FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft power plant and aircraft proper. Aircraft power plant 2 comprises engine 6, engine mounting structure 4 and nacelle 5 surrounding engine 6 and provided with air intake 32 and sections of fan housing 34. Besides, power plant comprises support 49 whereon fan housing is fitted to move thereon. Power plant comprises jointing aerodynamic cover 33 equipped with mounting appliances arranged on said support 40 and element 4.
EFFECT: improved aerodynamics of aircraft.
10 cl, 9 dwg
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Authors
Dates
2011-11-10—Published
2007-07-10—Filed