发明名称 Precision aerial delivery system
摘要 A system and methods for deployment operations from an airborne vehicle are presented. A designated location of a target is received at a flight control system coupled to a location tracking guided container comprising an agent. The location tracking guided container is ejected at an ejection point from the airborne vehicle approximately above the designated location of the target to descend at a descent rate and a descent angle. A calculated path to the designated location is calculated based on the designated location and a current location of the location tracking guided container. The location tracking guided container is aerodynamically guided by a glide control structure to fly along the calculated path from the ejection point to a load release altitude near the designated location of the target. The agent is delivered to the designated location of the target by releasing the agent at the load release altitude near the designated location.
申请公布号 US9120570(B2) 申请公布日期 2015.09.01
申请号 US201313776733 申请日期 2013.02.26
申请人 The Boeing Company 发明人 Hoisington Zachary Charles;Rawdon Blaine Knight
分类号 B64D1/16;B64D1/08;A62C3/02 主分类号 B64D1/16
代理机构 McDonnell Boehnen Hulbert & Berghoff LLP 代理人 McDonnell Boehnen Hulbert & Berghoff LLP
主权项 1. A method for deployment operations from an airborne vehicle, the method comprising: receiving a designated location of a target by a flight control system coupled to a location tracking guided container comprising a fire-suppression agent; ejecting at an ejection point the location tracking guided container from the airborne vehicle approximately above the designated location of the target to descend at a descent rate and a descent angle; calculating during descent, by a processor in the location tracking guided container, a calculated path to the designated location based on the designated location and a current location of the location tracking guided container; aerodynamically guiding the location tracking guided container by a glide control structure coupled thereto under control of the processor in the location tracking guided container independent of the airborne vehicle to fly along the calculated path from the ejection point to a load release altitude near the designated location of the target, controlling an actuator to operate a first suppression agent flow-control valve to control a flow rate of the fire suppression agent based on an operational condition of the location tracking guided container; and delivering the fire-suppression agent to the designated location of the target by releasing the agent at the load release altitude near the designated location.
地址 Chicago IL US