USD471854S1 - Supersonic aircraft - Google Patents

Supersonic aircraft Download PDF

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Publication number
USD471854S1
USD471854S1 US29/160,797 US16079702F USD471854S US D471854 S1 USD471854 S1 US D471854S1 US 16079702 F US16079702 F US 16079702F US D471854 S USD471854 S US D471854S
Authority
US
United States
Prior art keywords
supersonic aircraft
supersonic
aircraft
view
elevation view
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US29/160,797
Inventor
Bruce S. Rouleau
David H. Graham
Ross S. Reynolds
Barnaby S. Wainfan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Northrop Grumman Systems Corp
Original Assignee
Northrop Grumman Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Northrop Grumman Corp filed Critical Northrop Grumman Corp
Priority to US29/160,797 priority Critical patent/USD471854S1/en
Assigned to NORTHROP GRUMMAN CORPORATION reassignment NORTHROP GRUMMAN CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GRAHAM, DAVID H., REYNOLDS, ROSS S., ROULEAU, BRUCE S., WAINFAN, BARNABY S.
Application granted granted Critical
Publication of USD471854S1 publication Critical patent/USD471854S1/en
Assigned to NORTHROP GRUMMAN SYSTEMS CORPORATION reassignment NORTHROP GRUMMAN SYSTEMS CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: NORTHROP GRUMMAN CORPORATION
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

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.

Claims (1)

  1. The ornamental design for a supersonic aircraft, as shown.
US29/160,797 2002-05-15 2002-05-15 Supersonic aircraft Expired - Lifetime USD471854S1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US29/160,797 USD471854S1 (en) 2002-05-15 2002-05-15 Supersonic aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29/160,797 USD471854S1 (en) 2002-05-15 2002-05-15 Supersonic aircraft

Publications (1)

Publication Number Publication Date
USD471854S1 true USD471854S1 (en) 2003-03-18

Family

ID=22578494

Family Applications (1)

Application Number Title Priority Date Filing Date
US29/160,797 Expired - Lifetime USD471854S1 (en) 2002-05-15 2002-05-15 Supersonic aircraft

Country Status (1)

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US (1) USD471854S1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040016845A1 (en) * 2001-01-19 2004-01-29 Nelson Chester P. Integrated and/or modular high-speed aircraft
US20060157613A1 (en) * 2005-01-19 2006-07-20 Adamson Eric E Supersonic aircraft with active lift distribution control for reducing sonic boom
US20110133021A1 (en) * 2009-09-29 2011-06-09 Hypermach Aerospace Industries Incorporated Supersonic aircraft with shockwave canceling aerodynamic configuration
US20140224924A1 (en) * 2013-02-14 2014-08-14 Gulfstream Aerospace Corporation Systems and methods for controlling a magnitude of a sonic boom
US20150108269A1 (en) * 2012-12-07 2015-04-23 Richard H. Lugg Hypersonic aircraft

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6938854B2 (en) 2001-01-19 2005-09-06 The Boeing Company Integrated and/or modular high-speed aircraft
US20040016845A1 (en) * 2001-01-19 2004-01-29 Nelson Chester P. Integrated and/or modular high-speed aircraft
US20060157613A1 (en) * 2005-01-19 2006-07-20 Adamson Eric E Supersonic aircraft with active lift distribution control for reducing sonic boom
US20110133021A1 (en) * 2009-09-29 2011-06-09 Hypermach Aerospace Industries Incorporated Supersonic aircraft with shockwave canceling aerodynamic configuration
US8453961B2 (en) * 2009-09-29 2013-06-04 Richard H. Lugg Supersonic aircraft with shockwave canceling aerodynamic configuration
US20150108269A1 (en) * 2012-12-07 2015-04-23 Richard H. Lugg Hypersonic aircraft
US10232937B2 (en) * 2012-12-07 2019-03-19 Hypermach Aerospace Industries, Inc. Hypersonic aircraft
US20140224926A1 (en) * 2013-02-14 2014-08-14 Gulfstream Aerospace Corporation Systems and methods for controlling a magnitude of a sonic boom
US20140224927A1 (en) * 2013-02-14 2014-08-14 Gulfstream Aerospace Corporation Systems and methods for controlling a magnitude of a sonic boom
US9446839B2 (en) 2013-02-14 2016-09-20 Gulfstream Aerospace Corporation Systems and methods for controlling a magnitude of a sonic boom
US9561847B2 (en) * 2013-02-14 2017-02-07 Gulfstream Aerospace Corporation Systems and methods for controlling a magnitude of a sonic boom
US9580169B2 (en) * 2013-02-14 2017-02-28 Gulfstream Aerospace Corporation Systems and methods for controlling a magnitude of a sonic boom
US10093410B2 (en) * 2013-02-14 2018-10-09 Gulfstream Aerospace Corporation Systems and methods for controlling a magnitude of a sonic boom
US20140224924A1 (en) * 2013-02-14 2014-08-14 Gulfstream Aerospace Corporation Systems and methods for controlling a magnitude of a sonic boom
US10351226B2 (en) * 2013-02-14 2019-07-16 Gulfstream Aerospace Corporation Systems and methods for controlling a magnitude of a sonic boom

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