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1. 发明授权

US08451144B2 Flaps overspeed advisory system 有权
标题翻译：襟翼超速咨询系统
公开(公告)号：US08451144B2
公开(公告)日：2013-05-28
申请号：US12365778
申请日：2009-02-04
申请人： Yasuo Ishihara , Steve Johnson , Kevin J Conner
发明人： Yasuo Ishihara , Steve Johnson , Kevin J Conner
IPC分类号： G08B23/00
CPC分类号： G01C23/00 , B64D43/02 , G05D1/0055
摘要： A flap advisory system provides an advisory to a pilot informing that a speed of the aircraft should be attended to because of a current or desired flap setting. More specifically, the flap advisory system compares a measured airspeed of the aircraft either directly to a flap placard speed or to a marginal speed range set below the flap placard speed for a given flap setting. If the measured airspeed is determined to be excessive then the system provides an advisory indicating the airspeed is too fast. Further, the system may provide an advisory when a movement of a flap handle is detected such that continued movement of the flap handle would place the flaps in a setting that is inappropriate for the measured airspeed.
摘要翻译：襟翼咨询系统向飞行员提供通知，指示飞机的速度应由于当前或期望的襟翼设置而受到照顾。更具体地，襟翼咨询系统将飞行器的测量空速直接与折翼标牌速度相比较，或者对于给定的襟翼设置，将设置在襟翼标牌速度下方的边缘速度范围进行比较。如果测量的空速被确定为过高，则系统提供一个指示空速太快的建议。此外，当检测到襟翼手柄的移动时，系统可以提供咨询，使得襟翼手柄的持续移动将襟翼置于不适于测量的空速的设置中。

2. 发明申请

US20100198432A1 STABLE APPROACH MONITOR (SAM) SYSTEM 有权
标题翻译：稳定的方法监视器（SAM）系统
公开(公告)号：US20100198432A1
公开(公告)日：2010-08-05
申请号：US12365751
申请日：2009-02-04
申请人： Yasuo Ishihara , Kevin J. Conner , Steve Johnson
发明人： Yasuo Ishihara , Kevin J. Conner , Steve Johnson
IPC分类号： G05D1/00
CPC分类号： G08G5/025 , G01C23/005 , G05D1/0676
摘要： An improved stable approach monitor (SAM) system provides an audible advisory to a pilot when an aircraft is on a final landing approach. More specifically, the SAM system compares a measured airspeed of the aircraft to a predetermined flap placard speed. If the measured airspeed exceeds the predetermined flap placard speed then the improved SAM system provides an audible advisory indicating the airspeed of the aircraft is too fast. Advantageously, this audible advisory should prevent the pilot from attempting to deploy the flaps at an excessive airspeed and in turn focuses the pilot's attention on the problem at hand, which would be to reduce the airspeed of the aircraft. Once the airspeed is equal to or below the predetermined flap placard speed, the improved SAM system may provide another audible advisory informing the pilot to commence deployment of the flaps.
摘要翻译：改进的稳定进场监视（SAM）系统为飞行员在最终着陆方法时提供可听见的咨询。更具体地，SAM系统将飞行器的测量空速与预定的挡板标示速度进行比较。如果测量的空速超过预定的挡板标示速度，则改进的SAM系统提供了一个可听见的建议，指示飞机的空速太快。有利的是，这种可听见的咨询应该防止飞行员试图以过高的空速来部署襟翼，从而将飞行员的注意力集中在手头的问题上，这将是减少飞机的空速。一旦空速等于或低于预定的翼片标示速度，改进的SAM系统可以提供另一个可听见的建议，通知飞行员开始襟翼的展开。

3. 发明授权

US08600586B2 Stable approach monitor (SAM) system 有权
标题翻译：稳定进场监视（SAM）系统
公开(公告)号：US08600586B2
公开(公告)日：2013-12-03
申请号：US12365751
申请日：2009-02-04
申请人： Yasuo Ishihara , Kevin J Conner , Steve Johnson
发明人： Yasuo Ishihara , Kevin J Conner , Steve Johnson
IPC分类号： G05D1/00
CPC分类号： G08G5/025 , G01C23/005 , G05D1/0676
摘要： An improved stable approach monitor (SAM) system provides an audible advisory to a pilot when an aircraft is on a final landing approach. More specifically, the SAM system compares a measured airspeed of the aircraft to a predetermined flap placard speed. If the measured airspeed exceeds the predetermined flap placard speed then the improved SAM system provides an audible advisory indicating the airspeed of the aircraft is too fast. Advantageously, this audible advisory should prevent the pilot from attempting to deploy the flaps at an excessive airspeed and in turn focuses the pilot's attention on the problem at hand, which would be to reduce the airspeed of the aircraft. Once the airspeed is equal to or below the predetermined flap placard speed, the improved SAM system may provide another audible advisory informing the pilot to commence deployment of the flaps.
摘要翻译：改进的稳定进场监视（SAM）系统为飞行员在最终着陆方法时提供可听见的咨询。更具体地，SAM系统将飞行器的测量空速与预定的挡板标示速度进行比较。如果测量的空速超过预定的挡板标示速度，则改进的SAM系统提供了一个可听见的建议，指示飞机的空速太快。有利的是，这种可听见的咨询应该防止飞行员试图以过高的空速来部署襟翼，从而将飞行员的注意力集中在手头的问题上，这将是减少飞机的空速。一旦空速等于或低于预定的翼片标示速度，改进的SAM系统可以提供另一个可听见的建议，通知飞行员开始襟翼的展开。

4. 发明申请

US20100194599A1 FLAPS OVERSPEED ADVISORY SYSTEM 有权
标题翻译： FLAPS OVERSPEED咨询系统
公开(公告)号：US20100194599A1
公开(公告)日：2010-08-05
申请号：US12365778
申请日：2009-02-04
申请人： Yasuo Ishihara , Steve Johnson , Kevin J. Conner
发明人： Yasuo Ishihara , Steve Johnson , Kevin J. Conner
IPC分类号： G08B23/00
CPC分类号： G01C23/00 , B64D43/02 , G05D1/0055
摘要： A flap advisory system provides an advisory to a pilot informing that a speed of the aircraft should be attended to because of a current or desired flap setting. More specifically, the flap advisory system compares a measured airspeed of the aircraft either directly to a flap placard speed or to a marginal speed range set below the flap placard speed for a given flap setting. If the measured airspeed is determined to be excessive then the system provides an advisory indicating the airspeed is too fast. Further, the system may provide an advisory when a movement of a flap handle is detected such that continued movement of the flap handle would place the flaps in a setting that is inappropriate for the measured airspeed.
摘要翻译：襟翼咨询系统向飞行员提供通知，指示飞机的速度应由于当前或期望的襟翼设置而受到照顾。更具体地，襟翼咨询系统将飞行器的测量空速直接与折翼标牌速度相比较，或者对于给定的襟翼设置，将设置在襟翼标牌速度下方的边缘速度范围进行比较。如果测量的空速被确定为过高，则系统提供一个指示空速太快的建议。此外，当检测到襟翼手柄的移动时，系统可以提供咨询，使得襟翼手柄的持续移动将襟翼置于不适于测量的空速的设置中。

5. 发明授权

US08532848B2 Systems and methods for alerting potential tailstrike during landing 有权
标题翻译：在着陆期间提醒潜在尾迹的系统和方法
公开(公告)号：US08532848B2
公开(公告)日：2013-09-10
申请号：US12907392
申请日：2010-10-19
申请人： Yasuo Ishihara , Steve Johnson
发明人： Yasuo Ishihara , Steve Johnson
IPC分类号： G05D1/08
CPC分类号： B64D45/04 , B64C25/00 , B64D2045/008
摘要： Systems and methods for alerting for potential tailstrike during landing. A processing device located onboard an aircraft determines whether the aircraft is in a landing operational mode. If the aircraft is determined within the landing operational mode, the processing device determines whether aircraft speed is less than a previously defined threshold speed and generates an alert signal if it is determined that the aircraft's speed is less than the previously defined threshold speed. An output device located onboard the aircraft, outputs an alert based on the generated alert signal.
摘要翻译：用于在着陆期间潜在尾迹的警报的系统和方法。位于飞行器上的处理装置确定飞行器是否处于着陆操作模式。如果在着陆操作模式下确定飞行器，则处理装置确定飞行器速度是否小于先前定义的阈值速度，并且如果确定飞行器的速度小于先前定义的阈值速度，则产生报警信号。位于飞机上的输出设备基于生成的警报信号输出警报。

6. 发明申请

US20060080008A1 SYSTEM AND METHOD FOR USING AIRPORT INFORMATION BASED ON FLYING ENVIRONMENT 审中-公开
标题翻译：使用基于飞行环境的机场信息的系统和方法
公开(公告)号：US20060080008A1
公开(公告)日：2006-04-13
申请号：US11161346
申请日：2005-07-29
申请人： Yasuo Ishihara , Steve Johnson , Kevin Conner
发明人： Yasuo Ishihara , Steve Johnson , Kevin Conner
IPC分类号： G01C23/00
CPC分类号： G08G5/025 , G08G5/0065 , G08G5/0078
摘要： Methods, systems, and computer program products for using airport information based on the flying environment. In one embodiment, a method of using airport information based on the flying environment includes determining height, ground speed, and if a helicopter is taking off based on determined height, determined ground speed, a takeoff height value and a takeoff speed value. In one embodiment, the helicopter is determined to be taking off when the determined height is less than the takeoff height value and when the determined ground speed is less than the takeoff speed value.
摘要翻译：基于飞行环境使用机场信息的方法，系统和计算机程序产品。在一个实施例中，基于飞行环境使用机场信息的方法包括确定高度，地面速度，以及如果直升机基于确定的高度，确定的地面速度，起飞高度值和起飞速度值起飞。在一个实施例中，当确定的高度小于起飞高度值时以及当确定的地面速度小于起飞速度值时，确定直升机正在起飞。

7. 发明申请

US20130106623A1 SYSTEMS AND METHODS FOR ADJUSTING SINK RATE ALERT ENVELOPE FOR SPECIAL LANDING ZONES 有权
标题翻译：用于调整特殊土地区的波动警报信号的系统和方法
公开(公告)号：US20130106623A1
公开(公告)日：2013-05-02
申请号：US13286141
申请日：2011-10-31
申请人： Yasuo Ishihara , Steve Johnson , Gary A. Ostrom
发明人： Yasuo Ishihara , Steve Johnson , Gary A. Ostrom
IPC分类号： G08B23/00
CPC分类号： G01C23/00 , B64D45/04 , G01C21/00 , G05D1/0676 , G08G5/0021 , G08G5/0086 , G08G5/025
摘要： Systems and methods for improving sink rate alerting for rotary wing aircraft. In one example, the system includes a radio altimeter that produces an altitude value, a processor that is in signal communication with the user interface device and the radio altimeter. The processor receives an altitude value, a position value for the aircraft and landing zone (LZ) information. The processor determines if the aircraft is on an approach to land at an LZ that is raised above surrounding terrain based on the received position value and LZ information. The processor receives sink rate information for the aircraft and generates a sink rate alert based on the received sink rate information and the aircraft altitude value if the sink rate information is greater than a sink rate value adjusted according to the LZ information. An output device outputs the generated sink rate alert. The LZ information includes an altitude value.
摘要翻译：用于改善旋翼飞机的下沉速率警报的系统和方法。在一个示例中，系统包括产生高度值的无线电高度计，与用户接口设备和无线电高度计信号通信的处理器。处理器接收高度值，飞机和着陆区（LZ）信息的位置值。处理器根据接收到的位置值和LZ信息确定飞机是否处于在周围地形以上升起的LZ的地面上。处理器接收飞行器的汇率信息，并且如果汇率信息大于根据LZ信息调整的汇率值，则基于接收的汇率信息和飞机高度值，生成汇率报警。输出设备输出生成的下降速率警报。 LZ信息包括高度值。

8. 发明授权

US08116923B2 Stabilized approach monitor 有权
标题翻译：稳定的进场监视器
公开(公告)号：US08116923B2
公开(公告)日：2012-02-14
申请号：US12621794
申请日：2009-11-19
申请人： Yasuo Ishihara , Steve Johnson
发明人： Yasuo Ishihara , Steve Johnson
IPC分类号： B64D45/04 , G06F19/00 , G01C23/00 , B64D45/00
CPC分类号： G05D1/0676 , G08G5/0021 , G08G5/02 , G08G5/025
摘要： Systems and methods for suppressing an unstable alert when the aircraft is in the process of landing on a temporarily displaced threshold. In an example process, a processor on the aircraft determines the aircraft is on an approach to landing on a runway based on information received from one or more data sources on the aircraft, then retrieves predefined glideslope information for the runway from a memory device that is in signal communication with the processor. Next, the processor determines whether position of the aircraft is above the predefined glideslope by a first threshold amount. If the aircraft is determined to be above the predefined glideslope by the first threshold amount, the processor issues an unstable alert only if a flight path angle of the aircraft is greater than an angle of the predefined glideslope by a second threshold amount.
摘要翻译：当飞机正在临时移动的阈值上着陆的过程中用于抑制不稳定警报的系统和方法。在示例过程中，飞行器上的处理器基于从飞机上的一个或多个数据源接收到的信息来确定飞行器正在着陆在跑道上，然后从存储器设备中检索用于跑道的预定滑翔信息，与处理器进行信号通信。接下来，处理器确定飞行器的位置是否高于预定滑行边界第一阈值量。如果飞行器被确定为高于预定滑翔道第一阈值量，则只有当飞行器的飞行路径角度大于预定滑翔坡的角度达到第二阈值量时，处理器才发出不稳定的警报。

9. 发明授权

US08098176B2 Systems and methods for adjusting landing gear alert envelope for offshore platforms and building-top landings 有权
标题翻译：调整离岸平台和建筑物顶部着陆装置报警信号的系统和方法
公开(公告)号：US08098176B2
公开(公告)日：2012-01-17
申请号：US12821536
申请日：2010-06-23
申请人： Yasuo Ishihara , Steve Johnson , Gary Ostrom
发明人： Yasuo Ishihara , Steve Johnson , Gary Ostrom
IPC分类号： G08B23/00
CPC分类号： B64D45/0005
摘要： Systems and methods for improving landing gear alerting on a rotary wing aircraft. An example system includes a user interface device that allows a user to set a bug altitude value and a radio altimeter that produces an altitude value, both of which are in communication with a processor. The processor receives a bug altitude setting, generates a landing gear alert altitude value based on the received bug altitude setting and a predefined additive, receives a radio altitude value for the rotary-wing aircraft, and generates a landing gear alert if the radio altitude value is less than the landing gear alert altitude value and the landing gear is not in a landing position. An output device in signal communication with the processor, outputs the generated landing gear alert.
摘要翻译：用于改进旋翼机上起落架警报的系统和方法。示例性系统包括允许用户设置错误高度值的用户界面设备和产生高度值的无线电高度计，两者都与处理器通信。处理器接收到错误高度设置，根据接收到的臭虫高度设置和预定义的添加量生成起落架警报高度值，接收旋翼飞机的无线电高度值，并产生起落架警报，如果无线电高度值小于起落架报警高度值，起落架不在着陆位置。与处理器进行信号通信的输出设备输出生成的起落架警报。

10. 发明申请

US20110320070A1 SYSTEMS AND METHODS FOR ADJUSTING TARGET APPROACH SPEED 有权
标题翻译：用于调整目标方法速度的系统和方法
公开(公告)号：US20110320070A1
公开(公告)日：2011-12-29
申请号：US12821445
申请日：2010-06-23
申请人： Yasuo Ishihara , Steve Johnson
发明人： Yasuo Ishihara , Steve Johnson
IPC分类号： G06F19/00 , G05D1/06
CPC分类号： G05D1/0676 , B64D43/02 , G08G5/0091 , G08G5/025
摘要： Systems and methods for adjusting target approach speed for use in a “Too Fast” approach to landing condition. An exemplary system stores predefined maximum wind setting and a predefined reference speed and a pilot set bug speed value. A processing device sets a target speed equal to the bug speed, if the bug speed is less than the reference speed plus a value associated with a predefined maximum wind setting, and sets the target speed equal to the reference speed plus the max wind added value, if the manual bug speed is not less than the reference speed plus the max wind added value. An output device outputs an alert if the received aircraft speed is greater than the set target speed plus a predefined error value when the received aircraft location is within a threshold value of a touchdown point.
摘要翻译：调整目标进近速度的系统和方法用于“太快”的着陆条件。示例性系统存储预定义的最大风力设定和预定的参考速度和飞行员设置的错误速度值。如果错误速度小于参考速度加上与预定义的最大风力设定相关联的值，则处理设备将目标速度设置为等于故障速度，并将目标速度设置为等于参考速度加上最大风力附加值，如果手动的错误速度不低于参考速度加上最大风量附加值。如果所接收的飞行器位置在接地点的阈值内，则所接收到的飞行器速度大于设定的目标速度加上预定义的误差值，则输出设备输出报警。

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