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    • 4. 发明授权
    • Method of shielding and coating an airfoil
    • 屏蔽和涂覆翼型的方法
    • US07939135B2
    • 2011-05-10
    • US12326292
    • 2008-12-02
    • Harvey R. ToppenDean N. Marszal
    • Harvey R. ToppenDean N. Marszal
    • B05D1/32
    • C25D5/022B05B12/20
    • A gas turbine engine is used for power generation or propulsion and includes vanes. Each vane includes a trailing edge having a curvature and cooling slots that cool the vane. A photochemical edge shield includes an edge and projections that project from the edge. Before coating the vane, the photochemical edge shield is positioned on the vane such that each of the projections is received in one of the cooling slots. A ceramic coating is then applied to the vane. The photochemical edge shield prevents the ceramic coating from entering and clogging the cooling slots of the vane during the ceramic coating process.
    • 燃气涡轮发动机用于发电或推进,并且包括叶片。 每个叶片包括具有曲率的后缘和冷却叶片的冷却槽。 光化学边缘护罩包括从边缘突出的边缘和突起。 在涂覆叶片之前,光化学边缘护罩定位在叶片上,使得每个突起被容纳在一个冷却槽中。 然后将陶瓷涂层施加到叶片上。 光化学边缘防护层可以防止陶瓷涂层在陶瓷涂层过程中进入和堵塞叶片的冷却槽。
    • 7. 发明授权
    • Coating fixture for a turbine engine blade
    • 用于涡轮发动机叶片的涂层固定装置
    • US5792267A
    • 1998-08-11
    • US858002
    • 1997-05-16
    • Dean N. MarszalRussell A. Beers
    • Dean N. MarszalRussell A. Beers
    • B05B15/04C23C4/00B05C13/00
    • B05B15/045C23C4/01
    • A fixture (90) for use in selectively applying a protective coating to a gas turbine engine blade (10) includes a base (92) having a blade retention slot (102), and a disposable shield (110). The shield (110) includes a sheet metal sleeve (112) and a cap (114) having a window (116) the cap being affixed to one end of the sleeve. When fully assembled with the blade properly positioned in the fixture only those portions of the blade selected to be coated are exposed. Additional features such as a locator dowel (104) extending from the floor of the slot and mutually cooperative track (121) and nub (122) assist in locating the blade correctly in the fixture and orienting the window with respect to the blade platform (16). A lock exemplified by a groove (128) and the nub (122) resists separation of the shield from the base during coating operations.
    • 用于选择性地将保护涂层施加到燃气涡轮发动机叶片(10)的固定装置(90)包括具有刀片保持槽(102)和一次性屏蔽(110)的基座(92)。 所述屏蔽件(110)包括金属板套管(112)和具有窗口(116)的盖子(114),所述盖子固定在所述套筒的一端。 当与正确定位在夹具中的刀片完全组装时,仅暴露了被选择被涂覆的刀片的那些部分。 诸如从狭槽的底板和相互协调的轨道(121)和凸块(122)延伸的定位器销钉(104)的附加特征有助于将刀片正确地定位在固定装置中并使窗口相对于刀片平台(16)定向 )。 由凹槽(128)和凸块(122)示例的锁在涂覆操作期间抵抗了护罩与基座的分离。