Supersonic aircraft with in-flight refueling system

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Description

FIG. 1 is a top, front and left side perspective view of supersonic aircraft with in-flight refueling system, embodying our new design;

FIG. 2 is a left side elevational view thereof;

FIG. 3 is a front elevational view thereof;

FIG. 4 is a rear elevational view thereof;

FIG. 5 is a top plan view thereof;

FIG. 6 is a bottom plan view thereof; and,

FIG. 7 is a top, front and left side perspective view thereof with the wings shown in a folded position.

Claims

The ornamental design for supersonic aircraft with in-flight refueling system, as shown and described.

Referenced Cited
U.S. Patent Documents
D317897 July 2, 1991 Antonov et al.
D319042 August 13, 1991 Babak et al.
D332080 December 29, 1992 Sandusky, Jr. et al.
4643374 February 17, 1987 Friederich
4896846 January 30, 1990 Strom
5526999 June 18, 1996 Meston
Foreign Patent Documents
44033 January 1998 RU
Patent History
Patent number: D439876
Type: Grant
Filed: Apr 22, 1999
Date of Patent: Apr 3, 2001
Assignee: Zakrytoe Actsionernoe Obshchestvo “Otdelenie morskikh sistem OKB im. P.O. Sukhogo” (Moscow)
Inventors: Mikhail P. Simonov (Moscow), Viktor I. Merkulov (Khabarovsk Territory), Yury L. Ivanov (Moscow), Konstantin K. Marbashev (Moscow), Aleksandr Y. Maranov (Khabarovsk Territory), Anatoly S. Klyagin (Moscow), Leonid G. Chernov (Moscow)
Primary Examiner: Kay H. Chin
Attorney, Agent or Law Firm: Oblon, Spivak, McClelland, Maier & Neustadt, P.C.
Application Number: 29/103,739