发明名称 Adjustable payload enclosure for wing
摘要 An enclosure (100) for carrying an adjustable payload (150). The enclosure (100) is beneficially used on a rotorcraft blade or other similar structure. The enclosure (100) has a first element (104, 106) having a first flange (124, 126) and an upper element (102). The first element (104, 106) has an upper surface (170) which has a first angle (160) with respect to a lower surface of the first flange (124, 126) in a direction extending from an inboard direction to an outboard direction. The upper element (102) has a lower surface (172) which has a second angle (158) with respect to an upper surface (114) of said upper element (102) in a direction extending from an inboard direction to an outboard direction, the lower surface (172) being in contact with the upper surface (170) of said first element (104, 106), the second angle (158) being in a direction which is opposite to the direction of said first angle (160). The first element (104, 106) and the upper element (102) define a cavity for holding a payload (150).
申请公布号 EP2711293(A2) 申请公布日期 2014.03.26
申请号 EP20130185958 申请日期 2013.09.25
申请人 THE BOEING COMPANY 发明人 GILL - III, FRANK JOSEPH;CAWTHORNE, MATTHEW HOWARD;CLINE, CHRISTOPHER JAMES;PANNEERSELVAM, DINESH;FAY, RUSSELL EDDY
分类号 B64C27/473 主分类号 B64C27/473
代理机构 代理人
主权项
地址