"FLAT PITCH MANIFOLD AIR PRESSURE"
Piston engine
helicopters have a unique warning system and safety device built
into the helicopter that is often neglected and not understood by
many pilots.
This device is none
other than the humble Manifold Air Pressure
Gauge - similar to the picture above.
The Manifold Air
Pressure (MAP) gauge measures the amount of air passing into the
cylinders from the carburetor.
At any fixed Engine RPM with
both magnetos working and the engine in good nick -
the MAP is also an indicator of Brake HP produced by the
engine.
The air flow, into the
engine when it is running, is
controlled by the pilot, through movement of the throttle and/or
collective.
These, in turn, move rods or cables which are connected
to and operate a round disc in the carburetor called “the throttle butterfly valve”.
Most Australian
and NZ piston machines are sourced from the USA and the Aus MAP gauge is
calibrated in “inches of mercury”.
A low power setting would
be 10 inches while 28 inches is near to maximum available power in most
normally aspirated engines @ sea level.
Unless the air filter is
removed as well as any inlet air ducts, the 28 inches MAP at
sea level std day is caused by air friction in the inlet
system and the air filter slowing the air down as it passes
through it.
When the collective
is fully down, an accurate and calibrated MAP gauge is actually indicating how much
engine Horse Power is required to drive ALL the helicopter
mechanical systems under a particular rotor pitch configuration,
system friction load and
DA.
For example, @
S/level, a typical non – turbo charged piston engine will indicate
12 inches of MAP when the collective pitch control is fully down and
the rotor is operating at flight RPM (104% on the R22).
Because the
collective is full down, the MAP gauge is now indicating what is
called “Flat Pitch MAP”.
Can we use this
flat pitch information to help us with safety data about our
metal steed?
Flat pitch MAP
easily indicates if your engine has: