Vertical take-off and landing (VTOL) winged air vehicle with complementary angled rotors

Abstract

Description

FIG. 1 is a front perspective view of a vertical take-off and landing (VTOL) winged air vehicle with complementary angled rotors showing our new design;

FIG. 2 is a rear perspective view of the embodiment of FIG. 1;

FIG. 3 is a front elevational view of FIG. 1;

FIG. 4 is a rear elevational view of FIG. 1;

FIG. 5 is a right side elevational view of FIG. 1;

FIG. 6 is a left side elevational view of FIG. 1;

FIG. 7 is top plan view of FIG. 1; and,

FIG. 8 is a bottom plan view of FIG. 1.

Claims

The ornamental design for a vertical take-off and landing (VTOL) winged air vehicle with complementary angled rotors, as shown and described.