the twist angle of the carbon fiber bundle surface layer is 2.0° to 30.5°.
48 . A carbon fiber having a strand elastic modulus of 360 GPa or more, a strand strength of 3.5 GPa or more, a single-fiber diameter of 6.0 μm or more, and a total fineness, which is a product of the single-fiber fineness (g/km) and the filament number (number) of the carbon fiber, of 740 g/km or more, wherein the twist angle of the carbon fiber bundle surface layer is 4.8° to 10.0°.
49 . A carbon fiber having a strand elastic modulus of 360 GPa or more, a strand strength of 3.5 GPa or more, a single-fiber diameter of 6.0 μm or more, and a total fineness, which is a product of the single-fiber fineness (g/km) and the filament number (number) of the carbon fiber, of 740 g/km or more, wherein the crystallite size Lc (nm) and the orientation parameter of crystallites π 002 (%) satisfy the relationship represented by formula (3):
π 002 ≥4.0× Lc+ 73.2 (3).
50 . A carbon fiber having a strand elastic modulus of 360 GPa or more, a strand strength of 3.5 GPa or more, a single-fiber diameter of 6.0 μm or more, and a total fineness, which is a product of the single-fiber fineness (g/km) and the filament number (number) of the carbon fiber, of 740 g/km or more, wherein the crystallite size Lc is 2.2 to 3.5 nm.
51 . A carbon fiber having a strand elastic modulus of 360 GPa or more, a strand strength of 3.5 GPa or more, a single-fiber diameter of 6.0 μm or more, and a total fineness, which is a product of the single-fiber fineness (g/km) and the filament number (number) of the carbon fiber, of 740 g/km or more, wherein the strand elastic modulus E (GPa) and the crystallite size Lc (nm) satisfy the relationship represented by formula (4):
E×Lc −0.5 ≥200 (GPa/nm 0.5 ) (4).Join the waitlist — get patent alerts
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