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Why
a Diesel Engine?
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Benefits of the
diesel-cycle engine include:
Desirable
Fuel Type:
Low flammability and worldwide availability of Jet-A or diesel
fuel is valued in all applications; current aviation fuel for
the IO-360 and other high compression engines is leaded and
will eventually be made unavailable by the EPA (Environmental
Protection Agency), making those engines unusable.
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Fuel
Efficiency:
The Delta Diesel Engine is designed to BSFC (brake specific fuel
consumption) of .37 lb/hp/hr versus current avgas-powered aviation
engine book BSFC of .59 lb/hp/hr at 75% and above.
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Lower
Fuel Cost: 20-30%
more range per gallon. Also, cost per gallon of Jet-A averages
$0.09 less than 100LL aviation fuel in the U.S. The price differential
is much greater in Europe.*
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Electromagnetic
Noise Elimination:
Absence of an ignition system reduces interference with navigational
and communication systems; for military applications, this is
desirable for tactical reasons.
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Simplicity
of Operation:
Single-lever power operation (no mixture control).
Durability:
Inherent in diesels
because diesel and jet fuels provide more lubricity and because
no electrical system (magnetos or electronic ignition) is required.
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Smoothness:
A two-stroke diesel
has four power pulses per revolution with continuous positive
torque applied to the propeller (versus two pulses per revolution
with approximately 30 degrees of negative torque in four-stroke/four-cylinder
engines).
Liquid-Cooling:
Reduces overcooling
in descents from altitude. Also, reduced thermal variance in
operation allows tighter manufacturing tolerances, leading to
increased power and fuel efficiency.
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Durability:
The 2-stroke piston-ported design reduces the parts count by
eliminating valves, valve train and cam shaft. Lliquid
cooling reduces fatigue and unified cylinder and block design
eliminates studs, gaskets and bolts.
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Reliability:
Fail-safe design aspects
have been incorporated, including backup air, redundancy of fuel
pumps and limited operation at reduced power without coolant.
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Small
Size and Light Weight:
The V-design is stout and compact; use of advanced materials and
focus on low weight as a design criteria will result in a V-8
model producing nearly 1 horsepower per pound. The V-4 is at least
30 lbs lighter than the equivalent aviation engine (comparisons
at fully installed weight) and hundreds of pounds lighter than
equivalent marine diesels. For new aircraft designs, the V configuration
also allows a more rounded cowling, permitting aerodynamic and
propeller noise reduction improvements.
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*
As a recent e-mail stated: "In Europe and particularly the U.K.
economic benefits are more pronounced due the prohibitive price
of both petrol and avgas ... Jet A ... does not cost more than
£0.30 per liter ($0.45) as opposed to petrol or avgas at £0.80
per liter ($1.28). Also given the improved economy of your engine
it is not difficult to show a saving of £5000.00 ($8000.00)
per year in fuel on only 210 hours engine time. Conservative
hourly savings work out at £25.00 per hour ($40.00) in a Velocity
or Cozy MK4. £100.00 ($160.00) of fuel will carry you 2100nm
with the DeltaHawk or 630nm with the Lycoming 360. While in
practice these saving may not be quite so large they will still
be considerable, probably over 50%. ... The incredible savings
this side of the water would probably make conversion from other
engine types a very real economic proposition even with the
cost of a new engine!!"
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For more history
and information, check out . . .

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