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公开(公告)号：US6019315A
公开(公告)日：2000-02-01
申请号：US942591
申请日：1997-10-02
IPC分类号： B64C1/14
CPC分类号： B64C1/1423
摘要： A door and its frame especially in an aircraft are constructed for circulating air through the structure for preventing cold air from forming near the door in an aircraft cabin. For this purpose at least one air flow channel is provided in the door construction. The air flow channel communicates with at least one inlet port with at least one outlet port so positioned that air circulation is maintained through the door structure. The outlet port passes preferably through a cabin floor for discharging cold air into a space below the cabin floor.
摘要翻译： 门和其框架尤其是在飞行器中被构造用于使空气循环通过结构，以防止冷空气在飞机机舱内的门附近形成。 为此目的，在门结构中提供至少一个气流通道。 空气流动通道与至少一个入口端口连通，至少一个出口端口定位成通过门结构保持空气循环。 出口优选通过机舱地板，用于将冷空气排放到机舱底部的空间内。
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32.发明授权公开(公告)号：US07802732B2
公开(公告)日：2010-09-28
申请号：US10582570
申请日：2004-12-30
申请人： Thomas Scherer , Torsten Schwan , Georg Mühlthaler , Jan Dittmar
发明人： Thomas Scherer , Torsten Schwan , Georg Mühlthaler , Jan Dittmar
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , Y02T50/44
摘要： A device for temperature regulation of sections of the interior of an aircraft includes a controlled mixer valve for the mixing of engine bleed air and air that is cooler than the engine bleed air in order to obtain pre-tempered mixed air flowing out of the mixer valve; a distribution line connected to the outlet of the mixer valve which is connected to the respective sections by at least two supply lines; individual heating units assigned to the respective sections; sensors assigned to the individual sections for the respective actual temperatures; transmitters for the respective nominal temperatures; and a regulator unit which controls the mixer valve dependent upon the respective nominal temperatures and the respective actual temperatures in the individual areas.
摘要翻译： 用于飞行器内部的部分温度调节的装置包括用于混合发动机排出空气和比发动机放气更冷的空气的受控混合器阀，以获得从混合器阀流出的预调温混合空气 ; 连接到混合器阀的出口的分配线，其通过至少两条供应管线连接到各个部分; 分配给各个部分的各个加热单元; 分配给相应实际温度的各个部分的传感器; 发射机相应的标称温度; 以及调节器单元，其根据相应的标称温度和各个区域中的相应实际温度来控制混合器阀。
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公开(公告)号：US07766276B2
公开(公告)日：2010-08-03
申请号：US11614314
申请日：2006-12-21
申请人： Uwe Buchholz , Thomas Scherer
发明人： Uwe Buchholz , Thomas Scherer
IPC分类号： B64C1/18
CPC分类号： B64C1/18 , B64C1/068 , B64D13/00 , B64D2013/003 , B64D2013/0625
摘要： Aircraft fuselage with an upper deck, constructed as a passenger area, and a lower deck, including a freight area, and with a ventilation installation for the upper deck and lower deck, wherein a bilge area is constructed as a vacuum chamber against the freight area and is connected to the lower deck solely via flow orifices in the abutment area between a lower floor and the fuselage wall.
摘要翻译： 具有作为乘客区域构建的上甲板的飞机机身和包括货运区域的下甲板以及用于上甲板和下甲板的通风装置，其中舱底区域被构造为对货区的真空室 并且仅通过底板和机身壁之间的邻接区域中的流动孔口连接到下层甲板。
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公开(公告)号：US20100096118A1
公开(公告)日：2010-04-22
申请号：US12520240
申请日：2007-12-12
摘要： The invention concerns a cooling system for an aircraft with an air inlet (4) through which air from the environment of the aircraft enters a ram air channel (2), and an air outlet (6) through which air emerges from the ram air channel (2). A heat exchanger (10) is arranged in the ram air channel (2). A ventilation device (8) is in fluid communication with the ram air channel (2). Also connected to the ram air channel (2) is a distribution line (12) to cool at least one heat-loaded component of the aircraft, in particular a cabin air conditioning system, and/or to ventilate an installation space of the at least one heat-loaded component.
摘要翻译： 本发明涉及一种用于具有空气入口（4）的飞行器的冷却系统，来自飞行器环境的空气通过该进气口进入冲压空气通道（2）和空气出口（6），空气从冲压空气通道 （2）。 热交换器（10）设置在冲压空气通道（2）中。 通风装置（8）与冲压空气通道（2）流体连通。 还连接到冲压空气通道（2）的是分配线（12），用于冷却飞机的至少一个加热部件，特别是机舱空调系统，和/或至少使安装空间通风 一个热负荷组件。
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公开(公告)号：US07433354B2
公开(公告)日：2008-10-07
申请号：US11014284
申请日：2004-12-16
申请人： Thomas Scherer , Volker Von Doehlen
发明人： Thomas Scherer , Volker Von Doehlen
CPC分类号： H04L12/413 , H04L2012/40215 , H04L2012/40273
摘要： The present invention relates to a bus system for transmitting a data packet between multiple devices in an aircraft, which is based on the CAN data bus system, but has an expanded identification field, in which a fixed region is designed for identification of the manifold aircraft systems, through which each aircraft system may be addressed uniquely. According to an exemplary embodiment, the data packet may be sent with different priorities, through which “important” data packets have priority on the transmission medium.
摘要翻译： 本发明涉及一种用于在飞机中的多个设备之间传输数据分组的总线系统，其基于CAN数据总线系统，但具有扩展的识别字段，其中固定区域被设计用于识别多媒体飞行器 系统，每个飞机系统可以通过该系统被唯一地寻址。 根据示例性实施例，可以以不同的优先级发送数据分组，通过该优先级，“重要”数据分组在传输介质上具有优先权。
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36.发明申请公开(公告)号：US20080134703A1
公开(公告)日：2008-06-12
申请号：US10584901
申请日：2004-12-30
CPC分类号： B64D13/06 , B64D11/04 , B64D2013/0629 , B64D2013/0674 , F25B2400/06 , F25D17/02 , Y02T50/56
摘要： In a cooling system (10) for cooling heat-generating installations (44, 46, 48) in an aircraft, with a refrigerating installation (12), at least one refrigeration consumer (44, 46, 48) and a refrigeration transport system (14) connecting the refrigerating installation (12) and the refrigeration consumer (44,46, 48), it is provided that the refrigerating installation (12) comprises at least one refrigeration machine (18, 20) which covers the maximum refrigeration requirement of the at least one refrigeration consumer (44, 46, 48) and in that the at least one refrigeration consumer (44, 46, 48) is supplied with cold generated in the refrigerating installation (12) via a refrigerating agent circulating in the refrigeration transport system (14).
摘要翻译： 在用于冷却飞机中的发热设备（44,46,48）的冷却系统（10）中，具有冷藏设备（12），至少一个制冷消耗器（44,46,48）和制冷运输系统 14）连接制冷装置（12）和制冷消耗装置（44,46,48）时，制冷装置（12）包括至少一个制冷机（18,20） 至少一个制冷消耗器（44,46,48），并且所述至少一个制冷消耗器（44,46,48）经由在所述制冷运输系统中循环的制冷剂在所述制冷装置（12）中产生冷 （14）。
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公开(公告)号：US20070125906A1
公开(公告)日：2007-06-07
申请号：US10582572
申请日：2004-12-30
IPC分类号： B64D33/02
CPC分类号： F02C7/042 , B64D13/00 , F02C6/08 , Y02T50/56 , Y02T50/671 , Y10T137/0536 , Y10T137/0645
摘要： A ram air channel (10) for the supply of ambient air in an aircraft includes a first air inlet (12) and a main flow channel (16) which extends downstream of the first air inlet (12). In order to guarantee that the systems on board the aircraft are supplied, in a simple and reliable way, with the required ambient air in any operational state of the aircraft, ie. both during the flight and on the ground, the ram air channel (10) has a second air inlet (24) which is independent from the first air inlet (12).
摘要翻译： 用于在飞行器中供应环境空气的冲压空气通道（10）包括在第一空气入口（12）的下游延伸的第一空气入口（12）和主流动通道（16）。 为了保证飞机上的系统能够以简单可靠的方式提供飞机任何运行状态下所需的环境空气，即。 在飞行中和在地面上，冲压空气通道（10）具有独立于第一空气入口（12）的第二进气口（24）。
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38.发明申请公开(公告)号：US20070119584A1
公开(公告)日：2007-05-31
申请号：US10582570
申请日：2004-12-30
申请人： Thomas Scherer , Torsten Schwan , Georg Muhlthaler
发明人： Thomas Scherer , Torsten Schwan , Georg Muhlthaler
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , Y02T50/44
摘要： A process for temperature regulation of sections of the interior of an aircraft with the following steps: recording of the respective actual temperatures and the respective nominal temperatures in the individual sections; mixing of engine bleed air and air which is cooler than the engine bleed air in order to obtain pre-tempered mixed air at a temperature which essentially corresponds to the lowest of the nominal temperatures recorded; distribution of the pre-tempered mixed air to all sections; and post-tempering of the mixed air distributed to the sections with higher nominal temperature corresponding to the differences between the respective nominal temperatures and the respective actual temperatures can be carried out in a device with a controlled mixer valve for the mixing of engine bleed air and air that is cooler than the engine bleed air in order to obtain pre-tempered mixed air flowing out of the mixer valve; to a distribution line connected to the outlet of the mixer valve which is connected to the respective sections by means of at least two supply lines; individual heating units assigned to the respective sections; sensors assigned to the individual sections for the respective actual temperatures and transmitters for the respective nominal temperatures; a regulator unit which controls the mixer valve dependent upon the respective nominal temperatures and the respective actual temperatures in the individual areas in such a way that the pre-tempered mixed air is of a temperature which essentially corresponds to the lowest of the nominal temperatures for all sections, and which controls the heating units assigned to the other sections corresponding to the differences between the respective nominal temperatures and the respective actual temperatures.
摘要翻译： 一种用于对飞行器内部的部分进行温度调节的过程，具有以下步骤：在各个部分中记录相应的实际温度和相应的标称温度; 混合发动机排出空气和比发动机放气更冷的空气，以获得基本上对应于记录的最低标称温度的温度的预调温混合空气; 将预调混合空气分配到所有区段; 并且分配到具有相应于相应标称温度和相应实际温度之间的差异的具有较高标称温度的部分的混合空气的后回火可以在具有受控混合器阀的装置中进行，用于混合发动机排放空气和 比发动机冷却的空气排出空气，以获得从混合器阀流出的预调温混合空气; 连接到通过至少两条供应管线连接到各个部分的混合器阀的出口的分配线路; 分配给各个部分的各个加热单元; 分配给相应实际温度的各个部分的传感器和相应标称温度的发射器; 调节器单元，其根据相应的标称温度和各个区域中的相应实际温度来控制混合器阀，使得预调温混合空气的温度基本上对应于所有的最低标称温度 并且其控制分配给对应于相应标称温度和相应实际温度之间的差异的其它部分的加热单元。
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公开(公告)号：US20060000790A1
公开(公告)日：2006-01-05
申请号：US10883285
申请日：2004-06-30
申请人： Harrison Smiddy , Thomas Scherer
发明人： Harrison Smiddy , Thomas Scherer
IPC分类号： A47F5/00
CPC分类号： B42F7/06 , B43L1/00 , B43M99/001
摘要： An improved organizer is provided that may be hung on a CPU, cubicle partition, file cabinet or other structure commonly found in an office or work place. The organizer may include a single backing member connected to a variety of organizing elements or may be of a saddle-type where two backing members are connected together by one or more overhang straps thereby providing organizing elements on either side of the structure, such as a CPU. The organizing elements include pockets, trays, baskets, bulletin boards, dry erase boards and other types of display surfaces.
摘要翻译： 提供了一种改进的组织器，其可以挂在CPU，隔间分区，文件柜或办公室或工作场所常见的其他结构中。 组织器可以包括连接到各种组织元件的单个背衬构件，或者可以是鞍式，其中两个背衬构件通过一个或多个悬垂带连接在一起，从而在结构的两侧提供组织元件，例如 中央处理器。 组织元素包括口袋，托盘，篮子，公告板，干擦板和其他类型的显示表面。
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公开(公告)号：US20050189360A1
公开(公告)日：2005-09-01
申请号：US11009722
申请日：2004-12-10
申请人： Brandi Loucks , Thomas Scherer , Fred Reber
发明人： Brandi Loucks , Thomas Scherer , Fred Reber
CPC分类号： D06F95/002
摘要： A laundry basket has a bottom panel with a perimeter. A contiguous side wall extends generally upward from the perimeter of the bottom panel and terminates at an upper end. A basket interior is defined above the bottom panel and bounded by the side wall. A curved wall section of the side wall is curved concavely inward toward the basket interior. The bottom panel and the contiguous side wall, including the curved wall section, are formed of a primary material. A cushion pad is positioned generally at the upper end of the curved wall section and is formed from a secondary material that is softer than the primary material of the curved wall portion.
摘要翻译： 洗衣篮具有带有周边的底板。 连续的侧壁从底板的周边大致向上延伸并终止于上端。 篮子内部被限定在底板上方并且由侧壁限定。 侧壁的弯曲壁部分朝向篮内部凹入地向内弯曲。 包括弯曲壁部分的底板和相邻侧壁由主要材料形成。 缓冲垫通常位于弯曲壁部分的上端，并且由比弯曲壁部分的主要材料软的次级材料形成。
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