New member has questions`
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New member has questions`
Hello I'm Dave Zichek and I became a member to pick your brains about the Mazda rotary engine, which to me appears to be a compact robust and powerful engine I plan on using in my experimental Mustang II aircraft.
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What I need to know is it possible to get 300hp out of a 12A Mazda using two large turbo's and replacing the apex seal with that out of a 13B turbo?
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http://www.rotaryaviation.com/engine_products.htm
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Normally aspirated, you can easily get around that 300 crank HP level from a 3 rotor / 20B.
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why not 13b?
It would be a lot easier to find a 13b for cheaper and be able to get the parts and power out of it than the 12a, but I'm not sure what the limitations are for an aircraft engine.
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12A/13B for experimental AC
The biggest concern is weight that is why a 12A or 13B turbo is appealing you can get the power of a Lycoming IO 540 with the weight of an IO 360 by the way what would be the typical rpm of a 12A/13B twin turbo producing 300HP?
thanks Dave Z
thanks Dave Z
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