B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
244/47
B64D 29/02 (2006.01) B64C 21/06 (2006.01) B64D 29/00 (2006.01) B64D 33/02 (2006.01) F01D 5/14 (2006.01) F02C 7/04 (2006.01)
Patent
CA 2012248
13DV-8904 ABSTRACT OF THE DISCLOSURE A hybrid laminar flow nacelle for housing an engine of an aircraft includes an outer annular cowl having a leading lip and radially spaced and axially extending annular outer and inner forward surf ace . portions which merge at the leading lip. The nacelle incorporates a suction bleed system between the surfaces and a tailored outer surface geometry shape for producing reduced friction drag laminar flow over the outer cowl at cruise operation of the aircraft and producing separation-free flow over the inner surf ace of the cowl at off-cruise operation of the aircraft.
Lahti Daniel J.
Mungur Permanad
Stockman Norbert O.
Yates David E.
Company General Electric
Craig Wilson And Company
Lahti Daniel J.
Mungur Permanad
Stockman Norbert O.
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