FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Support frame 40 is closed by streamlined cowl 46 and rear suspension 44a, 44b mounted on rigid suspension structure 4. Note here that said frame is equipped with suspension structure 42 mounted on engine nacelle air intake 32.
EFFECT: decreased overall dimensions.
15 cl, 7 dwg
Authors
Dates
2012-12-10—Published
2008-08-22—Filed