Aircraft engine nacelle having circular arc profile

Details Aircraft engine nacelle having circular arc profile Aircraft engine nacelle having circular arc profile

F - Mech Eng,Light,Heat,Weapons

02

C

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

Patent

CA 2072417

13DV-10268 ABSTRACT OF THE DISCLOSURE A nacelle having an inlet whose front view portrays an elliptical shape and whose side view conforms to a circular arc profile. The circular arc profile is determined by three hilite points located at extreme top, side and bottom locations of the nacelle with each hilite location being set at an individually predetermined distance from a plane which is perpendicular to the inlet centerline.

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