公开(公告)号：CA2428755A1

公开(公告)日：2003-11-22

申请号：CA2428755

申请日：2003-05-14

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LOMASNEY GARY M ,  JAWOROWSKI MARK R ,  PUTNAM JOHN W ,  PARKOS JOSEPH J JR

IPC: C25D11/06 ,  C23C22/34 ,  C23C22/78 ,  C25D11/08 ,  C25D11/18 ,  C25D11/24 ,  C25D11/10 ,  C25D11/02

Abstract: A metal substrate is anodized in a phosphoric acid anodizing solution. The anodized metal substrate is thereafter contacted with a hexavalent chromium free, trivalent chromium containing acid solution to coat the anodized metal substrate. The coated anodized metal substrate can be adhesively bonded to another such treated metal substrate to form a composite article. The resulting article exhibits excellent bonding and corrosion properties.

公开(公告)号：EP2971531A4

公开(公告)日：2016-11-30

申请号：EP14769262

申请日：2014-03-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BOGUE WILLIAM ,  TABOR TIMOTHY J ,  PARKOS JOSEPH J JR

IPC: F01D5/14 ,  C23C4/02 ,  C23C4/04 ,  C23C4/11 ,  C23C4/134 ,  C23C28/04 ,  C25D11/02 ,  C25D11/04 ,  C25D11/08 ,  C25D11/10 ,  C25D11/18 ,  F01D5/28 ,  F01D11/04 ,  F01D11/08

CPC classification number: F01D5/288 ,  C23C4/02 ,  C23C4/11 ,  C23C4/134 ,  C23C28/04 ,  C25D11/022 ,  C25D11/04 ,  C25D11/08 ,  C25D11/10 ,  C25D11/18 ,  F01D11/08 ,  F05D2220/36 ,  F05D2230/31 ,  F05D2230/312 ,  F05D2240/307 ,  F05D2300/121

Abstract: A blade (100) has an airfoil (106) having a leading edge (114), a trailing edge (116), a pressure side (118), and a suction side (120) and extending from an inboard end (110) to a tip (112). An attachment root (108) is at the inboard end. The blade comprises an aluminum alloy substrate (102) and a coating at the tip (130). The coating (130) comprises an anodic layer (160) atop the substrate and an aluminum oxide layer (162) atop the anodic layer.

公开(公告)号：EP0813956A1

公开(公告)日：1997-12-29

申请号：EP97100661

申请日：1997-01-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PARKOS JOSEPH J JR ,  KLEIN JOHN J ,  HERTEL CHRISTOPHER J ,  BLACKBURN LOUIS

IPC: B64C3/00 ,  B32B15/08 ,  B32B15/082 ,  C08J5/12 ,  F01D5/28 ,  B32B31/12

CPC classification number: B32B15/08 ,  B32B15/18 ,  B32B27/304 ,  B32B37/00 ,  B32B2038/0076 ,  B32B2305/72 ,  B32B2309/025 ,  B32B2309/125 ,  B32B2311/00 ,  B32B2327/12 ,  B32B2603/00 ,  F01D5/282 ,  F05D2240/303 ,  Y02T50/672 ,  Y02T50/673 ,  Y10T29/49337 ,  Y10T428/24777 ,  Y10T428/24994 ,  Y10T428/24995 ,  Y10T428/249951 ,  Y10T428/249952 ,  Y10T428/28 ,  Y10T428/2878 ,  Y10T428/31511 ,  Y10T428/31529 ,  Y10T428/3154 ,  Y10T428/31544 ,  Y10T428/31678 ,  Y10T442/2984

Abstract: The present invention related to a method for providing a composite structure and the composite structure formed thereby. The method broadly comprises the steps of: providing a core structure (12) formed from a non-metallic composite material in a substantially uncured state; applying a fluoroelestomer film (14) in a substantially uncured state over surface portions of said core structure (12); placing a metallic structure (16) over a portion of said core structure, said metallic structure having inner surfaces which contacts said fluoroelastomer film (14), and molding said composite structure under conditions of heat and pressure for a time sufficient to co-cure said fluoroelastomer film (14) and said non-metallic core structure material (12) and to form a bond between said fluoroelastomer film and said inner surfaces of said metallic structure. The method of the present invention may be used to manufacture original metal/composite ssssstructures as well as to refurbish metal/composite structures such as fan exit guide vanes for jet engines.

Abstract translation: 本发明涉及一种提供复合结构的方法和由此形成的复合结构。 该方法广泛地包括以下步骤：提供由基本上未固化状态的非金属复合材料形成的芯结构（12） 在所述芯结构（12）的表面部分上施加基本上未固化状态的氟硅胶（14）; 将金属结构（16）放置在所述芯结构的一部分上，所述金属结构具有接触所述含氟弹性体膜（14）的内表面，并且在热和压力条件下模制所述复合结构足以共同固化所述 含氟弹性体膜（14）和所述非金属芯结构材料（12），并且在所述含氟弹性体膜和所述金属结构的所述内表面之间形成结合。 本发明的方法可用于制造原始金属/复合材料结构以及翻新金属/复合结构，例如用于喷气发动机的风扇出口导向叶片。