发明名称 Method for the production of a combustion chamber for solid propellant rocket motor
摘要 Sectors of tubes are adhesively fixed around a prefabricated propellant, the sectors being juxtaposed edge to edge to constitute a cylindrical tube, and a winding is formed around the tube at least in circumferential direction. The front and rear walls which are equipped with a seating and a tuyere, can be joined to the tubular structure formed by the tube sectors, by adhesive means on the inside of that structure, or as a variant, by means of a helical winding formed simultaneously on the wall and on the tubular structure.
申请公布号 US5032201(A) 申请公布日期 1991.07.16
申请号 US19890346352 申请日期 1989.04.28
申请人 SOCIETE ANONYME: SOCIETE EUROPEENNE DE PROPULSION 发明人 CRAPIZ, DINO
分类号 B21D53/00;F02K9/34 主分类号 B21D53/00
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