公开(公告)号：US5038561A

公开(公告)日：1991-08-13

申请号：US398961

申请日：1989-08-28

Applicant: Michael J. Chase

Inventor： Michael J. Chase

IPC: F02K9/34 ,  F02K9/40 ,  F42B15/34

CPC classification number: F02K9/40 ,  F02K9/346 ,  F42B15/34 ,  Y10S428/902

Abstract: A thermal insulator for a rocket motor body comprises a member adapted to be fitted as a sleeve on the outer surface of the body the member comprising a composite of cork having on its outer surface a layer of fibre reinforced polymeric material wherein a substantial proportion of the fibre reinforcement comprises fibres of low-conducting material.

公开(公告)号：USD495694S1

公开(公告)日：2004-09-07

申请号：US29183397

申请日：2003-06-11

Applicant: Michael J. Chase ,  David Needleman

Designer： Michael J. Chase ,  David Needleman

公开(公告)号：US4104878A

公开(公告)日：1978-08-08

申请号：US750018

申请日：1976-12-13

Applicant: Michael J. Chase

Inventor： Michael J. Chase

IPC: F02K9/28 ,  F02K9/97 ,  F16K17/40 ,  F02K9/04

CPC classification number: F02K9/28 ,  F02K9/978 ,  F16K17/403

Abstract: A plug for closing an opening in a partition between rocket motor chambers is made in segments and will resist a relatively high pressure differential between the chambers in one direction but will unblock the opening in response to a relatively low pressure differential between the chambers in the other direction.

Abstract translation: 用于封闭火箭发动机室之间的隔板中的开口的塞子被制成段，并且将抵抗在一个方向上的室之间的相对较高的压力差，但是响应于另一个室之间的相对较低的压差而解除开口 方向。