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    • 4. 发明公开
    • Hard anodize of cold spray aluminum layer
    • 冷喷涂铝层的硬阳极氧化
    • EP2204473A2
    • 2010-07-07
    • EP09252862.9
    • 2009-12-22
    • United Technologies Corporation
    • Bogue, WilliamLomasney, Gary M.Derosa, Robert J.Bunting, Billie W.Parkos, Joseph
    • C23C24/04C25D11/08C25D11/16C25D11/24
    • C23C24/04C23C28/322C23C28/345C25D11/08C25D11/16C25D11/24C25D11/30F01D5/288F05D2230/31F05D2230/90F05D2300/121
    • A process for repairing components (60) includes the steps of providing a component (60) having an affected area (44) on a surface (45) of a component (60) to be repaired; depositing a repair material over the affected area (44) on the surface (45) of the component (60) so that the repair material plastically deforms without melting and bonds to the affected area (44) upon impact with the affected area (44) and thereby covers the affected area (44); providing a sulfuric acid based anodizing solution; anodizing a deposited repair material on the surface (45) of said component (60) in the sulfuric acid based anodizing solution; consuming only a portion of the deposited repair material to form a hard anodized coating layer upon the deposited repair material to form a hard anodized coated component (60); providing a corrosion resistant sealant solution; and contacting a hard anodized coated component with the corrosion resistant sealant solution to form a corrosion resistant sealant coating on the hard anodized coated component (60).
    • 用于修复部件(60)的方法包括以下步骤:在待修复的部件(60)的表面(45)上提供具有受影响区域(44)的部件(60) 将修复材料沉积在部件(60)的表面(45)上的受影响区域(44)上,使得修复材料在没有熔化的情况下塑性变形并且在与受影响区域(44)撞击时结合到受影响区域(44) 从而覆盖受影响的区域(44); 提供硫酸基阳极氧化溶液; 在所述硫酸基阳极氧化溶液中将沉积的修复材料阳极氧化在所述部件(60)的表面(45)上; 仅消耗一部分沉积的修复材料以在沉积的修复材料上形成硬质阳极氧化涂层以形成硬质阳极氧化涂层组件(60); 提供耐腐蚀密封剂溶液; 以及使硬质阳极氧化涂层部件与耐腐蚀密封剂溶液接触以在硬质阳极氧化涂层部件(60)上形成耐腐蚀密封剂涂层。
    • 5. 发明公开
    • Fan exit guide vane and method of repairing therof
    • Verfahren und Vorrichtung zur Reparatur einerBläserausgangsleitschaufel
    • EP1911931A2
    • 2008-04-16
    • EP07254018.0
    • 2007-10-10
    • United Technologies Corporation
    • Bogue, WilliamGolias, John J.
    • F01D5/00F01D9/04F04D29/54
    • F01D5/005B23P6/005F01D9/042F04D29/542F04D29/644Y02T50/672Y02T50/673Y10T29/4924
    • A replacement fan exit guide vane assembly (220) for installation between an inner case (116) and an outer case (118) of a gas turbine engine (100) includes an airfoil structure (222) having an outer end (224) and an inner end (226), a wedge structure (232) connected to the outer end (224) of the airfoil structure (222), a base plate (246) positioned between the outer end (224) of the airfoil structure (222) and the outer case (118), a conformable material (244), and a slip collar (230) having an opening (234) therethrough and a recess (236) formed along the opening (234). The airfoil structure (222) extends through the opening (234), and the recess (236) accepts the wedge structure (232) to create an interference fit between the slip collar (230) and the base plate (246). The conformable material (244, 244A) is disposed along the opening (234) and the recess (236) in the slip collar (230), and also along the baseplate (246), in order to provide dampening relative to the airfoil structure (232) and the wedge structure (232).
    • 用于安装在燃气涡轮发动机(100)的内壳体(116)和外壳体(118)之间的替换风扇出口导叶组件(220)包括具有外端(224)的翼型结构(222) 内端(226),连接到翼型结构(222)的外端(224)的楔形结构(232),定位在翼型结构(222)的外端(224)之间的基板(246)和 外壳(118),适形材料(244)和具有穿过其中的开口(234)的滑环(230)和沿着开口(234)形成的凹部(236)。 翼型结构(222)延伸穿过开口(234),并且凹部(236)接受楔形结构(232)以在滑动环(230)和基板(246)之间形成过盈配合。 顺应性材料(244,244A)沿滑动轴环(230)中的开口(234)和凹部(236)以及基板(246)设置,以便相对于翼型结构( 232)和楔形结构(232)。