Curved centerline air intake for a gas turbine engine

Details Curved centerline air intake for a gas turbine engine Curved centerline air intake for a gas turbine engine

F - Mech Eng,Light,Heat,Weapons

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F02C 7/04 (2006.01) B64D 33/02 (2006.01)

Patent

CA 1140349

13DV-7424 CURVED CENTERLINE AIR INTAKE FOR A GAS TURBINE ENGINE ABSTRACT OF THE DISCLOSURE An inlet for a gas turbine engine is disposed about a curved centerline for the purpose of accepting intake air that is flowing at an angle to engine centerline and progressively turning that intake airflow along a curved path into alignment with the engine. This curved inlet is intended for use in under-the- wing locations and similar regions where airflow direction is altered by aerodynamic characteristics of the airplane. By curving the inlet, aerodynamic loss and acoustic generation and emission are decreased.

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