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US07780410B2 Method and apparatus for gas turbine engines 有权
燃气轮机发动机的方法和装置

Method and apparatus for gas turbine engines
摘要:
A method of assembling a gas turbine engine includes providing at least one blade assembly. The method also includes forming at least one blade tip fuse within at least a portion of the at least one blade assembly. The method further includes coupling the at least one blade assembly into the gas turbine engine. The blade assembly includes an airfoil and a metal leading edge (MLE) coupled to at least a portion of the airfoil. The MLE includes the at least one blade tip fuse.
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