FIELD: transport; aerotechnics.
SUBSTANCE: support for installation of main reduction gear with rotor hull body with cylindrical hull element, basement, rib reinforcement, and units for attachment of main reduction gear. Basement has flat-topped in plane with essentially L-shaped cross-section. Vertical basement seat is equipped with additional plate. Cylindrical hull element between free ends of flat-topped basement changes shape for flat U-form element with convex part turned down from plane within which units for attachment of main reduction gear are located along perimeter of cylindrical hull element. Additional plate in plane approximately follows basement contours, but it is closed over perimeter and has essentially T-shaped cross-section. Above-mentioned units for attachment of main reduction gear are made as bosses of cylindrical hull element with shaped cylindrical orifices.
EFFECT: optimal rotor load transfer, taking of concentrated operation loads.
2 cl, 9 dwg
Title | Year | Author | Number |
---|---|---|---|
SUPPORT FOR MOUNTING MAIN GEAR BOX WITH ROTOR | 2010 |
|
RU2448868C1 |
HELICOPTER AIRFRAME STRUCTURE | 2013 |
|
RU2539612C2 |
METHOD FOR TESTING CENTRAL PART OF FUSELAGE OF LIGHT HELICOPTER | 2023 |
|
RU2816120C1 |
FUSELAGE OF LIGHT HELICOPTER | 2006 |
|
RU2324622C2 |
METHOD OF TRANSPORTING Mi-8 HELICOPTER BY TRAILER AND EQUIPMENT FOR LOCATING AND LOCKING HELICOPTER FOR TRANSPORTATION | 2007 |
|
RU2347711C2 |
HELICOPTER FUSELAGE | 1993 |
|
RU2090450C1 |
HELICOPTER PRIMARY GEARBOX | 1993 |
|
RU2065381C1 |
RESCUE SYSTEM WITH EXTERNAL SUSPENSION BRACKET OF AIRCRAFT | 2014 |
|
RU2563291C1 |
UNMANNED HIGH-SPEED HELICOPTER, DESANTIFIED FROM PLANE AIRCRAFT | 2016 |
|
RU2627975C2 |
HIGH-SPEED HELICOPTER-AMPHIBIOUS AIRCRAFT | 2017 |
|
RU2655249C1 |
Authors
Dates
2009-01-10—Published
2007-01-15—Filed