公开(公告)号：US08367992B1

公开(公告)日：2013-02-05

申请号：US12977519

申请日：2010-12-23

申请人： Mehul Patel ,  T Terry Ng ,  Alan B Cain ,  Zak Sowle ,  Jack DiCocco

发明人： Mehul Patel ,  T Terry Ng ,  Alan B Cain ,  Zak Sowle ,  Jack DiCocco

IPC分类号： F42B10/02 ,  B64C3/54

CPC分类号： F42B10/64 ,  F41G7/20 ,  F42B3/006 ,  F42B10/02 ,  F42B15/00 ,  F42B15/01 ,  F42B15/36 ,  F42B19/01

摘要： The present invention relates to an aircraft, missile, projectile, or underwater vehicle with an improved control system and a method for increasing the maneuverability or stability of an aircraft, missile, projectile, or underwater vehicle. More particularly, the present invention relates to a method for increasing the maneuverability or stability of an aircraft, missile, underwater vehicle or projectile through the use of removable control surfaces. The technical advantage of the removable control surface system (or “removable control surface”) over other systems is that the removable control surface system enables the aircraft, missile, underwater vehicle or projectile to have two or more design configurations, each configuration being tailored to the aircraft, missile, projectile, or underwater vehicle's specific stability or maneuverability requirements during a specific portion of the flight.

摘要翻译： 本发明涉及一种具有改进的控制系统的飞机，导弹，射弹或水下车辆，以及用于增加飞机，导弹，射弹或水下航行器的机动性或稳定性的方法。 更具体地说，本发明涉及通过使用可拆卸的控制表面来提高飞机，导弹，水下航行器或射弹的机动性或稳定性的方法。 可移动控制表面系统（或可移除控制面）在其他系统上的技术优点在于，可移动控制面系统使得飞机，导弹，水下航行器或射弹能够具有两个或多个设计配置，每个配置适合飞机 ，导弹，射弹或水下航行器在特定部分飞行过程中的具体稳定性或机动性要求。

公开(公告)号：US10060777B2

公开(公告)日：2018-08-28

申请号：US15146805

申请日：2016-05-04

申请人： Alan B Cain ,  Stanislav Gordeyev ,  R. Mark Rennie

发明人： Alan B Cain ,  Stanislav Gordeyev ,  R. Mark Rennie

IPC分类号： G01M9/06 ,  G01F1/66

CPC分类号： G01F1/661 ,  G01F1/7086 ,  G01F1/712 ,  G01M9/065 ,  G01M9/067 ,  G01P5/26

摘要： An “air-data probe” system measures at least one component of freestream velocity by tracking the motion of a laser-induced breakdown (“LIB”) spark created in a freestream flow. Neutral density filters are positioned or deployed so that the brightness of the initial LIB spark doesn't over saturate the LIB sensor system. This allows for more consistent tracking of the LIB spark throughout the duration of the LIB spark, including the later stages where the LIB spark is not nearly as bright as the initial LIB spark, thereby allowing all or substantially all of the light generated by the LIB spark to reach the sensors. This provides for enhanced visibility and more accurate detection of the LIB spark over time and as air density changes.