发明名称 WING SLOT SEAL
摘要 A low cost, lightweight frangible wing slot seal can be applied to a guidance wing slot of a folding fin aerial rocket or missile, providing a barrier against exposure of internal missile components to external contaminants, while allowing unhindered deployment of missile guidance wings simply by bursting through the seals. The simple design is nearly foolproof, and has no impact the likelihood of weapon failure. The seal is a flexible sheet which is sufficiently thin so as not to exceed the required volume envelope of the missile. The sheet includes a burst seam, which is breached when impacted by the leading edge of a deploying wing. No additional wing deployment force is required, and after deployment the seal has minimal impact on the aerodynamic performance of the wing.
申请公布号 EP2556327(B1) 申请公布日期 2016.06.08
申请号 EP20110801286 申请日期 2011.04.07
申请人 BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. 发明人 BARRY, WILLIAM, D.;WINKLER, ROBERT;FRANZINI, JOHN R.;CLEVELAND, KENNETH, D.;BUTLAND, ADAM
分类号 F42B10/18;F42B10/12;F42B10/14;F42B39/00 主分类号 F42B10/18
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