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1. 发明授权

US07070144B1 Aircraft and missile afterbody flow control device and method of controlling flow 有权
标题翻译：飞机和导弹后体流量控制装置及流量控制方法
公开(公告)号：US07070144B1
公开(公告)日：2006-07-04
申请号：US10750422
申请日：2003-12-30
申请人： Jack DiCocco , Troy Prince , Mehul Patel , Tsun Ming Terry Ng
发明人： Jack DiCocco , Troy Prince , Mehul Patel , Tsun Ming Terry Ng
IPC分类号： B64C21/00
CPC分类号： B64C21/00 , B64C5/12 , F41G7/00 , F42B10/14 , F42B10/60 , F42B10/62 , F42B15/01 , G05D1/0088
摘要： The present invention relates to an afterbody flow control system and more particularly to aircraft or missile flow control system for enhanced maneuverability and stabilization. The present invention further relates to a method of operating the flow control system.In one embodiment, the present invention includes a missile or aircraft comprising an afterbody and a forebody; at least one activatable flow effector on the missile or aircraft afterbody; at least one sensor each having a signal, the at least one sensor being positioned to detect forces or flow conditions on the missile or aircraft afterbody; and a closed loop control system; wherein the closed loop control system is used for activating and deactivating the at least one activatable flow effector based on at least in part the signal of the at least one sensor.
摘要翻译：本发明涉及后体流量控制系统，更具体地涉及用于增强机动性和稳定性的飞机或导弹流量控制系统。本发明还涉及一种操作流量控制系统的方法。在一个实施例中，本发明包括一个包括后身体和前体的导弹或飞机; 在导弹或飞机后身上至少有一个可激活的流动执行器; 每个具有信号的至少一个传感器，所述至少一个传感器被定位成检测导弹或飞机后身上的力或流动状况; 和闭环控制系统; 其中所述闭环控制系统用于至少部分地基于所述至少一个传感器的信号来激活和去激活所述至少一个可激活的流动效应器。

2. 发明授权

US09637223B1 Aircraft and missile afterbody flow control device and method of controlling flow 有权
公开(公告)号：US09637223B1
公开(公告)日：2017-05-02
申请号：US13457686
申请日：2012-04-27
申请人： Jack DiCocco , Troy Prince , Mehul Patel , Tsun Ming Terry Ng
发明人： Jack DiCocco , Troy Prince , Mehul Patel , Tsun Ming Terry Ng
IPC分类号： B64C21/00
CPC分类号： B64C21/00 , B64C5/12 , F41G7/00 , F42B10/14 , F42B10/60 , F42B10/62 , F42B15/01 , G05D1/0088
摘要： An afterbody flow control system is used for aircraft or missile flow control to provide enhanced maneuverability and stabilization. A method of operating the flow control system is also described. The missile or aircraft comprises an afterbody and a forebody; at least one activatable flow effector on the missile or aircraft afterbody; at least one sensor having a signal, the at least one sensor being positioned to detect forces or flow conditions on the missile or aircraft afterbody; and a closed loop control system; wherein the closed loop control system is used for activating and deactivating the at least one activatable flow effector based on at least in part the signal of the at least one sensor.

3. 发明授权

US08191833B1 Aircraft and missile afterbody flow control device and method of controlling flow 有权
标题翻译：飞机和导弹后体流量控制装置及流量控制方法
公开(公告)号：US08191833B1
公开(公告)日：2012-06-05
申请号：US11415534
申请日：2006-05-02
申请人： Jack DiCocco , Troy Prince , Mehul Patel , Tsun Ming Terry Ng
发明人： Jack DiCocco , Troy Prince , Mehul Patel , Tsun Ming Terry Ng
IPC分类号： B64C21/00
CPC分类号： B64C21/00 , B64C5/12 , F41G7/00 , F42B10/14 , F42B10/60 , F42B10/62 , F42B15/01 , G05D1/0088
摘要： The present invention relates to an afterbody flow control system and more particularly to aircraft or missile flow control system for enhanced maneuverability and stabilization. The present invention further relates to a method of operating the flow control system.In one embodiment, the present invention includes a missile or aircraft comprising an afterbody and a forebody; at least one activatable flow effector on the missile or aircraft afterbody; at least one sensor each having a signal, the at least one sensor being positioned to detect forces or flow conditions on the missile or aircraft afterbody; and a closed loop control system; wherein the closed loop control system is used for activating and deactivating the at least one activatable flow effector based on at least in part the signal of the at least one sensor.
摘要翻译：本发明涉及后体流量控制系统，更具体地涉及用于增强机动性和稳定性的飞机或导弹流量控制系统。本发明还涉及一种操作流量控制系统的方法。在一个实施例中，本发明包括一个包括后身体和前体的导弹或飞机; 在导弹或飞机后身上至少有一个可激活的流动执行器; 每个具有信号的至少一个传感器，所述至少一个传感器被定位成检测导弹或飞机后身上的力或流动状况; 和闭环控制系统; 其中所述闭环控制系统用于至少部分地基于所述至少一个传感器的信号来激活和去激活所述至少一个可激活的流动效应器。

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