Balanced radial engine
OwnerMichael P. Goldowskyinventor
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OwnerMichael P. Goldowskyinventor
Estimating the term…
A low cost multi cylinder radial aircraft engine is composed of an even number of individually functional, single cylinder slider crank model engines. They are mounted to a plate to form equally spaced radially oriented cylinders. In the preferred embodiment, use of standard, low cost, & mass produced two cycles engines are used. This in conjunction with a novel exhaust muffler and throttle mechanism results in a low cost radial engine. The individual engine shafts surround and are parallel to a central output shaft. Pinion gears on each shaft transfer power to a larger sun gear on the output shaft. This gearing synchronizes opposed pistons to reach top dead center at the same time resulting in vibration free piston motion and perfect balance of the entire engine. Said gearing also provides speed reduction for use of large diameter scale propellers. A rear mounted throttle mechanism controls individual carburetor throttles. Each cylinder radially exhausts into a donut shaped exhaust manifold that also serves as a muffler at the front of the engine. It very effectively lowers cylinder exhaust noise by using opposed flow impingement. The muffler also utilizes turbulent gas cooling to greatly reduce exhaust gas temperature and energy. This results in very low noise like its 4 cycle competitor.
An internal combustion radial engine composed of an even number of identical and fully functional single cylinder slider crank 2-cycle or 4-cycle engines, each engine comprising a piston, linkage means, carburetor means, and shaft, said engines being positioned in pairs in a common plane, said pistons are in line and diametrally opposed, said engine shafts are parallel to one another and to a central output shaft and having synchronizing means positioned on said engine shafts for coupling said engine shafts to the output shaft whereby diametrally opposite pistons radially move in phase synchronism thereby cancelling all piston and linkage means inertial forces, said output shaft projects from said synchronizing means past a front of the radial engine and said engine shafts project from said engines to the synchronizing means opposite in direction to said output shaft.
An internal combustion radial engine composed of an even number of identical and fully functional single cylinder slider crank 2 cycle or 4 cycle engines, each engine comprising a piston, linkage means, carburetor means, and shaft, said engines being positioned in pairs in a common plane, said pistons are in line and diametrally opposed, said engine shafts are parallel to one another and to a central output shaft, and having gears attached on said engine shafts for coupling said engine shafts to the output shaft, said output shafts projects from the gears past a front of the radial engine and said engine shafts project from said engines to the gears opposite in direction to said output shaft, throttle means to synchronize a throttle of each engine, and muffler means consisting of a generally donut shaped exhaust manifold surrounding said output shaft at the front of said radial engine with passage means for the exhaust gas of said engines to be injected into the manifold.
Dependencies are inferred from the claim text.