Developing the CarterCopter :
The original test rig for trying out the rotor and rotor control mechanisms.
Developing the CarterCopter :
The original test-rig cockpit.
Developing the CarterCopter :
The prop hub showing the arm used to change blade pitch - like the main
rotor the prop is built on a mono-constructed composite I-beam.
The black material is the hub of the I-beam.
The I-beam is warped to effect a pitch-change.
Developing the CarterCopter :
The 7' 10" diameter composite Prop.
Developing the CarterCopter :
Putting the 7' 10" diameter Prop into perspective.
Developing the CarterCopter :
The NASCAR V6 Engine minus the turbo-chargers. Shows the belt used to
pre-rotate the rotor.
Developing the CarterCopter :
The complete engine assembly being checked for weight and balance.
Developing the CarterCopter :
The prop and engine fitted.
Developing the CarterCopter :
The rotorhead testrig - shows the collective control arms, and the tilt
spindle pushrod arms and levers. The main collective control rod comes
up thru the middle.
Also shows the universal joint and the 'parallelogram' shock-absorbing
mechanism that allows the rotor to move fore & aft yet maintains current
collective and tilt (indirect cyclic) settings.
As with the prop-hub, the black composite material that the rotor blades
are part of, is the hub of the mono constructed rotor I-beam. That in turn
is clamped to the teeter hinge pivot-plate just above it. The teeter uses
Delta-3 (pivot being offset from the normal 90 degrees).
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THIS SITE = www.internetage.com.au/cartercopters/
D.Marker email: dmarker@zeta.org.au
R.Anderson email:
cartercopter@casagrande.com
- 04 Dec 1998
Created: 01 Dec 1998 - Updated: 04 Dec 1998
Copyright © 1998 Internet Age Pty Ltd