发明名称 Mid turbine frame system for gas turbine engine
摘要 A gas turbine engine has an engine casing component, such as a mid turbine frame system, which may includes an outer case (30) surrounding a spoke or strut casing (32). Load transfer spokes (36) of the spoke casing (32) extend between the outer case (30) and an inner case (34) of the spoke casing (32). A bearing housing (50) supported by the engine casing may include a fuse arrangement (58; 60) for isolating bearing seizure loads from the engine casing. A seal arrangement may be provided to centralize the rotors after the fuse fails. The mid turbine frame may be provided to have a desired flexibility through the configuration of the casing and bearings in design.
申请公布号 EP2851523(B1) 申请公布日期 2017.03.22
申请号 EP20140193105 申请日期 2009.10.01
申请人 Pratt & Whitney Canada Corp. 发明人 Durocher, Eric;Pietrobon, John;Nguyen, Lam
分类号 F01D25/28;F01D9/06;F01D21/04 主分类号 F01D25/28
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