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Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine










Image Number 6 for United States Patent #7971826.

An aircraft engine assembly including an engine, an engine suspension pylon, and a heat exchanger system including an outlet located between the box and the engine, aft from the aft engine suspension. Furthermore, the outlet of the heat exchanger system is provided on an outlet pipe connected to the exchanger and passing through a structural block fixed on a box, between the box and the engine.








 
 
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