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The ornamental design for a supersonic aircraft, as shown.
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FIG. 1 is a perspective view of the ornamental design of a supersonic aircraft showing our new design;
FIG. 2 is a top plan view of the supersonic aircraft;
FIG. 3 us a right side elevation view of the supersonic aircraft, with the left side being a mirror image, and with the broken line showing for illustrative purposes only and forming no part of the claimed design;
FIG. 4 is a front elevation view of the supersonic aircraft; and,
FIG. 5 is a rear elevation view of the supersonic aircraft.
Wainfan, Barnaby S., Rouleau, Bruce S., Graham, David H., Reynolds, Ross S.
| Patent | Priority | Assignee | Title |
| 10093410, | Feb 14 2013 | Gulfstream Aerospace Corporation | Systems and methods for controlling a magnitude of a sonic boom |
| 10232937, | Dec 07 2012 | HYPERMACH AEROSPACE INDUSTRIES, INC | Hypersonic aircraft |
| 10351226, | Feb 14 2013 | Gulfstream Aerospace Corporation | Systems and methods for controlling a magnitude of a sonic boom |
| 6938854, | Jan 19 2001 | The Boeing Company | Integrated and/or modular high-speed aircraft |
| 8453961, | Sep 29 2009 | HYPERMACH AEROSPACE INDUSTRIES INCORPORATED | Supersonic aircraft with shockwave canceling aerodynamic configuration |
| 9446839, | Feb 14 2013 | Gulfstream Aerospace Corporation | Systems and methods for controlling a magnitude of a sonic boom |
| 9561847, | Feb 14 2013 | Gulfstream Aerospace Corporation | Systems and methods for controlling a magnitude of a sonic boom |
| 9580169, | Feb 14 2013 | Gulfstream Aerospace Corporation | Systems and methods for controlling a magnitude of a sonic boom |
| D496074, | Dec 26 2003 | Aircraft | |
| ER7044, |
| Patent | Priority | Assignee | Title |
| 4336913, | Oct 02 1979 | Compound wing aircraft | |
| 4828204, | Aug 13 1979 | The Boeing Company | Supersonic airplane |
| 5062595, | Jul 19 1988 | University of Southern California | Delta wing with lift enhancing flap |
| 5322242, | Jul 08 1991 | Aerion Intellectual Property Management Corporation | High efficiency, supersonic aircraft |
| 5348256, | May 13 1992 | Boeing Company, the | Supersonic aircraft and method |
| 5538201, | Dec 14 1993 | Northrop Grumman Corporation | Supersonic natural laminar flow wing |
| 213528, | |||
| D268107, | Apr 25 1980 | Fairchild Industries, Inc. | Aircraft |
| D269176, | Aug 13 1979 | The Boeing Company | Supersonic airplane |
| D326081, | Mar 16 1990 | McDonnell Douglas Corporation | Airplane |
| D342717, | Oct 29 1992 | Northrop Grumman Systems Corporation | Aircraft |
| D364600, | Apr 20 1994 | The Testor Corporation | Airplane |
| D381938, | Aug 31 1995 | Northrop Grumman Systems Corporation | Tactical aircraft decoy, conjugal tandem design |
| D394039, | Jun 23 1997 | BOEING NORTH AMERICAN, INC | Airplane |
| D417184, | Mar 02 1999 | Lockheed Martin Corporation | Supersonic business jet |
| D458577, | Oct 25 1999 | Spy plane |
| Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
| May 14 2002 | ROULEAU, BRUCE S | Northrop Grumman Corporation | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 012913 | /0603 | |
| May 14 2002 | GRAHAM, DAVID H | Northrop Grumman Corporation | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 012913 | /0603 | |
| May 14 2002 | REYNOLDS, ROSS S | Northrop Grumman Corporation | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 012913 | /0603 | |
| May 14 2002 | WAINFAN, BARNABY S | Northrop Grumman Corporation | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 012913 | /0603 | |
| May 15 2002 | Northrop Grumman Corporation | (assignment on the face of the patent) | / | |||
| Jan 04 2011 | Northrop Grumman Corporation | Northrop Grumman Systems Corporation | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 025597 | /0505 |
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