Patent ID: 8286737
Filing Date: 2012-10-16
Classification: B64C,Y02T

Abstract:
1. A ball drive assembly for a vertical takeoff and land aircraft having a plurality of supports extending outwardly from a central aircraft body, the ball drive assembly for one of said supports comprising in combination: a) a ball housing carried by said one support, b) a substantially completely spherical and substantially rigid, solid ball in said housing, c) said ball having a through bore terminating in a pair of diametrically opposed openings and a tubular drive shaft extending completely through said bore and with its ends protruding from both openings, said drive shaft being completely rigid with said ball, d) an axle positioned inside and extending through said drive shaft, and having ends extending past the protruding ends of said drive shaft, e) spacer bearings disposed between said tubular drive shaft and said axle, f) a motor driven ring gear turnably mounted in said drive housing, and pinion gears for transmitting power from said ring gear simultaneously to both ends of said drive shaft so as to rotate the ball about the axle, and g) a motor driven steering ring gear turnably mounted in said drive housing, the ends of said axle extending into and being rigid with said steering ring gear such that turning of the steering gear ring applies oppositely directed forces to both opposite ends of the axle respectively, for swivelling the ball about a vertical axis.