Surface configuration of an airplane
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Description
FIG. 1 is a front elevational view of a surface configuration of an airplane showing my new design;
FIG. 2 is a left side elevational view thereof;
FIG. 3 is a right side elevational view thereof;
FIG. 4 is a rear elevational view thereof;
FIG. 5 is a top plan view thereof;
FIG. 6 is a front perspective view thereof; and,
FIG. 7 is a rear perspective view thereof.
The dash lines included depict environment and are not part of the claimed design.
Referenced Cited
Patent History
Patent number: D421955
Type: Grant
Filed: May 14, 1999
Date of Patent: Mar 28, 2000
Assignee: Dornier Luftfahrt GmbH
Inventor: Reinhold Birrenbach (Markdorf)
Primary Examiner: Kay H. Chin
Law Firm: Evenson, McKeown, Edwards & Lenahan, P.L.L.C.
Application Number: 0/105,010
Type: Grant
Filed: May 14, 1999
Date of Patent: Mar 28, 2000
Assignee: Dornier Luftfahrt GmbH
Inventor: Reinhold Birrenbach (Markdorf)
Primary Examiner: Kay H. Chin
Law Firm: Evenson, McKeown, Edwards & Lenahan, P.L.L.C.
Application Number: 0/105,010
Classifications
Current U.S. Class:
T-tail Empennage, I.e., Stabilizer Mounted At Top Of Rudder Or Vertical Fin (D12/337);
Aircraft, Spacecraft, Or Fuselage (D12/319);
Wing-mounted Engine (D12/341)
International Classification: 1207;
International Classification: 1207;