Supersonic business jet
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Description
FIG. 1 is a top right rear perspective view of a supersonic business jet;
FIG. 2 is a top plan view thereof;
FIG. 3 is a left side elevation view thereof, right side being a mirror image;
FIG. 4 is a bottom plan view thereof;
FIG. 5 is a rear elevation view thereof; and,
FIG. 6 is a front elevation view thereof.
Referenced Cited
U.S. Patent Documents
D231094 | April 1974 | Schmidt |
3478989 | November 1969 | Bielefeldt |
5348256 | September 20, 1994 | Parikh |
Patent History
Patent number: D417184
Type: Grant
Filed: Mar 2, 1999
Date of Patent: Nov 30, 1999
Assignee: Lockheed Martin Corporation (Palmdale, CA)
Inventors: Tom Hartmann (Canyon Country, CA), John M. Morgenstern (Palmdale, CA), Daniel Sokol (Canyon Country, CA)
Primary Examiner: Kay H. Chin
Attorney: Robert A. Schruhl
Application Number: 0/101,387
Type: Grant
Filed: Mar 2, 1999
Date of Patent: Nov 30, 1999
Assignee: Lockheed Martin Corporation (Palmdale, CA)
Inventors: Tom Hartmann (Canyon Country, CA), John M. Morgenstern (Palmdale, CA), Daniel Sokol (Canyon Country, CA)
Primary Examiner: Kay H. Chin
Attorney: Robert A. Schruhl
Application Number: 0/101,387
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);
Canard Configuration Or With Plural Distinct Wings (D12/331)
International Classification: 1207;
International Classification: 1207;