FIELD: transport.
SUBSTANCE: power plant 1 comprises engine 6, engine fixation 5 and engine nacelle 3 equipped with sections of fan housing 34. Fixation 4 comprises rigid structure 8 and front aerodynamic structure 24 made up of support assembly 40 coated by aerodynamic fairing 46 and sections of fan housing hinged thereto. Said support assembly 40 has rear fasteners 44a, 44b arranged on rigid structure 8 of fixation 4 and is provided with front fasteners 42 secured on fan housing of aircraft engine 6.
EFFECT: better aerodynamic properties.
11 cl, 4 dwg
Authors
Dates
2011-09-20—Published
2007-07-10—Filed