公开(公告)号：US08946603B2

公开(公告)日：2015-02-03

申请号：US13234895

申请日：2011-09-16

申请人： Kenneth M. Reynolds ,  Charles F. Forster

发明人： Kenneth M. Reynolds ,  Charles F. Forster

IPC分类号： H05B3/06 ,  H05B3/00 ,  H05B11/00 ,  E03B7/10 ,  F16L53/00 ,  F24H1/10 ,  H05B3/78 ,  B64D11/02

CPC分类号： F16L53/008 ,  B64D11/02 ,  F16L53/38

摘要： An aircraft drain/fill fitting includes a housing adapted for being fitted into an opening between an aircraft interior and an aircraft exterior. The housing has an interior housing segment fluidly coaxially communicating with an exterior housing segment to define a liquid flow path therethrough, and a heater for applying heat to the interior housing segment. A hollow insert element is positioned in the interior housing segment in heat transfer contact with an inner wall of the interior housing segment. An elongate heat transfer probe is positioned in heat transfer contact with the hollow insert element and extends into the exterior housing segment to reduce the incidence of freezing of liquid in the exterior housing segment.

摘要翻译： 飞机排水/填充配件包括适于安装在飞行器内部和飞行器外部之间的开口中的壳体。 壳体具有与外部壳体段流体同轴地连通以限定穿过其中的液体流动通道的内部壳体段和用于向内部壳体段施加热量的加热器。 中空插入元件与内部壳体段的内壁热传递接触地定位在内部壳体段中。 细长的热传递探针定位成与中空插入元件传热接触并延伸到外部壳体段中以减少外部壳体段中的液体的冻结的发生。

公开(公告)号：US20130068752A1

公开(公告)日：2013-03-21

申请号：US13234895

申请日：2011-09-16

申请人： Kenneth M. Reynolds ,  Charles F. Forster

发明人： Kenneth M. Reynolds ,  Charles F. Forster

IPC分类号： H05B3/06

CPC分类号： F16L53/008 ,  B64D11/02 ,  F16L53/38

摘要： An aircraft drain/fill fitting includes a housing adapted for being fitted into an opening between an aircraft interior and an aircraft exterior. The housing has an interior housing segment fluidly coaxially communicating with an exterior housing segment to define a liquid flow path therethrough, and a heater for applying heat to the interior housing segment. A hollow insert element is positioned in the interior housing segment in heat transfer contact with an inner wall of the interior housing segment. An elongate heat transfer probe is positioned in heat transfer contact with the hollow insert element and extends into the exterior housing segment to reduce the incidence of freezing of liquid in the exterior housing segment.

摘要翻译： 飞机排水/填充配件包括适于安装在飞行器内部和飞行器外部之间的开口中的壳体。 壳体具有与外部壳体段流体同轴地连通以限定穿过其中的液体流动通道的内部壳体段和用于向内部壳体段施加热量的加热器。 中空插入元件与内部壳体段的内壁热传递接触地定位在内部壳体段中。 细长的热传递探针定位成与中空插入元件传热接触并延伸到外部壳体段中以减少外部壳体段中的液体的冻结的发生。