Method for producing a molded body
09926237 ยท 2018-03-27
Assignee
Inventors
- Jeremias Schoenfeld (Huettenberg, DE)
- Roland Weiss (Huettenberg, DE)
- Gotthard NAUDITT (Huettenberg, DE)
Cpc classification
C04B35/524
CHEMISTRY; METALLURGY
C04B35/573
CHEMISTRY; METALLURGY
C04B2235/616
CHEMISTRY; METALLURGY
F23D14/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01F25/43161
PERFORMING OPERATIONS; TRANSPORTING
C04B2235/6026
CHEMISTRY; METALLURGY
C04B35/80
CHEMISTRY; METALLURGY
F23D2212/105
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C04B35/571
CHEMISTRY; METALLURGY
F23D2213/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C04B2235/614
CHEMISTRY; METALLURGY
H05B3/148
ELECTRICITY
C04B2235/483
CHEMISTRY; METALLURGY
C04B2235/5445
CHEMISTRY; METALLURGY
C04B2235/5436
CHEMISTRY; METALLURGY
C04B2235/80
CHEMISTRY; METALLURGY
International classification
B29C63/02
PERFORMING OPERATIONS; TRANSPORTING
C04B35/80
CHEMISTRY; METALLURGY
C04B35/573
CHEMISTRY; METALLURGY
C04B35/524
CHEMISTRY; METALLURGY
C04B35/571
CHEMISTRY; METALLURGY
F23D14/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The invention relates to a method for producing a molded body, having a silicon carbide support matrix and an integral carbon structure, wherein a base body on the basis of a powder mixture containing silicon carbide or silicon and carbon and of a binder is built in layers in a generative method, and wherein a pyrolysis of the base body is effected for realizing the molded body after the binder has been cured, wherein the carbon content of the carbon structure is adjusted by way of the pyrolysis of the binder and by way of the carbon content of the powder mixture or infiltration of a carbon material into the silicon carbide support matrix.
Claims
1. A method for producing a molded body having a silicon carbide support matrix and an integral carbon structure, said method comprising: building a layered base body using a generative method from a powder mixture containing carbon, a binder, and at least one of silicon and silicon carbide; curing the binder; and pyrolyzing the base body including the binder after the binder has been cured to form the molded body, said pyrolyzing forming a silicon carbide support matrix and an integral carbon structure, wherein a carbon content of the carbon structure is defined by a free carbon in its entirety and is adjusted by way of the pyrolysis of the binder and by way of the carbon content of the powder mixture or infiltration of a carbon material into the silicon carbide support matrix.
2. The method according to claim 1, in which the powder mixture presents a carbon content between 0 and 30% by weight.
3. The method according to claim 2, in which the powder mixture presents a carbon content between 10 and 20% by weight.
4. The method according to claim 1, in which the powder mixture presents an SiC particle fraction having particles of an average grain size D.sub.s50 between 0.5 and 100 m.
5. The method according to claim 4, in which the average grain size D.sub.s50 is between 2 and 60 m.
6. The method according to claim 5, in which the average grain size D.sub.s50 is between 3 and 10 m.
7. The method according to claim 1, in which for adjusting the carbon content of the molded body, following the pyrolysis of the base body, the infiltration of the silicon carbide support matrix with a polymer is effected, said polymer being transformed into carbon with the aid of a following pyrolysis.
8. The method according to claim 7, in which the polymer comprises a polymer containing silicon or silicon carbide.
9. The method according to claim 7, in which prepolymers are used as the polymer.
10. The method of claim 9, wherein the prepolymers are selected from the group consisting polyimides, and cyanate ester resins.
11. The method according to claim 7, in which phenolic resins, furan resins, cyanate ester resins are used as the polymer.
12. The method of claim 7, wherein the polymers are selected from the group consisting of siloxanes, silazanes, carbosiloxanes, carbosilazanes, and carbosilanes.
13. The method according to claim 1, in which an infiltration of the silicon carbide support matrix with silicon is effected following the pyrolysis.
14. The method according to claim 1, in which an infiltration of the silicon carbide support matrix with silicon carbide is effected following the pyrolysis.
15. The method according to claim 14, in which the infiltration of the silicon carbide support matrix with silicon carbide is effected by way of vapor deposition of silicon carbide.
16. The method according to claim 15, in which the vapor deposition of silicon carbide is effected in a CVI method or CVD method.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) In the figures:
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
DETAILED DESCRIPTION OF THE EXAMPLE EMBODIMENTS
(10)
(11) In a central area 17 of the molded body 22, the slits 12 and 13 in each instance run helically in the longitudinal direction along the circumference of the tube wall 11 up to an upper end 18 of the resistance heating element. The slits 12 and 13 in this way form two heating coils 19 and 20, which are linked to each other at their upper end in an annular portion 32. The resistance heating element is heated during operation substantially in the area of the heating coils 19 and 20. The resistance heating element is realized in one piece and substantially consists of silicon carbide and carbon.
(12)
(13) In
(14)
(15)
(16)
(17) Finally, a coating with silicon carbide particles 28 is effected with the CVD method for realizing the silicon carbide coating 26 being illustrated in
(18)
(19) The molded body 40 being realized as a static mixer presents a three-dimensional lattice structure 45, which is formed from interlaced material crosspieces 46, 47 of the molded body 40. Here, as
(20) By way of example,
(21) The method being illustrated in
(22) The result of the pyrolysis is a mechanically stable molded body 22, 40, whose proportion of free carbon for realizing a carbon structure is determined by the composition of the powder mixture 50 or by a residue proportion of free carbon remaining after a reactive firing of silicon and carbon.
(23) Any free carbon proportions which might have remained at the surface of the molded body 22, 40, and which are not present in an encapsulated form in the silicon carbide support matrix, can be transformed, after an infiltration with silicon, into silicon carbide in a subsequent reactive firing that might be carried out in a further furnace working.
(24) In order to preclude that there is any free silicon in the silicon carbide support matrix or at the surface of the molded body after the reactive firing, in a further furnace working, the free silicon can be evaporated in a vacuum atmosphere.