Partially buoyant aerial vehicle
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Description
FIG. 1 is a top right side and front perspective view of the vehicle
FIG. 2 is a right side elevational view of the vehicle with the left side being a mirror image
FIG. 3 is a top plan view of the vehicle
FIG. 4 is a bottom plan view of the vehicle
FIG. 5 is a front elevation view of the vehicle
FIG. 6 is a rear elevation view of the vehicle; and,
FIG. 7 is a top right side and front perspective view of a second embodiment of the partially buoyant aerial vehicle.
Referenced Cited
Patent History
Patent number: D418804
Type: Grant
Filed: Jun 22, 1998
Date of Patent: Jan 11, 2000
Assignee: Lockheed Martin Corporation (Palmdale, CA)
Inventors: Edsel R. Glasgow (Glendale, CA), Grant E. Carichner (Valencia, CA)
Primary Examiner: Kay H. Chin
Attorney: Robert A. Schrubl
Application Number: 0/90,064
Type: Grant
Filed: Jun 22, 1998
Date of Patent: Jan 11, 2000
Assignee: Lockheed Martin Corporation (Palmdale, CA)
Inventors: Edsel R. Glasgow (Glendale, CA), Grant E. Carichner (Valencia, CA)
Primary Examiner: Kay H. Chin
Attorney: Robert A. Schrubl
Application Number: 0/90,064
Classifications
Current U.S. Class:
Lighter-than-air, I.e., Lift Provided By Hot Air Or Gas (D12/323);
Horizontal Stabilizer Conforms To And Continues Wing Or Fuselage Configuration, E.g., Lifting Body Type (D12/333)
International Classification: 1207;
International Classification: 1207;