会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 5. 发明申请
    • Method for the display of cartographic information on an aeroplane screen
    • 在飞机屏幕上显示制图信息的方法
    • US20040174275A1
    • 2004-09-09
    • US10479407
    • 2003-12-03
    • Erick Coppolino
    • G08B021/00G05D001/00
    • G01C23/00
    • The invention relates to the field of methods of displaying cartographic information on aircraft screen. This is a method of display, on an aircraft screen, of several windows (2D5, 3D, VP, HP) each representing a distinct aspect of the terrain of a scene overflown by the aircraft, characterized in that the method can present a simultaneous display of at least three intercorrelated windows which are, a 2D5 window representing a plan view overlaid with relief information, a 3D window representing a three-dimensional view, a profile window (VP) representing a profile view. The invention can in particular be applied to a specific screen dedicated to on-helicopter mission conduct.
    • 本发明涉及飞机屏幕上显示制图信息的方法领域。 这是在飞行器屏幕上显示几个窗口(2D5,3D,VP,HP)的方法,每个窗口表示飞机溢出的场景的不同方面,其特征在于,该方法可以呈现同时显示 至少三个相互关联的窗口,其是表示覆盖有浮雕信息的平面图的2D5窗口,表示三维视图的3D窗口,表示轮廓视图的轮廓窗口(VP)。 本发明特别适用于专用于直升机任务行为的特定屏幕。
    • 6. 发明申请
    • Method and an apparatus for predicting intake manifold pressure of an internal-combustion engine
    • 用于预测内燃机的进气歧管压力的方法和装置
    • US20040162665A1
    • 2004-08-19
    • US10695486
    • 2003-10-29
    • Yuji YasuiAkihiro ShinjoMichihiko Matsumoto
    • G05D001/00B60T007/12
    • G05B13/0275F02D41/1404F02D2200/0402F02D2200/0408
    • A method and an apparatus for predicting intake manifold pressure are presented, to compensate for a large lag or a large time delay without producing an overshot or discontinuous behaviors of a predicted value. The method comprises the step of obtaining a difference of values of a variable to be predicted and a difference of values of another variable ahead of the variable to be predicted. The method further comprises the step of filtering the differences with adaptive filters. The method further comprises the step of obtaining a predicted difference of values of the variable to be predicted, through algorithm of estimation with fuzzy reasoning. The method further comprises the step of adding the predicted difference of values of the variable to be predicted, to a current value of the variable to be predicted, to obtain a predicted value of the variable to be predicted.
    • 提出了一种用于预测进气歧管压力的方法和装置,以补偿大的滞后或大的时间延迟,而不产生预测值的过冲或不连续的行为。 该方法包括以下步骤:获得要预测的变量的值的差异和预测的变量之前的另一个变量的值的差。 该方法还包括用自适应滤波器滤除差异的步骤。 该方法还包括通过使用模糊推理的估计算法获得待预测变量值的预测差值的步骤。 该方法还包括以下步骤:将要预测的变量的值的预测差相加到要预测的变量的当前值,以获得要预测的变量的预测值。
    • 10. 发明申请
    • Process and system for moving a control surface of an aircraft
    • 用于移动飞机控制面的过程和系统
    • US20040111190A1
    • 2004-06-10
    • US10654621
    • 2003-09-04
    • Marc Van De KreekeGuillaume Cassein
    • G05D001/00
    • B64C13/50Y02T50/44
    • An electric control system (1) comprises a control unit (4) which comprises a member (5) able to be actuated by a pilot and a means of load-wise protection (7), and which delivers a first deflection order representative of the action exerted by the pilot on the member (5), and of the contribution made by the means of load-wise protection (7), an actuator (11) which moves said control surface (2) about an axis (Z-Z), as a function of a deflection order, and a correction device (12) which comprises a means (13) for determining a second deflection order making it possible to limit the load, to which a stabilizer element of the aircraft is subjected, to a maximum load, and a means (14) for choosing one of the first and second deflection orders, which is transmitted to said actuator (11) so as to move said control surface (2).
    • 电控制系统(1)包括控制单元(4),该控制单元包括能够由导向装置致动的构件(5)和负载保护装置(7),并且传递第一偏转顺序, 由飞行员对构件(5)施加的作用以及通过负载保护装置(7)作出的贡献,使所述控制表面(2)绕轴线(ZZ)移动的致动器(11)作为 偏转顺序的功能和校正装置(12),其包括用于确定第二偏转顺序的装置(13),使得可以将飞机的稳定器元件所经受的载荷限制在最大载荷 ,以及用于选择第一和第二偏转顺序之一的装置(14),其被传送到所述致动器(11)以便移动所述控制表面(2)。