Patent ID: 8376268
Filing Date: 2013-02-19
Classification: B64C

Abstract:
1. A flight management system, use in relation to an aviation vehicle, comprising a thrust vectoring device for producing thrust, having a nozzle, a pivoting half cylinder side, a pivoting sphere with an inner-threaded aperture, a rotation pin, a passageway, a centered main panel slot, a deployment device, a threaded rod, an outer triangular panel with cut-out, a support means, a continuous hinge, a pivoting hydraulic cylinder, and a triangular main panel, an air deflecting device for producing thrust, having an open-ended box structure, a box securing plate, a motor shaft, a motor, a motor mount, a flat disc base, a support roller, and a rubber seal, and a computing system having storage storing machine-executable instructions configured for execution by the computing system in order to cause the computing system to receive operation requirements, the operation requirements used to orient the thrust device and/or the air deflecting device.