发明名称 |
TRUNNION RETENTION FOR A TURBINE ENGINE |
摘要 |
A fan (38) for a gas turbine engine is provided. The fan (38) includes a plurality of fan blades (40), a disk (42), and a trunnion mechanism (90) for attaching the fan blades (40) to the disk (42). The disk (42) can be formed of a plurality of individual disk segments (92), with the trunnion mechanism (90) attaching one of the plurality of fan blades (40) to a respective disk segment (92). A retention member (102) is also provided. The retention member (102) includes a means for catching a portion of the trunnion mechanism (90) should a primary attachment system (96) of the trunnion mechanism (90) fail. |
申请公布号 |
EP3109481(A3) |
申请公布日期 |
2017.03.01 |
申请号 |
EP20160175693 |
申请日期 |
2016.06.22 |
申请人 |
General Electric Company |
发明人 |
MILLER, Brandon Wayne;NIERGARTH, Daniel Alan;PRENTICE, Ian Francis |
分类号 |
F04D27/00;B64C11/06;F01D5/30;F01D7/00;F01D21/04;F02K3/04;F04D29/36 |
主分类号 |
F04D27/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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