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    • 1. 发明授权
    • Hybrid vehicle
    • 混合动力汽车
    • US09014900B2
    • 2015-04-21
    • US14220516
    • 2014-03-20
    • Koji HokoiMakoto Hirai
    • Koji HokoiMakoto Hirai
    • B60W20/00B60W10/06B60W10/08B60W10/26
    • B60W20/40B60W10/06B60W10/08B60W10/26B60W20/12B60W20/13B60W20/14B60W2510/244B60W2550/143B60W2550/402Y02T10/6286Y10S903/93
    • A hybrid vehicle includes: an engine; a motor; a battery; a navigation system; and a controller configured to carry out navigation coordination traveling, the controller being configured to stop the navigation coordination traveling when a state of charge of the battery becomes lower than or equal to a first switching threshold, the controller being configured to resume the navigation coordination traveling when the state of charge of the battery becomes higher than or equal to a second switching threshold higher than the first switching threshold, the controller being configured to set a first predetermined state of charge for the first switching threshold when there is no regenerative travel section, and the controller being configured to set a second predetermined state of charge lower than the first predetermined state of charge when there is the regenerative travel section.
    • 混合动力车辆包括:发动机; 电机 一个电池 导航系统; 以及控制器,其执行导航协调行进,所述控制器被配置为当所述电池的充电状态变为低于或等于第一切换阈值时停止所述导航协调行进,所述控制器被配置为恢复导航协调行进 当所述电池的充电状态变得高于或等于高于所述第一开关阈值的第二开关阈值时,所述控制器被配置为当没有再生行驶部时设定所述第一开关阈值的第一预定充电状态, 并且所述控制器被配置为当存在所述再生行驶部时,设定比所述第一预定充电状态低的第二预定充电状态。
    • 2. 发明授权
    • High-lift device, wing, and noise reduction structure for high-lift device
    • 用于高升力装置的高升力装置,机翼和降噪结构
    • US09010692B2
    • 2015-04-21
    • US13557400
    • 2012-07-25
    • Makoto HiraiIchiro Maeda
    • Makoto HiraiIchiro Maeda
    • B64C9/24
    • B64C9/24B64C2009/143
    • A high-lift device suppresses the occurrence of aerodynamic noise while minimizing an increase in airframe weight. The device includes a slat main body disposed to be able to extend from and retract into a main wing, and a concave part formed on the slat main body at a location facing the main wing and able to accommodate at least a part of a leading edge of the main wing. The device also includes an airflow control part disposed at an area in the concave part facing an upper surface of the main wing, that is accommodated between the main wing and the concave part when the slat main body is retracted into the main wing, and that suppresses turbulence colliding against the area in the concave part facing the upper surface of the main wing when the slat main body is extended from the main wing.
    • 高升力装置抑制气动噪声的发生,同时使机身重量增加最小化。 该装置包括:能够从主翼延伸并缩回到主翼中的板条主体;以及在面向主翼的位置上形成在板条主体上的凹部,能够容纳至少一部分前缘 的主翼。 该装置还包括一个气流控制部分,该气流控制部分设置在面对主翼的上表面的凹入部分的区域中,当该翼翼主体缩回到主翼中时,该气流控制部分被容纳在主翼和凹部之间,并且 当板条主体从主翼部延伸时,抑制湍流与面向主翼的上表面的凹部中的区域碰撞。