发明名称 Contemporary composite polar boss
摘要 Composite polar bosses applied in rocket motor cases have very desirable characteristics. The lead time for a boss can be reduced from 6-12 months to 2-3 months. Weight savings for the boss are about 20-40%. A composite polar boss which attaches closures to solid fueled rocket motor cases is disclosed. This polar boss is a carbonized fabrication which sits within a circumferential indentation within the motor case, and has a threaded inner circumference which permits the closure to be attached thereto. The materials of the boss are selected to permit a service temperature of 350 degrees F.
申请公布号 US4807531(A) 申请公布日期 1989.02.28
申请号 US19870109557 申请日期 1987.10.16
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE 发明人 REYNOLDS, HUGH M.;KAWABATA, CURT M.
分类号 F02K9/34;(IPC1-7):F42B4/06 主分类号 F02K9/34
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