Invention Grant
- Patent Title: Turbine airfoil tip shelf and squealer pocket cooling
- Patent Title (中): 涡轮机翼尖架和尖叫口袋冷却
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Application No.: US14250166Application Date: 2014-04-10
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Publication No.: US09284845B2Publication Date: 2016-03-15
- Inventor: Scott D. Lewis , Dominic J. Mongillo, Jr. , Steven Bruce Gautschi , Christopher Corcoran
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Kinney & Lange, P.A.
- Main IPC: F01D5/20
- IPC: F01D5/20

Abstract:
An airfoil comprises pressure and suction surfaces extending from a root section to a tip section of the airfoil. The airfoil also comprises a leading edge and trailing edge defining a chord length therebetween. A tip shelf is formed along the tip section between the pressure surface and a tip shelf wall, the tip shelf wall being spaced between the pressure surface and the suction surface. A squealer pocket is formed along the tip section between the tip shelf wall and a squealer tip wall extending from the suction surface. The tip shelf extends from within 10% of the cord length measured from the leading edge to within 10% of the chord length measured from the trailing edge. The squealer pocket extends from within 10% of the chord length measured from the leading edge to terminate less than 85% of the chord length measured from the trailing edge.
Public/Granted literature
- US20150118063A1 TURBINE AIRFOIL TIP SHELF AND SQUEALER POCKET COOLING Public/Granted day:2015-04-30
Information query
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