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Publication numberWO2003076224 A3
Publication typeApplication
Application numberPCT/US2003/006496
Publication date2 Dec 2004
Filing date3 Mar 2003
Priority date4 Mar 2002
Also published asWO2003076224A2
Publication numberPCT/2003/6496, PCT/US/2003/006496, PCT/US/2003/06496, PCT/US/3/006496, PCT/US/3/06496, PCT/US2003/006496, PCT/US2003/06496, PCT/US2003006496, PCT/US200306496, PCT/US3/006496, PCT/US3/06496, PCT/US3006496, PCT/US306496, WO 03076224 A3, WO 03076224A3, WO 2003/076224 A3, WO 2003076224 A3, WO 2003076224A3, WO-A3-03076224, WO-A3-2003076224, WO03076224 A3, WO03076224A3, WO2003/076224A3, WO2003076224 A3, WO2003076224A3
InventorsGeorge A Teacherson
ApplicantGeorge A Teacherson
Export CitationBiBTeX, EndNote, RefMan
External Links: Patentscope, Espacenet
Ducted channel wing, high-lift devices and vehicles therefor
WO 2003076224 A3
Abstract
A channel-wing-ducted propulsor (30) high-lift combination is provided with additional high-lift generating devices (40) and the optional further combination of an ejector nozzle (43) for enhanced thrust which all may be provided with means for varying the lift vector generated by the device and also have variably directed thrust. Various vehicles using the propulsor are described as are method and means for using and controlling them.
Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US4819576 *20 Jan 198811 Apr 1989Shaw Chung Chen CHydrofoil - submarine vessel system
US5182960 *10 Dec 19912 Feb 1993Allied-Signal Inc.Bevel gear drive arrangement
US5215015 *16 Apr 19921 Jun 1993Hitachi, Ltd.Track system and vehicle having both magnetic and aerodynamic levitation, with wings on the vehicle carrying the whole weight at normal operating speeds
US6607162 *20 Apr 200119 Aug 2003Bae Systems PlcRing-wing aircraft
US6708086 *21 Jun 200116 Mar 2004Sue M. RichardVehicle computer
Classifications
International ClassificationB63H1/16, B64C15/00, B63B1/22, B60K, B63H11/103
Cooperative ClassificationB63H11/103
European ClassificationB63H11/103
Legal Events
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