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2. Premixed flame - Wikipedia

   en.wikipedia.org/wiki/Premixed_flame

   The premixed flame interface propagates through the mixture until the entire charge is depleted. [1] The propagation speed of a premixed flame is known as the flame speed (or burning velocity) which depends on the convection-diffusion-reaction balance within the flame, i.e. on its inner chemical structure. The premixed flame is characterised as ...

3. Hirth F-23 - Wikipedia

   en.wikipedia.org/wiki/Hirth_F-23

   A belt reduction drive system, fuel injection, tuned exhaust and electric start are optional. [1] [2] The engine runs on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil. Recommended time between overhauls is 1000 hours. [1] [2] The F-23 produces 50 hp (37 kW) at 6150 rpm and 40 hp (30 kW) at 5500 rpm. [1] [2]

4. Hirth 2702 - Wikipedia

   en.wikipedia.org/wiki/Hirth_2702

   Fuel system: 1 X Bing 34mm slide type carburetor; Fuel type: unleaded 93 octane auto fuel; Oil system: 50:1 fuel/oil premix; Cooling system: free air or fan; Reduction gear: G-50 gearbox with reduction ratios of 2.16:1, 2.29:1, 2.59:1, 3.16:1, or 3.65:1, or a multi-element cog belt drive

5. Hirth 3701 - Wikipedia

   en.wikipedia.org/wiki/Hirth_3701

   Fuel system: 3 X Bing 34 mm slide type carburetors or fuel injection; Fuel type: unleaded 93 octane auto fuel; Oil system: 50:1 fuel/oil premix or oil injection; Cooling system: liquid; Reduction gear: G-50 gearbox with reduction ratios of 2.16:1, 2.29:1, 2.59:1, 3.16:1, or 3.65:1

6. Partially premixed combustion - Wikipedia

   en.wikipedia.org/wiki/Partially_premixed_combustion

   This premixed charge is too lean to ignite during the compression stroke – the charge will ignite after the last fuel injection ends near TDC. The fuel efficiency and working principle of a PPC engine resemble those of Diesel engine, but the PPC engine can be run with a variety of fuels. Also, the partially premixed charge burns clean. [6]

7. Zanzottera MZ 301 - Wikipedia

   en.wikipedia.org/wiki/Zanzottera_MZ_301

   The Zanzottera MZ 301 is a three-cylinder, in-line two-stroke, dual ignition aircraft engine designed for ultralight aircraft. [1] [2]The engine was originally designed and produced by Zanzottera Technologies of Italy, but the design was sold, along with the rest of the company's two-stroke ultralight aircraft engine line, to Compact Radial Engines of Surrey, British Columbia, Canada. [2]