Gas turbine engine nacelle

Details Gas turbine engine nacelle Gas turbine engine nacelle

B - Operations, Transporting

64

D

60/89

B64D 33/02 (2006.01) B64D 29/00 (2006.01) F02C 7/04 (2006.01)

Patent

CA 1257971

- 10 - Abstract Gas Turbine Engine Nacelle A nacelle structure (14) for a gas turbine engine (4) extends upstream from the engine air inlet (10) and includes an external surface (18) and an internal surface (16). The external surface (18) is concentric about a linear centerline (22) which is disposed parallel to the free airflow stream (6) encountered by the nacelle (14) in flight. The internal surface (16) is concentric about a curved centerline (30), the curved centerline (30) being parallel to the free airflow stream (6) at the nacelle inlet (12) and parallel to the engine centerline (26) at the engine air inlet (10) for smoothly directing the internal airflow stream (32) into the engine air inlet (10).

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