发明名称 Launched air vehicle system
摘要 <p>A launch canister for ejection from a submerged launch platform, the launch canister being adapted for ejection in a direction substantially along a first axis of the launch canister and comprising: an enclosure for carrying a UAV; a nose cap releasably located in a launch opening at a forward end of the launch canister; a launch mechanism for driving a UAV carried in the enclosure out of the launch canister through the launch opening in a direction substantially along said first axis; and a water surface sensor for detecting when the nose cap of the canister broaches the surface of the water; wherein the launch canister is configured to, on the water surface sensor detecting that the nose cap of the canister has broached the surface of the water, immediately release the nose cap and initiate the launch mechanism to drive a UAV carried in the enclosure out of the launch canister through the launch opening.</p>
申请公布号 GB2514770(B) 申请公布日期 2015.08.05
申请号 GB20130009841 申请日期 2013.06.03
申请人 LOCKHEED MARTIN CORPORATION 发明人 THOMAS WILLIAM SMOKER
分类号 F41F3/07;B63G8/28;B63G8/30 主分类号 F41F3/07
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