发明名称 Pneumatically actuated control surface for airframe body
摘要 A projectile may include a body having an external surface, a stagnation port on the external surface, and a cavity. A spoiler may be translatable in the cavity between a retracted position, wherein the spoiler is substantially completely disposed in the cavity, and an extended position, wherein the spoiler projects from the external surface of the body. A pair of ports may be formed in the walls of the cavity. The pair of ports may be selectively fluidly communicable with the stagnation port. The spoiler may be translatable by pressurizing one of the pair of ports with compressed air and venting the other of the pair of ports. In the extended position, the spoiler may disturb an airstream around the projectile to induce a guidance maneuver for the projectile.
申请公布号 US8525090(B1) 申请公布日期 2013.09.03
申请号 US20100821315 申请日期 2010.06.23
申请人 CAHAYLA JASON R.;THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY 发明人 CAHAYLA JASON R.
分类号 F42B15/01 主分类号 F42B15/01
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