发明名称 Rocket nozzle comprising pyrolytic graphite-silicon carbide inserts
摘要 A method for making said rigid pyrolytic graphite article comprising winding a continuous, individual, refractory filament or strand around a shaped form and simultaneously pyrolyzing a mixture of methyl trichlorosilane and a hydrocarbon gas onto the filament or strand at about the point of winding contact to nucleate pyrolytic graphite and SiC from the filament or strand, winding additional turns of the filament or strand around the form, each additional turn being spaced from previously wound turns and, as each of the additional turns is wound, simultaneously pyrolyzing the mixture of methyl trichlorosilane and hydrocarbon gas thereon at about the point of winding contact and on the codeposited pyrolytic graphite and SiC nucleated from previously wound turns.
申请公布号 US4029844(A) 申请公布日期 1977.06.14
申请号 US19750551470 申请日期 1975.02.20
申请人 ATLANTIC RESEARCH CORPORATION 发明人 OLCOTT, EUGENE L.
分类号 C01B31/00;C04B35/52;C04B35/83;C23C16/22;C23C16/32;(IPC1-7):C23C11/10;C01B31/36;B05D7/20;B32B9/00 主分类号 C01B31/00
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