公开(公告)号：US20050178907A1

公开(公告)日：2005-08-18

申请号：US11041616

申请日：2005-01-24

申请人： Mitchell Piorkowski ,  Paul Bandy ,  Darrell Gaston ,  Binh Truong ,  Dwight Schaeffer ,  Shannon Kupfer ,  Steven Flickinger ,  Julie Shinn ,  James Johnson ,  Steven Wehr ,  Mark Smith

发明人： Mitchell Piorkowski ,  Paul Bandy ,  Darrell Gaston ,  Binh Truong ,  Dwight Schaeffer ,  Shannon Kupfer ,  Steven Flickinger ,  Julie Shinn ,  James Johnson ,  Steven Wehr ,  Mark Smith

IPC分类号： B64C1/14 ,  B64D45/00 ,  G07C9/00 ,  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。

公开(公告)号：US20050218266A1

公开(公告)日：2005-10-06

申请号：US11128809

申请日：2005-05-13

申请人： Paul Bandy ,  Darrell Gaston ,  Binh Truong ,  Dwight Schaeffer ,  Shannon Kupfer ,  Steven Flickinger ,  Steven Wehr ,  James Johnson ,  Julie Shinn ,  Mark Smith

发明人： Paul Bandy ,  Darrell Gaston ,  Binh Truong ,  Dwight Schaeffer ,  Shannon Kupfer ,  Steven Flickinger ,  Steven Wehr ,  James Johnson ,  Julie Shinn ,  Mark Smith

IPC分类号： B64C1/14 ,  B64D45/00 ,  G07C9/00 ,  B64D11/00

CPC分类号： B64D45/0015 ,  B64C1/1469 ,  B64C2001/009 ,  G07C9/00142 ,  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. The switch further provides a cut-off switch which enables the power to be removed from the system if necessary. In addition, a display system may be employed to notify the occupants of the cockpit that entry into the cockpit has been requested.

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。 该开关进一步提供一个截止开关，其能够在必要时从系统中移除电力。 此外，可以使用显示系统来通知驾驶舱的乘客已经请求进入驾驶舱的入口。

公开(公告)号：US20070030172A1

公开(公告)日：2007-02-08

申请号：US11199043

申请日：2005-08-08

申请人： Paul Bandy ,  Darrell Gaston ,  Toan Le ,  Dwight Schaeffer ,  Robert Metzger ,  Dai Pham

发明人： Paul Bandy ,  Darrell Gaston ,  Toan Le ,  Dwight Schaeffer ,  Robert Metzger ,  Dai 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。

公开(公告)号：US20070093915A1

公开(公告)日：2007-04-26

申请号：US11566101

申请日：2006-12-01

申请人： Paul Bandy ,  Darrell Gaston ,  Toan Le

发明人： Paul Bandy ,  Darrell Gaston ,  Toan Le

IPC分类号： G05B13/02 ,  G05B19/18

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为模拟数据。

公开(公告)号：US20070030185A1

公开(公告)日：2007-02-08

申请号：US11196691

申请日：2005-08-03

申请人： Paul Bandy ,  Darrell Gaston ,  Toan Le

发明人： Paul Bandy ,  Darrell Gaston ,  Toan Le

IPC分类号： H03M9/00

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.

公开(公告)号：US20070013556A1

公开(公告)日：2007-01-18

申请号：US11181513

申请日：2005-07-14

申请人： Darrell Gaston

发明人： Darrell Gaston

IPC分类号： G08B21/00

CPC分类号： H01H19/60 ,  H01H36/0006

摘要： An apparatus and method for rotary code-based control for command systems. A flight deck module comprises a knob connected to a shaft; a plurality of sensors affixed to a surface of a printed circuit board, the printed circuit board connected to the shaft; and a carrier platter. The carrier platter is connected to the shaft and a plurality of sources is affixed onto a first side of the carrier platter in an arcuate orientation (such as in a circular fashion along the circumference of the carrier platter or spanning a sector of a circle).

摘要翻译： 一种用于命令系统的旋转码型控制的装置和方法。 飞行甲板模块包括连接到轴的旋钮; 多个传感器固定在印刷电路板的表面上，印刷电路板连接到轴上; 和一个载体拼盘。 载体盘片连接到轴上，并且多个源以弧形取向（例如沿着载架拼盘的圆周或跨越圆形扇形的圆形方式）固定在载体盘片的第一侧上。