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Reuben, Garrick, Collin
 Standard Engine used in
small aircraft
 Piston torque and
horsepower are decided by
bore and stroke
 Generally powers a propeller
 Can be found in most
transportation vehicles
 Supercharges and Turbos
can be added to increase
power output
 A radial engine has 1
or more rows of
cylinders arranged in a
circle around the
crankcase.
 Every row must have an
odd number of
cylinders, in order to
operate smoothly.
 The incorporation of Ethanol into
the production of airplane engines
is a big breakthrough in the fight
for supporting nature and
reducing the amount of fossil
fuels used in everyday flying.
 Fagen Inc. has taken Ethanol to a
new level. It is now used for high
performance stunts in air shows,
instead of having low HP.
 For Example: The Ethanol-
Powered Fagen MX2 has a
whopping 400+ HP and top speed
of 275 mph.
 Internal Combustion
engine; uses a rotary
design
 4 Stroke Cycle
 Developed in the 1950’s
and only recently was
perfected by Mazda
 Simpler, Lighter, and have
less moving parts than
piston powered engines of
the same power output
 Uses updraft from the
props to store energy
 Able to use solar power to
help fly
 Some have a battery for
takeoff. After takeoff, it
runs completely on solar
power.
 Generally glider shaped,
for maximum lift with
minimum power
 Very inefficient design for an aircraft engine
 Drives a compressor which fires into the jet
engine
 Very fuel inefficient and produces less or
equal power as a conventional jet engine
 Low fuel economy, however, cheap and easy to
build.
 Not very fast
 Pulse jet diagram: First part of the cycle: air flows
through the intake (1), and mixed with fuel (2).
Second part: the valve (3) is closed and the ignited
fuel-air mix (4) propels the craft.
 Used in a few
German planes
 BMW 803 – one of the
most powerful attempts
at a hyper engine.
 28-Cylinders, 3950
Horsepower
 Crankshaft was too weak,
so they used direct
connected props.
 HP/LB ratio is about 0.6
 Uses direct cycle jet
engines powered by a
nuclear reactor
 Soviets were putting in
great effort into
developing the engine
 Very unsafe, however
very powerful if
successful

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Propulsion

  • 2.  Standard Engine used in small aircraft  Piston torque and horsepower are decided by bore and stroke  Generally powers a propeller  Can be found in most transportation vehicles  Supercharges and Turbos can be added to increase power output
  • 3.  A radial engine has 1 or more rows of cylinders arranged in a circle around the crankcase.  Every row must have an odd number of cylinders, in order to operate smoothly.
  • 4.  The incorporation of Ethanol into the production of airplane engines is a big breakthrough in the fight for supporting nature and reducing the amount of fossil fuels used in everyday flying.  Fagen Inc. has taken Ethanol to a new level. It is now used for high performance stunts in air shows, instead of having low HP.  For Example: The Ethanol- Powered Fagen MX2 has a whopping 400+ HP and top speed of 275 mph.
  • 5.  Internal Combustion engine; uses a rotary design  4 Stroke Cycle  Developed in the 1950’s and only recently was perfected by Mazda  Simpler, Lighter, and have less moving parts than piston powered engines of the same power output
  • 6.  Uses updraft from the props to store energy  Able to use solar power to help fly  Some have a battery for takeoff. After takeoff, it runs completely on solar power.  Generally glider shaped, for maximum lift with minimum power
  • 7.  Very inefficient design for an aircraft engine  Drives a compressor which fires into the jet engine  Very fuel inefficient and produces less or equal power as a conventional jet engine
  • 8.  Low fuel economy, however, cheap and easy to build.  Not very fast  Pulse jet diagram: First part of the cycle: air flows through the intake (1), and mixed with fuel (2). Second part: the valve (3) is closed and the ignited fuel-air mix (4) propels the craft.  Used in a few German planes
  • 9.  BMW 803 – one of the most powerful attempts at a hyper engine.  28-Cylinders, 3950 Horsepower  Crankshaft was too weak, so they used direct connected props.  HP/LB ratio is about 0.6
  • 10.  Uses direct cycle jet engines powered by a nuclear reactor  Soviets were putting in great effort into developing the engine  Very unsafe, however very powerful if successful