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1.发明授权Systems and methods for intelligent alerting for cabin altitude depressurization 有权用于机舱高度减压的智能报警系统和方法公开(公告)号：US07670214B2
公开(公告)日：2010-03-02
申请号：US11469376
申请日：2006-08-31
Applicant: Kevin J Conner , Yasuo Ishihara , Charles D. Bateman
Inventor： Kevin J Conner , Yasuo Ishihara , Charles D. Bateman
CPC classification number: B64D13/02
Abstract: Methods and systems for providing a depressurization alert. An example method includes receiving a cabin depressurization discrete signal, determining if the cabin depressurization discrete signal is valid, and issuing a cabin depressurization alert, if the cabin depressurization discrete signal was determined to be valid. In accordance with further aspects of the invention, a time delay is executed before the receiving, determining, and issuing steps are repeated. The cabin depressurization discrete signal is determined not valid if uncorrected pressure is not greater than a predefined altitude. The uncorrected pressure is a raw pressure value produced by a Pitot-Static system. Also, the cabin depressurization discrete signal is determined not valid if the aircraft's altitude above an intended runway is not greater than a first predefined value. Additionally, the cabin depressurization discrete signal is determined not valid if an aircraft's altitude above terrain is not greater than a second predefined value.
Abstract translation: 提供减压警报的方法和系统。 一种示例性方法包括：如果客舱减压离散信号被确定为有效，则接收客舱减压离散信号，确定客舱减压离散信号是否有效，并发出机舱减压警报。 根据本发明的其它方面，在重复接收，确定和发出步骤之前执行时间延迟。 如果未校正的压力不大于预定高度，则舱室减压离散信号被确定为无效。 未校正的压力是由皮托静力系统产生的原始压力值。 此外，如果飞机在预期跑道上方的高度不大于第一预定值，则机舱减压离散信号被确定为无效。 此外，如果飞机在地形上方的高度不大于第二预定义值，则机舱减压离散信号被确定为无效。
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2.发明授权Ground proximity warning system having modified terrain closure rate warning on glide slope approach 失效地面接近警告系统在滑坡斜坡方面进行了修改后的地形关闭率警告
公开(公告)号：US4684948A
公开(公告)日：1987-08-04
申请号：US512208
申请日：1983-07-08
Applicant: Charles D. Bateman
Inventor： Charles D. Bateman
Abstract: An aircraft ground proximity warning system having an excessive terrain closure warning mode and a below glide slope warning mode monitors the glide slope signal and modifies the terrain closure warning envelope to accept a lesser terrain clearance when the aircraft is within the glide slope beam.
Abstract translation: 具有过度地形闭合警告模式和下滑坡警告模式的飞机地面接近警戒系统监视滑翔坡度信号，并修改地形关闭警告信号，以在飞行器处于滑翔坡度波束内时接受较小的地形间隙。
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公开(公告)号：US5225829A
公开(公告)日：1993-07-06
申请号：US697831
申请日：1991-05-09
Applicant: Charles D. Bateman
Inventor： Charles D. Bateman
IPC: G05D1/06
CPC classification number: G05D1/0615 , G05D1/0676
Abstract: A low airspeed alerting system for alerting the pilot of an aircraft of insufficient airspeed during a landing monitors various readily available signals representative of flight parameters of an aircraft such as pitch angle, vertical speed and true airspeed and advises the pilot when the airspeed of the aircraft is approaching an airspeed (kinetic energy) that is too low with respect to the ground to maintain the aircraft flying along the desired flight path without stalling, or without action by the pilot in time to recover.
Abstract translation: 一个低空速警报系统，用于在着陆期间提醒航空器空中飞行员空载不足，监视各种可用的代表航空器飞行参数的信号，如俯仰角，垂直速度和真实空速，并在飞行员的空速时向飞行员提供建议 正在接近相对于地面太低的空速（动能），以保持飞机沿着所需的飞行路线飞行而不停顿，或者没有及时采取行动来恢复。
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4.发明授权
公开(公告)号：US5166682A
公开(公告)日：1992-11-24
申请号：US666094
申请日：1991-03-07
Applicant: Charles D. Bateman
Inventor： Charles D. Bateman
CPC classification number: G05D1/0607 , G01C5/06 , G01P1/10 , G01S1/047
Abstract: A ground proximity warning system monitors the descent rate of an aircraft and generates a warning if the descent rate is excessive for the current altitude above ground of the aircraft according to a predetermined relationship. The predetermined relationship is altered as a function of the deviation of the aircraft from the glidescope to generate the warning earlier if the aircraft is below the glidescope and later if the aircraft is above the glidescope. The warning is given as a specific aural message indicating the specific flight parameters of the aircraft.
Abstract translation: 地面接近警报系统监视飞行器的下降率，并根据预定的关系对飞机地面上的当前高度的下降率过大，并产生警告。 如果飞机低于滑行镜，并且如果飞机高于滑行镜，则预定关系被改变为飞机与滑行镜的偏差的函数以产生警告。 该警告是作为指示飞机的特定飞行参数的特定听觉信息给出的。
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公开(公告)号：US5059964A
公开(公告)日：1991-10-22
申请号：US444513
申请日：1989-12-01
Applicant: Charles D. Bateman
Inventor： Charles D. Bateman
IPC: G05D1/06
CPC classification number: G05D1/0615
Abstract: An instrument (10) is disclosed for an aircraft having a windshear warning system to vary the threshold alarm setting as a function of a thermodynamic property of the air and as a function of local geographic and seasonal conditions. Specifically, a function generator 16 and other circuitry is disclosed. The output from the function generator 16 and other circuitry is then added to a fixed threshold acceleraton signal to produce a threshold alarm signal which has a value that is a function of the temperature of the air, in a basic embodiment.
Abstract translation: 公开了一种具有风切变警报系统的飞机的仪器（10），以根据空气的热力学性质和作为当地地理和季节条件的函数改变阈值报警设置。 具体地，公开了功能发生器16和其它电路。 然后，在基本实施例中，来自功能发生器16和其它电路的输出被加到固定的阈值加速度信号上以产生具有作为空气温度的函数的值的阈值报警信号。
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Patent Agency Ranking
公开(公告)号：US4646244A
公开(公告)日：1987-02-24
申请号：US576450
申请日：1984-02-02
Applicant: Charles D. Bateman , Michael M. Grove
Inventor： Charles D. Bateman , Michael M. Grove
CPC classification number: G08G5/045 , G01C5/005 , G08G5/0086
Abstract: A terrain advisory system utilizes stored data representative of terrain and other obstacles in predetermined geographical areas of interest to provide advisory warnings of the proximity of terrain, obstacles and restricted areas as they are approached. When used in a vehicle such as an aircraft, the system monitors the position, altitude, ground speed, ground track and the vertical speed of the vehicle and provides advisory indications of the position and path of travel of the vehicle with respect to obstacles and terrain. Such advisory indications may take the form of voice warnings describing the nature and position of any obstacles, or a visual display showing the position of the obstacles and terrain with respect to the vehicle.
Abstract translation: 地形咨询系统利用代表预期地理区域的地形和其他障碍物的存储数据，以便在接近地形，障碍物和限制区域时提供关于邻近的咨询警告。 当用于诸如飞行器的车辆中时，系统监视车辆的位置，高度，地面速度，地面轨迹和垂直速度，并且提供车辆相对于障碍物和地形的位置和行进路线的咨询指示 。 这种咨询指示可以采取描述任何障碍物的性质和位置的语音警告的形式，或者显示障碍物和地形相对于车辆的位置的视觉显示。
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7.发明申请SYSTEMS AND METHODS FOR INTELLIGENT ALERTING FOR CABIN ALTITUDE DEPRESSURIZATION 有权用于智能警报用于客舱高度减少的系统和方法公开(公告)号：US20080057849A1
公开(公告)日：2008-03-06
申请号：US11469376
申请日：2006-08-31
Applicant: Kevin J. Conner , Yasuo Ishihara , Charles D. Bateman
Inventor： Kevin J. Conner , Yasuo Ishihara , Charles D. Bateman
CPC classification number: B64D13/02
Abstract: Methods and systems for providing a depressurization alert. An example method includes receiving a cabin depressurization discrete signal, determining if the cabin depressurization discrete signal is valid, and issuing a cabin depressurization alert, if the cabin depressurization discrete signal was determined to be valid. In accordance with further aspects of the invention, a time delay is executed before the receiving, determining, and issuing steps are repeated. The cabin depressurization discrete signal is determined not valid if uncorrected pressure is not greater than a predefined altitude. The uncorrected pressure is a raw pressure value produced by a Pitot-Static system. Also, the cabin depressurization discrete signal is determined not valid if the aircraft's altitude above an intended runway is not greater than a first predefined value. Additionally, the cabin depressurization discrete signal is determined not valid if an aircraft's altitude above terrain is not greater than a second predefined value.
Abstract translation: 提供减压警报的方法和系统。 一种示例性方法包括：如果客舱减压离散信号被确定为有效，则接收客舱减压离散信号，确定客舱减压离散信号是否有效，并发出机舱减压警报。 根据本发明的其它方面，在重复接收，确定和发出步骤之前执行时间延迟。 如果未校正的压力不大于预定高度，则舱室减压离散信号被确定为无效。 未校正的压力是由皮托静力系统产生的原始压力值。 此外，如果飞机在预期跑道上方的高度不大于第一预定值，则机舱减压离散信号被确定为无效。 此外，如果飞机在地形上方的高度不大于第二预定义值，则机舱减压离散信号被确定为无效。
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公开(公告)号：US4914436A
公开(公告)日：1990-04-03
申请号：US35112
申请日：1987-04-06
Applicant: Charles D. Bateman , Michael M. Grove
Inventor： Charles D. Bateman , Michael M. Grove
CPC classification number: G05D1/0676
Abstract: A ground proximity warning system is disclosed which can recognize when an aircraft is on a final approach to an airport without utilizing a landing flap signal input. Airports together with the surrounding terrain topography are modeled by a simple geometric shape, such as, an inverted truncated cone, and stored on-board the aircraft. The system uses navigational data to determine the distance of the aircraft from the geometric model. Once the aircraft is determined to be within the area defined by the geometric model, the system provides an enabling envelope indicative that the aircraft is on a final approach for enabling various ground proximity warning systems. Also disclosed is a system for altering the enabling envelope as a function of the aircraft's alignment with a particular runway.
Abstract translation: 公开了一种地面接近警报系统，其可以识别何时飞行器最终接近机场而不使用着陆挡板信号输入。 与周围地形地形一起的机场由简单的几何形状建模，例如倒立的截锥，并存储在飞机上。 该系统使用导航数据来确定飞机与几何模型的距离。 一旦飞行器被确定在由几何模型限定的区域之内，系统就提供一个启用信号，指示飞机处于最终方法，以实现各种地面接近警报系统。 还公开了一种用于根据飞机与特定跑道的对准来改变启用包络的系统。
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公开(公告)号：US4905000A
公开(公告)日：1990-02-27
申请号：US34807
申请日：1987-04-03
Applicant: Charles D. Bateman
Inventor： Charles D. Bateman
CPC classification number: G05D1/0615
Abstract: An instrument (10) is disclosed for an aircraft having a windshear warning system to vary the threshold alarm setting as a function of a thermodynamic property of the air and as a function of local geographic and seasonal conditions. Specifically, a function generator 16 and other circuitry is disclosed. The output from the function generator 16 and other circuitry is then added to a fixed threshold acceleration signal to produce a threshold alarm signal which has a value that is a function of the temperature of the air, in a basic embodiment.
Abstract translation: 公开了一种用于具有风切变警报系统的飞机的仪器（10），以根据空气的热力学性质和作为当地地理和季节条件的函数改变阈值报警设置。 具体地，公开了功能发生器16和其它电路。 然后，在基本实施例中，功能发生器16和其它电路的输出被添加到固定阈值加速度信号，以产生具有作为空气温度的函数的值的阈值警报信号。
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公开(公告)号：US4574360A
公开(公告)日：1986-03-04
申请号：US481487
申请日：1983-04-01
Applicant: Charles D. Bateman
Inventor： Charles D. Bateman
CPC classification number: G01G19/07
Abstract: A helicopter weight measuring system for detecting the loaded weight of a helicopter operating under partial or full hover conditions while the wheels of the helicopter are contacting the ground includes means for sensing loading on the landing gear of the helicopter and means for determining the lift produced by a rotating wing of the helicopter. The sensed loading on the landing gear is added to the calculated lift to produce an indication of total helicopter loading.
Abstract translation: 一种直升机重量测量系统，用于在直升机的车轮接触地面的同时检测在部分或全部悬停状态下操作的直升机的重量，包括用于感测直升机起落架上的载荷的装置和用于确定由直升机产生的升力的装置 直升机的旋转翼。 将起落架上感测到的载荷加到计算出的升降机上，以产生总直升机载荷的指示。
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