公开(公告)号：US20130020432A1

公开(公告)日：2013-01-24

申请号：US13552263

申请日：2012-07-18

申请人： Itzhak YOGEV ,  Michael SHEPSHELOVICH ,  Danny ABRAMOV

发明人： Itzhak YOGEV ,  Michael SHEPSHELOVICH ,  Danny ABRAMOV

IPC分类号： B64C9/32 ,  B64C15/02 ,  B64C9/06

CPC分类号： B64C9/12 ,  B64C9/323 ,  B64C9/326 ,  B64C15/02 ,  Y02T50/32

摘要： A method for providing a controllable side force to an air vehicle having a vertical stabilizer arrangement includes (a) selectively causing the vertical stabilizer arrangement to generate a first side force in a first side direction to provide the controllable side force, the first side force inducing a corresponding first yaw moment in a first yaw direction; and (b) selectively providing to the air vehicle a second yaw moment in a second yaw direction, the second yaw moment being induced by a force component of an auxiliary force applied to the air vehicle, the force component being in a force direction that is non-parallel with respect to the first side direction and the force component being spaced from a center of gravity of the air vehicle; wherein the second yaw direction is opposed to the first yaw direction. Also disclosed is a corresponding auxiliary yaw generating system.

摘要翻译： 一种用于向具有垂直稳定器装置的机动车辆提供可控侧力的方法包括：（a）选择性地使垂直稳定器装置在第一侧方向上产生第一侧力以提供可控的侧向力，第一侧向力 在第一偏转方向上相应的第一横摆力矩; 以及（b）选择性地向所述空中交通工具提供在第二偏转方向上的第二横摆力矩，所述第二横摆力矩由施加到所述空中车辆的辅助力的力分量感应，所述力分量处于 相对于第一侧方向不平行，并且力分量与空中交通工具的重心间隔开; 其中所述第二偏转方向与所述第一偏转方向相对。 还公开了相应的辅助偏航产生系统。