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1. 发明公开

EP3182150A1 FREQUENCY MODULATED CONTINUOUS WAVE RADIO ALTIMETER SPECTRAL MONITORING 有权
标题翻译：华盛顿州威斯康星州威斯康星州
公开(公告)号：EP3182150A1
公开(公告)日：2017-06-21
申请号：EP16199899.2
申请日：2016-11-21
申请人： Honeywell International Inc.
发明人： Franceschini, Michael R , Muldoon, Kelly P , Timm, Steven L
IPC分类号： G01S7/02 , G01S13/32 , G01S13/88 , G01C5/00 , G01S7/35
CPC分类号： G01S13/882 , G01C5/005 , G01S7/021 , G01S7/352 , G01S2007/358 , H04W4/70
摘要： In one embodiment, a radio altimeter tracking filter is provided. The filter comprises: a wireless radio interface; a processor coupled to the wireless radio interface; a memory coupled to the wireless radio interface; wherein the wireless radio interface is configured to wirelessly receive a radio altimeter signal and convert the radio altimeter signal to a baseband frequency signal, wherein the a radio altimeter signal sweeps across a first frequency spectrum between a first frequency and a second frequency; wherein the processor is configured to pass the baseband frequency signal through a filter executed by the processor, the filter comprising a passband having a first bandwidth, and wherein the filter outputs a plurality of spectral chirps in response to the baseband frequency signal passing through the first bandwidth; wherein the processor is configured to process the plurality of spectral chirps to output characteristic parameters that characterize the radio altimeter signal.
摘要翻译：在一个实施例中，提供无线电高度计跟踪滤波器。该滤波器包括：无线无线电接口; 耦合到所述无线电接口的处理器; 耦合到所述无线电接口的存储器; 其中所述无线无线电接口被配置为无线地接收无线电高度计信号并将所述无线电高度计信号转换为基带频率信号，其中所述无线电高度计信号扫过第一频率和第二频率之间的第一频谱; 其中所述处理器被配置为通过由所述处理器执行的滤波器传递所述基带频率信号，所述滤波器包括具有第一带宽的通带，并且其中所述滤波器响应于所述基带频率信号通过所述第一带宽而输出多个频谱啁啾带宽; 其中所述处理器被配置为处理所述多个光谱啁啾，以输出表征所述无线电高度计信号的特征参数。

2. 发明公开

EP3108206A1 MOBILE DEVICE POSITIONING BASED ON INDEPENDENTLY OBTAINED BAROMETRIC PRESSURE MEASUREMENTS 审中-公开
标题翻译：定位移动设备基于独立GOT大气压力测量结果
公开(公告)号：EP3108206A1
公开(公告)日：2016-12-28
申请号：EP15708406.2
申请日：2015-02-20
申请人： Qualcomm Incorporated
发明人： GARIN, Lionel Jacques , VENKATRAMAN, Sai Pradeep , ZHANG, Gengsheng , LIU, Weiyi
IPC分类号： G01C5/06 , G01C21/20 , G01S5/02
CPC分类号： G01C5/005 , G01C5/06 , G01C21/206 , G01S5/0257 , G01S19/49
摘要： Various techniques are provided which may be implemented as methods, apparatuses and articles of manufacture for use by a mobile device. In certain example implementations, a mobile device may process a barometric pressure measurement indicative of an altitude effect and a weather effect to determine a first parameter corresponding to the altitude effect and a second parameter corresponding to the weather. Such a mobile device may further determine whether it may be transitioning or may have transitioned from an initial level to another level of a multiple level structure based, at least in part, on the first and second parameters.

3. 发明公开

EP2830032A1 Aircraft flight deck display, system and method for displaying integrated minimum safe altitude and minimum vectoring altitude information on a display device in an aircraft 有权
标题翻译：飞机驾驶舱显示器和系统以及用于显示的方法在飞行器集成Mindestsicherheitshöhen-和Mindestvektorisierungshöheninformationen在显示装置上
公开(公告)号：EP2830032A1
公开(公告)日：2015-01-28
申请号：EP14177349.9
申请日：2014-07-16
申请人： Honeywell International Inc.
发明人： Pepitone, Dave , Khatwa, Ratan , Burgin, Roger W. , Ball, Jerry
IPC分类号： G08G5/00
CPC分类号： G01C5/005 , B64D43/00 , G08G5/0021
摘要： A method is provided for displaying integrated minimum vectoring and safe altitude information on a display device in an aircraft. The method comprises displaying a graphical representation of a safe altitude sector and a vectoring altitude sector on the display device, and displaying a graphical representation of the aircraft on the display device to indicate the current location of the aircraft and a minimum altitude value associated therewith. The safe altitude sector corresponds to a first geographic area having a designated minimum safe altitude value associated therewith. The vectoring altitude sector corresponds to a second geographic area having a designated minimum vectoring altitude value associated therewith that is below the designated minimum safe altitude value. The graphical representation of the aircraft is displayed within at least one of the graphical representation of the safe altitude sector and the graphical representation of the vectoring altitude sector.
摘要翻译：提供了一种用于在飞机上的显示装置上显示集成最低引导和安全高度信息的方法。该方法包括显示一个安全高度扇区的图形表示和所述显示装置上的引导高度扇区，和在显示装置上显示所述飞行器的图形表示，以指示飞行器的当前位置，并与相关联的有最低高度值。安全高度扇区对应于具有相关联的有一个指定的最低安全高度值的第一地理区域。的引导高度扇区对应于具有指定最低引导与有关联的高度值的第二地理区域确实低于指定最低安全高度值。该机的图形表示的安全高度部门的图形表示和引导高度扇区的图形表示的至少一个内显示。

4. 发明授权

EP2349839B1 A METHOD OF OPERATING AN AIRCRAFT FUEL MANAGEMENT SYSTEM 有权
标题翻译：一种用于操作飞机燃料管理系统
公开(公告)号：EP2349839B1
公开(公告)日：2015-01-07
申请号：EP08875684.6
申请日：2008-11-25
申请人： Airbus Operations Limited
发明人： SJUNGARGÅRD, Petter , CASE, Ian , BURCKHART, Antoine , SPOTTISWOODE, Michael
IPC分类号： B64C17/10 , B64D37/00 , G01F23/00
CPC分类号： B64C17/10 , B64D37/00 , B64D37/14 , G01C5/005 , G01C23/00 , G01F23/0076 , G05D1/0816

5. 发明授权

EP1692463B1 METHODS AND SYSTEMS FOR GENERATING A TERRAIN ELEVATION MAP IN A CARTESIAN FORMAT 有权
标题翻译：方法和系统用于在笛卡尔格式地形高卡
公开(公告)号：EP1692463B1
公开(公告)日：2014-11-19
申请号：EP04817955.0
申请日：2004-12-06
申请人： Honeywell International Inc.
发明人： CHRISTIANSON, Paul, E.
IPC分类号： G01C23/00 , G01C5/00 , G09B29/10 , G09B29/12
CPC分类号： G09B29/12 , G01C5/005 , G01C23/00

6. 发明授权

EP1579173B1 DISPOSITIF D'AFFICHAGE ANTICOLLISION TERRAIN EMBARQUE 有权
标题翻译： ONBOARD-TERRAINANKOLISIONANZEIGEEINRICHTUNG
公开(公告)号：EP1579173B1
公开(公告)日：2014-11-19
申请号：EP03799529.7
申请日：2003-12-02
申请人： Thales
发明人： MEUNIER, Hugues, Thales Intellectual Property
IPC分类号： G01C5/00
CPC分类号： G01C5/005

7. 发明公开

EP2631672A1 Aircraft radar altimeter structure 有权
标题翻译： Flugzeugradarhöhenmesserstruktur
公开(公告)号：EP2631672A1
公开(公告)日：2013-08-28
申请号：EP13154997.4
申请日：2013-02-12
申请人： Honeywell International Inc.
发明人： Holt, Keone J.
IPC分类号： G01S13/88
CPC分类号： G01S13/882 , G01C5/005 , G01S13/94 , G01S2007/027 , H01Q1/12 , H01Q1/22 , H01Q1/27 , H01Q1/28 , H01Q1/286 , H01Q1/287 , Y10T29/49018
摘要： Embodiments described herein are directed towards a radar altimeter for mounting onto an aircraft. The radar altimeter includes a base configured to mount to an external surface of an aircraft, the base having an inner portion and a flange disposed around the inner portion, wherein the inner portion has a generally rectangular geometry defining a long dimension and a short dimension. A chassis is mounted to the base and has a planar portion that is disposed perpendicular to a plane formed by the base. A plurality of circuit boards are mounted to the planar portion of the chassis and disposed parallel to the planar portion of the chassis. The base is configured to mount over a second aperture in the external surface of the aircraft such that the chassis and the plurality of circuit boards are placed through the aperture and are disposed inside of the aircraft.
摘要翻译：本文描述的实施例针对用于安装到飞机上的雷达高度计。雷达高度计包括构造成安装到飞行器的外表面的底座，底座具有围绕内部部分设置的内部部分和凸缘，其中内部部分具有限定长尺寸和短尺寸的大致矩形几何形状。机架安装在基座上，并具有垂直于由基座形成的平面设置的平面部分。多个电路板被安装到底盘的平面部分并且平行于底盘的平面部分设置。基座被配置成安装在飞行器的外表面中的第二孔上，使得底盘和多个电路板被放置穿过孔并设置在飞行器的内部。

8. 发明授权

EP2126513B1 ROTARY WING AIRCRAFT PROXIMITY WARNING SYSTEM WITH A GEOGRAPHICALLY BASED AVOIDANCE SYSTEM 有权
标题翻译： APPROACH预警系统的挥杆平面与预防系统的地理基础
公开(公告)号：EP2126513B1
公开(公告)日：2012-02-15
申请号：EP07875012.2
申请日：2007-12-04
申请人： Sikorsky Aircraft Corporation
发明人： MATUSKA, David G. , ANTTILA, Donald S. , KRONAUER, Brad J.
IPC分类号： G01C21/00
CPC分类号： G01C5/005 , G01C21/00 , G05D1/0858
摘要： A proximity warning system which controls a transmission power output of the proximity sensor suite in response to an aircraft position being within a predefined minimum threshold of at least one sensitive area.

9. 发明授权

EP1373850B1 REDUNDANT ALTIMETER SYSTEM WITH SELF-GENERATING DYNAMIC CORRECTION CURVE 有权
标题翻译：与自体产生的动态校正曲线冗余高度表系统
公开(公告)号：EP1373850B1
公开(公告)日：2012-01-25
申请号：EP02746300.9
申请日：2002-03-01
申请人： Innovative Solutions and Support, Inc.
发明人： HEDRICK, Geoffrey, S., M.
IPC分类号： G01C5/06
CPC分类号： G01C25/005 , G01C5/005
摘要： In an aircraft conventionally-including a redundant pair of independent primary altitude determination systems of accuracy certified for RVSM operations, an initially loosely calibrated backup altimeter (32) receives independent static pressure data for use in calculating altitude.

10. 发明公开

EP2349839A1 A METHOD OF OPERATING AN AIRCRAFT FUEL MANAGEMENT SYSTEM 有权
标题翻译：一种用于操作飞机燃料管理系统
公开(公告)号：EP2349839A1
公开(公告)日：2011-08-03
申请号：EP08875684.6
申请日：2008-11-25
申请人： Airbus Operations Limited
发明人： SJUNGARGÅRD, Petter , CASE, Ian , BURCKHART, Antoine , SPOTTISWOODE, Michael
IPC分类号： B64D37/14
CPC分类号： B64C17/10 , B64D37/00 , B64D37/14 , G01C5/005 , G01C23/00 , G01F23/0076 , G05D1/0816
摘要： A method of operating an aircraft fuel management system for an aircraft having at least one fuel tank, each fuel tank having an associated fuel quantity indicator arranged to provide an indication of the amount of fuel in the associated fuel tank, the method comprising calculating a value for the amount of fuel on board (FOB_FailedFQI) the aircraft to be utilised by the fuel management system in the event of a failure of at least one of the fuel quantity indicators, the amount of fuel on board being calculated as a value for the initial amount of fuel on board (FOBinit) minus the amount of fuel used. Additionally or alternatively a value for the gross weight centre of gravity of the aircraft is calculated using an assigned value of fuel for each of the fuel tanks having an associated failed fuel quantity indicator.

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