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Title: US5916633: Fabrication of carbon/carbon composites by forced flow-thermal gradient chemical vapor infiltration
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Country: US United States of America

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36 pages

 
Inventor: Lackey, Walter Jackson; Marietta, GA
Vaidyaraman, Sundar; Atlanta, GA

Assignee: Georgia Tech Research Corporation, Atlanta, GA
other patents from GEORGIA TECH RESEARCH CORP. (221085) (approx. 433)
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Published / Filed: 1999-06-29 / 1995-05-19

Application Number: US1995000445425

IPC Code: Advanced: C04B 35/83; C23C 16/04; C23C 16/26;
Core: more...
IPC-7: C23C 16/26;

ECLA Code: C04B35/83; C23C16/04D; C23C16/26;

U.S. Class: Current: 427/249.3; 427/008; 427/228; 427/249.4; 427/255.24;
Original: 427/249; 427/008; 427/255.1; 427/228;

Field of Search: 427/008,249,255.1,228

Priority Number:
1995-05-19  US1995000445425

Abstract: The fabrication of carbon/carbon composite disks using forced flow-thermal gradient chemical vapor infiltration process using propylene diluted with hydrogen as the reagent is disclosed. The independent variables included concentration of the reagent, total flow rate and preform bottom temperature. The response variables included infiltration time, final porosity, rate of weight gain and deposition rate. The infiltration time and rate of weight gain are affected only by the three independent variables. The densification of the composites is monitored by the back pressure. The composites were cut into slices 1 cm long, 4 mm wide and 2 mm deep to measure the uniformity of densification, which varied very little within a composite. Coating thickness as a function of position increased exponentially from the cold side to the hot side of the composite. The coating thicknesses near the cold side and the hot side are used to calculate the rate constant for the pyrolysis of propylene in the preform. The activation energy is approximately 18.6 Kcal/mol and the rate constant is given by 1n k=8.2--9375.1/T (K)

Attorney, Agent or Firm: Deveau, Colton & Marquis ;

Primary / Asst. Examiners: Beck, Shrive; Meeks, Timothy

Maintenance Status: E2 Expired  Check current status

INPADOC Legal Status: Show legal status actions

Family: None

First Claim:
Show all 25 claims
What is claimed is:     1. A method for fabricating carbon fiber-carbon matrix composites comprising the steps of:
  • a. preparing a preform consisting essentially of multiple layers of carbon cloth;
  • b. placing the preform in a furnace reactor chamber comprising a feed end and a discharge end, wherein said preform approximately conforms in dimension and shape to the inside walls of said furnace reactor chamber;
  • c. establishing a thermal gradient across the preform;
  • d. introducing a process feed gas comprising a carbon source into the furnace reactor chamber through the feed end; and
  • f. establishing a pressure gradient across said preform by maintaining the pressure at the feed end approximately 3.4 kPa or more above the pressure at the discharge end, thereby forcing the process feed gas to flow through the preform resulting in the deposition of carbon from the carbon source within the preform, the pressure at the feed end increasing as the carbon is deposited within the preform.


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Forward References: Show 6 U.S. patent(s) that reference this one

       
U.S. References: Go to Result Set: All U.S. references   |  Forward references (6)   |   Backward references (3)   |   Citation Link

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Patent  Pub.Date  Inventor Assignee   Title
Buy PDF- 8pp US4580524  1986-04 Lackey, Jr. et al.  The United States of America as represented by the United States Department of Energy Process for the preparation of fiber-reinforced ceramic composites by chemical vapor deposition
Buy PDF- 11pp US5348774  1994-09 Golecki et al.  AlliedSignal Inc. Method of rapidly densifying a porous structure
Buy PDF- 27pp US5480678  1996-01 Rudolph et al.  The B. F. Goodrich Company Apparatus for use with CVI/CVD processes
       
Foreign References: None

Other Abstract Info: CHEMABS 131(04)048257Q CHEMABS 131(04)048257Q DERABS C1999-384705 DERABS C1999-384705

Other References:
  • Kimura, et al., High Temp. High Press. 13, 193 (1980) (month unknown).
  • Beaty, R.L. and D.V. Kiplinger, Nucl. Appl. Tech., 8, 488 (1970) (month unknown).
  • Sugiyama, K., and T. Nakamura, J. Mat. Sci. Lett., 6, 331, (1987) (month unknown). (3 pages) Cited by 2 patents
  • Buckley, J.D., and Dan D. Edie, Noyes Publications, Park Ridge, N.J., pp. 111-118, and 211-215 (1993) (month unknown).
  • Lackey, W.J., T.L. Starr, Fiber Reinforced Ceramic Composites, ed. by K.S. Mazdiyansi, 397-449 (Noyes Publications, N.J. 1991) (month unknown).
  • Vaidyaraman, S., W.J. Lackey, G.B. Freeman, P.K. Agrawa, and M.D. Langman, J. Mat. Res., vol. 10, No. 6, Jun., 1995.
  • McAllister, P., J.F. Hendricks and E.E. Wolf, Carbon, 28, 579 (1990) (month unknown). (10 pages)
  • Oh, S.H., and J.Y. Lee, Carbon, 26, 763-769 (1988) (month unknown). (6 pages) Cited by 3 patents
  • Box, G.E.P. and D.R. Cox, J. Royal Stat. Soc. B., 26. 211 (1964) (month unknown).
  • Caputo, A.J., R.A. Lowden and D.P. Stinton, Improvements in the Fabrication of Ceramic-Fiber-Ceramic-Matrix Composites by Chemical Vapor Infiltration, ORNL/TM-9651, Oak Ridge Nat. Lab., Oak Ridge, TN (Jun. 1985).
  • Tesner, P.A., Chemistry and Physics of Carbon, ed. P.A. Thrower, 19, 65 (1983) (month unknown), pp. 66-161.
  • Oh, S.M., and J.Y. Lee, Carbon, 27, 423-430 (1989) (month unknown). (8 pages)
  • Marinkovic, S. and S. Dimitrijevic, Carbon, 23, 691-95 (1985) (month unknown). (9 pages)
  • Savage, G. Carbon-Carbon Composites, Chapman & Hall, N.Y., 1993 (no month).
  • Thomas, C.R. ed., Essentials of Carbon-Carbon Composites, Royal Society of Chemistry, London, 1993. (no month).
  • Oh et al. Carbon, vol. 27, No. 3, pp. 423-430 (1989). (month unknown). (8 pages)
  • Vaidyaraman et al. "Rapid Processing of Carbon-Carbon Composites by Forced-Flow Thermal Gradient Chemical Vapor Infiltration", Materials Research Society Symposium Proceedings, v. 365, 1995, pp. 325-330 (month unknown).
  • Kotlensky, "A Review of CVD Carbon Infiltration of Porous Substrates", Proc. 16th Nat. Symposium of the Soc. of Aerospace Mat. & Proc. Eng., Apr., 1971, pp. 257-265.


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