FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft power plant. Power plant 1 comprises engine 6 and its attachments arrangement between wing 2 and engine. Said attachment comprises stiff structure 8 and engine attachments 6. Aircraft power plant 1 comprises stiff structure 8 and engine attachments 6. Sad attachments consist of first 10 and second 12 suspensions. Note here that fist suspension 10 is made up of two lateral semi-assemblies 10a each secured on engine fan housing while second suspension 12 is secured on front part of engine central housing 22.
EFFECT: simplified design, engine reduced sag.
18 cl, 12 dwg
Authors
Dates
2011-07-27—Published
2006-09-22—Filed