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CarterCopter CC-RTW
For X-Plane 6.12
© Mark Fisher, 2002
Note: A Pilots Operating Handbook (POH) is a primer
on the operation of a specific aircraft. This POH is intended as a primer
on the operation of the X-Plane model of the CarterCopter Round-the-Wold
attempt aircraft (CC-RTW). It is designed to run under the flight simulator
X-Plane, available from www.x-plane.com.
The X-Plane model is freeware; it may be freely modified, copied, and redistributed,
provided a) it is not part of any for-profit package other than X-Plane
itself, and b) credit for this design is given to Mark Fisher and Austin
Meyer.
This model:
For a number of reasons, this model is not an exact replica of the real
CCTD. "Flying" techniques discussed here should not be taken as a full
and direct description of skills needed in the real CCTD.
Overview:
The CarterCopter is a hybrid aircraft. It operates in three modes:
-
Between 0 and 60 knots, it functions as a helicopter, taking power
from inertia of the rotor. Since power is not fed into the rotor from the
aircraft, it does not have the anti-torque problems of conventional helicopters.
It only operates in this mode for a short time, however! What is really
dangerous is low airspeed and low rotor rpm (as in any gyro).
-
Between 70 and 140 knots, it functions as an autogiro. The wings
only supply a small fraction of lift.
-
Between 140 and 220 knots, it functions as a fixed wing aircraft. The
rotor is still there, but is only taking enough energy out of the airstream
to avoid folding up around 100 rpm.
At all times, "steer small." Work to find the smallest input that
will have the desired effect. Over control only masks the response of the
aircraft.
As a general rule DON'T let forward speed drop below about 70knots (certainly
keep above 50-60) unless you are coming in for a zero roll landing or at
high altitude and experimenting.
Unique Controls:
There is an unfamiliar control on the throttle quadrant the "Rotor Trim"
lever. This does not directly control the rotor. Instead it controls
the link between the elevator trim and the rotor pitch cyclic. In the "up"
position, the rotor mirrors the pitch trim, allowing pitch control before
the elevator is effective. In the "down" position, the rotor pitch cyclic
is not affected by elevator trim.
There is also a "collective" control. This controls the pitch of the
rotor blades. This is used as a lift control in helicopter mode, and as
a rotor rpm control in autogiro and fixed wing modes. This control is
vital. If necessary, transfer your throttle to joystick-button control,
and set your throttle slider to operate as a collective.
Jump Take-Offs (zero roll take-off)
Principles:
The CC-RTW will be attempting to go around the world as a rotorcraft. Thus,
it must take off without moving forward. At takeoff, the CCTD has
two sources of energy: the thrust of the engine-prop unit, and lift from
the inertia-rotor unit.
The CC-RTW will be acting as a helicopter for the first 10 vertical
feet of flight, and then use JATO boost to transition to autogiro mode
at 40 Ft. AGL, where it will accelerate in ground effect to high-Mu flight
at 130 knots.
The period of time between takeoff and the establishment of flight speed
is quite short. The entire period should be treated as a takeoff if there
is any delay in establishing flight, the aircraft should be landed again
immediately.
-
The first step is to store sufficient takeoff energy in the rotor system.
This is done via the "Pre-Rotate" buttons.
Procedure:
-
Set up instruments:
-
Set altimeter.
-
Set radios.
-
Set autopilot to planned cruise altitude.
-
Set VVI to desired vertical speed (100).
-
Rotor trim at top.
-
Engage third button (ROT) on Electronic Flight Instrumentation System (EFIS).
-
Collective at 0°.
-
Pitch trim 50% back
-
Throttle at idle.
-
Fuel load 7000 lbs.
-
Set up weather and location: Las Vegas North Las Vegas, ~ 32°
F.
-
Start engine throttle at idle collective at zero pitch.
-
Engage pre-rotator apply full throttle. In reality, the spin up takes
three minutes.
-
At 250 rotor rpm, gently pull stick back to a spindle angle of 5.0.
-
Commence steady but swift (not fast) pull on collective up to 100%. When
the wheels leave ther ground, release pre-rotator.
-
As the drive prop spins up, fire JATO.
-
Keep nose level as the aircraft accelerates along runway to 70 kts.
Immediately begin to reduce collective.
-
Retract gear once flying speed is achieved (reduces drag and allows faster
airspeed build up).
-
Fly in ground effect 100 feet AGL, till high Mu flight is established.
Climb Out to Low Speed Cruise
Principles:
The CCTD will be operating as a conventional autogiro. The rotor
will be tipped back around 5°, and will be supporting over half the
weight. Rotor rpm will be around 160 rpm. (More rpm = greater drag and
less forward speed and greater engine power is needed the goal here is
to minimize fuel consumption and avoid using excessive engine power.) Too
little collective and the rotor rpm will go over 300 and this needs more
power from the engine to keep up airspeed.
Don't drop below about 70 knots (certainly keep above 50-60 as it can
be difficult to regain speed ESPECIALLY if flying at a low altitude).
Procedure:
-
Retract wheels to reduce drag and gain forward speed.
-
Climb out to about 1500 feet.
-
Once at cruise altitude, ease back to about 2/3 1/2 throttle. Bring rotor
trim to "min." Trim elevator to 130 knots.
-
Adjust collective so that you have between 160 rotor rpm
High Speed Cruise
Principles:
The CCTD will be operating primarily as a fixed wing aircraft. As
the aircraft is trimmed forward to balance increasing wing lift, the rotor
will be almost completely aligned with the line of flight. Because it is
not absorbing energy, 1) it will slow down to under 100 RPM, and 2) the
reduced drag will allow the CCTD to continue to accelerate. This is that
"High m " flight!
Procedure:
-
In level flight, bring engine power to 80%.
-
As speed builds, use forward elevator trim. "Steer small" avoid jerky
control inputs.
-
Reduce collective to 0°. Click on "STAT" button on EFIS. Use rotor
trim to minimize "F-A Spindle."
-
In this model, try adding one notch flaps to make it past the drag hump.
-
As speed builds, retract flaps.
-
If rotor speed drops below 60, adjust with collective. "Less is more"
lower pitch allows the rotor to windmill.
-
In X-Plane, you may see the lift vectors of each lifting surface press
<Ctrl "/"> twice.
Descent from High Speed Cruise
The CCTD will be operating primarily as a fixed wing aircraft. As
power is reduced and aircraft is trimmed forward to maintain speed, the
rotor will be almost completely aligned with the line of flight. High m
flight will continue.
Transition to Autogiro Mode
As power is reduced and trim is brought back to maintain altitude, the
rotor disk will capture more airflow and gain energy, increasing its rpm.
To build rpm more rapidly, reduce the collective to 2° until rotor
speed is around 300 rpm, then increase collective to maintain that speed.
Run-On Landings
With rotor stabilized at 300 rpm, adjust engine power for desired rate
of descent. Advance rotor trim to full. Fly a normal approach, but use
collective to flare. Pulling back on the stick will tip rotor back, slowing
the aircraft, but reducing braking effectiveness.
Vertical Landings (zero roll landing)
Principles:
The CCTD is now going to enter helicopter mode, using the stored
energy of the rotor to control descent. Caution: at 250 rotor rpm,
there is only enough energy for one descent you cant hover!
Procedure:
-
Lower gear!
-
Come in at about 500-750 ft AGL over the end of the runway.
-
You need to be at 70-80 knots or less and with min collective. The trick
is to lower engine power (but keep hand on the throttle) and do what ever
it takes to spin the rotor up as fast as possible.
-
As you head down the runway at about 400ft AGL pull back on the stick and
go nose up watch your airspeed closely, use light power and light forward
stick if the sink rate becomes too fast or if airspeed slows too much.
-
Be ready to pull steady collective if you need to slow descent but remember
that this slows the rotor and you need as much rotor speed as you can get
and keep.
-
At about 100 ft allow CC to settle apply light collective to ensure a
slow last few feet down. You can hit the deck at up to 20 ft/sec. What
ever you do, avoid flying backward just prior to reaching the runway.