Puch Magnum/Maxi


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'Gromit' is going freepower! 49cc Puch Magnum/Maxi single speed
'twist and go' scooter engine.
My intention is to use the relatively large gear ratio between the
crankshaft pinion and drive gear for use in a gearbox for a freepower
setup as opposed to using pure thrust for propulsion. With a freepower,
the exhaust gases from the jet are passed through a second larger
turbine wheel which is connected to the rear wheel via a speed
reducing gearbox and chain final drive. Freepower turbine wheels
spin at anything from 30,000-50,000rpm which needs to be brought down
to more managable final drive outputs of 5,000-10,000rpm, hence the
need for large gear ratios. My reason for deciding to go the freepower
route was potential lack of thrust. A freepower setup makes more
efficient use of the exhaust gases giving greater power and
acceleration and even with my two relatively small turbos, has the
potential to outperform even the largest of the gas guzzling pure
thrust types! ;o) |
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Puch Magnum/Maxi 2

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Engine reduced to essential components. Some
fettling work on the crankcases to be done, in particular the shroud
around the automatic clutch which needs to be removed. |
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Freepower Turbine Design

 
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Top two pictures are my first designs for a freepower based on
what others have done. This is going to the biggest challenge to date
in particular construction of the wheel itself which has to stand up
to high speeds and temperatures.
.......... Result! Making the turbine wheel would have been a
huge task to construct let alone the safety aspect if it ever decided
to 'let go'! Luckily a member of the DIYGasturbines group kindly
donated a spare first stage turbine wheel from a commercial Allison
250 ( thanks John "racketmotorman" Wallis! ), and has more than likely
saved me from potentially spitting turbine blades or worse..! ;o) The
wheel in question can be seen most clearly in the lower picture where
it has been sectioned for display purposes and is the same as the
intact one immediately to the right, only slightly smaller with a
diameter of 158mm. If you look closely you can see that there is
severe damage to the blades due to over heating, hopefully this won't
happen with mine..! ;o) |
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| Allison 250 Turbine Wheel




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...and here it is..! ;o) Outer diameter 157mm, hub
diameter 128mm, blade height 14.5mm. Shaft diameter is 20mm, ideal for
fitting standard ball bearing. Thread on shaft 20tpi but odd diameter,
will have to get a 'nut' machined for this. Heavy for it's size,
amazing to think it's going to be spinning at 30-35k rpm! |
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Modified Engine Case



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Top diagram showing preliminary design and section
through turbine shaft. Engine cases have been modified by removing the magneto
shroud which was redundant. The bottom picture shows the position of
the oil burner pump for providing oil to the gears. As the meshing
gears are going to be running at high speed, the use of a pump as
opposed to an oil bath is necessary to force oil at high pressure into
the meshing gears. The pump will be driven via a worm and wheel
arrangement of about a 20:1 ratio mounted on the turbine shaft inside
the original crankcase housing. Coupling to the pump will be via a
double universal joint. |
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Turbine And Gears



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Large gear and pinion with a ratio 5:1. With the
turbine spinning at 35,000rpm, gives an output of 7,000rpm, slow
enough for a chain and sprocket final drive to the rear wheel. |
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Turbine Scroll



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1:1 scale mock-up of the turbine scroll for the
freepower. Adapter tube shown detached. The design is based on what
others have done, intuitive guesswork and aesthetics! ;o) The idea is
that the exhaust gases from the combined turbos will be fed via a
single pipe into the scroll, redirecting the gases correctly onto the
turbine wheel and hence converting the kinetic energy of the gases
into rotational motion. The real scroll will be made from about
1.5-2.0mm thick mild steel sheet. Stainless would be nice but my
welding skills don't stretch that far. ;o) |
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Turbine Scroll 2


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Adapter tube attached. The bottom two pictures show
the turbine as it will be positioned. Not shown is the turbine wheel
shroud which will be made from 5mm thick walled mild steel tube. The
depth of the tube will be about 20mm, just about enough to cover the
blades so that the gases can't bypass the wheel until they have given
up as much of their energy as possible. In addition, clearance between
the blade tips and shroud will need to be tight, not much more than
about 0.5mm, so positional accuracy needs to be ensured in
construction.. ;o) |
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Freepower Turbine Design 2



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Preliminary Blender mock-ups of the design of the freepower. |
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Scroll Work
 
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Some of the parts cut out for the freepower scroll.
Mild steel sheet 1mm thick. Going to be tricky lining things up let
alone welding..! Easiest way to cut off a straight piece of pipe is to
use a strip of paper and wrap around the pipe ( top left ). Once wrapped, the edge of the
paper naturally forms a neat cutting line around and perpendicular to
the axis of the pipe.
Needed to reduce the size of inner part of the
scroll as it was cut from a larger diameter piece of tubing. Using the
vice as a press and a Vee-block, working round 1cm at a time with a
bit of added heat ( bottom right ) |
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Shaft and Shaft Tunnel

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Free machining mild steel bar ( EN1A ) for making a
shaft (30mm Dia) just for dimensioning purposes which will eventually
be made up from a harder steel. The bar for the shaft tunnel (50mm Dia) will have
to be cut to length and completely drilled out to accept the shaft and
bearings. This is going to be a tough and labourious job.. ;o) |

 
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My first lathe a Myford ML2 circa 1937. Just
recently set up and adjusted. Never really used a lathe before, first
excersize was to design and make a lathe steady from wheel bearings to
support end of shaft tunnel. With steady made, I can start the process
of boring out...... |
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Freepower Shroud


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Shroud ring 5mm thick mild steel. Had to cut and
re-weld to close the gap between blade tips and shroud to 0.5mm all
round. This should just about give enough clearance to allow for
turbine wheel expansion without incurring too much bypass losses. |
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