

Miles wrote:Why not start by stating what your needs are?
Leaving aside the myths regarding the merits of inrunners vs outrunners... I thought the BMC motor was an outrunner, too?

however it also appears that inrunners are more capable of moving more weight and are better suited for high torque, low rpm scenarios.

Thud wrote:however it also appears that inrunners are more capable of moving more weight and are better suited for high torque, low rpm scenarios.
please link to your source for that information.
it is in total contradiction to everything Ive learned.


Miles wrote:Outrunners have the advantage of a larger airgap radius for a given overall diameter. This is because a PM rotor take up less space than the stator. For a comparison of inrunners vs outrunners see: viewtopic.php?p=302385#p302385
Direct drive hub motors are outrunners.
The BMC motor you posted the link to is an outrunner. If you take the outer casing off, it's probably a similar size to the Turnigy.
As we don't have a proper specification for the BMC (just a load of marketing drivel), it's difficult to compare them. The Turnigy seems to be optimised to run faster and so will have greater power to weight ratio.


LegendLength wrote:Moving an aircraft requires a different amount of power than moving a bike, so I imagine that's why those values are different.
I was interested a few years ago in electric, human-sized ornithopters. I did some rough calculations on minimum power requirements if you want me to dig them up. Pretty sure a 10 kW (continuous) motor would do it from memory.
Hard part of course is working out the drive mechanism. My initial desire was to use electric motors as an assist for the pilots arms while flapping the wings. But I quickly realized motors don't like to be started and stopped twice per second! I even looked at linear motors ( http://en.wikipedia.org/wiki/Linear_motor ) but they seem quite heavy and not strong for side-loads.
You should post details of your research if you get time. There's an aircraft sub-form here I think.

The best sink rate I could find for an existing hang glider was about 0.8 m/s at 8 m/s (17 mph). The glider was the Condor which is a large learning glider and travels very slowly.
This means the pilot would be effectively lifting their own weight 3 feet every second, which is about 1 kW. For human power you need about half that or less, otherwise it's too much for a non-athlete.

LegendLength wrote:Wow that video is amazing if true, I'll be following its progress.
The actual power requirements for a flapping-winged aircraft are obviously difficult to work out because it depends on the efficiency of the craft (i.e. "sink rate"). But a way to take a simple view is to look at the efficiency of existing hang gliders and work from there as a best case scenario:
From http://www.ornithopter.org/forum/showthread.php?t=429:The best sink rate I could find for an existing hang glider was about 0.8 m/s at 8 m/s (17 mph). The glider was the Condor which is a large learning glider and travels very slowly.
This means the pilot would be effectively lifting their own weight 3 feet every second, which is about 1 kW. For human power you need about half that or less, otherwise it's too much for a non-athlete.
So in other words if you wanted to power a hang glider with a propeller, you'd need a 1 kW motor. That assumes the motor is 100% efficient, as well as the controller, wiring harness and propeller. Of course in real life motors are more likely going to be 90% efficient, controllers 95 perhaps and the propulsion is around 80% using a good propeller.
You'd multiply all those efficiencies together and get a value of like 0.90 * 0.95 * 0.80 = 0.68 . That means the whole system's efficiency is 68% . So to get 1 kW at the wing tips you'd need to feed it that 32% extra that gets wasted by the system which would be 1.32 kW input power for level flight (i.e. no climbing ability).
These figures are all rough of course and using the best case scenario of a well designed glider. But it's just to demonstrate a way of working through the numbers to help get a feel for the absolute minimum power requirements. For an ornithopter I feel the propulsion will be quite inefficient compared to a glider (I reckon only 50% at best) and the weight will be large. So if I had a gun to my head I'd choose at least a 10 kW motor.




You won't be able to use that turnigy in any kind of EV. It has very low inductivity and will kill any bicycle/motorcycle motor controller.

circuit wrote:You won't be able to use that turnigy in any kind of EV. It has very low inductivity and will kill any bicycle/motorcycle motor controller.

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