发明名称 AUTONOMOUS TETHERED AIRCRAFT “LAPA”
摘要 There is disclosed an autonomous tethered aircraft comprising a body in the form of a gas-filled shell having the form of a lifting wing with an internal channel for a wind power station, a power system, a cable wiring, a tether, a winch, a container with instruments, a wind plant with a wind wheel, a reduction gear and an electric generator. Thus, the shell of aircraft has the shape of a swept lifting wing consisting of the upper airtight wing with at least one horizontal partition inside, and the lower aerodynamic wing with a porous surface of the wings, which interior surfaces and horizontal partition are connected at the intersections with a through vertical diaphragm and form a frame of power system of lifting wing, which divides its interior space into compartments, each of which is in the aerodynamic wing on the front and side surfaces has at least one opening, and in the airtight wing in horizontal rows is connected to a system of supply–removal of compressed air and comprises a ballonet. The ballonets are located in horizontal rows and connected to each other and the system of supply-removal of compressed gas that is lighter than air, and to the lower surface of the power frame in the areas of connection of edges and porous surface of an aerodynamic wing with edges of through vertical diaphragms fixed uniformly along their length by ends of ropes of suspended rigging a loading platform is attached in the form of a metal girder, which front edge is attached to the suspended rigging, which gives the lifting wing a swept shape, and is a pyramidal shell filled with gas lighter than air and is formed by connection of the edges of its surface with the edges of front surface of the shell of lifting wing, which top is attached to the connecting unit and is connected by straps of rope distribution with front edges of the frame of power system of shell of lifting wing attached uniformly along their length and in the areas of connection with the through vertical diaphragms and horizontal partition, and rigging consists of “goose legs”, slopes and slings.
申请公布号 UA94016(C2) 申请公布日期 2011.03.25
申请号 UA20100011208 申请日期 2010.09.20
申请人 OMELCHENKO SERHII MYKOLAIOVYCH 发明人 OMELCHENKO SERHII MYKOLAIOVYCH
分类号 B64B1/50 主分类号 B64B1/50
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