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    • 4. 发明申请
    • Laser Welded Fasteners
    • 激光焊接紧固件
    • US20090308850A1
    • 2009-12-17
    • US12477323
    • 2009-06-03
    • John E. Hill
    • John E. Hill
    • B23K26/14
    • B23K33/008B23K26/14B23K26/244B23K2101/34B23K2103/08
    • A method of manufacturing a vehicle structure including a laser welded fastener includes positioning a first panel in engagement with a second panel to provide access to the first panel by a laser beam. The first panel is laser welded to the second panel. A fastener including projections axially extending from a first surface of a flange are formed. The projections are engaged with a surface of the first panel to space apart the first surface of the flange from the surface of the first panel. Laser welding is initiated by directing a laser beam toward one of the flange of the fastener and the first panel. Gas is vented from an area between the first surface of the flange and the surface of the first panel. The flange is laser welded to the first panel.
    • 一种制造包括激光焊接紧固件的车辆结构的方法包括将第一面板定位成与第二面板接合,以通过激光束来访问第一面板。 第一个面板被激光焊接到第二个面板。 形成包括从凸缘的第一表面轴向延伸的凸起的紧固件。 突起与第一面板的表面接合,以将凸缘的第一表面与第一面板的表面间隔开。 通过将激光束引导到紧固件的凸缘和第一面板之一来启动激光焊接。 气体从凸缘的第一表面和第一面板的表面之间的区域排出。 法兰被激光焊接到第一个面板上。
    • 5. 发明申请
    • Spot Welding Tip for a Spot Welding Machine
    • 点焊机点焊焊头
    • US20080296267A1
    • 2008-12-04
    • US12090924
    • 2005-12-06
    • John E. Hill
    • John E. Hill
    • B23K11/30
    • B23K11/3009
    • A spot welding tip for use in a spot welding machine includes a base portion having a longitudinal base axis that passes through a center of the base portion. A tip portion extends from the base portion and provides a contact surface. The tip portion includes a longitudinal tip axis that passes through a center of the tip portion and a center of the contact surface. The spot welding tip includes a transverse axis that is perpendicular to both the base axis and the tip axis. The base axis and the tip axis are parallel to one another and offset from one another by a length. The contact surface is angled with respect to the transverse axis by an angle.
    • 用于点焊机的点焊头包括具有穿过基部的中心的纵向基轴的基部。 尖端部分从基部延伸并提供接触表面。 尖端部分包括穿过尖端部分的中心和接触表面的中心的纵向尖端轴线。 点焊尖端包括垂直于基部轴线和尖端轴线的横向轴线。 基轴和尖端轴彼此平行并且彼此偏移长度。 接触表面相对于横向轴线成一定角度。
    • 6. 发明授权
    • Composition for cleaning grease-traps and septic tanks control
    • 用于清洁油脂捕集器和化粪池控制的组成
    • US5885950A
    • 1999-03-23
    • US789932
    • 1997-01-28
    • Parker DaleJohn E. Hill
    • Parker DaleJohn E. Hill
    • C11D3/30C11D3/38C11D3/48C11D3/386C11D3/18
    • C11D3/48C11D3/30C11D3/381
    • A composition and methods for cleaning grease-traps, septic tank control, discharge water from industrial meat and poultry processing and packing plants, lift stations and municipal systems. The composition comprises preservatives at a concentration of about 0.35%, by weight, a non-ionic surfactant at a concentration of about 8%, by weight, triethanolamine at a concentration of about 2%, by weight and a fermentation supernatant at a concentration of about 12.14%, by weight. In a preferred embodiment of the present invention the composition comprises a fermentation supernatant from a Saccharomyces cerevisiae culture, sodium benzoate, imidazolidinyl urea, diazolidinyl urea, triethanolamine and a polyoxyethlene alcohol surfactant.
    • 用于清洁油脂捕集器,化粪池控制,工业肉类和家禽加工和包装厂排放水,起重站和市政系统的组合物和方法。 组合物包含浓度为约0.35重量%的浓度为约8重量%的浓度为约2重量%的三乙醇胺的浓度为约0.35重量%的非离子表面活性剂和浓度为约2重量%的发酵上清液 约12.14%(重量)。 在本发明的优选实施方案中,组合物包含来自酿酒酵母培养物的发酵上清液,苯甲酸钠,咪唑烷基脲,重氮烷基脲,三乙醇胺和聚氧乙烯醇表面活性剂。
    • 8. 发明授权
    • Aircraft engine mount adapter and method
    • 飞机发动机适配器和方法
    • US5127606A
    • 1992-07-07
    • US614884
    • 1990-11-16
    • Chi F. ChanJohn E. Hill
    • Chi F. ChanJohn E. Hill
    • B64D27/18B64D27/26
    • B64D27/26B64D27/18
    • An aircraft engine mount adapter and method is provided that permits the coupling of an aircraft engine to an aircraft when the pickup points on the engine are incompatible with the location of the mounting pins on the aircraft. The adapter consists of an arcuate shaped member having sufficient lateral curvature so as to be selectively positionable along the length and about the circumference of the engine's casing. Means for locking onto the mounting pins are disposed along the outer surface of the member. The member has a plurality of flanges which are bolted to flanges extending outwards from the engine's casing.
    • 提供一种飞机发动机安装适配器和方法,其允许当发动机上的拾取点与飞机上的安装销的位置不兼容时将飞机发动机与飞行器耦合。 适配器由具有足够侧向曲率的弧形构件组成,以便沿着发动机壳体的长度和周围可以选择性地定位。 用于锁定到安装销上的装置沿着构件的外表面设置。 该构件具有多个凸缘,这些凸缘螺栓连接到从发动机壳体向外延伸的凸缘。