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US Patent 8256707 Engine mounting configuration for a turbofan gas turbine engine

Patent 8256707 was granted and assigned to United Technologies on September, 2012 by the United States Patent and Trademark Office.

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Patent abstract

An engine mounting configuration reacts engine thrust at an aft mount. The engine mounting configuration reduces backbone bending of the engine, intermediate case distortion and frees-up space within the core nacelle.

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