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公开(公告)号：US20130120165A1
公开(公告)日：2013-05-16
申请号：US13641325
申请日：2010-12-22
IPC分类号： B60Q1/00
CPC分类号： G01C23/00 , B60Q1/00 , B64C27/00 , B64C27/006 , B64C27/04 , B64C27/52 , B64C29/00 , B64C39/024 , B64C2201/108 , B64C2201/121 , B64D43/00 , B64D45/00 , G01C21/00 , G01D7/02 , G05D17/02
摘要： A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.
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公开(公告)号：US20120101666A1
公开(公告)日：2012-04-26
申请号：US13380925
申请日：2009-07-27
CPC分类号： B64D25/00 , B64D2201/00
摘要： An occupant protection system for an aircraft comprising a sensor system for sensing flight condition information and a control system, which includes an impending crash detection system and an impact detection system. The impending crash detection system receives flight information from the sensors determines whether a crash is likely to occur. If an impending crash is detected, the impending crash detection system activates impact modes of a first group of aircraft systems. The impact detection system receives flight information from the sensor system and determines whether an impact has occurred or is occurring. If an impact is detected, the impact detection system activates impact modes of a second group of aircraft systems.
摘要翻译： 一种用于飞行器的乘员保护系统，包括用于感测飞行情况信息的传感器系统和包括即将发生的碰撞检测系统和冲击检测系统的控制系统。 即将发生的碰撞检测系统从传感器接收飞行信息，确定是否可能发生碰撞。 如果检测到即将发生的碰撞，即将发生的碰撞检测系统激活第一组飞行器系统的冲击模式。 冲击检测系统从传感器系统接收飞行信息，并确定影响是否发生或正在发生。 如果检测到冲击，冲击检测系统激活第二组飞行器系统的冲击模式。
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公开(公告)号：US09035802B2
公开(公告)日：2015-05-19
申请号：US13641325
申请日：2010-12-22
CPC分类号： G01C23/00 , B60Q1/00 , B64C27/00 , B64C27/006 , B64C27/04 , B64C27/52 , B64C29/00 , B64C39/024 , B64C2201/108 , B64C2201/121 , B64D43/00 , B64D45/00 , G01C21/00 , G01D7/02 , G05D17/02
摘要： A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.
摘要翻译： 电力安全系统被配置为在飞行器中提供电力信息。 电力安全系统包括具有电力需求指示器和功率可用指示器的电力安全仪器，每个指示器位于显示器上。 所需电源指示灯和电源指示灯的位置表示执行悬停飞行操作所需的电力和功率。 电力安全系统可以在飞行计划模式或当前飞行模式下操作。 电力安全系统使用至少一个传感器来测量对所需功率和可用功率有影响的变量。
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4.发明申请Variable speed gearbox with an independently variable speed tail rotor system for a rotary wing aircraft 有权具有独立变速的尾翼转子系统的变速齿轮箱，用于旋翼飞机公开(公告)号：US20070125907A1
公开(公告)日：2007-06-07
申请号：US11292556
申请日：2005-12-02
申请人： Nicholas Lappos , Edward Karedes , Harsh Vinayak , Yuriy Gmirya
发明人： Nicholas Lappos , Edward Karedes , Harsh Vinayak , Yuriy Gmirya
IPC分类号： B64D35/00
CPC分类号： B64C27/14 , B64C27/12 , B64C2027/8236
摘要： A gearbox of a rotary-wing aircraft includes at least one variable speed system which optimizes the main rotor speed for different flight regimes such as a hover flight profile and a high speed cruise flight profile for any rotary wing aircraft while maintaining an independently variable tail rotor speed.
摘要翻译： 旋翼飞机的变速箱包括至少一个变速系统，其优化用于不同飞行状态的主转子速度，例如用于任何旋转翼飞机的悬停飞行剖面和高速巡航飞行剖面，同时保持独立变量的尾部转子 速度。
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公开(公告)号：US20150321769A1
公开(公告)日：2015-11-12
申请号：US14715236
申请日：2015-05-18
CPC分类号： G01C23/00 , B60Q1/00 , B64C27/00 , B64C27/006 , B64C27/04 , B64C27/52 , B64C29/00 , B64C39/024 , B64C2201/108 , B64C2201/121 , B64D43/00 , B64D45/00 , G01C21/00 , G01D7/02 , G05D17/02
摘要： A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.
摘要翻译： 电力安全系统被配置为在飞行器中提供电力信息。 电力安全系统包括具有电力需求指示器和功率可用指示器的电力安全仪器，每个都位于显示器上。 所需电源指示灯和电源指示灯的位置表示执行悬停飞行操作所需的电力和功率。 电力安全系统可以在飞行计划模式或当前飞行模式下操作。 电力安全系统使用至少一个传感器来测量对所需功率和可用功率有影响的变量。
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公开(公告)号：US08588996B2
公开(公告)日：2013-11-19
申请号：US13380925
申请日：2009-07-27
IPC分类号： G05D3/00
CPC分类号： B64D25/00 , B64D2201/00
摘要： An occupant protection system for an aircraft comprising a sensor system for sensing flight condition information and a control system, which includes an impending crash detection system and an impact detection system. The impending crash detection system receives flight information from the sensors determines whether a crash is likely to occur. If an impending crash is detected, the impending crash detection system activates impact modes of a first group of aircraft systems. The impact detection system receives flight information from the sensor system and determines whether an impact has occurred or is occurring. If an impact is detected, the impact detection system activates impact modes of a second group of aircraft systems.
摘要翻译： 一种用于飞行器的乘员保护系统，包括用于感测飞行情况信息的传感器系统和包括即将发生的碰撞检测系统和冲击检测系统的控制系统。 即将发生的碰撞检测系统从传感器接收飞行信息，确定是否可能发生碰撞。 如果检测到即将发生的碰撞，即将发生的碰撞检测系统激活第一组飞行器系统的冲击模式。 冲击检测系统从传感器系统接收飞行信息，并确定影响是否发生或正在发生。 如果检测到冲击，冲击检测系统激活第二组飞行器系统的冲击模式。
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