ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE
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United States of America Patent
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Issued Date -
Mar 7, 2024
app pub date -
Jun 28, 2023
filing date -
Jun 2, 2008
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Abstract
A gas turbine engine includes, among other things, a propulsor section including a rotor and blades, a gear train, a compressor section and a turbine section. A static structure includes a first case and a second case. The first case includes a first engine mount location. The second case includes a second engine mount location. The first engine mount location is axially near the gear train.
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