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1. 发明授权

US08398025B2 Avionic door lock system 有权
标题翻译：航空门锁系统
公开(公告)号：US08398025B2
公开(公告)日：2013-03-19
申请号：US11041616
申请日：2005-01-24
申请人： Mitchell J Piorkowski , Paul W Bandy , Darrell W Gaston, Jr. , Binh C Truong , Dwight R Schaeffer , Shannon J Kupfer , Steven D Flickinger , Julie M Shinn , James J Johnson , Steven L Wehr , Mark E Smith
发明人： Mitchell J Piorkowski , Paul W Bandy , Darrell W Gaston, Jr. , Binh C Truong , Dwight R Schaeffer , Shannon J Kupfer , Steven D Flickinger , Julie M Shinn , James J Johnson , Steven L Wehr , Mark E Smith
IPC分类号： B64C1/14 , B64D11/00
CPC分类号： G07C9/00142 , B64C1/1469 , B64C2001/009 , B64D45/0015 , G07C9/0069
摘要： A security system adapted for use on an aircraft to prevent unauthorized access into a cockpit area of the aircraft via a cockpit door. The system includes a keypad accessible by individuals in a cabin area of the aircraft. A logic system is in communication with the keypad and also with a switch disposed inside the cockpit. Occupants of the cockpit, via the switch, have the ability to manually unlock the cockpit door, to deny the request for entry, or to do nothing, in which case the door will be automatically unlocked after the expiration of a predetermined time interval. A pressure sensor in communication with the controller allows the electronic door locking member to be automatically overridden, and the door immediately opened, in the event of a decompression condition occurring in the cockpit.
摘要翻译：适于在飞机上使用的安全系统，以防止驾驶舱门未经授权地进入飞机的驾驶舱区域。该系统包括可由飞机机舱区域中的个人访问的键盘。逻辑系统与键盘通信，并且还具有设置在驾驶舱内部的开关。驾驶舱的乘客通过开关能够手动解锁驾驶舱门，拒绝进入请求或不做任何操作，在这种情况下门将在预定时间间隔到期后自动解锁。与控制器通信的压力传感器允许电子门锁定构件自动覆盖，并且在驾驶舱中发生减压状态的情况下，门立即打开。

2. 发明授权

US07312735B2 Parallel-to-serial converter 有权
标题翻译：并行到串行转换器
公开(公告)号：US07312735B2
公开(公告)日：2007-12-25
申请号：US11566101
申请日：2006-12-01
申请人： Paul W. Bandy , Darrell W. Gaston , Toan D. Le
发明人： Paul W. Bandy , Darrell W. Gaston , Toan D. Le
IPC分类号： H03M1/00
CPC分类号： H03M9/00
摘要： Method and system on an aircraft for converting plural data inputs and plural data outputs from a parallel format to a serial format is provided. The system includes an integrated software module that accepts plural variable number of inputs and generates a plural variable number of outputs; an analog input processing module that receives plural analog inputs, converts the analog inputs to digital data and sends the digital data to the integrated software module; a digital input processing module that receives discrete digital inputs and transfers the digital inputs to the integrated software module; a digital output module that receives data from the integrated software module; and an analog output module that receives digital data from the integrated software module and converts the digital data into analog data by using a digital to analog converter.
摘要翻译：提供了一种用于将多个数据输入和多个数据输出从并行格式转换为串行格式的飞行器上的方法和系统。该系统包括接收多个可变数目的输入并产生多个可变数目的输出的集成软件模块; 模拟输入处理模块，其接收多个模拟输入，将模拟输入转换成数字数据，并将数字数据发送到集成软件模块; 数字输入处理模块，其接收离散数字输入并将数字输入传送到集成软件模块; 数字输出模块，用于从集成软件模块接收数据; 以及模拟输出模块，其从集成软件模块接收数字数据，并通过使用数模转换器将数字数据转换成模拟数据。

3. 发明授权

US07180437B1 Parallel-to-serial converter 有权
公开(公告)号：US07180437B1
公开(公告)日：2007-02-20
申请号：US11196691
申请日：2005-08-03
申请人： Paul W. Bandy , Darrell W. Gaston , Toan D. Le
发明人： Paul W. Bandy , Darrell W. Gaston , Toan D. Le
IPC分类号： H03M1/00
CPC分类号： H03M9/00
摘要： Method and system on an aircraft for converting plural data inputs and plural data outputs from a parallel format to a serial format is provided. The system includes an integrated software module that accepts plural variable number of inputs and generates a plural variable number of outputs; an analog input processing module that receives plural analog inputs, converts the analog inputs to digital data and sends the digital data to the integrated software module; a digital input processing module that receives discrete digital inputs and transfers the digital inputs to the integrated software module; a digital output module that receives data from the integrated software module; and an analog output module that receives digital data from the integrated software module and converts the digital data into analog data by using a digital to analog converter.

4. 发明授权

US07327283B2 System and apparatus for flight deck module integration 有权
标题翻译：飞行甲板模块集成系统和装置
公开(公告)号：US07327283B2
公开(公告)日：2008-02-05
申请号：US11199043
申请日：2005-08-08
申请人： Paul W. Bandy , Darrell W. Gaston , Toan D. Le , Dwight R. Schaeffer , Robert W. Metzger , Dai H. Pham
发明人： Paul W. Bandy , Darrell W. Gaston , Toan D. Le , Dwight R. Schaeffer , Robert W. Metzger , Dai H. Pham
IPC分类号： G08B21/00
CPC分类号： G01C23/005
摘要： An integrated communication system in an aircraft is provided. The system includes a plurality of solid state flight deck modules in an integrated flight deck panel, wherein the solid state flight deck modules include a microcontroller for interfacing with at least one data bus controller via a local bus; and a light emitting diode (LED) module for controlling backlit illumination of the integrated flight deck panel. The controller sends information to plural solid state flight deck modules via local buses and uses a system bus to communicate with aircraft subsystems. The controller also uses a central power supply module to supply regulated power to the plural solid state flight deck modules. Furthermore, at least one solid state flight deck module includes an integrated panel brightness control module, master brightness control module and/or a master dim and test control module.
摘要翻译：提供飞机中的集成通信系统。该系统在集成飞行甲板面板中包括多个固态飞行甲板模块，其中固态飞行甲板模块包括微控制器，用于经由本地总线与至少一个数据总线控制器进行接口; 以及用于控制集成飞行甲板面板的背光照明的发光二极管（LED）模块。控制器通过本地总线向多个固态飞行甲板模块发送信息，并使用系统总线与飞机子系统进行通信。控制器还使用中央电源模块向多个固态驾驶舱模块提供调节的电力。此外，至少一个固态飞行甲板模块包括集成的面板亮度控制模块，主亮度控制模块和/或主模糊和测试控制模块。

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