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    • 11. 发明申请
    • Sheet transport device and image forming apparatus including same
    • 片材输送装置和包括其的图像形成装置
    • US20090148214A1
    • 2009-06-11
    • US12314311
    • 2008-12-08
    • Yasuharu GamanNobuo Inoue
    • Yasuharu GamanNobuo Inoue
    • G03G15/00
    • G03G15/6573G03G2215/0043G03G2215/00438G03G2215/00586G03G2215/007
    • A sheet transport device and an image forming apparatus that includes the sheet transport device. The sheet transport device includes a reverse-transport roller, at least one roller guide, and a shaft. The reverse-transport roller is provided to a diverging point of a sheet reversing portion from which a recording medium enters or exits and is configured to transport the recording medium to the sheet reversing portion. At least one roller guide is provided in a vicinity of an end face of at least one side of the reverse-transport roller and is configured to prevent the reverse-transport roller from contacting the recording medium when reversing the recording medium. The reverse-transport roller and the roller guide are disposed on the shaft. Friction of a peripheral surface of the roller guide is configured to be substantially less than that of the recording medium.
    • 一种纸张传送装置和包括纸张传送装置的图像形成装置。 片材输送装置包括反向输送辊,至少一个辊引导件和轴。 反向传送辊被提供到片材反转部分的发散点,记录介质从该反转部分的进出处被构造成将记录介质输送到片材反转部分。 在反向输送辊的至少一侧的端面附近设置有至少一个辊引导件,并且构造成在反转记录介质时防止反向传送辊与记录介质接触。 反向输送辊和滚子引导件设置在轴上。 滚子引导件的外围表面的摩擦力被构造成基本上小于记录介质的摩擦。
    • 16. 发明申请
    • ANTI-ICING SYSTEM, WING, AIRCRAFT, AND ANTI-ICING METHOD
    • 防盗系统,WING,飞机和防盗方法
    • US20130181093A1
    • 2013-07-18
    • US13824639
    • 2011-12-26
    • Nobuo Inoue
    • Nobuo Inoue
    • B64D15/00
    • B64D15/00
    • Provided are an anti-icing system, wing, aircraft, and anti-icing method which prevent icing on the aircraft flying in an environment under icing conditions, using a simple configuration. An anti-icing system according to the present invention generates a pressure wave by aiming at supercooled airborne water droplets existing in a traveling direction of an aircraft (10) and thereby changes the water droplets into ice by means of the pressure wave. To impart an acceleration of, for example, 10 G to the water droplets, the pressure wave is set to produce 0.9 to 3.3 [Pa] at a predetermined location by taking attenuation into consideration.
    • 提供了一种防冰结构,机翼,飞机和防冰方法,可以防止结冰在结冰环境中飞行的飞机,使用简单的配置。 根据本发明的防冰系统通过瞄准存在于飞行器(10)的行进方向上的过冷空气水滴产生压力波,并且由此通过压力波将水滴变成冰。 为了赋予水滴例如10G的加速度,通过考虑衰减,压力波被设定为在预定位置处产生0.9至3.3 [Pa]。