Fluidic propulsive device for an aircraft

Abstract

Description

FIG. 1 is a front perspective view of a fluidic propulsive device for an aircraft in a horizontal thrust configuration, showing my new design;

FIG. 2 is a top plan view thereof;

FIG. 3 is a bottom plan view thereof;

FIG. 4 is a left side elevation view thereof;

FIG. 5 is a right side elevation view thereof;

FIG. 6 is a front elevation view thereof;

FIG. 7 is a rear elevation view thereof;

FIG. 8 is front perspective view of the fluidic propulsive device for an aircraft of FIGS. 1-7 shown in a downward thrust configuration;

FIG. 9 is a top plan view thereof;

FIG. 10 is a bottom plan view thereof;

FIG. 11 is a left side elevation view thereof;

FIG. 12 is a right side elevation view thereof;

FIG. 13 is a front elevation view thereof;

FIG. 14 is a rear elevation view thereof;

FIG. 15 is front perspective view of the fluidic propulsive device for an aircraft of FIGS. 1-14 shown in a split upward and downward thrust configuration;

FIG. 16 is a top plan view thereof;

FIG. 17 is a bottom plan view thereof;

FIG. 18 is a left side elevation view thereof;

FIG. 19 is a right side elevation view thereof;

FIG. 20 is a front elevation view thereof; and,

FIG. 21 is a rear elevation view thereof;

Claims

I claim the ornamental design for a fluidic propulsive device for an aircraft, as shown.