Invention Grant
- Patent Title: Turbine blade tip cooling system
- Patent Title (中): 涡轮叶尖冷却系统
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Application No.: US11939592Application Date: 2007-11-14
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Publication No.: US07934906B2Publication Date: 2011-05-03
- Inventor: Xubin Gu , George Liang
- Applicant: Xubin Gu , George Liang
- Applicant Address: US FL Orlando
- Assignee: Siemens Energy, Inc.
- Current Assignee: Siemens Energy, Inc.
- Current Assignee Address: US FL Orlando
- Main IPC: F01D5/18
- IPC: F01D5/18

Abstract:
A turbine blade for a turbine engine having a cooling system in the turbine blade formed from at least one elongated tip cooling chamber forming a portion of the cooling system and at least partially defined by the tip wall proximate to the first end. An inner surface of the tip wall may include a plurality of curved bumper protrusions extending from the inner surface radially inward toward the root. The cooling system may include a plurality of ribs generally aligned with the trailing edge, and the curved bumper protrusions may be offset in a chordwise direction relative to the ribs. A throat section may extend between a first forwardmost curved bumper protrusion and a second immediately adjacent downstream curved bumper protrusion and may be offset radially outward from an inner tip surface, thereby creating a first recessed tip slot with a reduced tip wall thickness.
Public/Granted literature
- US20090123292A1 Turbine Blade Tip Cooling System Public/Granted day:2009-05-14
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