发明名称 |
HIGH TEMPERATURE COMPOSITE PROJECTILE BARREL |
摘要 |
A composite projectile barrel is disclosed comprising a polymer matrix composite outer shell that accommodates higher temperature loading. In one embodiment, the invention comprises an outer shell fabricated from carbon fibers and polyimide resin having a glass transition temperature greater than 500° F. In another embodiment, the resin mixture includes a plurality of sizes of aluminum particles, between about 0.1 microns and 10.0 microns in diameter and of approximately spherical shape, as a thermal conductive additive. |
申请公布号 |
US2016209143(A1) |
申请公布日期 |
2016.07.21 |
申请号 |
US201414914694 |
申请日期 |
2014.08.28 |
申请人 |
PROOF RESEARCH, INC. |
发明人 |
Curliss David B.;Lincoln Jason E.;Degerness Michael K. |
分类号 |
F41A21/04 |
主分类号 |
F41A21/04 |
代理机构 |
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代理人 |
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主权项 |
1. A barrel for directing the path of a dischargeable projectile, comprising:
an inner liner defining an axial bore; and an outer shell surrounding and in direct contact with the inner liner, said outer shell fabricated from a polymer matrix composite (PMC), said PMC comprising fibers and a resin mixture, said resin mixture comprising a resin having a glass transition temperature greater than 500° F. |
地址 |
Columbia Falls MT US |