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1. 发明授权

US4541595A Removable interior window unit for aircraft 失效
标题翻译：飞机内置可拆卸机组
公开(公告)号：US4541595A
公开(公告)日：1985-09-17
申请号：US479674
申请日：1983-03-28
申请人： Peter E. Fiala , Gerald E. Davis , Alan J. Tuma , Jack E. Hart
发明人： Peter E. Fiala , Gerald E. Davis , Alan J. Tuma , Jack E. Hart
IPC分类号： B64C1/14
CPC分类号： B64C1/1492 , Y10T292/0901 , Y10T292/0902
摘要： In an aircraft having a pressure window mounted in the hull, an interior window assembly is removably mounted in an interior wall spaced from the hull. The interior window assembly is in register with the pressure window to enable occupants of the aircraft to view the outside. The interior wall has an opening formed therein to accept the interior window assembly and the portions of the wall surrounding the opening are biased toward the interior of the aircraft. The interior window assembly includes a windowpane mounted in a frame. The frame includes a flange that overlies the inboard surface of the portions of the wall surrounding the opening, and the bias of the wall portions is exerted on the flange. A constraint means is affixed to the hull of the aircraft and releasably engages the frame to constrain the frame from inboard movement. The bias force of the wall portions and the constraint means cooperate to hold the window in place. Preferably, the interior wall is comprised of stiffly flexible panel members that are flexed upon placement of the window assembly into the opening and tend to return to their unflexed state, thereby exerting the bias force on the flange.
摘要翻译：在具有安装在船体中的压力窗的飞行器中，内部窗组件可移除地安装在与船体间隔开的内壁中。内部窗组件与压力窗口对准，以使飞机的乘客能够观察外部。内壁具有形成在其中的开口以接纳内部窗户组件，并且围绕开口的壁的部分朝向飞行器的内部偏置。内窗组件包括安装在框架中的窗玻璃。框架包括覆盖围绕开口的壁的部分的内侧表面的凸缘，并且壁部分的偏压施加在凸缘上。约束装置固定在飞行器的船体上并且可释放地接合框架以将框架从内侧运动限制。壁部分和约束装置的偏压力协调以将窗口保持在适当的位置。优选地，内壁由刚性柔性的面板构件组成，其在将窗组件放置在开口中时弯曲，并且倾向于返回到其非折叠状态，从而在凸缘上施加偏压力。

2. 发明授权

US5882386A Device for separating moisture from gas vented from an aircraft 失效
标题翻译：从飞机排出的气体中分离水分的装置
公开(公告)号：US5882386A
公开(公告)日：1999-03-16
申请号：US948614
申请日：1997-10-10
申请人： Blayne A. McAferty , Timothy W. Morgan , Peter E. Fiala
发明人： Blayne A. McAferty , Timothy W. Morgan , Peter E. Fiala
IPC分类号： B01D45/08 , B01D53/26
CPC分类号： B01D45/08 , B01D53/26
摘要： A device for separating moisture from a gas flow which is vented from an interior region of an aircraft to a region exterior to the aircraft. In a preferred embodiment, a vessel having an inlet port coupled to the interior region of the aircraft, an outlet port coupled to the region exterior to the aircraft, and at least one baffle member positioned between the inlet port and the outlet port. The baffle member extends away from a wall of the vessel, at least partially transverse to a flow of gas passing through the vessel from the inlet port to the outlet port. The flow passes adjacent to the at least one baffle member such that a surface of the baffle member collects moisture thereon. The moisture is returned, via a canted vessel surface, through the inlet port of the vessel and to the interior region of the aircraft.
摘要翻译：用于从气流的内部区域排出到飞机外部区域的气流分离湿气的装置。在优选实施例中，具有联接到飞行器的内部区域的入口端口的船舶，连接到飞行器外部的区域的出口端口和位于入口端口和出口端口之间的至少一个挡板构件。挡板构件远离容器的壁延伸，至少部分横向于从入口到出口通过容器的气体流。流体流过邻近于至少一个挡板构件，使得挡板构件的表面在其上收集水分。水分通过倾斜的容器表面通过容器的入口和飞行器的内部区域返回。

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