Airplane
Description
FIG. 1 is a top plan view of an airplane showing my new design;
FIG. 2 is a side elevational view thereof, with the opposite side being identical;
FIG. 3 is a front elevational view thereof;
FIG. 4 is a rear elevational view thereof;
FIG. 5 is a side elevational view thereof, with the engines in an alternate position; and
FIG. 6 is a front elevational view of the airplane of FIG. 5.
The bottom of the airplane not shown is unornamented.
Referenced Cited
U.S. Patent Documents
D205694 | September 1966 | Petry |
D227606 | July 1973 | Rellis |
3030051 | April 1962 | Kerry et al. |
3532301 | October 1970 | Swatton |
Patent History
Patent number: D259713
Type: Grant
Filed: Jul 31, 1978
Date of Patent: Jun 30, 1981
Inventor: Perry B. Johnson (Paterson, NJ)
Primary Examiner: Sam Rosen
Law Firm: Samuelson & Jacob
Application Number: 5/929,854
Type: Grant
Filed: Jul 31, 1978
Date of Patent: Jun 30, 1981
Inventor: Perry B. Johnson (Paterson, NJ)
Primary Examiner: Sam Rosen
Law Firm: Samuelson & Jacob
Application Number: 5/929,854
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;