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1. 发明申请

WO2008112530A3 FLIGHT MANAGEMENT SYSTEM FOR GENERATING VARIABLE THRUST CUTBACK DURING AIRCRAFT DEPARTURE 审中-公开
标题翻译：在飞机出发期间生成可变扭矩切换的飞行管理系统
公开(公告)号：WO2008112530A3
公开(公告)日：2009-10-22
申请号：PCT/US2008056174
申请日：2008-03-07
申请人： GEN ELECTRIC , DEJONGE MICHAEL K
发明人： DEJONGE MICHAEL K
IPC分类号： G05D1/06
CPC分类号： G05D1/0661
摘要： A flight management system is provided for generating a variable thrust cutback during aircraft departure. The flight management system includes memory storing a sound exposure level limit for a navigation flight and storing expected sound exposure levels for an aircraft, and one or more inputs for receiving sensed aircraft variables including altitude and airspeed. The system also includes a processor for processing the sensed altitude and airspeed and stored sound exposure levels. The processor further computes an engine thrust value that complies with the sound exposure level limit based on the altitude, airspeed and the sound exposure levels for controlling aircraft throttle during departure.
摘要翻译：提供飞行管理系统，用于在飞机起飞期间产生可变推力裁减。飞行管理系统包括存储导航飞行的声音暴露级别限制并存储飞行器的预期声音暴露水平的存储器，以及用于接收感测的飞行器变量（包括高度和空速）的一个或多个输入。该系统还包括用于处理所感测的高度和空速以及存储的声音暴露水平的处理器。处理器进一步计算出符合声音暴露水平极限的发动机推力值，其基于在起飞期间控制飞机油门的高度，空速和声音暴露水平。

2. 发明申请

WO2008112530A2 FLIGHT MANAGEMENT SYSTEM FOR GENERATING VARIABLE THRUST CUTBACK DURING AIRCRAFT DEPARTURE 审中-公开
标题翻译：在飞机出发期间生成可变扭矩切换的飞行管理系统
公开(公告)号：WO2008112530A2
公开(公告)日：2008-09-18
申请号：PCT/US2008/056174
申请日：2008-03-07
申请人： GENERAL ELECTRIC COMPANY , DEJONGE, Michael, K.
发明人： DEJONGE, Michael, K.
IPC分类号： G05D1/06
CPC分类号： G05D1/0661
摘要： A flight management system is provided for generating a variable thrust cutback during aircraft departure. The flight management system includes memory storing a sound exposure level limit for a navigation flight and storing expected sound exposure levels for an aircraft, and one or more inputs for receiving sensed aircraft variables including altitude and airspeed. The system also includes a processor for processing the sensed altitude and airspeed and stored sound exposure levels. The processor further computes an engine thrust value that complies with the sound exposure level limit based on the altitude, airspeed and the sound exposure levels for controlling aircraft throttle during departure.
摘要翻译：提供飞行管理系统，用于在飞机起飞期间产生可变推力裁减。飞行管理系统包括存储导航飞行的声音暴露级别限制并存储飞行器的预期声音暴露水平的存储器，以及用于接收感测的飞行器变量（包括高度和空速）的一个或多个输入。该系统还包括用于处理所感测的高度和空速以及存储的声音暴露水平的处理器。处理器进一步计算出符合声音暴露水平极限的发动机推力值，其基于在起飞期间控制飞机油门的高度，空速和声音暴露水平。

3. 发明申请

WO2008112527A3 METHOD OF GENERATING VARIABLE THRUST CUTBACK DURING AIRCRAFT DEPARTURE 审中-公开
标题翻译：在飞机出发时产生可变扭矩的方法
公开(公告)号：WO2008112527A3
公开(公告)日：2009-10-22
申请号：PCT/US2008056170
申请日：2008-03-07
申请人： GEN ELECTRIC , DEJONGE MICHAEL K
发明人： DEJONGE MICHAEL K
IPC分类号： G05D1/06
CPC分类号： G05D1/0661
摘要： A method of producing a variable thrust cutback of an aircraft during aircraft departure is provided. The method includes the steps of storing expected sound exposure levels for an aircraft in memory, and storing a sound exposure level limit for a navigation flight in memory. The method also includes the steps of determining aircraft altitude and determining aircraft airspeed. The method further includes the steps of computing an engine thrust value that complies with the sound exposure level limit based on the altitude, airspeed and the sound exposure levels, and outputting the computed engine thrust value for use in controlling the aircraft during departure.
摘要翻译：提供了一种在飞机起飞期间生产飞机可变推力裁减的方法。该方法包括以下步骤：将存储器中的飞行器的预期声音曝光水平存储在存储器中，并将导航飞行的声音曝光水平限制存储在存储器中。该方法还包括确定飞机高度并确定飞机空速的步骤。该方法还包括以下步骤：基于高度，空速和声音暴露水平计算符合声音暴露水平极限的发动机推力值，并输出计算出的发动机推力值以用于在起飞期间控制飞行器。

4. 发明申请

WO2008112527A2 METHOD OF GENERATING VARIABLE THRUST CUTBACK DURING AIRCRAFT DEPARTURE 审中-公开
标题翻译：在飞机出发时产生可变扭矩的方法
公开(公告)号：WO2008112527A2
公开(公告)日：2008-09-18
申请号：PCT/US2008/056170
申请日：2008-03-07
申请人： GENERAL ELECTRIC COMPANY , DEJONGE, Michael, K.
发明人： DEJONGE, Michael, K.
CPC分类号： G05D1/0661
摘要： A method of producing a variable thrust cutback of an aircraft during aircraft departure is provided. The method includes the steps of storing expected sound exposure levels for an aircraft in memory, and storing a sound exposure level limit for a navigation flight in memory. The method also includes the steps of determining aircraft altitude and determining aircraft airspeed. The method further includes the steps of computing an engine thrust value that complies with the sound exposure level limit based on the altitude, airspeed and the sound exposure levels, and outputting the computed engine thrust value for use in controlling the aircraft during departure.
摘要翻译：提供了一种在飞机起飞期间生产飞机可变推力裁减的方法。该方法包括以下步骤：将存储器中的飞行器的预期声音曝光水平存储在存储器中，并将导航飞行的声音曝光水平限制存储在存储器中。该方法还包括确定飞机高度并确定飞机空速的步骤。该方法还包括以下步骤：基于高度，空速和声音暴露水平计算符合声音暴露水平极限的发动机推力值，并且输出用于在起飞期间控制飞行器的计算的发动机推力值。

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