Item 0925
DESIGN: UniCopter ~
Power Train - Assembly - 6º Crankshaft, All GearFor use with the Rotax 912 and 914.
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Drawing:

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Possible Disadvantages:
The larger diameter of components behind the pilot's head necessitate that he sit further forward; but this may be necessary anyway for CG
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Option:
If the CG and the aerodynamics of the fuselage will allow the engine to be moved aft 2.75" then the Rotax dog and disks on the propeller shaft can be included, in their standard location.
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Advantages:
Total of 8 gears. Three gear sets between engine and each rotor.
Having the pilot slightly further ahead give more room for fuel or payload, at the center of gravity.
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Arraignment of Components & their Design Pages:
Engine:
Rotors:
Rotor Brake:
Consider locating it on x-shaft on opposite side from centrifugal clutch. ![]()
Notes:
This is designed for the Rotax 912 or 914 engine with custom gearbox. See
Consider running the engine at a lower rpm, and decrease the power train ratio proportionately. In other words, de-rate the engine.
The engine's center of gravity is slightly to the starboard of the crafts centerline. Assuming there is clearance between the side of the engine and the fuselage, the engine might be shifted and inch or so to port to make room for the centrifugal clutch.
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Notes re Final Spiral Bevel Gear Sets:
See
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Notes re Rotational Spike Absorber:
There must be a device for minimizing the rotational spikes from the engine since this will result in a considerable lengthening of the power train's reliability and life.
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General Thoughts:
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Center of Gravity of Engine:
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X = -9.5" |
Z = 9.75" |
Y = |
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Last Revised: February 19, 2002