Delta rotor wing aircraft
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Description
FIG. 1 is a front, top and left side perspective view of a delta rotor wing aircraft showing my new design;
FIG. 2 is a front, top and right side perspective view thereof;
FIG. 3 is a front, bottom and right side perspective view thereof;
FIG. 4 is a top plan view thereof;
FIG. 5 is a front elevational view thereof;
FIG. 6 is a left side elevational view thereof;
FIG. 7 is a top plan view thereof, showing the blades of both top and bottom counter rotating rotors extended radially outward from the center of each rotor;
FIG. 8 is a front elevational view of FIG. 7; and
FIG. 9 is a left side elevational view of FIG. 7, the right side view being a mirror image of that shown.
Referenced Cited
Patent History
Patent number: D319041
Type: Grant
Filed: Mar 24, 1988
Date of Patent: Aug 13, 1991
Assignee: Lockheed Corporation (Calabasas, CA)
Inventor: Jerry W. Phillips (Roswell, GA)
Primary Examiner: Kay H. Chin
Attorney: Eric R. Katz
Application Number: 7/172,742
Type: Grant
Filed: Mar 24, 1988
Date of Patent: Aug 13, 1991
Assignee: Lockheed Corporation (Calabasas, CA)
Inventor: Jerry W. Phillips (Roswell, GA)
Primary Examiner: Kay H. Chin
Attorney: Eric R. Katz
Application Number: 7/172,742
Classifications
Current U.S. Class:
Canard Configuration Or With Plural Distinct Wings (D12/331)