发明名称 Aerodynamic air foil surfaces for in-flight control for projectiles
摘要 Aerodynamical air foil surface and subsurface expressions and/or impressions of varied geometrics, angles of attack, heights and depths, comprising part of a projectile surface itself to create McClain effect molecular friction/pressure/temperature reaction flight control surfaces which automatically achieve in all fluids and velocities of flight self-stablizing spin and rotation, increased height of trajectory with corresponding enhancement of range and distance, kinetic energies, inducing smooth laminar boundary layer flows, substantially decreasing drag effects, synergistically combined to constitute a major technological improvement in performance of all projectiles.
申请公布号 US4996924(A) 申请公布日期 1991.03.05
申请号 US19890342632 申请日期 1989.04.20
申请人 MCCLAIN, HARRY T. 发明人 MCCLAIN, HARRY T.
分类号 F42B10/24 主分类号 F42B10/24
代理机构 代理人
主权项
地址