- Patent Title: Gas turbine engine airfoil with tip leading edge shelf discourager
-
Application No.: US16002688Application Date: 2018-06-07
-
Publication No.: US11028703B2Publication Date: 2021-06-08
- Inventor: Emma J. Place
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Bachman & LaPointe, P.C.
- Main IPC: F01D5/20
- IPC: F01D5/20 ; F01D5/18 ; F01D11/08

Abstract:
An airfoil including a pressure sidewall and a suction sidewall extending from a root section of the airfoil to a tip region of the airfoil and a leading edge and a trailing edge defines a chord length of the airfoil therebetween. A tip shelf is formed along the tip region of the airfoil between the pressure sidewall and a tip shelf wall with a tip shelf discourager that extends from the tip shelf.
Information query
IPC分类: