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公开(公告)号：US20090248366A1
公开(公告)日：2009-10-01
申请号：US12055341
申请日：2008-03-26
IPC分类号： G06F15/00
摘要： An aircraft component assembly has an aircraft component for an aircraft. A sensor is configured to monitor the aircraft component. A local wireless transmitter is provided for communication with a remote receiver. In addition, a local wireless receiver is provided for communication with the remote transmitter. A processor is in communication with the sensor. The processor is configured to control the sensor, the local wireless transmitter and the local wireless receiver. A power source is configured to generate energy proximate the installed aircraft component.
摘要翻译： 飞机部件组件具有用于飞行器的飞行器部件。 传感器被配置为监视飞行器部件。 提供本地无线发射机用于与远程接收机通信。 此外，提供本地无线接收器用于与远程发射机通信。 处理器与传感器通信。 处理器被配置为控制传感器，本地无线发射器和本地无线接收器。 电源被配置为在安装的飞行器部件附近产生能量。
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2.发明授权公开(公告)号：US08335609B2
公开(公告)日：2012-12-18
申请号：US12692711
申请日：2010-01-25
IPC分类号： G06F7/00
CPC分类号： G07C5/0808 , G07C5/008
摘要： A method of exposing and recording embedded avionics data using dynamically assigned labels assigns a first plurality of data labels to aircraft controller parameters designated for at least one aircraft sub-controller. A second plurality of data labels are dynamically assigned to desired embedded parameters of an aircraft main controller. At least one data word storing one of the desired embedded parameters is created. The at least one data word has one of the second plurality of data labels. The at least one data word is exposed by transmitting the at least one data word to a selective recording device. The selective recording device records the at least one data word.
摘要翻译： 使用动态分配的标签曝光和记录嵌入式航空电子数据的方法将第一多个数据标签分配给为至少一个飞行器子控制器指定的飞行器控制器参数。 动态地将第二多个数据标签分配给飞行器主控制器的期望的嵌入参数。 创建存储期望的嵌入参数之一的至少一个数据字。 所述至少一个数据字具有第二多个数据标签中的一个。 通过将至少一个数据字发送到选择性记录装置来暴露所述至少一个数据字。 选择记录装置记录至少一个数据字。
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公开(公告)号：US20120191830A1
公开(公告)日：2012-07-26
申请号：US13012880
申请日：2011-01-25
IPC分类号： G06F15/173
CPC分类号： G06Q10/06
摘要： The example avionic data communication management arrangement includes a common infrastructure having a first account and a second account. The first account is configured to receive and store avionic data collected from a first aircraft. The second account is configured to receive and store avionic data collected from a second aircraft that is from a different airline than the first aircraft. The avionic data within the first account and the avionic data within the second account can both be accessed or managed by an administrating entity.
摘要翻译： 示例性航空电子数据通信管理装置包括具有第一帐户和第二帐户的公共基础设施。 第一个帐户配置为接收和存储从第一架飞机收集的航空电子数据。 第二帐户被配置为接收和存储从与第一飞行器不同的航空公司从第二飞机收集的航空电子数据。 第一个帐户内的航空电子数据和第二个帐户内的航空电子数据都可以被管理实体访问或管理。
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公开(公告)号：US08527240B2
公开(公告)日：2013-09-03
申请号：US12055341
申请日：2008-03-26
摘要： An aircraft component assembly has an aircraft component for an aircraft. A sensor is configured to monitor the aircraft component. A local wireless transmitter is provided for communication with a remote receiver. In addition, a local wireless receiver is provided for communication with the remote transmitter. A processor is in communication with the sensor. The processor is configured to control the sensor, the local wireless transmitter and the local wireless receiver. A power source is configured to generate energy proximate the installed aircraft component.
摘要翻译： 飞机部件组件具有用于飞行器的飞行器部件。 传感器被配置为监视飞行器部件。 提供本地无线发射机用于与远程接收机通信。 此外，提供本地无线接收器用于与远程发射机通信。 处理器与传感器通信。 处理器被配置为控制传感器，本地无线发射器和本地无线接收器。 电源被配置为在安装的飞行器部件附近产生能量。
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公开(公告)号：US4248056A
公开(公告)日：1981-02-03
申请号：US38126
申请日：1979-05-11
申请人： William H. Beacham
发明人： William H. Beacham
CPC分类号： F25B30/02 , F25B31/006
摘要： This invention relates to a heat reclaiming device for a heat pump. The heat reclaimer is able to absorb heat from the compressor by circulating cooling fluid through a circuit which is mounted in good heat transfer relationship with the condenser, then around the shell of the motor-compressor and lastly around the hollow tube which connects the condenser to the compressor. The reclaiming circuit is connected into a fluid circulating loop which is used to supply heat to the evaporator coil of the heat pump.
摘要翻译： 本发明涉及一种用于热泵的热回收装置。 热回收机能够通过将冷却流体循环通过与冷凝器以良好的热传递关系安装的电路，然后围绕电动机 - 压缩机的壳体并且最后围绕将冷凝器连接到的中空管的循环来吸收来自压缩机的热量 压缩机。 回收回路连接到用于向热泵的蒸发器盘管供热的流体循环回路中。
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公开(公告)号：US08965291B2
公开(公告)日：2015-02-24
申请号：US12835031
申请日：2010-07-13
CPC分类号： H04W72/085 , H04B7/18506 , H04L12/5692 , H04W72/00 , H04W72/02 , H04W76/10 , H04W84/06
摘要： An example avionic data communication method includes establishing a plurality of available channels using a channel controller. The channel controller also establishes a quality of service for each of the plurality of available channels. The channel controller then selects one of the available channels. The quality of service of the selected channel is not less than the quality of service of another channel within the plurality of available channels. The method then communicates a type of data using the selected channel.
摘要翻译： 示例性航空电子数据通信方法包括使用信道控制器建立多个可用信道。 信道控制器还为多个可用信道中的每一个建立服务质量。 频道控制器然后选择一个可用频道。 所选频道的服务质量不低于多个可用频道内另一频道的服务质量。 然后，该方法使用所选择的信道来传送一种类型的数据。
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公开(公告)号：US20110252295A1
公开(公告)日：2011-10-13
申请号：US12757449
申请日：2010-04-09
CPC分类号： G06F11/1004 , G07C5/008
摘要： An example method of verifying avionic data includes establishing a first cyclical redundancy check value associated with a data file. The first cyclical redundancy value is established on an aircraft. The method transmits the data file from the aircraft to a ground system. The method receives a second cyclical redundancy check value associated with the data file. The second cyclical redundancy check value is established by the ground system. The method determines the transmitted data file integrity by comparing the first cyclical redundancy check value to the second cyclical redundancy check value. An example aircraft avionic data verification arrangement includes a collector device that assembles avionic data into a data file that is transmittable to a ground system. A controller is programmed to provide a first cyclical redundancy check value associated with the data file and to identify errors in the data file received by the ground system based on a comparison between the first cyclical redundancy check value and a second cyclical redundancy check value established by the ground system.
摘要翻译： 验证航空电子数据的示例性方法包括建立与数据文件相关联的第一循环冗余校验值。 第一个循环冗余值是在飞机上建立的。 该方法将数据文件从飞机发送到地面系统。 该方法接收与数据文件相关联的第二循环冗余校验值。 第二个循环冗余校验值由地面系统建立。 该方法通过将第一循环冗余校验值与第二循环冗余校验值进行比较来确定发送的数据文件的完整性。 飞机航空电子数据验证装置的示例包括将航空电子数据组装成可传输到地面系统的数据文件的收集器装置。 控制器被编程为提供与数据文件相关联的第一循环冗余校验值，并且基于第一循环冗余校验值与由第二循环冗余校验值建立的第二循环冗余校验值之间的比较来识别由地面系统接收的数据文件中的错误 地面系统。
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公开(公告)号：US20090243854A1
公开(公告)日：2009-10-01
申请号：US12055345
申请日：2008-03-26
IPC分类号： G08B13/22
CPC分类号： G06Q10/06 , G06Q50/30 , G07C5/008 , G07C5/0841
摘要： A method of aircraft maintenance involves storing part information relating to an aircraft part on the aircraft part. The part information is wirelessly transmitting from the aircraft part to a receiver. A note of a change relating to the aircraft part is made. The part information with the note of the change relating to the aircraft part is electronically stored at a location remote from the aircraft part.
摘要翻译： 飞机维修的方法涉及在飞机部件上存储有关飞行器部件的部件信息。 部件信息从飞行器部件无线地传送到接收器。 记录有关飞机零件的更改。 具有关于飞机部件的改变的部分信息被电子地存储在远离飞行器部件的位置处。
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公开(公告)号：US20120015606A1
公开(公告)日：2012-01-19
申请号：US12835031
申请日：2010-07-13
IPC分类号： H04B17/00
CPC分类号： H04W72/085 , H04B7/18506 , H04L12/5692 , H04W72/00 , H04W72/02 , H04W76/10 , H04W84/06
摘要： An example avionic data communication method includes establishing a plurality of available channels using a channel controller. The channel controller also establishes a quality of service for each of the plurality of available channels. The channel controller then selects one of the available channels. The quality of service of the selected channel is not less than the quality of service of another channel within the plurality of available channels. The method then communicates a type of data using the selected channel.
摘要翻译： 示例性航空电子数据通信方法包括使用信道控制器建立多个可用信道。 信道控制器还为多个可用信道中的每一个建立服务质量。 频道控制器然后选择一个可用频道。 所选频道的服务质量不低于多个可用频道内另一频道的服务质量。 然后，该方法使用所选择的信道来传送一种类型的数据。
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公开(公告)号：US20110184607A1
公开(公告)日：2011-07-28
申请号：US12692711
申请日：2010-01-25
CPC分类号： G07C5/0808 , G07C5/008
摘要： A method of exposing and recording embedded avionics data using dynamically assigned labels assigns a first plurality of data labels to aircraft controller parameters designated for at least one aircraft sub-controller. A second plurality of data labels are dynamically assigned to desired embedded parameters of an aircraft main controller. At least one data word storing one of the desired embedded parameters is created. The at least one data word has one of the second plurality of data labels. The at least one data word is exposed by transmitting the at least one data word to a selective recording device. The selective recording device records the at least one data word.
摘要翻译： 使用动态分配的标签曝光和记录嵌入式航空电子数据的方法将第一多个数据标签分配给为至少一个飞行器子控制器指定的飞行器控制器参数。 动态地将第二多个数据标签分配给飞行器主控制器的期望的嵌入参数。 创建存储期望的嵌入参数之一的至少一个数据字。 所述至少一个数据字具有第二多个数据标签中的一个。 通过将至少一个数据字发送到选择性记录装置来暴露所述至少一个数据字。 选择记录装置记录至少一个数据字。
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