Flying object

摘要

By using the interaction between the wind flow and the stabilizer arranged in the wind flow and along the direction of the wind flow, this invention provides the flying object that secures the stability of device or aircraft or stabilizer itself unified with the stabilizer by above effect. The interaction mentioned above is that when the wind flow hits the stabilizer at a certain angle, the wind flow changes the direction, and the power corresponding its reaction is given to the stabilizer by its reaction.

主权项

1. A flying object, comprising:
a wind flow generating device; and one or more radial stabilizing wings arranged along a center axis of a wind flow in the form of a coaxial line in a wind flow generated by the wind flow generating device, wherein said radial stabilizing wings are arranged such that a relationship between a vertical distance nGC between a center point of total wind flow pressure obtained by synthesizing a center point of wind flow pressure of the respective stabilizing wings and a center of gravity of the flying object, and a vertical distance nGW between a center point of outside wind pressure and the center of gravity of the flying object, is represented by formula (26), wherein:
[H]nGC=[W]nGW  (26) providing that:[H]=π⁡(HC+Ha)+1π⁢H0(21)[W]=SW[SC](25)[SC]=SC+Sa+1π⁢S0(23)HC=SCr02,Ha=Sar02,H0=S0r02(43) where, r0: a diameter of the wind flow generating device; SC: an area obtained by converting an area of said radial stabilizing wing inside of a spreading wind flow generating device wind into an area of said radial stabilizing wing inside of a shrunk wind flow generating device wind, when the spreading wind flow generating device wind is shrunk such that the wind flow generating device wind flows as a parallel wind flow without changing an air density directly under wind flow generating device, but a calculation of shrinking rate is as follows: a horizontal line on said radial stabilizing wing located at any distance from the wind flow generating device, and a width of spreading of the wind flow generating device wind on its horizontal line be rW, a width of said radial stabilizing wing inside of the wind flow generating device wind be ra, and the width of said radial stabilizing wing on its horizontal line after shrinking be r, and r is represented by formula (3), in whichr=ra⁡(r0rw)(3) Sa: the area of said radial stabilizing wing inside of exceeding part of the shrunk wind flow generating device wind when the area of said radial stabilizing wing inside of the exceeding wind flow generating device wind from inside of said spreading wind flow generating device wind is shrunk at a shrinking rate represented by formula (3), and in which S0: the area (except the area where the wind flow generating device wind is flowing) of said radial stabilizing wing of the wind flow generating device periphery, and SW: a projection area of the flying object.