Supersonic airplane
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Description
FIG. 1 is an upper perspective view of a supersonic airplane depicting my new design;
FIG. 2 is a side elevational view thereof;
FIG. 3 is a top plan view thereof;
FIG. 4 is a bottom plan view thereof;
FIG. 5 is a front elevational view thereof; and
FIG. 6 is a rear elevational view thereof.
Referenced Cited
U.S. Patent Documents
D204331 | April 1966 | Robins et al. |
D206299 | November 1966 | Rellis |
D208678 | September 1967 | Schairer et al. |
D212564 | October 1968 | Sutter et al. |
D215894 | November 1969 | Rellis |
D216921 | March 1970 | Friebel |
3430446 | March 1969 | McCloy |
Patent History
Patent number: D269176
Type: Grant
Filed: Aug 13, 1979
Date of Patent: May 31, 1983
Assignee: The Boeing Company (Seattle, WA)
Inventor: Gottfried O. Friebel (Bellevue, WA)
Primary Examiner: T. Tung
Attorneys: H. Gus Hartmann, Bernard A. Donahue
Application Number: 6/66,160
Type: Grant
Filed: Aug 13, 1979
Date of Patent: May 31, 1983
Assignee: The Boeing Company (Seattle, WA)
Inventor: Gottfried O. Friebel (Bellevue, WA)
Primary Examiner: T. Tung
Attorneys: H. Gus Hartmann, Bernard A. Donahue
Application Number: 6/66,160
Classifications
Current U.S. Class:
Plural Distinct Rudders (8) (D12/338);
Horizontal Stabilizer Conforms To And Continues Wing Or Fuselage Configuration, E.g., Lifting Body Type (D12/333);
Pylon-mounted Engine (D12/340);
Jet Propelled (D12/343)
International Classification: D1207;
International Classification: D1207;