Invention Grant
- Patent Title: Turbine engine rotor disc with cooling passage
- Patent Title (中): 具有冷却通道的涡轮发动机转子盘
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Application No.: US12310285Application Date: 2007-08-15
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Publication No.: US08348615B2Publication Date: 2013-01-08
- Inventor: Richard Bluck , Paul Jacklin
- Applicant: Richard Bluck , Paul Jacklin
- Applicant Address: DE München
- Assignee: Siemens Aktiengesellschaft
- Current Assignee: Siemens Aktiengesellschaft
- Current Assignee Address: DE München
- Priority: EP06017536 20060823
- International Application: PCT/EP2007/058434 WO 20070815
- International Announcement: WO2008/022954 WO 20080228
- Main IPC: F01D5/18
- IPC: F01D5/18

Abstract:
Disclosed is a gas turbine engine rotor disc with a plurality of cooling passages having an essentially radial orientation relative to an axis of rotation of the rotor disc, each cooling passage having an inlet and an outlet and being included relative to a rotor disc surface and a cut-out arranged at the passage at an outlet end of the passage. Each cooling passage terminating in a slot is arranged in the periphery of the rotor disc. Each slot is sized and configured to receive a glade root.
Public/Granted literature
- US20100014958A1 TURBINE ENGINE ROTOR DISC WITH COOLING PASSAGE Public/Granted day:2010-01-21
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