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Publication numberUSD428381 S
Publication typeGrant
Application numberUS 29/093,380
Publication dateJul 18, 2000
Filing dateSep 8, 1998
Publication number093380, 29093380, US D428381 S, US D428381S, US-S-D428381, USD428381 S, USD428381S
InventorsThomas M. Hartmann, John M. Morgenstern, Daniel H. Sokol
Original AssigneeLockheed Martin Corporation
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Supersonic business jet
US D428381 S
Abstract  available in
Images(5)
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Claims(1)
  1. The ornamental design for a supersonic business jet, as shown.
Description

FIG. 1 is a top and right side perspective view of a supersonic business jet showing our new design;

FIG. 2 is a left 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 by
Citing PatentFiling datePublication dateApplicantTitle
US6698684Mar 22, 2002Mar 2, 2004Gulfstream Aerospace CorporationSupersonic aircraft with spike for controlling and reducing sonic boom
US8083171May 26, 2007Dec 27, 2011Gulfstream Aerospace CorporationSupersonic aircraft for reducing sonic boom effects at ground level
US8286434Dec 27, 2011Oct 16, 2012Gulfstream Aerospace CorporationIsentropic compression inlet for supersonic aircraft
US8327645Dec 27, 2011Dec 11, 2012Gulfstream Aerospace CorporationIsentropic compression inlet for supersonic aircraft
US8333076Dec 15, 2006Dec 18, 2012Gulfstream Aerospace CorporationIsentropic compression inlet for supersonic aircraft
US8393158Dec 7, 2007Mar 12, 2013Gulfstream Aerospace CorporationLow shock strength inlet
US8453961 *Sep 29, 2010Jun 4, 2013Richard H. LuggSupersonic aircraft with shockwave canceling aerodynamic configuration
US8739514Oct 24, 2008Jun 3, 2014Gulfstream Aerospace CorporationLow shock strength propulsion system
US8783039Oct 23, 2009Jul 22, 2014Gulfstream Aerospace CorporationLow shock strength propulsion system
US8789789May 23, 2011Jul 29, 2014Gulfstream Aerospace CorporationSupersonic aircraft with spike for controlling and reducing sonic boom
US9027583Dec 5, 2012May 12, 2015Gulfstream Aerospace CorporationLow shock strength inlet
US9334801Aug 2, 2012May 10, 2016Gulfstream Aerospace CorporationSupersonic aircraft jet engine installation
US9482155Sep 27, 2012Nov 1, 2016Gulfstream Aerospace CorporationIsentropic compression inlet for supersonic aircraft
US20060157613 *Jan 19, 2005Jul 20, 2006Adamson Eric ESupersonic aircraft with active lift distribution control for reducing sonic boom
US20080271787 *Dec 15, 2006Nov 6, 2008Henne Preston AIsentropic compression inlet for supersonic aircraft
US20090107557 *Dec 7, 2007Apr 30, 2009Conners Timothy RLow shock strength inlet
US20100012777 *May 26, 2007Jan 21, 2010Henne Preston ASupersonic Aircraft with Spike for Controlling and Reducing Sonic Boom
US20100043389 *Oct 24, 2008Feb 25, 2010Gulfstream Aerospace CorporationLow shock strength propulsion system
US20110133021 *Sep 29, 2010Jun 9, 2011Hypermach Aerospace Industries IncorporatedSupersonic aircraft with shockwave canceling aerodynamic configuration
US20150108269 *Dec 6, 2013Apr 23, 2015Richard H. LuggHypersonic aircraft
Classifications
U.S. ClassificationD12/332, D12/333, D12/341