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公开(公告)号：US3988713A
公开(公告)日：1976-10-26
申请号：US555680
申请日：1975-03-05
Applicant: Charles Donald Bateman
Inventor： Charles Donald Bateman
CPC classification number: G01C5/005 , G05D1/0607
Abstract: An aircraft instrument for warning the pilot that the aircraft is in an unsafe condition in proximity to the ground. The instrument has inputs representing aircraft configuration, flight condition with respect to the ground, and glide slope. Detector circuits process the inputs and give a warning of unsafe proximity to the ground. The boundary conditions for the warning are selected to avoid false warnings. A glide slope detector distinguishes between a valid glide slope signal and spurious signals, without need for pilot input.
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公开(公告)号：US3946358A
公开(公告)日：1976-03-23
申请号：US480727
申请日：1974-06-19
Applicant: Charles Donald Bateman
Inventor： Charles Donald Bateman
CPC classification number: G08G5/0021 , G01C5/005 , G05D1/0607 , G08G5/025
Abstract: An aircraft instrument for warning the pilot that the aircraft is in an unsafe condition in proximity to the ground. The instrument has inputs representing aircraft configuration, flight condition with respect to the ground, and glide slope. Detector circuits process the inputs and give a warning of unsafe proximity to the ground. The boundary conditions for the warning are selected to avoid false warnings. A glide slope detector distinguishes between a valid glide slope signal and spurious signals, without need for pilot input.
Abstract translation: 一架飞机仪表，用于向飞行员发出警告，指示飞机在靠近地面处于不安全状态。 仪器具有代表飞机配置，相对于地面的飞行状况和滑翔坡的输入。 检测器电路处理输入并发出不安全接近地面的警告。 选择警告的边界条件以避免误警。 滑翔坡检测器区分有效的滑翔坡信号和杂散信号，无需导频输入。
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公开(公告)号：US3936796A
公开(公告)日：1976-02-03
申请号：US544484
申请日：1975-01-27
Applicant: Charles Donald Bateman
Inventor： Charles Donald Bateman
CPC classification number: G05D1/0607 , G01C5/005
Abstract: An aircraft instrument for warning the pilot that the aircraft is in an unsafe condition in proximity to the ground. The instrument has inputs representing aircraft configuration, flight condition with respect to the ground, and glide slope. Detector circuits process the inputs and give a warning of unsafe proximity to the ground. The boundary conditions for the warning are selected to avoid false warnings. A glide slope detector distinguishes between a valid glide slope signal and spurious signals, without need for pilot input.
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公开(公告)号：US4030065A
公开(公告)日：1977-06-14
申请号：US706519
申请日：1976-07-19
Applicant: Charles Donald Bateman
Inventor： Charles Donald Bateman
IPC: B64D45/04 , G01C5/00 , G01C21/00 , G01C21/20 , G01S11/02 , G01S13/10 , G01S13/94 , G01S19/14 , G01S19/23 , G08G5/02
Abstract: By utilizing a radio altimeter in conjunction with a measure of the aircraft speed, landing gear position and flap position, an aircraft terrain warning system is made possible which provides a voice warning indicating that the aircraft is too low with respect to the terrain when the aircraft is above a predetermined speed. For aircraft speeds below the predetermined speed, a voice warning is provided when the aircraft is below a predetermined altitude with the landing gear up indicating that the aircraft is too low with the gear up and when the gear is down and the flaps are not in a landing position and the aircraft descends below a second predetermined altitude a voice warning is generated indicating that the aircraft is too low with flaps up.
Abstract translation: 通过利用无线电高度计与飞行器速度，起落架位置和襟翼位置的测量结合起来，使得飞机地形警告系统成为可能，其提供指示飞机相对于地形太低的语音警告，当飞行器 高于预定速度。 对于低于预定速度的飞机速度，当飞机低于预定高度时，提供语音警告，起落架向上指示飞机太低，并且当齿轮下降并且襟翼不在 着陆位置和飞行器下降到第二预定高度以下，产生语音警告，指示飞机太低而不能起飞。
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5.发明授权
公开(公告)号：US3934221A
公开(公告)日：1976-01-20
申请号：US556022
申请日：1975-03-06
Applicant: Charles Donald Bateman , Hans Rudolf Muller
Inventor： Charles Donald Bateman , Hans Rudolf Muller
CPC classification number: G01C5/005 , G05D1/0607
Abstract: In an aircraft terrain warning system utilizing a radar altimeter wherein the rate of closure to the terrain is compared with the aircraft's altitude above the terrain to generate a warning signal when the closure rate is excessive for a particular altitude, the closure rate signal is limited and biased depending upon the aircraft's closure rate and configuration in order to significantly increase the time response of the system while at the same time reducing nuisance warnings. The amplitude limit on the closure rate signal, is varied, above a predefined altitude, as a function of the closure rate signal in oreder to provide increased warning times at greater closure rates. Circuitry, responsive to the aircraft's flap positions, is also provided to alter the characteristics of rate limiter so as to provide warning parameters that more accurately reflect operating conditions at lower aircraft speeds.
Abstract translation: 在使用雷达高度计的飞机地形预警系统中，当对于特定高度的闭合速率过大时，与地形的关闭速率与飞机在地形上方的高度进行比较以产生警告信号，闭合速率信号受到限制， 这取决于飞机的关闭速率和配置，以便显着增加系统的时间响应，同时减少麻烦警告。 关闭速率信号的幅度限制在预定高度以上，作为关闭速率信号的函数而变化，以在更大的闭合速率下提供增加的警告时间。 还提供了响应于飞机的襟翼位置的电路，以改变速率限制器的特性，以便提供更准确地反映较低飞行器速度下的操作条件的警告参数。
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Patent Agency Ranking
公开(公告)号：US08949014B2
公开(公告)日：2015-02-03
申请号：US13564526
申请日：2012-08-01
Applicant: Charles Donald Bateman , Robert A. Champion , Ruy C. Brandao
Inventor： Charles Donald Bateman , Robert A. Champion , Ruy C. Brandao
IPC: G08B23/00
CPC classification number: G08G5/0078 , G08G1/096725 , G08G1/143 , G08G1/147 , G08G5/0008 , G08G5/0021 , G08G5/0091
Abstract: Systems and methods for improving the presentation of wake turbulence information. A processor located on an ownship receives position, heading and type information of another aircraft and position and heading information of the ownship. The processor determines if a possible wake condition exists from the other aircraft based on at least a portion of the received information and at least one predefined threshold and generates a wake icon if a wake condition is determined to exist. The wake condition exists when the ownship's altitude is below a first threshold altitude and above a second threshold altitude, wherein the first and second threshold altitudes are based on the other aircraft's altitude.
Abstract translation: 用于改善尾流湍流信息呈现的系统和方法。 位于自身的处理器可以接收另一架飞机的位置，航向和类型信息以及自身的位置和航向信息。 处理器基于所接收的信息的至少一部分和至少一个预定义的阈值来确定是否存在来自其他飞机的可能的唤醒条件，并且如果确定存在唤醒条件，则产生唤醒图标。 当所述本身的高度低于第一阈值高度并高于第二阈值高度时，所述唤醒条件存在，其中所述第一和第二阈值高度基于所述另一飞行器的高度。
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公开(公告)号：US20140039785A1
公开(公告)日：2014-02-06
申请号：US13564526
申请日：2012-08-01
Applicant: Charles Donald Bateman , Robert A. Champion , Ruy C. Brandao
Inventor： Charles Donald Bateman , Robert A. Champion , Ruy C. Brandao
IPC: B64D43/00
CPC classification number: G08G5/0078 , G08G1/096725 , G08G1/143 , G08G1/147 , G08G5/0008 , G08G5/0021 , G08G5/0091
Abstract: Systems and methods for improving the presentation of wake turbulence information. A processor located on an ownship receives position, heading and type information of another aircraft and position and heading information of the ownship. The processor determines if a possible wake condition exists from the other aircraft based on at least a portion of the received information and at least one predefined threshold and generates a wake icon if a wake condition is determined to exist. The wake condition exists when the ownship's altitude is below a first threshold altitude and above a second threshold altitude, wherein the first and second threshold altitudes are based on the other aircraft's altitude.
Abstract translation: 用于改善尾流湍流信息呈现的系统和方法。 位于自身的处理器可以接收另一架飞机的位置，航向和类型信息以及自身的位置和航向信息。 处理器基于所接收的信息的至少一部分和至少一个预定义的阈值来确定是否存在来自其他飞机的可能的唤醒条件，并且如果确定存在唤醒条件，则产生唤醒图标。 当所述本身的高度低于第一阈值高度并高于第二阈值高度时，所述唤醒条件存在，其中所述第一和第二阈值高度基于所述另一飞行器的高度。
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公开(公告)号：US4060793A
公开(公告)日：1977-11-29
申请号：US706518
申请日：1976-07-19
Applicant: Charles Donald Bateman
Inventor： Charles Donald Bateman
CPC classification number: G01C5/005
Abstract: In an aircraft ground proximity warning system that compares the rate of descent of an aircraft with its altitude above the terrain and in response thereto generates a warning signal when the aircraft's sink rate exceeds a predetermined limit for a particular altitude, a first type of advisory voice warning is generated for combinations of lesser descent rates and greater altitudes and a second type of imperative voice warning is generated for greater sink rates at lower altitudes where the danger of the aircraft impact with the terrain is more significant. In addition, the repetition rate of the advisory warning is increased as a function of increasing descent rate and the amplitude of the advisory warning can similarly be increased as function of increasing descent rate in order to call attention to an increasing undesirable operating condition.
Abstract translation: 在飞机地面接近警报系统中，将飞行器的下降速率与其高于地形的高度作比较，并且当飞机的下沉速率超过特定高度的预定极限时，产生警告信号，第一类咨询语音 对于较低的下降率和较高海拔的组合产生警告，并且产生第二种类型的命令式语音警报，用于在较低高度处的更大的汇率，其中飞机与地形的冲击危险性更大。 此外，咨询警告的重复率作为增加下降率的函数而增加，并且可以类似地增加咨询警告的幅度，作为增加下降速率的函数，以引起对不断增长的不期望的操作条件的注意。
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9.发明授权
公开(公告)号：US3958219A
公开(公告)日：1976-05-18
申请号：US596943
申请日：1975-07-18
Applicant: Charles Donald Bateman , Hans Rudolf Muller
Inventor： Charles Donald Bateman , Hans Rudolf Muller
CPC classification number: G01C5/005 , G05D1/0607
Abstract: In an aircraft terrain warning system utilizing a radar altimeter wherein the rate of closure to the terrain is compared with the aircraft's altitude above the terrain to generate a warning signal when the closure rate is excessive for a particular altitude, the closure rate signal is limited and biased depending upon the aircraft's closure rate and configuration in order to significantly increase the time response of the system while at the same time reducing nuisance warnings. The amplitude limit on the closure rate signal is varied, above a predefined altitude, as a function of the closure rate signal in order to provide increased warning times at greater closure rates. Circuitry, responsive to the aircraft's flap positions, is also provided to alter the characteristics of rate limiter so as to provide warning parameters that more accurately reflect operating conditions at lower aircraft speeds.
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公开(公告)号：US07274308B2
公开(公告)日：2007-09-25
申请号：US11164808
申请日：2005-12-06
Applicant: Charles Donald Bateman , David Bryan Alexander Fleming
Inventor： Charles Donald Bateman , David Bryan Alexander Fleming
IPC: G08G5/00
CPC classification number: G08G5/0021 , B64D45/0005 , B64D2045/001
Abstract: A processor, software code, and a method for generating warning indicating that flaps are not suitably in a take-off position. A first component is configured to receive a first signal indicative of one of a group of flaps positions, the group including a take-off position. A second component is configured to receive a second signal indicative of an aircraft position. A third component is configured to compare the aircraft position to the contents of a database and to, by the comparison, determine whether the aircraft position is within a runway perimeter. A fourth component is configured to generate an alarm when the aircraft is within the runway perimeter and the flaps position is not the take-off position.
Abstract translation: 处理器，软件代码和用于产生警告的方法，其指示襟翼不适合处于起飞位置。 第一部件被配置为接收指示一组襟翼位置中的一个的第一信号，该组包括起飞位置。 第二部件被配置为接收指示飞机位置的第二信号。 第三组件被配置为将飞机位置与数据库的内容进行比较，并且通过比较来确定飞机位置是否在跑道周边内。 第四组件被配置为当飞行器在跑道周边内并且襟翼位置不是起飞位置时产生报警。
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