Patent ID: 6769493
Filing Date: 2004-08-03
Classification: A01C,A01G,A62C,B64D,Y02A,Y02P,Y10S

Abstract:
A hybrid airship, platform system for delivering and dispersing large quantities of liquid while in flight and hovering modes over specified ground areas, where dynamic lift for said airship system is derived by its aerodynamically shaped body and engine fans to provide lift in an airstream, and static lift is achieved by a non-combustible lighter-than-air gas confined therewithin, said airship system comprising:a.) a semi rigid, light-weight frame encased within a skin and aerodynamically configured to provide lift in an air stream while in a flying and hovering modes over said specified ground areas; b.) means for flying said airship system, where said means include a plurality of engine fans and attitude stabilizing mechanisms to provide 3-axis stability and control; and, c.) a liquid control and dispensing mechanism disposed primarily within said frame, said mechanism including, i.) a liquid holding tank positioned along the center of gravity of said airship system, ii.) a manifold in liquid communication with said holding tank, when said manifold includes means for controlling the quantity of liquid passing therethrough, and iii.) a liquid distribution, piping and nozzle assembly in liquid communication with said manifold, where said assembly is exposed below said frame.