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The Two ways
for Reverse Operation:
First one
(preferrable) for new aircrafts:
Once the engine power lever is moved backwards and lifted over an idle
stop gate (protection against unintended reverse) into the beta range,
a micro switch will activate the solenoid valve, which opens the high
pressure servo line to the propeller. A cam will advance the power control
for increasing power to increase negative thrust.
Second one
(acceptable) for existing aircraft:
Instead of installing a complicated power lever and a cam, it is acceptable
to use a guarded switch for activating the solenoid valve, which opens
the high pressure line. As soon as the blades enter beta range, the engine
throttle can be used for increasing reverse thrust.
Once the system is
activated, a yellow warning light goes on and informs the pilot, that
the propeller blades have entered beta range. As an additional
protection against unintended reverse in flight, either the micro
switch of a retractable landing gear (if applicable) or an air pressure
switch installed at the aircraft speed indicator must close the power
line to the solenoid valve.
Return from reverse is performed by de-activating the
solenoid valve for leaving the high pressure mode. At this moment, the
high pressure servo line will be closed and normal operation with the
regular governed servo pressure is continued. Both the installed return
spring inside the hub and the counterweights move the blades automatically
back into a positive thrust angle.
Natural
composite blades with fiber reinforced epoxy cover and metal leading
edge protection are used to minimize weight at the highest amount of safety
against fatigue fractures due to vibrations.
Available certified
Propeller Models (pdf):
MTV-5-(
)-R (M), MTV-6-(
)-R (M), MTV-9-(
)-R (M), MTV-12-(
)-R (M),
MTV-14-(
)-R (M), MTV-16-(
)-R (M), MTV-21-(
)-R(M), MTV-22-(
)-R (M),
MTV-25-(
)-R (M), MTV-27-(
)-R (M)
Propeller
Designation System (pdf)
(Please report any bugs or suggestions to: support@mt-propeller.com
) 
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