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1.发明申请公开(公告)号：US20130211691A1
公开(公告)日：2013-08-15
申请号：US13806432
申请日：2011-06-16
申请人： Yannick Evra , Jean Michel Py , Pascal Rupert
发明人： Yannick Evra , Jean Michel Py , Pascal Rupert
IPC分类号： B64D31/00
CPC分类号： B64D31/00 , B64F5/60 , G05B9/02 , G05B17/02 , G05B19/0423 , G05B2219/13174 , G05B2219/13184 , G05B2219/13186 , G05B2219/23446 , G05B2219/24061 , G05B2219/24062
摘要： A system for real time simulation of the environment of an aeroengine includes a digital computer having its inputs switched by a selection module included in the computer either to a respective sensor or else to a substitution digital bus configured to convey substitution digital data generated by a real time simulator.
摘要翻译： 用于航空发动机的环境的实时模拟的系统包括数字计算机，其数字计算机具有由包括在计算机中的选择模块切换到相应的传感器的数字计算机，或者被配置为传送由真实生成的替代数字数据 时间模拟器。
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公开(公告)号：US09114883B2
公开(公告)日：2015-08-25
申请号：US13806432
申请日：2011-06-16
申请人： Yannick Evra , Jean Michel Py , Pascal Rupert
发明人： Yannick Evra , Jean Michel Py , Pascal Rupert
IPC分类号： B64D31/00 , B64F5/00 , G05B9/02 , G05B17/02 , G05B19/042
CPC分类号： B64D31/00 , B64F5/60 , G05B9/02 , G05B17/02 , G05B19/0423 , G05B2219/13174 , G05B2219/13184 , G05B2219/13186 , G05B2219/23446 , G05B2219/24061 , G05B2219/24062
摘要： A system for real time simulation of the environment of an aeroengine includes a digital computer having its inputs switched by a selection module included in the computer either to a respective sensor or else to a substitution digital bus configured to convey substitution digital data generated by a real time simulator.
摘要翻译： 用于航空发动机的环境的实时模拟的系统包括数字计算机，其数字计算机具有由包括在计算机中的选择模块切换到相应的传感器的数字计算机，或者被配置为传送由真实生成的替代数字数据 时间模拟器。
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3.发明申请TURBOMACHINE COMPRISING A PRIVILEGED INJECTION DEVICE AND CORRESPONDING INJECTION METHOD 有权包含特殊注射装置的涡轮机和相应的注射方法公开(公告)号：US20140000276A1
公开(公告)日：2014-01-02
申请号：US14000765
申请日：2012-02-17
IPC分类号： F02C7/22
CPC分类号： F02C7/22 , F02C7/228 , F02C9/28 , F02C9/34 , F05D2270/091 , F05D2270/309 , F05D2270/31
摘要： A turbomachine including: a combustion chamber, with a fuel injection device in the combustion chamber; a supply mechanism supplying fuel to the fuel injection device; a mechanism determining instantaneous variation of fuel flow rate of the supply mechanism; and a regulation mechanism regulating the fuel flow rate of the injection device according to the instantaneous variation of the fuel flow rate of the supply mechanism determined by the determination mechanism.
摘要翻译： 一种涡轮机，包括：燃烧室，在燃烧室中具有燃料喷射装置; 向燃料喷射装置供给燃料的供给机构; 确定供给机构的燃料流量的瞬时变化的机构; 以及调节机构，其根据由所述确定机构确定的所述供给机构的燃料流量的瞬时变化来调节所述喷射装置的燃料流量。
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公开(公告)号：US09938902B2
公开(公告)日：2018-04-10
申请号：US14000765
申请日：2012-02-17
CPC分类号： F02C7/22 , F02C7/228 , F02C9/28 , F02C9/34 , F05D2270/091 , F05D2270/309 , F05D2270/31
摘要： A turbomachine including: a combustion chamber, with a fuel injection device in the combustion chamber; a supply mechanism supplying fuel to the fuel injection device; a mechanism determining instantaneous variation of fuel flow rate of the supply mechanism; and a regulation mechanism regulating the fuel flow rate of the injection device according to the instantaneous variation of the fuel flow rate of the supply mechanism determined by the determination mechanism.
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