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    • 1. 发明授权
    • Aircraft comprising a device for influencing the directional stability of the aircraft, and a method for influencing the directional stability of the aircraft
    • 包括用于影响飞行器的方向稳定性的装置的飞行器以及影响飞行器的方向稳定性的方法
    • US09315255B2
    • 2016-04-19
    • US13255246
    • 2010-03-17
    • Carsten WeberMarkus FischerArnaud Namer
    • Carsten WeberMarkus FischerArnaud Namer
    • B64C5/06B64C9/32
    • B64C5/06B64C9/32Y02T50/32
    • An aircraft including a device for influencing the directional stability of the aircraft is provided. The device includes a control-input device; a flight control device; a sensor device for acquiring the rotation rates, including the yaw rates, of the aircraft; and at least one actuator, which is coupled with ailerons, spoilers, an elevator and a rudder. The flight control device includes a control function generating adjusting commands for the actuators for controlling the aircraft according to control commands. The aircraft includes two tail-mounted flaps, each including an actuator connected with the flight control device, situated symmetrically to each other and on opposite sides of the fuselage, and movable between retracted and extended positions. The control function is designed such that the adjusting commands that are generated on the basis of the control commands depending on the acquired rotation rates include adjusting commands to the actuators of the tail-mounted flaps.
    • 提供了包括用于影响飞行器的方向稳定性的装置的飞机。 该装置包括控制输入装置; 飞行控制装置; 用于获取飞行器的转速的传感器装置,包括偏航率; 以及与副翼,扰流器,电梯和方向舵耦合的至少一个致动器。 飞行控制装置包括控制功能,该控制功能根据控制命令产生用于控制飞行器的致动器的调节命令。 飞机包括两个尾部安装的翼片,每个翼片包括与飞行控制装置连接的致动器,其彼此对称并且在机身的相对侧上对准,并且可在缩回位置和伸出位置之间移动。 控制功能被设计成使得基于所获取的旋转速度而基于控制命令生成的调节命令包括调整到尾部安装的翼片的致动器的命令。
    • 2. 发明授权
    • Hybrid cooling system of an internal combustion engine
    • 内燃机混合冷却系统
    • US08893669B2
    • 2014-11-25
    • US13278941
    • 2011-10-21
    • Jan MehringBernd SteinerCarsten Weber
    • Jan MehringBernd SteinerCarsten Weber
    • F01P7/00F01P3/02F01M1/12F01P3/00
    • F01P3/02F01M2001/123F01P2003/008F01P2003/021F01P2003/024F01P2037/02
    • A hybrid cooling system for an engine is provided. The system comprises a block oil cooling circuit, a head coolant cooling circuit, the head and block circuits having a common heat exchanger. The system also includes a flow device in the head cooling circuit for preventing coolant flow in the head cooling circuit at least during a first phase of a warm-up phase of the internal combustion engine, a delivery device in the block cooling circuit which delivers engine oil constantly under pressure through the block cooling circuit to bearing points in a cylinder block and to bearing points in a cylinder head, and a control element arranged in a control line to reduce the delivery capacity of the delivery device through the block cooling circuit at least during the first phase of the warm-up phase. In this way, heat transfer in the common heat exchanger may be substantially prevented.
    • 提供了一种用于发动机的混合冷却系统。 该系统包括块油冷却回路,头部冷却剂冷却回路,头部和块状回路具有共同的热交换器。 该系统还包括头部冷却回路中的流动装置,用于至少在内燃机的预热阶段的第一阶段期间防止冷却剂在头部冷却回路中的流动;块冷却回路中的输送装置,其输送发动机 在压力下通过块体冷却回路将油保持在气缸体中的轴承点和气缸盖中的轴承点,以及布置在控制线中的控制元件,以至少通过块冷却回路减少输送装置的输送能力 在预热阶段的第一阶段。 以这种方式,可以基本上防止公共热交换器中的热传递。