Airplane
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Description
FIG. 1 is a perspective view taken from above and about three-quarter front of an airplane embodying the present design;
FIG. 2 is a top plan view thereof;
FIG. 3 is a front elevational thereof; and
FIG. 4 is a side elevation thereof.
Referenced Cited
U.S. Patent Documents
D119334 | March 1940 | Johnson |
D256905 | September 16, 1980 | McComas et al. |
3576300 | April 1971 | Palfreyman |
Patent History
Patent number: D269669
Type: Grant
Filed: Sep 11, 1980
Date of Patent: Jul 12, 1983
Assignee: Lockheed Corporation (Burbank, CA)
Inventors: John P. Hancock (Marietta, GA), Rollo G. Smethers, Jr. (Atlanta, GA)
Primary Examiner: Alan P. Douglas
Attorney: John J. Sullivan
Application Number: 6/186,722
Type: Grant
Filed: Sep 11, 1980
Date of Patent: Jul 12, 1983
Assignee: Lockheed Corporation (Burbank, CA)
Inventors: John P. Hancock (Marietta, GA), Rollo G. Smethers, Jr. (Atlanta, GA)
Primary Examiner: Alan P. Douglas
Attorney: John J. Sullivan
Application Number: 6/186,722
Classifications
Current U.S. Class:
Horizontal Stabilizer Ahead Of Wing (D12/332);
Plural Distinct Rudders (8) (D12/338);
Wing-mounted Engine (D12/341);
Canard (244/45A)
International Classification: D1207;
International Classification: D1207;