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公开(公告)号：US09851188B2
公开(公告)日：2017-12-26
申请号：US14076791
申请日：2013-11-11
Applicant: General Dynamics-OTS, Inc.
Inventor： Matthew D. Diehl , Eric Michael Schneck , Gregory Norman Bogan
CPC classification number: F42B15/36 , F16L13/06 , F16L35/00 , Y10T403/11
Abstract: A vessel, such as a rocket motor tube, comprised of an insert, and a joint that allows the insert to decouple from the vessel to relieve pressure when subjected to excessive temperatures and/or a predetermined temperature or temperature range.
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公开(公告)号：US20140284913A1
公开(公告)日：2014-09-25
申请号：US14076720
申请日：2013-11-11
Applicant: General Dynamics-OTS, Inc.
Inventor： Matthew D. Diehl , Eric Michael Schneck , Gregory Norman Bogan
IPC: F42B15/34
CPC classification number: F42B15/36 , F16L13/06 , F16L35/00 , Y10T403/11
Abstract: A vessel, such as a rocket motor tube, comprised of an insert, and a joint that allows the insert to decouple from the vessel to relieve pressure when subjected to excessive temperatures and/or a predetermined temperature or temperature range.
Abstract translation: 诸如火箭发动机管的容器，包括插入件和接头，其允许插入件在经受过度温度和/或预定温度或温度范围时与容器脱离以释放压力。
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公开(公告)号：US08919254B2
公开(公告)日：2014-12-30
申请号：US14076720
申请日：2013-11-11
Applicant: General Dynamics-OTS, Inc.
Inventor： Matthew D. Diehl , Eric Michael Schneck , Gregory Norman Bogan
CPC classification number: F42B15/36 , F16L13/06 , F16L35/00 , Y10T403/11
Abstract: A vessel, such as a rocket motor tube, comprised of an insert, and a joint that allows the insert to decouple from the vessel to relieve pressure when subjected to excessive temperatures and/or a predetermined temperature or temperature range.
Abstract translation: 诸如火箭发动机管的容器，包括插入件和接头，其允许插入件在经受过度温度和/或预定温度或温度范围时与容器脱离以释放压力。
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公开(公告)号：US20140306443A1
公开(公告)日：2014-10-16
申请号：US14076791
申请日：2013-11-11
Applicant: General Dynamics-OTS, Inc.
Inventor： Matthew D. Diehl , Eric Michael Schneck , Gregory Norman Bogan
IPC: F16L13/06
CPC classification number: F42B15/36 , F16L13/06 , F16L35/00 , Y10T403/11
Abstract: A vessel, such as a rocket motor tube, comprised of an insert, and a joint that allows the insert to decouple from the vessel to relieve pressure when subjected to excessive temperatures and/or a predetermined temperature or temperature range.
Abstract translation: 诸如火箭发动机管的容器，包括插入件和接头，其允许插入件在经受过度温度和/或预定温度或温度范围时与容器脱离以释放压力。
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