发明名称 GAS TURBINE ENGINE BEARING ARRANGEMENT
摘要 <p>An example gas turbine engine includes a housing and first and second spools coaxial with one another and arranged within the housing. The first spool is arranged within the second spool and extends between forward and aft ends. The aft end extends axially beyond the second spool. First and second bearings support the aft end of the first spool relative to the housing. An example method of assembling the gas turbine engine includes arranging a first spool within a second spool. First and second bearings are mounted between an aft end of the first spool and a fixed housing.</p>
申请公布号 EP2809890(A1) 申请公布日期 2014.12.10
申请号 EP20130744407 申请日期 2013.01.22
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MULDOON, MARC J.;SHERIDAN, WILLIAM G.;REINHARDT, GREGORY E.;SAVELA, GREGORY M.
分类号 F01D25/16;F02C7/06;F02K3/068 主分类号 F01D25/16
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