专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US08630756B2 Airplane position assurance monitor 有权
标题翻译：飞机位置保证监控
公开(公告)号：US08630756B2
公开(公告)日：2014-01-14
申请号：US13085310
申请日：2011-04-12
申请人： Steven L. Fleiger-Holmes , Timothy Allen Murphy , Jean Marie Crane
发明人： Steven L. Fleiger-Holmes , Timothy Allen Murphy , Jean Marie Crane
IPC分类号： G09F7/00
CPC分类号： G08G5/02 , B64D43/00 , B64D45/04 , G01C5/005 , G01S1/18 , G01S19/15 , G01S19/20 , G05D1/0676 , G08G5/0021 , G08G5/0026 , G08G5/025
摘要： An onboard monitor that ensures the accuracy of data representing the calculated position of an airplane during final approach to a runway. This airplane position assurance monitor is a software function that uses dissimilar sources of airplane position and runway data to ensure the accuracy of the respective data from those dissimilar sources. ILS data and GPS or GPS/Baro data are the dissimilar sources of airplane position data used by this function. This function will calculate the airplane's angular deviations from the runway centerline and from the glide slope with onboard equipment and then compares those angular deviations to the ILS angular deviation information.
摘要翻译：一个车载显示器，确保在最后接近跑道时表示飞机计算位置的数据的准确性。该飞机位置保证监视器是使用不同的飞机位置和跑道数据源的软件功能，以确保来自这些不同来源的各自数据的准确性。 ILS数据和GPS或GPS / Baro数据是该功能使用的飞机位置数据的不同来源。该功能将计算飞机与跑道中心线的角度偏差以及与车载设备的滑行斜率，然后将这些角度偏差与ILS角度偏差信息进行比较。

2. 发明申请

US20090284427A1 Unit comprised of a glidepath aerial and a support organ 有权
标题翻译：单位由滑翔天线和支援机构组成
公开(公告)号：US20090284427A1
公开(公告)日：2009-11-19
申请号：US12427102
申请日：2009-04-21
申请人： Rene Ceccom , Philippe Besson , Christian Nguyen
发明人： Rene Ceccom , Philippe Besson , Christian Nguyen
IPC分类号： H01Q1/28 , H01Q1/42 , H01Q1/52
CPC分类号： H01Q1/28 , G01S1/04 , G01S1/18 , H01Q1/50
摘要： The invention concerns a unit having a glidepath aerial (1) and a support organ (2) designed to be mounted on the front landing gear of an aircraft, with said landing gear forming an electrically conductive ground plane. According to the invention: this aerial (1) is mounted on the support organ (2) and is electrically insulated from this support organ (2) by insulating elements, the support organ (2) has a longitudinal dimension at least equal to around one quarter of the wavelength λ at which the aerial functions, so that the distance separating this aerial (1) and the ground plane is greater than λ/4, and the aerial (1) also has a transmission line (13, 15) designed to connect the aerial (1) to a receiver in the aircraft; this transmission line (13, 15) is surrounding by an electromagnetic shielding element (12) serving as a faradization screen for the transmission line (13, 15), and this element is designed to be electrically connected to the ground plane.
摘要翻译：本发明涉及具有滑翔天线（1）和设计成安装在飞行器的前起落架上的支撑器（2）的单元，所述起落架形成导电接地平面。根据本发明：该天线（1）安装在支撑器件（2）上并且通过绝缘元件与该支撑器件（2）电绝缘，支撑器官（2）具有至少等于大约一个的纵向尺寸天线的波长λ的四分之一起作用，使得分离该天线（1）和接地平面的距离大于λ/ 4，并且天线（1）还具有传输线（13,15），设计成将天线（1）连接到飞机上的接收器; 该传输线（13,15）由用作传输线（13,15）的法拉第屏蔽的电磁屏蔽元件（12）围绕，并且该元件被设计为电连接到接地层。

3. 发明授权

US07546183B1 In-flight verification of instrument landing system signals 有权
标题翻译：仪表着陆系统信号的飞行验证
公开(公告)号：US07546183B1
公开(公告)日：2009-06-09
申请号：US11373230
申请日：2006-03-10
申请人： Frank Marcum
发明人： Frank Marcum
IPC分类号： G05D1/00 , G06F19/00
CPC分类号： G01S1/022 , G01S1/18 , G01S19/15
摘要： An instrument landing system (ILS) provides signals in space receivable by an aircraft in flight to identify, for example, a point in space at which to start an approach along a glide slope path to a touchdown point on a runway. Atmospheric, ground and other conditions may cause transmission anomalies, so that the ILS signals identify a point in space displaced from its intended position. Systems and methods employed in flight use GPS or other positional data to determine the current displacement of such point, as identified by received ILS signals, from its intended position consistent with ILS specifications. In addition to reception and use of ILS and GPS signals, data on geographic runway location and correct ILS signal in space parameters is used for reference purposes in determining signal in space position discrepancies, glide slope path angular discrepancies, or both. The pilot can be alerted not to rely upon the ILS when discrepancies, which can vary on a short time basis and not be discernable from the ground, are determined to exceed safe limits.
摘要翻译：仪表着陆系统（ILS）提供飞行中飞机可接收的空间中的信号，以识别例如在沿着跑道上的接地点的滑翔坡道开始进近的空间中的一个点。大气，地面等条件可能导致传输异常，使得ILS信号识别位于其预期位置的空间中的一个点。在飞行中使用的系统和方法使用GPS或其他位置数据来确定由接收的ILS信号识别的这些点的当前位移与其与ILS规范一致的预期位置。除了接收和使用ILS和GPS信号之外，空间参数中的地理跑道位置和正确的ILS信号的数据也用于确定空间位置差异信号，滑坡斜率角差异或二者的参考。当可以在短时间内变化而不能从地面上辨别出差异时，飞行员可以被警告不依赖于ILS，这些差异被确定为超过安全限制。

4. 发明申请

US20050237235A1 Method and device for aiding the landing of an aircraft on a runway 有权
标题翻译：用于帮助飞机着陆在跑道上的方法和装置
公开(公告)号：US20050237235A1
公开(公告)日：2005-10-27
申请号：US11108116
申请日：2005-04-18
申请人： Michel Falcati , Gilles Tatham
发明人： Michel Falcati , Gilles Tatham
IPC分类号： B64D45/04 , G01S1/18 , G01S1/56 , G01S19/15 , G01S19/39 , G05D1/06 , G01S13/00
CPC分类号： G01S19/15 , G01S1/18 , G01S1/56 , G01S19/39
摘要： Method and device for aiding the landing of an aircraft on a runway. The device (1) uses an angular vertical position of the aircraft and comprises at least one landing aid radio means (2A), means (3) for determining in a stand-alone manner the position of the aircraft in latitude and longitude, means (4A) for determining the position of the threshold of said runway in latitude and longitude, and a computing unit (5) for, on the basis of said positions of the aircraft and of the threshold of the runway, correcting the angular vertical position of the aircraft, the angular vertical position thus corrected being used to aid the landing of the aircraft.
摘要翻译：用于帮助飞机着陆在跑道上的方法和装置。装置（1）使用飞行器的角度垂直位置，并且包括至少一个着陆辅助无线电装置（2A），用于以独立方式确定飞机在纬度和经度上的位置的装置（3）（4A），用于确定所述跑道在纬度和经度上的阈值的位置;以及计算单元（5），用于根据飞行器的所述位置和跑道的阈值，校正角度垂直位置飞机的角度垂直位置被用来帮助飞机着陆。

5. 发明申请

US20020040263A1 Glideslope monitor for aircraft 失效
标题翻译：飞机滑翔机监视器
公开(公告)号：US20020040263A1
公开(公告)日：2002-04-04
申请号：US09916633
申请日：2001-07-27
发明人： Steve C. Johnson , Yasuo Ishihara
IPC分类号： G08G005/00
CPC分类号： G08G5/025 , G01C5/005 , G01S1/022 , G01S1/18 , G05D1/0676
摘要： A system, method, and computer program product for alerting an aircraft flight crew of an inconsistency during an instrument landing system (ILS) approach to a selected runway. The system includes a component configured to receive glideslope and localizer signals, and a component configured to determine aircraft approach angle to runway end. Also, a component configured to alert the aircraft flight crew of an approach inconsistency, if the determined aircraft approach angle to runway end is less than a threshold angular value and one or more parameters based on aircraft position and the received glideslope and localizer signals are met. The component configured to determine aircraft approach angle to runway end determines the aircraft approach angle to runway end based on aircraft geometric altitude, a vertical figure of merit, a horizontal figure of merit, runway elevation, and aircraft distance to runway threshold.
摘要翻译：一种系统，方法和计算机程序产品，用于在对所选跑道进行仪器着陆系统（ILS）方法期间提醒飞机机组人员不一致。该系统包括配置成接收滑坡和定位器信号的部件，以及被配置为确定飞机到跑道端的飞机接近角度的部件。而且，如果所确定的飞行器对跑道端的接近角度小于阈值角度值并且基于飞机位置和接收到的滑坡和定位器信号达到一个或多个参数，则被配置为警告飞行员飞行机组的方法不一致的部件。配置为确定飞机接近角度的跑道结构的组件根据飞机几何高度，垂直品质因数，水平品质因数，跑道高程和飞机距离到跑道阈值来确定飞机到跑道端的接近角度。

6. 发明授权

US6097338A Instrument landing system glide path transmitter device 有权
标题翻译：仪表着陆系统滑翔道发射装置
公开(公告)号：US6097338A
公开(公告)日：2000-08-01
申请号：US147609
申请日：1999-03-24
申请人： Rainer Rupprecht , Jurgen Stammelbach , Herbert Kleiber
发明人： Rainer Rupprecht , Jurgen Stammelbach , Herbert Kleiber
IPC分类号： G01S1/14 , G01S1/18 , G08G5/02 , G01S1/16 , G01S1/30
CPC分类号： G08G5/0026 , G01S1/18 , G08G5/025
摘要： A glide path transmitter for an instrument landing system. The transmitter includes several antenna radiators by way of which high frequency signals containing various low frequency modulated carrier and side band components are radiated. The components overlap each other in the far field where they form a guide signal which can be evaluated by aircraft. Phases of the carrier oscillations of the radiated high frequency signals form the guide signal having a set relationship with each other. A separate digitally controlled modulator is provided for each high frequency signal fed to an antenna radiator. The modulator modulates the phase and amplitude of a high frequency oscillation fed thereto according to a given model and inputs the modulated high frequency signal into the antenna radiator allocated thereto, thus reducing the supply network expenditure.
摘要翻译： PCT No.PCT / EP98 / 03661 Sec。 371 1999年3月24日第 102（e）1999年3月24日PCT PCT 1998年5月22日PCT公布。公开号WO98 / 54546 日期1998年12月3日用于仪表着陆系统的滑翔道发射机。发射机包括几个天线辐射器，通过这些天线辐射器辐射包含各种低频调制载波和边带分量的高频信号。这些组件在远场中彼此重叠，在那里它们形成可由飞机评估的引导信号。辐射高频信号的载波振荡的相位形成彼此具有一定关系的引导信号。为馈送到天线辐射器的每个高频信号提供单独的数字控制调制器。调制器根据给定的模型调制馈送到其的高频振荡的相位和幅度，并将调制的高频信号输入到分配给它的天线辐射器，从而减少供电网络的支出。

7. 发明授权

US4599621A Two-frequency glide-path station for the standardized instrument-landing system ILS 失效
标题翻译：用于标准化仪表着陆系统ILS的双频滑道站
公开(公告)号：US4599621A
公开(公告)日：1986-07-08
申请号：US648853
申请日：1984-09-07
申请人： Helmut Rausch
发明人： Helmut Rausch
IPC分类号： G01S1/02 , G01S1/18 , G08G5/02 , G01S1/16
CPC分类号： G01S1/18 , G01S1/024
摘要： To monitor the course signals radiated by the two-frequency glide-path station with respect to course line and course width, and to monitor the clearance signal, the signals radiated by the antennas (A1, A2, A3) and a signal extracted directly from the transmitter (1) are so combined (5, 6, 7) that the clearance signal (CL), the sideband signal (SBO), and the carrier and sideband signal are obtained. These signals are evaluated (8) for monitoring purposes in a manner known per se.
摘要翻译：为了监测由双频滑翔站相对于路线和路线宽度辐射的航向信号，并监视间隙信号，由天线（A1，A2，A3）辐射的信号和直接从发射机（1）如此组合（5,6,7），获得间隙信号（CL），边带信号（SBO）以及载波和边带信号。以本身已知的方式对这些信号进行评估（8）以进行监视。

8. 发明授权

US4141522A Independent glide slope gain programming system 失效
标题翻译：独立滑坡增益编程系统
公开(公告)号：US4141522A
公开(公告)日：1979-02-27
申请号：US797161
申请日：1977-05-16
申请人： Antonius A. Lambregts
发明人： Antonius A. Lambregts
IPC分类号： G01S1/18 , G05D1/06 , G05D1/12
CPC分类号： G01S1/18 , G05D1/0676
摘要： A landing approach system for aircraft utilizing ILS (instrument landing system) beam guidance information which converts angular glide slope information into linear altitude deviation relative to the glide slope beam center, using computed range information.
摘要翻译：利用ILS（仪器着陆系统）光束引导信息的飞机的降落进近系统，其使用计算的范围信息将角滑翔坡信息转换成相对于滑翔坡度波束中心的线性高度偏差。

9. 发明授权

US3950754A Method of transmitting glide slope navigation signals for aircraft 失效
标题翻译：发射航空器滑坡导航信号的方法
公开(公告)号：US3950754A
公开(公告)日：1976-04-13
申请号：US473408
申请日：1974-05-28
申请人： Donald J. Toman
发明人： Donald J. Toman
IPC分类号： G01S1/18 , H01Q25/00 , G01S1/44
CPC分类号： H01Q25/00 , G01S1/18
摘要： A multiple element antenna array provides a separate beam of carrier signal from each element in a pattern of beams spaced at different angles above the horizon. The array is adjusted upwardly to avoid obstructions on the horizon, and a program of modulation is applied to the separate beams to define the desired glide slope path while compensating for the mechanical upward adjustment of the array.

10. 发明申请

US20170356757A1 Method and device for verifying a guidance signal 审中-公开
公开(公告)号：US20170356757A1
公开(公告)日：2017-12-14
申请号：US15614683
申请日：2017-06-06
申请人： Airbus Operations SAS
发明人： Thierry BOURRET , Nicolas MARCONNET
IPC分类号： G01C25/00 , G08G5/02 , G08G5/00 , G01C23/00 , G01C21/20
CPC分类号： G01C25/00 , G01C5/06 , G01C21/005 , G01C21/04 , G01C21/20 , G01C23/005 , G01S1/16 , G01S1/18 , G01S19/48 , G05D1/0676 , G08G5/0021 , G08G5/025
摘要： A verification method comprising a first step of measuring at least one position parameter of an aircraft and a first set of steps implemented after the flight of at least one aircraft, in an automatic and repetitive manner, comprising computing a geographical height of an aircraft with respect to the runway on the basis of the position parameters of an aircraft, computing an evaluated vertical deviation, between the geographical height and a reference height, and computing a vertical error on the basis of a comparison between the evaluated vertical deviation and the reference vertical deviation.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式