公开(公告)号：US20140086750A1

公开(公告)日：2014-03-27

申请号：US13625959

申请日：2012-09-25

申请人： Matthew Howard Cawthorne ,  Christopher James Cline ,  Dinesh Panneerselvam ,  Frank Joseph Gill, III ,  Russell Eddy Fay

发明人： Matthew Howard Cawthorne ,  Christopher James Cline ,  Dinesh Panneerselvam ,  Frank Joseph Gill, III ,  Russell Eddy Fay

IPC分类号： B64D9/00 ,  B23P15/04 ,  B29C65/00

CPC分类号： B64D9/00 ,  B23P15/04 ,  B29C65/002 ,  B64C27/008 ,  B64C27/473 ,  Y10T29/49337

摘要： An enclosure for carrying an adjustable payload. The enclosure is beneficially used on a rotorcraft blade or other similar structure. The enclosure has a first element having a first flange and an upper element. The first element has an upper surface which has a first angle with respect to a lower surface of the first flange in a direction extending from an inboard direction to an outboard direction. The upper element has a lower surface which has a second angle with respect to an upper surface of said upper element in a direction extending from an inboard direction to an outboard direction, the lower surface being in contact with the upper surface of said first element, the second angle being in a direction which is opposite to the direction of said first angle. The first element and the upper element define a cavity for holding a payload.

摘要翻译： 用于承载可调整有效载荷的外壳。 外壳有利地用于旋翼飞机刀片或其他类似的结构。 外壳具有第一元件，其具有第一凸缘和上部元件。 第一元件具有在从内侧方向延伸到外侧方向的方向上相对于第一凸缘的下表面具有第一角度的上表面。 上部元件具有下表面，该下表面在从内侧方向延伸到外侧方向的方向上相对于所述上部元件的上表面具有第二角度，下表面与所述第一元件的上表面接触， 所述第二角度在与所述第一角度的方向相反的方向上。 第一元件和上部元件限定用于保持有效载荷的空腔。

公开(公告)号：US09403594B2

公开(公告)日：2016-08-02

申请号：US13625959

申请日：2012-09-25

申请人： Frank Joseph Gill, III ,  Matthew Howard Cawthorne ,  Christopher James Cline ,  Dinesh Panneerselvam ,  Russell Eddy Fay

发明人： Frank Joseph Gill, III ,  Matthew Howard Cawthorne ,  Christopher James Cline ,  Dinesh Panneerselvam ,  Russell Eddy Fay

IPC分类号： B64D9/00 ,  B29C65/00 ,  B23P15/04 ,  B64C27/473 ,  B64C27/00

CPC分类号： B64D9/00 ,  B23P15/04 ,  B29C65/002 ,  B64C27/008 ,  B64C27/473 ,  Y10T29/49337

摘要： An enclosure for carrying an adjustable payload. The enclosure is beneficially used on a rotorcraft blade or other similar structure. The enclosure has a first element having a first flange and an upper element. The first element has an upper surface which has a first angle with respect to a lower surface of the first flange in a direction extending from an inboard direction to an outboard direction. The upper element has a lower surface which has a second angle with respect to an upper surface of said upper element in a direction extending from an inboard direction to an outboard direction, the lower surface being in contact with the upper surface of said first element, the second angle being in a direction which is opposite to the direction of said first angle. The first element and the upper element define a cavity for holding a payload.

摘要翻译： 用于承载可调整有效载荷的外壳。 外壳有利地用于旋翼飞机刀片或其他类似的结构。 外壳具有第一元件，其具有第一凸缘和上部元件。 第一元件具有在从内侧方向延伸到外侧方向的方向上相对于第一凸缘的下表面具有第一角度的上表面。 上部元件具有下表面，该下表面在从内侧方向延伸到外侧方向的方向上相对于所述上部元件的上表面具有第二角度，下表面与所述第一元件的上表面接触， 所述第二角度在与所述第一角度的方向相反的方向上。 第一元件和上部元件限定用于保持有效载荷的空腔。