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1. 发明授权

US06924744B2 Light emitting diode indicator 有权
标题翻译：发光二极管指示灯
公开(公告)号：US06924744B2
公开(公告)日：2005-08-02
申请号：US10329111
申请日：2002-12-23
申请人： Richard A. Bohlander , Robert W. Metzger , Dwight R. Schaeffer
发明人： Richard A. Bohlander , Robert W. Metzger , Dwight R. Schaeffer
IPC分类号： B60Q3/04 , F21S8/00 , G08B5/22
CPC分类号： B60Q3/14 , F21W2111/00 , F21Y2107/90 , F21Y2115/10 , Y10S362/80 , Y10S362/812
摘要： A Light Emitting Diode (LED) indicator that more efficiently dissipates heat generated by LEDs and other circuit components is provided. The LED indicator includes a housing and a printed circuit board contained within the housing. The printed circuit board includes first and second sides with two or more LEDs attached to the first and second sides of the printed circuit board and a regulating circuit for regulating current supplied to the LEDs. The regulating circuit includes a linear voltage regulator. The printed circuit board includes first and second thermal dissipation sections. The first thermal dissipation section is thermally connected with the two or more LEDs and the second thermal dissipation section is thermally connected with the linear voltage regulator. The housing is at least partially lined with a plurality of reflectors for reflecting light generated by the LEDs through a lens.
摘要翻译：提供了更有效地散发由LED和其他电路部件产生的热量的发光二极管（LED）指示器。 LED指示器包括壳体和包含在壳体内的印刷电路板。印刷电路板包括具有连接到印刷电路板的第一和第二侧上的两个或更多个LED的第一和第二侧以及用于调节供应到LED的电流的调节电路。调节电路包括一个线性稳压器。印刷电路板包括第一和第二散热部分。第一散热部分与两个或更多个LED热连接，并且第二散热部分与线性稳压器热连接。壳体至少部分地衬有多个用于通过透镜反射由LED产生的光的反射器。

2. 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。

3. 发明授权

US06587056B1 Solid state flight deck modules and components thereof 有权
标题翻译：固态飞行甲板模块及其组件
公开(公告)号：US06587056B1
公开(公告)日：2003-07-01
申请号：US09540103
申请日：2000-03-31
申请人： Charles R. Fraser , Robert W. Metzger , Marshall T. Okamoto , Dwight R. Schaeffer , Richard A. Bohlander , Toan D. Le , Barrie W. Hughlock , Richard M. Schatz , Rex McCleary
发明人： Charles R. Fraser , Robert W. Metzger , Marshall T. Okamoto , Dwight R. Schaeffer , Richard A. Bohlander , Toan D. Le , Barrie W. Hughlock , Richard M. Schatz , Rex McCleary
IPC分类号： G08B2100
CPC分类号： H03K17/97 , H01H13/023 , H01H13/564 , H01H19/635 , H01H27/063 , H01H2011/0043 , H01H2013/026 , H01H2019/143 , H01H2219/028 , H01H2219/06 , H01H2219/066 , H05K5/0017
摘要： A conventional light plate for a systems control panel is mounted on a machined front plate which, in turn, is maintained a predetermined uniform distance from a front printed wiring assembly (PWA). A plurality of systems control devices including one or more of switches (toggle switches, rotary switches, push button switches), rheostats and annunciators are mounted on the front plate and front PWA. Each of the systems control devices has one or more solid state elements mounted on the PWA. For example, the switches carry small magnets which, by manipulation of operating switch levers or knobs, move into and out of close proximity to magnet sensitive switching devices mounted on the front PWA.
摘要翻译：用于系统控制面板的传统的光板安装在机加工的前板上，该前板又与前印刷线路组件（PWA）保持预定的均匀距离。包括一个或多个开关（拨动开关，旋转开关，按钮开关），变阻器和信号器的多个系统控制装置安装在前板和前PWA上。每个系统控制装置具有安装在PWA上的一个或多个固态元件。例如，这些开关携带小的磁体，通过操作操作开关杆或旋钮，它们进入和离开安装在前PWA上的磁敏开关装置的外部。

4. 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。

5. 发明授权

US5695156A Aircraft vertical position control system 失效
标题翻译：飞机垂直位置控制系统
公开(公告)号：US5695156A
公开(公告)日：1997-12-09
申请号：US441284
申请日：1995-05-15
申请人： Guner Firuz , Dwight R. Schaeffer
发明人： Guner Firuz , Dwight R. Schaeffer
IPC分类号： G05D1/06 , G05D1/08
CPC分类号： G05D1/0607
摘要： Aircraft input signals of selected altitude (h.sub.s), selected vertical speed (h.sub.s), current altitude (h), current vertical speed (h), current pitch attitude (.theta.), current normal acceleration (N.sub.z) and current pitch rate (Q) are processed to produce an elevator command (.delta..sub.e) that will result in a smooth vertical transition of the aircraft for various autopilot vertical maneuvers, including altitude capture and hold, glideslope capture and hold, and flare control.
摘要翻译：所选高度（hs），所选垂直速度（+ E，点h + EE s），当前高度（h），当前垂直速度（+ E，点h + EE），当前俯仰姿态（theta）当前正常加速度（Nz）和当前俯仰速率（Q）被处理以产生将导致飞机对于各种自动驾驶仪垂直操纵的平滑垂直转换的升降机命令（delta e），包括高度捕捉和保持，下坡掠夺和持有和闪光控制。

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