Search Images Maps Play YouTube News Gmail Drive More »
Sign in
Screen reader users: click this link for accessible mode. Accessible mode has the same essential features but works better with your reader.

Patents

  1. Advanced Patent Search
Publication numberUSD417184 S
Publication typeGrant
Application numberUS 29/101,387
Publication dateNov 30, 1999
Filing dateMar 2, 1999
Publication number101387, 29101387, US D417184 S, US D417184S, US-S-D417184, USD417184 S, USD417184S
InventorsTom Hartmann, John M. Morgenstern, Daniel Sokol
Original AssigneeLockheed Martin Corporation
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Supersonic business jet
US D417184 S
Abstract  available in
Images(5)
Previous page
Next page
Claims(1)
  1. We claim the ornamental design for: supersonic business jet, as shown and described.
Description

FIG. 1 is a top right rear perspective view of a supersonic business jet;

FIG. 2 is a top plan view thereof;

FIG. 3 is a left side elevation view thereof, right side being a mirror image;

FIG. 4 is a bottom plan view thereof;

FIG. 5 is a rear elevation view thereof; and,

FIG. 6 is a front elevation view thereof.

Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US6575406Mar 22, 2001Jun 10, 2003The Boeing CompanyIntegrated and/or modular high-speed aircraft
US6651928Sep 5, 2002Nov 25, 2003The Boeing CompanyAircraft engine nacelles and methods for their manufacture
US6698684Mar 22, 2002Mar 2, 2004Gulfstream Aerospace CorporationSupersonic aircraft with spike for controlling and reducing sonic boom
US6705567May 6, 2002Mar 16, 2004The Boeing CompanyTandem wing aircraft and method for manufacturing and operating such aircraft
US6729577Dec 6, 2001May 4, 2004Lockheed Martin CorporationTail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom
US6938854Mar 21, 2003Sep 6, 2005The Boeing CompanyIntegrated and/or modular high-speed aircraft
US6959896 *Jul 3, 2003Nov 1, 2005Lockheed Martin CorporationPassive aerodynamic sonic boom suppression for supersonic aircraft
US6966524Nov 6, 2003Nov 22, 2005The Boeing CompanyAircraft engine nacelles and methods for their manufacture
US7252263Jul 29, 2004Aug 7, 2007Hawker Beechcraft CorporationDesign methods and configurations for supersonic aircraft
US7311287 *Mar 11, 2005Dec 25, 2007Supersonic Aerospace International, LlcMethods for incorporating area ruled surfaces in a supersonic aircraft
US7581697May 2, 2007Sep 1, 2009Hawker Beechcraft CorporationDesign methods and configurations for supersonic aircraft
US7644888May 15, 2002Jan 12, 2010The Boeing CompanyHigh-speed aircraft and methods for their manufacture
US7837142 *Oct 9, 2007Nov 23, 2010Aerion CorporationSupersonic aircraft jet engine
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
US8789789May 23, 2011Jul 29, 2014Gulfstream Aerospace CorporationSupersonic aircraft with spike for controlling and reducing sonic boom
US20110133021 *Sep 29, 2010Jun 9, 2011Hypermach Aerospace Industries IncorporatedSupersonic aircraft with shockwave canceling aerodynamic configuration
Classifications
U.S. ClassificationD12/333, D12/319, D12/331