公开(公告)号：WO2014197031A3

公开(公告)日：2015-02-26

申请号：PCT/US2014022932

申请日：2014-03-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HUSBAND JASON ,  LANCASTER DREW W

IPC: F02C7/24 ,  F01D25/08 ,  F04D29/58

CPC classification number: F01D11/122 ,  B05D5/083 ,  F01D5/02 ,  F01D11/127 ,  F01D21/045 ,  F01D25/24 ,  F02C7/24 ,  F04D29/526 ,  F05D2220/32 ,  F05D2220/36 ,  F05D2230/23 ,  F05D2230/60

Abstract: A fan case for a gas turbine engine includes a fan case surrounding a fan with fan blades. A liner is disposed between the fan case and the fan and is spaced a radial distance from the fan case. A torque stop is arranged between the fan case and the liner. A method for reducing fan case liner loads is also disclosed.

Abstract translation: 用于燃气涡轮发动机的风扇壳体包括围绕具有风扇叶片的风扇的风扇壳体。 衬套设置在风扇壳体和风扇之间并且与风扇壳体间隔开径向距离。 在风扇壳体和衬套之间设置有扭矩停止。 还公开了一种用于减小风扇箱衬套负载的方法。

公开(公告)号：EP2971600A4

公开(公告)日：2016-12-14

申请号：EP13880744

申请日：2013-12-03

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HUSBAND JASON ,  LANCASTER DREW W

IPC: F01D21/00 ,  F01D15/12 ,  F01D21/04 ,  F01D25/00 ,  F02C7/00

CPC classification number: F01D21/006 ,  F01D5/02 ,  F01D15/12 ,  F01D21/045 ,  F05D2220/323 ,  F05D2220/36 ,  F05D2260/40311 ,  F05D2260/902 ,  Y02T50/671

Abstract: A turbofan engine including a fan section including a plurality of fan blades rotatable about an axis, a compressor including a plurality of compressor blades, a turbine including a plurality of turbine blades and a geared architecture driven by the turbine for driving the fan section at a speed and direction different than the turbine is disclosed. A rub strip proximate at least one of the compressor blades, the turbine blades and the fan blades slows rotation when engaged. The rub strip generates a torque opposing rotation when in an engaged condition that is between 2 and 6 times a torque encountered in a non-engaged condition.