d03933
page 9 - 5
Jan. 01/2007
Effectivity: 912 Serie
OM Edition 1 / Rev. 0
BRP-Rotax
reduction ratio 912 UL / A / F 912 ULS / S
crankshaft : propeller shaft
2,27 : 1
2,43 : 1
(optional)
2,43 : 1
9.5) Propeller gearbox
See fig. 8.
For the engine type 912 two reduction ratios are available.
Depending on engine type, certification and configuration the propeller gear-
box is supplied with or without an overload clutch.
◆ NOTE: The overload clutch is installed on serial production on all
certified aircraft engines and on the non-certified aircraft
engines of configuration 3.
◆ NOTE: Fig. 8 shows a propeller gearbox of configuration 2 with the
integrated overload clutch.
The design incorporates a torsional shock absorber. The shock absorbing is
based on progressive torsional cushioning due to axial spring load acting on
a dog hub.
On the gearbox version with overload clutch the design incorporates a friction
damped free play at the dogs to warrant proper engine idling.
Due to this backlash at the dogs a distinct torsional impact arises at start, stop
and at sudden load changes, but due to the built-in overload clutch it will remain
harmless.
◆ NOTE: This overload clutch will also prevent any undue load to the
crankshaft in case of ground contact of the propeller.
Alternatively either a vacuum pump or a hydraulic governor for constant
speed propeller can be used. The drive is in each case via the propeller
reduction gear.
02531
fig. 8
02719
To Next Page
Loading...
