Invention Grant
- Patent Title: Metallic ceramic spool for a gas turbine engine
- Patent Title (中): 用于燃气轮机的金属陶瓷阀芯
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Application No.: US13180275Application Date: 2011-07-11
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Publication No.: US08984895B2Publication Date: 2015-03-24
- Inventor: James B. Kesseli , Matthew Stephen Baldwin
- Applicant: James B. Kesseli , Matthew Stephen Baldwin
- Applicant Address: US NH Hampton
- Assignee: ICR Turbine Engine Corporation
- Current Assignee: ICR Turbine Engine Corporation
- Current Assignee Address: US NH Hampton
- Agency: Sheridan Ross P.C.
- Main IPC: F02C7/20
- IPC: F02C7/20 ; F02C7/28 ; F01D11/14 ; F01D11/18 ; F01D15/02

Abstract:
A method and apparatus are disclosed for a gas turbine spool design combining metallic and ceramic components in a way that controls clearances between critical components over a range of engine operating temperatures and pressures. In a first embodiment, a ceramic turbine rotor rotates just inside a ceramic shroud and separated by a small clearance gap. The ceramic rotor is connected to a metallic volute. In order to accommodate the differential rates of thermal expansion between the ceramic rotor and metallic volute, an active clearance control system is used to maintain the desired axial clearance between ceramic rotor and the ceramic shroud over the range of engine operating temperatures. In a second embodiment, a ceramic turbine rotor rotates just inside a ceramic shroud which is part of a single piece ceramic volute/shroud assembly. As temperature increases, the ceramic volute expands at approximately the same rate as ceramic shroud and tends to increase the axial clearance gap between the ceramic rotor and ceramic shroud, but only by a small amount compared to a metallic volute attached to the shroud in the same way.
Public/Granted literature
- US20120017598A1 METALLIC CERAMIC SPOOL FOR A GAS TURBINE ENGINE Public/Granted day:2012-01-26
Information query
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