Propellers and Systems Flashcards

1
Q

Propeller Pitch

A
  • Distance in feet a propeller travels forward in one revolution
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2
Q

Theoretical (Geometric Pitch)

A

The distance the prop would travel if it were 100% effective

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3
Q

Practical (Effective) Pitch

A

The actual distance the prop travels

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4
Q

Propeller Slip

A

Difference between theoretical and practical pitch

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5
Q

Coarse Pitch (Low RPM)

A
  • Large angle (more torque), big bite of air
  • Travels forward a greater distance and moves at a slower speed
  • Used during cruise
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6
Q

Fine Pitch (High RPM)

A
  • Small angle (less torque), small bite of air
  • Travels forward a smaller distance and moves at a faster speed
  • Used during Takeoff and climb
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7
Q

Fixed Pitch Propellers

A
  • Common in Most training aircraft
  • Pitch optimized for both climb and cruise performance (blade angle constant)
  • Less efficiency, more fuel consumption
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8
Q

Variable Pitch - Adjustable Pitch

A
  • Blade Angle can be adjusted on the ground
  • Good for adapting the aircraft to a specific role
  • Prop can’t be adjusted in flight
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9
Q

Variable Pitch - Controllable Pitch

A
  • Blade Angle can be adjusted in flight
  • Pilot can optimize performance for given phases of flight
  • Disadvantage is that blades must constantly be readjusted
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10
Q

Variable Pitch - Constant Speed Prop

A
  • Blade Angles adjust automatically to maintain constant RPM
  • More complex system, heavier, requires more maintenance
  • Uses engine oil and nitrogen pressure to control blade angle
  • Prop control in cockpit adjusts set RPM
  • Prop goes to full fine if engine fails
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11
Q

Prop Governor

A
  • Contains rotating flyweights geared to engine
  • Flyweights sense engine speed
  • Oil enters or leaves prop hub base on flyweights which changes prop angle
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12
Q

Constant Speed Prop Power Increase

A
  1. Mixture
  2. Prop
  3. Throttle
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13
Q

Constant Speed Prop Power Decrease

A
  1. Throttle
  2. Prop
  3. Mixture
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14
Q

Constant Speed Prop Overspeed

A
  • Occurs when conditions try to increase prop RPM by decreasing load
  • Prop moves into finer pitch to counter
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15
Q

Constant Speed Prop Underspeed

A

-Occurs when conditions try to decrease prop RPM by increasing load
- Prop moves into coarser pitch to counter

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16
Q

Fuel Mixture

A
  • Octane (Fuel Inhibitor)
  • Heptane (Fuel Promoter)
17
Q

Octane

A

Prevents fuel detonation and smooth controlled burning

18
Q

Fuel Grades

A
  • Octane rating usually determined by compression ratio of engine
  • Number equivalent to percent octane (74 Octane)
  • If over 100, expressed as performance number, the higher the number, the better
  • Always use HIGHER grade, lower can cause detonation and engine damage
  • Higher only causes lead fouling of spark plugs
19
Q

80/87 Octane

A
  • Red
  • 6 lbs/gal
  • Gasoline Base
20
Q

100LL

A
  • Blue
  • 6 lbs/gal
  • Gasoline Base
21
Q

100/130 Octane

A
  • Green
  • 6 lbs/gal
  • Gasoline Base
22
Q

Jet A1

A
  • Clear or Straw
  • 7 lbs/gal
  • Kerosene Base
23
Q

Carburetor

A
  • Measures correct quantity of fuel
  • Vaporizes Fuel
  • Mixes fuel and air in proper proportion
  • Delivers mixture to cylinders
  • Amount of air regulated by throttle (butterfly valve)
24
Q

Too Rich Mixture

A
  • Unburned Fuel expelled through exhaust
  • Fouled plugs, Rough running, loss of power
25
Q

Too Lean Mixture

A
  • Hotter Engine, runs rough
  • Causes backfiring and detonation
26
Q

3 Ways to set mixture

A
  • RPM
  • Fuel Flow Gauge
  • Exhaust Gas Temperature (EGT)
27
Q

Fuel Vaporization Carburetor Ice

A
  • Heat absorbed from surround air to vaporize fuel
  • Reduces temp by 30ºC
  • Water vapour will freeze if air is moist
28
Q

Throttle Carburetor Ice

A
  • Low pressure in venturi and around butterfly valve reduces air temperature by 30ºC
  • Ice can form and block passages or restrict movement of throttle
  • Chokes airflow to engine
29
Q

Impact Carburetor Ice

A
  • Can occur if flying in visible moisture in temps below zero
  • builds up on intake, filter screen, and butterfly valve
  • chokes airflow to engine
30
Q

Carburetor Heat

A
  • Takes unfiltered hot air from muffler
  • Hot air is less dense so mixture should be leaned
31
Q

Fuel Injection System

A
  • No carb ice, better fuel flow, faster throttle response
  • precise control of mixture, better fuel distribution
  • Better in cold weather
  • Increased overall engine efficiency
  • alternate air source may be used if intake becomes blocked
  • much worse on hot days due to vapour lock
  • difficult to restart engine due to fuel starvation
32
Q

Turbocharger

A
  • Fools engine into thinking it is working at sea level
  • Uses energy of hot exhaust gases to power a compressor
  • Boosts intake air pressure
33
Q

Supercharger

A
  • Fools engine into thinking it is working at sea level
  • Uses rotational energy of crankshaft to power a compressor
  • Boosts fuel/air mixture pressure
34
Q

Short Stack Exhaust System

A
  • Used on non-turbocharged or low power engines
  • 1 Exhaust stack on either side of the engine
35
Q

Collector Exhaust System

A
  • Used on all turbocharged engines and larger engines
  • All Exhaust gases collected in one common exhaust collector tube
36
Q

Ignition System Components

A
  • 2 Magnetos
  • 2 Spark Plugs in each cylinder
  • Ignition leads
  • Magneto Switch
37
Q

The Magneto

A
  • Not attached to battery or electrical system
  • Generates low tension current and transforms it into high tension current
  • Distributes current to individual spark plugs at desired time to have them fire
  • Mags off = circuit grounded
  • Mag on = complete circuit
  • Ground wire broken means a live mag
38
Q

Shielding

A
  • Purpose is to prevent ignition current from interfering with other electrical systems
  • Accomplished by grounding all other systems to the airframe