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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|