Airplane
Description
FIG. 1 is a top plan view of an airplane showing my new design;
FIG. 2 is a side elevational view of FIG. 1, the other side being identical;
FIG. 3 is a front elevational view of FIG. 1;
FIG. 4 is a rear elevational view of FIG. 1;
FIG. 5 is a side elevational view similar to FIG. 2, but with the engines in an alternate position, and
FIG. 6 is a front elevational view of FIG. 5.
Referenced Cited
U.S. Patent Documents
D90840 | October 1933 | Ferris |
D189562 | January 1961 | Nelson |
3096952 | July 1963 | Roppel |
3284028 | November 1966 | Robertson |
3606210 | September 1971 | Busby |
Patent History
Patent number: D267171
Type: Grant
Filed: May 27, 1980
Date of Patent: Dec 7, 1982
Inventor: Perry B. Johnson (Paterson, NJ)
Primary Examiner: James M. Gandy
Law Firm: Samuelson & Jacob
Application Number: 6/153,066
Type: Grant
Filed: May 27, 1980
Date of Patent: Dec 7, 1982
Inventor: Perry B. Johnson (Paterson, NJ)
Primary Examiner: James M. Gandy
Law Firm: Samuelson & Jacob
Application Number: 6/153,066
Classifications
Current U.S. Class:
Vertical Takeoff Type (D12/326);
Horizontal Stabilizer Conforms To And Continues Wing Or Fuselage Configuration, E.g., Lifting Body Type (D12/333)
International Classification: D1207;
International Classification: D1207;