A gas turbine engine has a rear mounting assembly incorporating a mounting apparatus attached to a bypass duct wall with a link device for transferring core portion related inertia-induced loads, from an MTF of the core portion in a short circuit across an annular bypass air passage to the bypass duct wall.
申请公布号
CA2702501(A1)
申请公布日期
2010.11.15
申请号
CA20102702501
申请日期
2010.04.29
申请人
PRATT & WHITNEY CANADA CORP.
发明人
HEYERMAN, JEFFREY BERNARD;OLVER, BRYAN W.;FIELDING, BRUCE;SMYTHE, CARL
