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    • 56. 发明授权
    • Ink-jet printing method and print
    • 喷墨打印方式和打印
    • US06224204B1
    • 2001-05-01
    • US08547463
    • 1995-10-24
    • Makoto Aoki
    • Makoto Aoki
    • B41J201
    • B41J3/4078B41J11/002D06P1/0004D06P5/001D06P5/30
    • Disclosed herein is an ink-jet printing method comprising ejecting inks by an ink-jet printing apparatus to conduct printing on a cloth, wherein a cloth having water absorption of at least 3 seconds as determined by a method (dropping method) prescribed by JIS L-1096 A is used as said cloth, a shot-in ink quantity per unit area of the cloth is changed to conduct gradation control, and a shot-in ink quantity per ink upon printing of the maximum color density is adjusted within a range of from not less than 8.0 &mgr;g/mm2 to not more than 35.0 &mgr;g/mm2.
    • 本文公开了一种喷墨打印方法,其包括通过喷墨打印设备喷射油墨以在布上进行印刷,其中通过JIS L规定的方法(滴加法)测定吸水率为至少3秒的布 -1096A用作所述布,改变布的每单位面积的喷射量,以进行灰度控制,并且在最大颜色密度打印时每墨水的喷射墨量调节在 从不小于8.0mug / mm2至不大于35.0mug / mm2。
    • 57. 发明授权
    • Electrophotographic photosensitive member having surface of non-monocrystalline carbon with controlled wear loss
    • 具有非单晶碳表面的电子照相感光构件具有受控的磨损损失
    • US06183930B2
    • 2001-02-06
    • US09218632
    • 1998-12-22
    • Shigenori UedaJunichiro HashizumeMakoto Aoki
    • Shigenori UedaJunichiro HashizumeMakoto Aoki
    • G03G2100
    • G03G21/0017G03G5/08285G03G5/14704
    • For stably obtaining high-quality images with good cleaning properties, with neither occurrence of uneven scraping of a surface layer of a light receiving member nor fusion of a toner, and without occurrence of an image defect even without provision of a heater, the wear loss of the surface layer of a non-monocrystalline hydrogenated carbon film is made not less than 1 Å/10,000 sheets nor more than 10 Å/10,000 sheets after completion of copying processes of A4-size transfer sheets, each copying process including developing an image on a light receiving member with a developer having an average grain diameter of 5 to 8 &mgr;m, then transferring the developer image onto a transfer medium, and thereafter scrape-cleaning the surface of the light receiving member with an elastic rubber blade having the hardness of not less than 70 nor more than 80.
    • 为了稳定地获得具有良好清洁性能的高质量图像,即使没有加热器也不会发生光接收部件的表面层的不均匀刮擦,也不会发生调色剂的熔融,并且即使没有加热器也不会发生图像缺陷,磨损 的非单晶氢化碳膜的表面层在A4尺寸转印纸的复印过程完成之后不小于1 / 10,000张,不大于10埃/ 10,000张,每个复印过程包括显影图像 具有平均粒径为5〜8μm的显影剂的光接收元件,然后将显影剂图像转印到转印介质上,然后用硬度不高的弹性橡胶刮刀刮擦光接收元件的表面 小于70,不超过80。
    • 60. 发明授权
    • helicopter blade aerofoil
    • 直升机叶片机翼
    • US5957662A
    • 1999-09-28
    • US945300
    • 1997-10-17
    • Makoto AokiHiroki NishimuraEiichi Yamakawa
    • Makoto AokiHiroki NishimuraEiichi Yamakawa
    • B64C27/46B64C3/14B64C27/467
    • B64C27/467B64C3/14Y10S416/02Y10S416/05
    • In a helicopter blade aerofoil, upper and lower surfaces thereof are defined by the following coordinates, and the leading edge profile of the aerofoil is defined by the following leading edge radius and center of circle. Thus drag divergence Mach number Mdd and maximum lift coefficient Clmax can be increased and the level of noise can be reduced.______________________________________X/C Yup/C Ylow/C______________________________________0.00000 0.00000 0.000000.00250 0.00781 -0.005580.00500 0.01131 -0.007650.00750 0.01423 -0.008740.01000 0.01660 -0.009640.01750 0.02224 -0.011560.02500 0.02658 -0.012760.50000 0.03585 -0.015680.07500 0.04128 -0.017580.10000 0.04480 -0.019010.15000 0.04893 -0.021130.20000 0.05095 -0.023060.25000 0.05181 -0.024920.30000 0.05200 -0.026470.35000 0.05179 -0.027600.40000 0.05129 -0.028210.45000 0.05038 -0.028270.50000 0.04888 -0.027750.55000 0.04673 -0.026620.60000 0.04393 -0.024910.65000 0.04037 -0.022680.70000 0.03592 -0.019960.75000 0.03052 -0.016820.80000 0.02430 -0.013370.85000 0.01751 -0.009740.90000 0.01046 -0.005970.95000 0.00407 -0.002361.00000 0.00207 -0.00079______________________________________ Leading edge radius r/C = 0.00844, Center of circle X/C = 0.00842, Y/C = 0.00064,
    • PCT No.PCT / JP97 / 00674 Sec。 371日期1997年10月17日第 102(e)1997年10月17日PCT 1997年3月5日PCT公布。 公开号WO97 / 32780 PCT 日期1997年9月12日在直升机叶片机翼中,其上表面和下表面由以下坐标限定,机翼的前缘轮廓由以下前缘半径和圆心定义。 因此,可以增加拖曳发散马赫数Mdd和最大提升系数Clmax,并且可以降低噪声水平。 - X / C Yup / C Ylow / C - 0.00000 0.00000 0.00000 - 0.00250 0.00781 -0.00558 - 0.00500 0.01131 -0.00765 - 0.00750 0.01423 -0.00874 - 0.01000 0.01660 -0.00964 - 0.01750 0.02224 -0.01156 - 0.02500 0.02658 -0.01276 - 0.50000 0.03585 -0.01568 - 0.07500 0.04128 -0.01758 -0.10000 0.04480 -0.01901-0.15000 0.04893 -0.02113 -0.20000 0.05095 -0.02306 -0.25000 0.05181 -0.02492-0.30000 0.05200 -0.02647 -0.35000 0.05179 -0.02760-0.40000 0.05129 -0.02821-0.45000 0.05038 -0.02827-0.50000 0.04888 -0.02775 - 0.55000 0.04673 -0.02662 - 0.60000 0.04393 -0.02491 - 0.65000 0.04037 -0.02268 - 0.70000 0.03592 -0.01996 - 0.75000 0.03052 -0.01682 - 0.80000 0.02430 -0.01337 - 0.85000 0.01751 -0.00974 - 0.90000 0.01046 -0.00597 - 0.95000 0.00407 -0.00236 - 1.00000 0.00207 -0.00079 - 前缘半径r / C = 0.00844, - 圆心X / C = 0.00842,Y / C = 0.00064, -