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
    • 8. 发明授权
    • Electric circuit with power amplifier for piezoelectric actuators
    • 具有压电执行器功率放大器的电路
    • US09484843B2
    • 2016-11-01
    • US14067148
    • 2013-10-30
    • AIRBUS HELICOPTERS DEUTSCHLAND GMBHEADS DEUTSCHLAND GMBH
    • Boris GrohmannStefan Storm
    • H01L41/09H02N2/06B64C27/00B64C27/72
    • H02N2/065B64C27/001B64C2027/7283Y02T50/34
    • An electric circuit with one power amplifier (V1) for at least two piezoelectric actuators (C1, C2), said piezoelectric actuators (C1, C2) being in preferably antagonist arrangement connected mechanically in series and being connected electrically with each other and operated or clocked by a control circuit, such as a pulse modulator circuit, for time-variant energizing of the piezoelectric actuators (C1, C2) in push-pull fashion, said power amplifier (V1) being connected to a junction point between the two piezoelectric actuators (C1, C2), characterized in that said power amplifier (V1) is connected to a one directional diode (D1) and in that two buffer capacitors (C3, C4) and two static resistors (R3, R4) are provided downstream the one directional diode (D1) with regard to the power amplifier (V1).
    • 具有用于至少两个压电致动器(C1,C2)的一个功率放大器(V1)的电路,所述压电致动器(C1,C2)优选地是串联连接并且彼此电连接并且被操作 通过诸如脉冲调制器电路的控制电路,用于以推挽方式对压电致动器(C1,C2)进行时变激励,所述功率放大器(V1)连接到两个压电致动器之间的连接点 C1,C2),其特征在于,所述功率放大器(V1)连接到单向二极管(D1),并且在一个方向下游提供两个缓冲电容器(C3,C4)和两个静态电阻器(R3,R4) 关于功率放大器(V1)的二极管(D1)。
    • 9. 发明授权
    • Procedure for automatically landing an aircraft
    • 自动降落飞机的程序
    • US09443437B2
    • 2016-09-13
    • US12883845
    • 2010-09-16
    • Manfred Hiebl
    • Manfred Hiebl
    • G08G5/02G08G7/00G05D1/06G08G5/00
    • G08G5/025G05D1/0684G08G5/0013G08G5/0069G08G7/00
    • A procedure and system are provided for automatically landing an aircraft, particularly an unmanned aircraft on a moving, particularly floating landing platform, for example, on an aircraft carrier, the aircraft being equipped with an automatic navigation device and an automatic landing control device. The procedure includes detecting the position of an intended landing spot, detecting motion data of the landing platform, determining at least one imminent point in time at which the landing spot takes up a reference position, transmitting the point in time and the reference position of the landing spot to the landing control device of the aircraft, and controlling the aircraft such that it reaches the landing spot at the point in time.
    • 提供了一种程序和系统,用于自动着陆飞机,特别是在移动的,特别是浮动的着陆平台上的无人飞机,例如在航空母舰上,飞行器配备有自动导航装置和自动着陆控制装置。 该过程包括检测预期着陆点的位置,检测着陆平台的运动数据,确定着陆点占据参考位置的至少一个迫在眉睫的时间点,将时间点和 着陆点到飞机的着陆控制装置,并控制飞机,使其在该时间点到达着陆点。