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1. 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。

2. 发明公开

EP3280645A1 SYSTEM AND METHOD FOR ANGLE OF ATTACK INDICATION WITH NO DEDICATED SENSORS AND AIRCRAFT INFORMATION 审中-公开
标题翻译：用于没有专用传感器和飞机信息的角度攻击指示的系统和方法
公开(公告)号：EP3280645A1
公开(公告)日：2018-02-14
申请号：EP16777305.0
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.

3. 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。

4. 发明公开

EP2460351A2 AVIONICS DEVICES, SYSTEMS AND METHODS 审中-公开
标题翻译：航空仪器，制度和程序
公开(公告)号：EP2460351A2
公开(公告)日：2012-06-06
申请号：EP10806870.1
申请日：2010-07-26
申请人： 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.

5. 发明授权

EP2460351B1 AVIONICS DEVICES, SYSTEMS AND METHODS 有权
公开(公告)号：EP2460351B1
公开(公告)日：2019-09-04
申请号：EP10806870.1
申请日：2010-07-26
申请人： 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

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