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1. 发明申请

WO2008088575A1 ELECTRONIC FLIGHT DATA DISPLAY INSTRUMENT 审中-公开
标题翻译：电子飞行数据显示仪表
公开(公告)号：WO2008088575A1
公开(公告)日：2008-07-24
申请号：PCT/US2007/072853
申请日：2007-07-05
申请人： ASPEN AVIONICS INC. , BETHEL, Jeffrey
发明人： BETHEL, Jeffrey
IPC分类号： G06F19/00
CPC分类号： B64D43/00 , G01C23/00 , G01D7/02
摘要： An electronic display instrument configured to secure in a desired position over multiple pre-existing instrument holes in a dashboard of an aircraft in place of multiple conventional display instruments, each conventional instrument having a conventional readout. The instrument comprises a display screen having a plurality of readouts corresponding to the conventional readouts of the multiple conventional instruments that the electronic display instrument replaces. The instrument further includes a body having a front and a back opposite the front and a top and a bottom opposite the top. The body is positioned adjacent and connected to the display screen. The instrument also includes an electronics module protruding from the back of the body to position in one of the pre-existing instrument holes in the dashboard panel of the aircraft.
摘要翻译：一种电子显示仪器，其被配置为在飞行器的仪表板中的多个预先存在的仪器孔上固定在期望的位置，以代替多个常规显示仪器，每个常规仪器具有常规读出。该仪器包括显示屏，其具有与电子显示仪器所代替的多个常规仪器的常规读出相对应的多个读数。仪器还包括具有与前部相对的前部和后部以及与顶部相对的顶部和底部的本体。身体相邻并连接到显示屏。该仪器还包括一个电子模块，从电子模块的后部突出到位于飞行器仪表盘中的一个预先存在的仪器孔内。

2. 发明申请

WO2011017063A3 AVIONICS DEVICES, SYSTEMS AND METHODS 审中-公开
标题翻译： AVIONICS设备，系统和方法
公开(公告)号：WO2011017063A3
公开(公告)日：2011-03-31
申请号：PCT/US2010043285
申请日：2010-07-26
申请人： LYONS PETER , BETHEL JEFFREY , KYRIAKOS CONSTANTINOS , BRODEGARD WILLIAM , HEINZ PENNY , BERLIN DAVID , RIEB SEAN , MALERICH TONY , TURNER BRIAN , ASPEN AVIONICS INC
发明人： LYONS PETER , BETHEL JEFFREY , KYRIAKOS CONSTANTINOS , BRODEGARD WILLIAM , HEINZ PENNY , BERLIN DAVID , RIEB SEAN , MALERICH TONY , TURNER BRIAN
IPC分类号： H04N7/00
CPC分类号： G01C23/00 , G06F3/1423 , G09G2380/12
摘要： A method and system to select and display information on an avionics display screen is disclosed. The systems and methods allow for the selection and display of information using knobs to highlight and select the desired information for display. Also provided is a system for multiple pages or "tiles" within these pages for viewing windows simultaneously on a single screen of a display. The present general inventive concept also relates to systems and methods to provide multiple cues on an electronic display system altitude tape to a pilot in advance and impending approach to a predefined altitude. The present general inventive concept also relates to systems and methods to employ variable resolution topographical data based on display range for an avionics navigation display.
摘要翻译：公开了一种在航空电子显示屏上选择和显示信息的方法和系统。系统和方法允许使用旋钮选择和显示信息，以突出显示并选择所需的显示信息。还提供了用于在这些页面中的多个页面或“瓦片”的系统，用于在显示器的单个屏幕上同时观看窗口。本发明的总体构思还涉及在电子显示系统高度带上向飞行员提前提供多个提示并且即将到达预定高度的系统和方法。本发明总体构思还涉及基于航空电子导航显示器的显示范围采用可变分辨率地形数据的系统和方法。

3. 发明申请

WO2016164624A1 SYSTEM AND METHOD FOR ANGLE OF ATTACK INDICATION WITH NO DEDICATED SENSORS AND AIRCRAFT INFORMATION 审中-公开
标题翻译：没有专用传感器和飞机信息的攻击指示的系统和方法
公开(公告)号：WO2016164624A1
公开(公告)日：2016-10-13
申请号：PCT/US2016/026503
申请日：2016-04-07
申请人： ASPEN AVIONICS, INC. , CENTRO ITALIANO RICERCHE AEROSPAZIALI S.C.P.A.
发明人： GENITO, Nicola , CORRARO, Federico , GARBARINO, Luca , VITALE, Antonio , DE LELLIS, Ettore , BIBBY, David , RIEB, Sean , JONES, Kevin
IPC分类号： B64D43/00 , B64D43/02 , B64D45/00 , B64C13/02
CPC分类号： G01C23/00 , B64D43/02 , G06F8/61
摘要： A system for and method of indicating an angle of attack of an aircraft is provided. The system utilizes measurements from existing aircraft sensors so that a dedicated angle of attack sensor is not required. The system enables and benefits from a unique method that includes performing standard flight operations during a calibration flight. The system does not need any aerodynamic model of the aircraft because it utilizes information from the calibration flight to develop an estimated aerodynamic model of the specific airplane. The system utilizes the aerodynamic model and other information to estimate an angle of attack of the aircraft during flight. Finally, the system utilizes additional information to indicate the estimated angle of attack of the aircraft relative to an optimum angle of attack for the aircraft and/or a critical angle of attack of the aircraft. The system further enables recalibration, so as to accommodate aircraft aerodynamic modifications.
摘要翻译：提供了一种指示飞机的迎角的系统和方法。该系统利用现有飞行器传感器的测量结果，不需要专用的攻角传感器。该系统通过独特的方法实现并获益，包括在校准飞行期间执行标准飞行操作。该系统不需要飞机的任何空气动力学模型，因为它利用来自校准飞行的信息来开发特定飞机的估计空气动力学模型。该系统利用空气动力学模型和其他信息来估计飞行中飞机的迎角。最后，该系统利用附加信息来指示飞机相对于飞机的最佳迎角和/或飞机的临界迎角的估计迎角。该系统还能够重新校准，以适应飞机的空气动力学修改。

4. 发明申请

WO2011017063A2 AVIONICS DEVICES, SYSTEMS AND METHODS 审中-公开
标题翻译： AVIONICS设备，系统和方法
公开(公告)号：WO2011017063A2
公开(公告)日：2011-02-10
申请号：PCT/US2010/043285
申请日：2010-07-26
申请人： LYONS, Peter , BETHEL, Jeffrey , KYRIAKOS, Constantinos , BRODEGARD, William , HEINZ, Penny , BERLIN, David , RIEB, Sean , MALERICH, Tony , TURNER, Brian , ASPEN AVIONICS, INC.
发明人： LYONS, Peter , BETHEL, Jeffrey , KYRIAKOS, Constantinos , BRODEGARD, William , HEINZ, Penny , BERLIN, David , RIEB, Sean , MALERICH, Tony , TURNER, Brian
IPC分类号： H04N7/00
CPC分类号： G01C23/00 , G06F3/1423 , G09G2380/12
摘要： The present general inventive concept relates to methods and systems to select and display information on an avionics display screen. The systems and methods allow for the selection and display of information using knobs to highlight and select the desired information for display, eliminating the need for a cursor function. The systems and methods also provide for multiple pages and/or multiple windows or "tiles" within these pages and/or windows simultaneously on a single screen of a display, with each window, page, and/or tile being fully controlled independently when selected. The present general inventive concept also relates to systems and methods to provide multiple cues on an electronic display system altitude tape to a pilot in advance and impending approach to a predefined altitude. The present general inventive concept also relates to systems and methods to employ variable resolution topographical data based on display range for an avionics navigation display. The present general inventive concept provides a system and method to use alpha blending properties of a graphics processor to dim the display, effectively darkening it with neutral color overlays, beyond the last hardware dimming step.
摘要翻译：本发明总体构思涉及在航空电子显示屏上选择和显示信息的方法和系统。系统和方法允许使用旋钮选择和显示信息以突出显示并选择所需的显示信息，从而消除对光标功能的需要。系统和方法还在显示器的单个屏幕上同时提供这些页面和/或窗口内的多个页面和/或多个窗口或“瓦片”，当选择时，每个窗口，页面和/或瓦片被独立地完全控制。本发明的总体构思还涉及在电子显示系统高度带上向飞行员提前提供多个提示并且即将到达预定高度的系统和方法。本发明总体构思还涉及基于航空电子导航显示器的显示范围采用可变分辨率地形数据的系统和方法。本发明的总体构思提供了一种使用图形处理器的α混合特性来调暗显示器的系统和方法，该方法使中性色彩覆盖层有效地变暗，超出最后的硬件调光步骤。

5. 发明授权

US10634514B2 Avionics device, systems and methods of display 有权
公开(公告)号：US10634514B2
公开(公告)日：2020-04-28
申请号：US15013908
申请日：2016-02-02
申请人： Aspen Avionics, Inc.
发明人： Peter Lyons , Constantinos (Gus) Kyriakos , William (Bill) Brodegard , Penny Heinz , David Berlin
IPC分类号： G08B23/00 , G01C23/00 , G06F16/29 , G01W1/00 , G06T11/60 , G01C5/00 , G06F3/02 , G06F3/0481 , G06F3/0484
CPC分类号： G01C23/00 , G01C5/005 , G01C23/005 , G01W1/00 , G06F3/02 , G06F3/0481 , G06F3/04842 , G06F16/29 , G06T11/60 , Y02A90/15
摘要： The present general inventive concept relates to methods and systems to select and display information on an avionics display screen. The systems and methods allow for the selection and display of information using knobs to highlight and select the desired information for display, eliminating the need for a cursor function. The systems and methods also provide for multiple pages and/or multiple windows or “tiles” within these pages and/or windows simultaneously on a single screen of a display, with each window, page, and/or tile being fully controlled independently when selected. The present general inventive concept also relates to systems and methods to provide multiple cues on an electronic display system altitude tape to a pilot in advance and impending approach to a predefined altitude. The present general inventive concept also relates to systems and methods to employ variable resolution topographical data based on display range for an avionics navigation display.

6. 发明授权

US10150572B2 Electronic avionics systems and methods 有权
公开(公告)号：US10150572B2
公开(公告)日：2018-12-11
申请号：US15437315
申请日：2017-02-20
申请人： Aspen Avionics, Inc.
发明人： Peter Lyons , Jeffrey D. Bethel
IPC分类号： G01C21/00 , B64D43/00 , G01C23/00 , B64D45/00 , G07C5/08
摘要： The present general inventive concept relates to a system of method having an electronic flight display that meets the FAR 23.1311(b) regulatory requirement for redundant backup instruments in the cockpit. The present general inventive concept also provides a system and method to detect failures, obstructions, or improper operation of the aircraft pitot pressure sensing system using a combination of dissimilar sensor data that is independent from each other, e.g., allocated from different sources and employed for different purposes on different displays, and displays information on an avionics display screen.

7. 发明授权

US09960595B2 Airborne power system disconnect system and method 有权
公开(公告)号：US09960595B2
公开(公告)日：2018-05-01
申请号：US14987541
申请日：2016-01-04
申请人： Aspen Avionics, Inc.
发明人： Jeffrey Bethel , Peter Lyons
IPC分类号： H02J9/06 , H02J1/00 , H02M3/04
CPC分类号： H02J1/00 , B64D2221/00 , H02J9/06 , H02M3/04 , Y10T307/625
摘要： An system and method to automatically disconnect a retrofit electrical unit from an electrical system in the event of an emergency situation and maintain power to the retrofit electrical unit.

8. 发明申请

US20170353557A1 AVIONICS GATEWAY INTERFACE, SYSTEMS AND METHODS 审中-公开
公开(公告)号：US20170353557A1
公开(公告)日：2017-12-07
申请号：US15685201
申请日：2017-08-24
申请人： Aspen Avionics, Inc.
发明人： John UCZEKAJ , Brad HAYDEN , Peter LYONS , Constantinos KYRIAKOS , Joseph LYLE
IPC分类号： H04L29/08 , G06F21/71 , H04B7/185 , H04L29/06 , G06F21/60
摘要： Systems and methods are provided for FAA-certified avionics devices to safely interface with non-certified mobile telecommunications devices before, during, and after flight. Data transmitted to the certified devices do not affect functionality of the certified device unless and until a user acknowledges and/or confirms the data on the certified device. Thus, the integrity of the certified device is maintained.

9. 发明授权

US09800665B2 Avionics gateway interface, systems and methods 有权
公开(公告)号：US09800665B2
公开(公告)日：2017-10-24
申请号：US14942505
申请日：2015-11-16
申请人： Aspen Avionics, Inc.
发明人： John Uczekaj , Brad Hayden , Peter Lyons , Constantinos Kyriakos , Joseph Lyle
IPC分类号： G06F21/00 , H04L29/08 , G06F21/60 , G06F21/71 , H04B7/185 , H04L29/06
CPC分类号： H04L67/12 , G06F21/602 , G06F21/71 , H04B7/18506 , H04L63/02 , H04L63/0884 , H04L63/10
摘要： Systems and methods are provided for FAA-certified avionics devices to safely interface with non-certified mobile telecommunications devices before, during, and after flight. Data transmitted to the certified devices do not affect functionality of the certified device unless and until a user acknowledges and/or confirms the data on the certified device. Thus, the integrity of the certified device is maintained.

10. 发明申请

US20130314258A1 ELECTRONIC AVIONICS SYSTEMS AND METHODS 有权
标题翻译：电子海洋系统与方法
公开(公告)号：US20130314258A1
公开(公告)日：2013-11-28
申请号：US13960138
申请日：2013-08-06
申请人： Aspen Avionics, Inc.
发明人： Peter Lyons , Jeffrey D. Bethel
IPC分类号： B64D45/00
CPC分类号： B64D43/00 , B64D45/00 , G01C23/00 , G07C5/0808 , G07C5/0816
摘要： The present general inventive concept relates to a system of method having an electronic flight display that meets the FAR 23.1311(b) regulatory requirement for redundant backup instruments in the cockpit. The present general inventive concept also provides a system and method to detect failures, obstructions, or improper operation of the aircraft pitot pressure sensing system using a combination of dissimilar sensor data that is independent from each other, e.g., allocated from different sources and employed for different purposes on different displays, and displays information on an avionics display screen.
摘要翻译：本发明总体概念涉及一种具有电子飞行显示器的方法系统，该电子飞行显示器满足驾驶舱中冗余备用仪器的FAR 23.1311（b）法规要求。本发明总体构思还提供了一种使用彼此独立的不同传感器数据的组合来检测飞机皮托管压力感测系统的故障，障碍物或不正确操作的系统和方法，例如，从不同来源分配并用于不同显示屏上的不同目的，并在航空电子显示屏幕上显示信息。

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