Patent search ap:("UNITED TECHNOLOGIES CORPORATION") AND inv:"Dominic J Mongillo Page Jr."

1.

发明授权
Splayed tip features for gas turbine engine airfoil 有权

公开(公告)号：US10329916B2

公开(公告)日：2019-06-25

申请号：US14630814

申请日：2015-02-25

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： San Quach , Tracy A Propheter-Hinckley , Dominic J Mongillo, Jr. , Steven Bruce Gautschi

IPC: F01D5/18 , F01D5/14 , F01D5/28 , B22C9/10

Abstract: A component for a gas turbine engine includes a trailing edge tip corner that at least partially defines a trailing edge cavity and a multiple of corner features within the trailing edge cavity, the multiple of corner features splayed along the trailing edge tip corner.

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