发明名称 Method of and apparatus for fabricating a tool to form an asymmetrical constant cross section bore in the propellant in a solid rocket motor
摘要 An elongated flexible bag is fitted inside templates that have aligned openings therein corresponding in shape to that desired for a solid rocket motor propellant bore. With the bottom sealed, the bag is filled with a multiplicity of solid pieces each having a cross section substantially less than that of the bag. When filled, suction is applied to the bag by a vacuum needle to exhaust air therefrom until the bag is very tight on the solid pieces contained therein. The vacuum needle is then withdrawn, the hole made thereby is sealed, and the templates are removed from the bag. After use in loading a solid rocket motor with propellant, the bag is cut open, the solid pieces are removed, and the bag is peeled out of the bore in the propellant.
申请公布号 US4766799(A) 申请公布日期 1988.08.30
申请号 US19870087539 申请日期 1987.08.20
申请人 MORTON THIOKOL, INC. 发明人 OLLIFF, MARTIN T.
分类号 C06B21/00;F02K9/24;(IPC1-7):F42B33/00 主分类号 C06B21/00
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