hi brian,
i ran the designs through the performance codes, to try and do the best comparison i could. i am seeing the swept forward / swept back config about 2 decibels quieter than the straight blades. i kept the radius and power the same for both designs. given the drastically different geometry, that made the rpm for the straight blades half of the swept blades. so a 2:1 reduction gear is the only difference. the motor would be the same for this comparison.
they stated they did this for noise and not having exposed tips for drones. i'm not really sure that it's any safer though. if your finger got caught in the rotor it would still be a problem. for marine applications i'm thinking seaweed and lily pads would still get all mangled in there. the straight blades were slightly more efficient, so they made a little more thrust. it's a pretty negligible difference though. the cad model i showed has the annulus to try and duplicate the loop they have in their design. the annulus wouldn't cause any aero modeling issues and is easier to model in cad. performance wise, ducting/annulus/tip devices don't make any difference. so i usually don't use them. i only put that in the model to try and produce an equivalent to what they were doing. that loop they have to connect the blades would be an issue though. you would have to use 3d cfd to model that. i suspect it would cause performance degradation, to some extent.
in any event, i don't know that this is patent worthy or even really worthwhile. it limits your options a lot. there are a lot of things you can do to deal with noise. i'm not really sure this is the way to go. but to each their own. what's sad to see is this is just one of many configs you can run and for some reason they think they can patent it. if i were to really build something like this, i think i would do it the way i showed in the pictures, but leave the annulus off. the blades shown have 60 degrees of sweep. that's a massive amount. pretty much the maximum allowed, otherwise the blades double back and would be nonsensical.
anthony
Update 1; Added pictures of the swept geometry that was used in the comparison
Update 2; Added the normal swept geometry. It performs exactly the same as the swept forward / swept back config. This is another reason why the patent seems so senseless to me.
Update 3; I conducted another comparison, to try and make it more fair. Previously, the rpm difference benefited the swept design. It allowed the noise to be less, since the torque was higher for the straight blade. For the updated comparison, I kept radius, shp, and rpm the same. This makes torque the same as well. So the noise calcs are on an even playing field. As expected, the straight blade performed better. It had more efficiency, thrust, and comparable noise. So I definitely don't see an advantage to the torodial propeller. In fact, it's worse in a lot of ways. You can just use a regular swept blade config and get the exact same performance as the swept forward / swept back config (toroidal propeller). However, as mentioned, you can outperform a swept blade with straight blades. I added some pics of the updated swept design. The duct / annulus is of no benefit and adds weight and cost. So I wouldn't use it. If safety is a concern, for drones, you can just put a cage around the drone or props.
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