FeX32,
The patent was filed on 4/18/2017 (US 62485227), and I understand applications are published 18 months after filing, so it should appear soon. The patent has 26 claims stated in the highly confusing language of a patent lawyer. In the meantime, you can view a slightly outdated description of the engine with illustrations at
I have made several changes in response to comments by a consultant I hired (who worked on the Ecotech, Skyactiv, and Liquid Piston designs) and to reduce the complexity of the prototype. Included in the changes are a reduction in equivalency from (1.0 to 0.4) with peak temperature to 2150K to prevent NOX formation, direct routing within the cylinder block of intake charge from the air pump piston to the intake chamber to eliminate some rotor side seals, reduction of piston sets (each radial set comprised of 3 piston faces) from 12 to 6, and increase of cycles per revolution from 4 to 6. The last change, increase of cycles per revolution from 4 to 6, is accompanied by a reduction in RPM from 7,800 to 2,626 to allow use of a larger and more efficient propeller turning at a slower speed without requiring a reduction gear.
The numbers are still shifting a bit as I finalize the 50cc prototype design, but they currently indicate approximately 2.8 HP and 5.6 lb-ft torque at 2,626 RPM at better than 50% efficiency sustainable to 20,000 foot altitude in an engine that's 5.4" in diameter and 3" in thickness including all components required for operation other than the fuel and oil tanks. I'm planning to build the engine by 3D printing the components, milling the 3D models for better accuracy and finish using a DSLS 3000 mill (
centrifugal casting the components, then cleaning them up a few thousandths here and there with the same mill. I'm building my own test cell which will include a motoring dyno (constructed using a small electric motor/generator that can either be driven using an off-the-shelf motor controller or loaded using programmable electric load) as well as fuel consumption and emissions sensors. It's going to be a lot of fun!
enginesrus,
I don't think my engine competes with large turbines, and its integral supercharger lends itself best to high altitude applications. My power to weight ratio will be a little worse than a Wankel, but my reliability, efficiency, and emissions should be much better. I think the light aviation market is ideal, and it will likely be the last market to be impacted by electric propulsion due to concerns over weight and range.
Rod