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

- AeroVironment, Inc.
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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.

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Patent History
Patent number: D813143
Type: Grant
Filed: Nov 4, 2016
Date of Patent: Mar 20, 2018
Assignee: AeroVironment, Inc. (Monrovia, CA)
Inventors: Pavel Belik (Simi Valley, CA), Andrew Logan (Thousand Oaks, CA), Henry Won (Simi Valley, CA), Jeremy Tyler (Thousand Oaks, CA)
Primary Examiner: Robert M. Spear
Assistant Examiner: Marissa J Cash
Application Number: 29/583,481
Classifications
Current U.S. Class: Vertical Takeoff Type (D12/326)