公开(公告)号：US20110221093A1

公开(公告)日：2011-09-15

申请号：US12723241

申请日：2010-03-12

Applicant: Nathaniel Perrow ,  James Ray Starr ,  Matthew Ryan Baker

Inventor： Nathaniel Perrow ,  James Ray Starr ,  Matthew Ryan Baker

IPC: B29C33/58

CPC classification number: B29C70/44 ,  B29C33/505 ,  B29C33/58 ,  B29C70/48 ,  B29L2031/08 ,  B29L2031/085 ,  Y02P70/523

Abstract: A method and system for making and forming turbine blades. The method and system can include steps for determining stress loads on amore turbine blades; constructing one or more molds for components of the turbine blade in which a turbine-forming substance is injected; applying a resin to an interior portion of the one or more molds; forming one or more partitions within the one or more molds; coupling the one or more molds; injecting the blade-forming substance into the coupled one or more molds; regulating the pressure in the coupled one or more molds; voiding any excess air or resin in the coupled one or more molds; and allowing the blade-forming substance injected into the coupled one or more molds to harden.

Abstract translation: 一种用于制造和形成涡轮叶片的方法和系统。 该方法和系统可以包括确定多余涡轮叶片上的应力负荷的步骤; 为其中注入涡轮形成物质的涡轮叶片的部件构造一个或多个模具; 将树脂施加到所述一个或多个模具的内部; 在一个或多个模具内形成一个或多个隔板; 联接一个或多个模具; 将所述刀片形成物质注入所述联接的一个或多个模具中; 调节耦合的一个或多个模具中的压力; 在耦合的一个或多个模具中排空任何多余的空气或树脂; 并且允许注入到联接的一个或多个模具中的刀片形成物质硬化。