发明名称 WINGED VEHICLE WITH DEPLOYABLE WINGS MOUNTED TO A TRANSLATING PIVOT MECHANISM
摘要 A winged vehicle (20) has an elongated fuselage (22), and a wing mechanism (38) affixed to the fuselage (22). The wing mechanism (38) includes a pivot track (40) affixed to and extending lengthwise along the fuselage (22), a pivot body (42) engaged to and translatable along the pivot track (40). A pair of wings (44) is pivotably affixed to the pivot body (42) and is movable between a stowed position wherein the wings (44) lie relatively close to the fuselage (22) when the pivot body (42) is in a first position (48) along the pivot track (40), and a deployed position wherein the wings (44) are deployed to extend relatively outwardly from the fuselage (22) when the pivot body (42) is in a second position (50) along the pivot track (40). An actuator (58) is operable to move the wings (44) from the stowed position to the deployed position.
申请公布号 WO2004099707(A3) 申请公布日期 2004.12.29
申请号 WO2003US26312 申请日期 2003.08.21
申请人 RAYTHEON CO 发明人 BOUCHARD MARK L;HIGGINS KEVIN J;EISENTRAUT RUDOLPH A;PLEMMONS ROBERT S;KOESSLER JEFFREY H
分类号 F42B10/18;H01Q1/42;H01Q9/04;H01Q9/28;H01Q13/10;H01Q13/18;H01Q21/00;H01Q23/00 主分类号 F42B10/18
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