Gas turbine engine assemblies including strut-based vibration isolation mounts and methods for producing the same

摘要

Embodiments of a gas turbine engine assembly including a strut-based vibration isolation mount are provided, as are embodiments of a method for producing such a gas turbine engine assembly. In one embodiment, the gas turbine engine assembly includes a gas turbine engine and a vibration isolation mount. The vibration isolation mount includes, in turn, at least one three parameter axial strut having a first end attached to the gas turbine engine and having a second, opposing end configured to be attached to the airframe. The three parameter axial strut is tuned to minimize the transmission of vibrations from the gas turbine engine to the airframe during operation of the gas turbine engine.