发明名称 |
TURBINE ENGINE CASE MOUNT AND DISMOUNT |
摘要 |
<p>A method for mounting a gas turbine engine having a compressor section, a combustor section, a turbine section, a pylon and a rear mount bracket, includes positioning the mounting bracket between the gas turbine engine and the pylon. The mounting bracket is connected to the turbine case reacting a least a vertical load, a side load, a thrust load, and a torque load from the gas turbine engine through the mounting bracket. The mounting bracket is attached to the pylon reacting the same loads from the gas turbine engine.</p> |
申请公布号 |
WO2013138104(A1) |
申请公布日期 |
2013.09.19 |
申请号 |
WO2013US29006 |
申请日期 |
2013.03.05 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCIU, GABRIEL L.;ALVANOS, IOANNIS;MERRY, BRIAN D. |
分类号 |
F02K3/00;B64C1/00;F02K99/00 |
主分类号 |
F02K3/00 |
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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