by MeekRN » Wed Jan 14, 2009 11:29 pm
i have a similar problem. i have to move my throttle up about 25% before it starts to effect engine rpm, i have throttle sensativity as max and null zone as 0 in the settings on FSX.
[piston_engine]
//CAFE REPORT - RUN UP AGAINST BRAKES STATIC RPM 2662
power_scalar=1.00 //Piston power scalar
cylinder_displacement=95.8 //Cubic inches per cylinder 550 CUBIC INCH TOTAL ADJUSTED 4 HP
compression_ratio=8.5 //Compression ratio from LEGACY TEST REPORT 8.5
number_of_cylinders=6 //Number of cylinders
max_rated_rpm=2700 //Max rated RPM THIS IS MAX RPM - A CONSTANT SPEED PROP WILL LIMIT TO THIS VALUE
max_rated_hp=310 //Max rated HP CONTENTIAL IO-550-N 550 cubic inches NA FI
fuel_metering_type=0 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3 //Starter torque factor
turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=0 //Max design manifold pressure, (inHg)
min_design_mp=0 //Min design manifold pressure, (inHg)
critical_altitude=0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=1 //Automixture available? 0=FALSE, 1=TRUE A FI current designed engine will have automixture RECORD 507 should not have any impact on the power beings we are auto mixture.
auto_ignition=1 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar WAS1.0 Use .1 for dyno testing
propeller_type=0 //1
propeller_diameter=5.75 //5.75
propeller_blades=2
propeller_moi=4.900000
beta_max=40
beta_min=25
min_gov_rpm=1200.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=38.920000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=0 //Minimum RPM for prop feathering
beta_feather=0 //Feathering pitch angle (degrees)
power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees)