Comment by Tim Lucas on July 6, 2011 at 8:37pm If you sit on this thing during test flights like Ritchie is saying then yes you would be a fool, Common sense tells me you will fly it as a UAV first though, I know some guys that are going to fly a Gyrocopter as a UAV.
Your control system/ Gyros should be able to counteract the fact that no one is sitting in it if your pilot seat is not at centre of gravity. A quad copter is a dangerous craft for a human to sit on they rely too heavily on gyros etc one stuck gyro and this thing will flip fast This is not real common but can happen conventional helicopters are capable of auto rotational landings a fixed pitch quad is generally not Robert yours should if you hook it up right, I cant see it being something to rely on though I would have a fast deployable parachute or ejection seat which would be standard with a military test vehicle.
Even a small quad if one paremeter is out it can just flip when you try to take off sounds like your blades are around eye level.
Where are you located? if you get this going I would love to see it :)
Comment by fibrewire on July 16, 2011 at 7:23pm
Comment by Tim Lucas on July 17, 2011 at 6:46am I am quite aware of how these systems work as I have a couple of them sitting in the other room, also conventional helicopter systems, having studied aviation and also worked on real choppers
Please note: be it a collective pitch quad or a fixed pitch quad is irrelevant They both require Flight control systems & cannot be controlled properly with direct linkages to a cyclic or RC system.
You are basically using the same systems as a normal chopper uses on its tail rotor but 4 of them sprouting from a 4 way gearbox in the centre.
What stage are you currently at?
Comment by fibrewire on July 17, 2011 at 6:37pm Two 3-way gearbox, CVT on center axle. See here
I'm designing the monocoque fuselage now, but my main project is design of the blade roots and lead-lag damper plate.
The original blades for this aircraft are only about 12" long with a 2" chord, made of Roacell foam with a carbon fiber 'C' spar and tungsten weights for inertia. The new blades are 18" long with a 3.5" chord, made from a single piece of extruded aluminum. The roots for the new blades will be about 3.5" long, for a total blade diameter of 48".
The engine will produce 115 HP at the target RPM of 6000. Once the blades are built, I will begin testing to see what the optimum speed for lift is. The rotor with blades will be mounted to a pedestal built specifically for testing. The rotor will be mated to a 30HP 3600RPM electric motor, and lift generated will be measured by a load cell.
Comment by Tim Lucas on July 18, 2011 at 12:07am
Comment by fibrewire on July 18, 2011 at 12:09am Doesn't seem right, but four 48" rotors is the equivalent of one 16' rotor...
1400lbs static thrust???
Comment by fibrewire on July 18, 2011 at 12:41am
Comment by fibrewire on October 9, 2011 at 12:52am Still working on this, real life gets in the way. Someday I will post my progress.
Comment by fibrewire on December 25, 2011 at 11:52pm Pictures soon, also some proof-of-concept video + my rotor diameter
http://www.youtube.com/watch?v=qvxfo5oGaPA
http://www.youtube.com/watch?v=Vy5Ky50eGJs
Comment by fibrewire on October 2, 2012 at 10:12am 2.5 years and nobody has even attempted this yet? Real life gets in the way, but I'm the only dummy with big dreams? Guess I have to do this for real just so it can be "done"
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Season Two of the Trust Time Trial (T3) Contest has now begun. The fourth round is an accuracy round for multicopters, which requires contestants to fly a cube. The deadline is April 14th.58 members
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