Unmanned aircraft
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Description
FIG. 1 is a perspective view of the aircraft looking downward from the front;
FIG. 2 is a front view of the aircraft;
FIG. 3 is a rear view of the aircraft;
FIG. 4 is a top view of the aircraft;
FIG. 5 is a bottom view of the aircraft; and,
FIG. 6 is a side view of the aircraft.
Referenced Cited
U.S. Patent Documents
Other references
D281680 | December 10, 1985 | Henderson |
4662588 | May 5, 1987 | Henderson |
5090636 | February 25, 1992 | Sadowski |
5337975 | August 16, 1994 | Peinemann |
- Jane's All The Word's Aircraft, 1995-1996, p. 615, B-2A Spirit. Jane's All The World's Aircraft, 1982-1983, p. 808, IML ADDAX-S Supersonic Fighter.
Patent History
Patent number: D388392
Type: Grant
Filed: Nov 3, 1995
Date of Patent: Dec 30, 1997
Assignee: Lockheed Martin Corporation (Bethesda, MD)
Inventors: John E. McGinnis (Dunwoody, GA), Bruce R. Wright (Santa Clarita, CA)
Primary Examiner: Kay H. Chin
Attorney: Louis L. Dachs
Application Number: 0/46,001
Type: Grant
Filed: Nov 3, 1995
Date of Patent: Dec 30, 1997
Assignee: Lockheed Martin Corporation (Bethesda, MD)
Inventors: John E. McGinnis (Dunwoody, GA), Bruce R. Wright (Santa Clarita, CA)
Primary Examiner: Kay H. Chin
Attorney: Louis L. Dachs
Application Number: 0/46,001
Classifications
Current U.S. Class:
Horizontal Stabilizer Conforms To And Continues Wing Or Fuselage Configuration, E.g., Lifting Body Type (D12/333);
Aircraft, Spacecraft, Or Fuselage (D12/319)
International Classification: 1207;
International Classification: 1207;