Patent ID: 6053451
Filing Date: 2000-04-25
Classification: B64C

Abstract:
A remote-control flight vehicle structure comprising:an inner housing (12) fixedly mounted;an outer housing (11) rotatably mounted on said inner housing (12) along a vertical axis thereof, and a space (112) defined between said inner housing (12) and said outer housing (11);an annular wing (13) fixedly mounted an the outer periphery of said outer housing (11) to rotate therewith and inclined with a horizontal plane about a first included angle;a plurality of baffles (131) each fixedly mounted on a bottom portion of said annular wing (13) along a radial direction thereof and each inclined with said annular wing (13) about a second included angle;a platform (121) fixedly mounted in said inner housing (12); anda motor (123) mounted on said platform (121), and a rotary axle (124) including a first end portion rotatably mounted in said motor (123) and a second end portion extending through said inner housing (12) and fixed to said outer housing (11) for rotating said outer housing (11).