Propeller & Variable Pitch Propeller Flashcards
Creating forward movement from a propeller is the method of turning ____ motion into ____
Method of turning reciprocal motion into thrust
What are the 2 types of propeller
- Fixed pitch
- Variable pitch
The amount of lift produced by a propeller blade is dependant on what 2 factors
- Speed
- AoA
Why is an propeller designed to have less AoA at the tip than at the hub
Tips travel faster
More lift would be produced
More AoA at hub than at tips
If a propeller blade had the same AoA across its entire length, which section of the propeller would produce more lift?
THE TIP
The tip has greater distance to travel
It travels faster so would produce more lift with the same AoA as the centre of the blade
At the hub of a propeller blade, AoA is HIGHER or LOWER than the AoA at the tip
Hub = HIGHER
Tip = LOWER
The AoA of a propeller blade is dependent on which 2 factors
- Propeller Pitch (Blade angle)
- Forward Velocity
You can determine how far a propeller moves forward in one revolution based on what?
GEOMETRIC PITCH
The efficiency of fixed pitch propeller varies with what
AIRSPEED
Fixed pitched propeller in a climb, assuming power (throttle) constant
Airspeed INCREASES or DECREASES
DECREASES
Fixed pitched propeller in a climb, assuming power (throttle) constant
Relative airflow angle INCREASES or DECREASES
INCREASES
Fixed pitched propeller in a climb, assuming power (throttle) constant
Propeller AoA INCREASES or DECREASES
This has what effect on efficiency
- AoA INCREASES
- Efficiency DECREASES
Fixed pitched propeller in a climb, assuming power (throttle) constant
Propeller is EASIER or HARDER to push through the air
This has what effect on engine workload
- HARDER
- Workload INCREASES
Fixed pitched propeller in a climb, assuming power (throttle) constant
Engine RPM INCREASES or DECREASES
DECREASES
AoA has increased, prop takes bigger bites of the air
This takes more effort. Engine works harder and turns more slowly
Fixed pitched propeller in a descent, assuming power (throttle) constant
Airspeed INCREASES or DECREASES
INCREASES
Fixed pitched propeller in a descent, assuming power (throttle) constant
Relative airflow angle INCREASES or DECREASES
DECREASES
Fixed pitched propeller in a descent, assuming power (throttle) constant
Propeller AoA INCREASES or DECREASES
This has what effect on efficiency
- AoA DECREASES
- Efficiency INCREASES
Fixed pitched propeller in a descent, assuming power (throttle) constant
Propeller is HARDER or EASIER to push through the air
This has what effect on engine workload
- EASIER
- Workload DECREASES
Fixed pitched propeller in a descent, assuming power (throttle) constant
Engine RPM INCREASES or REDUCES
INCREASES
On an RPM gauge what is meant by the following
- Green Arc
- Red Line
- Normal Operating Range
- Never Exceed
What are 2 examples of propeller aerofoil damage
What effect does this have on efficiency
- Stone Chips
- Tip Damage
- Propeller less efficient
A propeller under high stress loads could suffer from what
STRUCTURAL FATIGUE
If a small part of a propeller tip were to detach, what could this result in
SEVERE VIBRATION
What is a key reasons for an engineering filing out nicks on a propeller blade
Prevent fatigue cracks forming and spreading
A variable pitch propeller
With a higher AoA;
1. ____ Lift
2. ____ to push through the air
- GREATER LIFT
- MORE DIFFICULT
A variable pitch propeller creates
With a lower AoA;
1. ____ Lift
2. ____ to push through the air
- LESS LIFT
- LESS DIFFICULT
A variable pitch propeller
Why do you change the blade angle at different airspeeds
Maintain best AoA
A variable pitch propeller
With a low forward speed (start of take off run), what happens to the flyweight, and what pitch angle is selected as a result
- MOVE IN
- FINE PITCH
Low blade angle
A variable pitch propeller
With a high forward speed (high speed descent), what happens to the flyweight, and what pitch angle is selected as a result
- MOVE OUT
- COARSE PITCH
High blade angle
A variable pitch propeller
Beyond what 2 limits will a variable pitch propeller become inefficient
- FINE PITCH STOP
- COARSE PITCH STOP
The mechanism that does automatic blade angle adjustment is known as what
CONSTANT SPEED UNIT
(CSU)
Variable pitched propeller in a climb, with power (throttle) constant
Propeller adjusts blade angle to INCREASE or REDUCE AoA
REDUCE AoA
Variable pitched propeller in a climb, with power (throttle) constant
When the propeller adjusts the blade angle, this makes the propeller EASIER or HARDER to push through the air
What effect does this have on engine workload
- EASIER
- REDUCED workload
Variable pitched propeller in a climb, with power (throttle) constant
If the propeller blade angle is adjusted and engine workload reduces, what effect does this have on RPM
RPM RECOVERS
Engine RPM reduces on climb
Blade angle reduces the blade AoA
Propeller is easier to push through air, reducing engine workload
This allows RPM to recover
In a CSU unit, what mechanism does oil pressure act against
SPRING
In a CSU Unit
- What does the spring try to do to the propeller pitch
- What is the oil pressure doing in response to this
- Force fully coarse pitch
- Acts against spring (fine pitch)
Variable pitch propeller
If a pilot sets low RPM, what pitch angle is set
LOW RPM = HIGH PITCH
High pitch = Coarse Pitch
Variable pitch propeller
If a pilot sets high RPM, what pitch angle is set
HIGH RPM = LOW PITCH
Low pitch = Fine pitch
With an increased RPM in a CSU, what will happen to the flyweight
MOVE OUTWARDS
In a CSU, if the flyweight move out, what effect does this have on;
- Oil pressure
- Spring position
- DECREASED PRESSURE
- COARSE AoA
In a CSU, if the flyweight moves in, what effect does this have on;
- Oil pressure
- Spring position
- INCREASED PRESSURE
- FINE AoA
Variable pitch propeller
An aircraft accelerating (descending) results in MORE or LESS inflow, which INCREASES or DECREASES the effective AoA. The flyweight will move IN or OUT
- MORE inflow
- DECREASED AoA
- OUT
Variable pitch propeller
An aircraft decelerating (climbing) results in MORE or LESS inflow, which INCREASES or DECREASES the effective AoA. The flyweight will move IN or OUT
- LESS inflow
- INCREASED AoA
- IN
Variable pitch propeller
As AoA decreases, the propeller is doing MORE or LESS work. RPM INCREASES or DECREASES
- LESS work
- INCRESED rpm
Variable pitch propeller
As AoA increases, the propeller is doing MORE or LESS work. RPM INCREASES or DECREASES
- MORE work
- DECREASED rpm
Variable pitch propeller
A pilot adjusts RPM control to LOW RPM. What effect does this have on the prop pitch
MORE COARSE
Variable pitch propeller
A pilot adjusts RPM control to HIGH RPM. What effect does this have on the prop pitch
MORE FINE
What colour is the RPM lever
BLUE
What colour is the Throttle lever
BLACK
Constant Speed Unit (CSU)
The blue lever controls ____ and instrumentation shows ____ via the ____ gauge
- RPM
- RPM
- RPM gauge
Constant Speed Unit (CSU)
The black lever controls ____ and instrumentation shows ____ via the ____ gauge
- POWER
- POWER PRODUCED
- MANIFOLD PRESSURE GAUGE
What does a Manifold Pressure (MAP) gauge messure
Pressure in the throat of the carburettor
Mounted after the butterfly valve
When the butterfly vavle is shut, the MAP gauge will indicate a HIGH or LOW pressure reading
LOW READING
When the butterfly valve is fully open, the MAP gauge will indicate a HIGH or LOW pressure reading
HIGH READING
Under what circumstance may a MAP gauge indicate a much higher than atmospheric pressure
Super or Turbo Charged engines
What happens to the engine if the wrong order of altering the MAP and RPM is applied?
LABOURED ENGINE
CSU and Engine management
What are the 3 steps to INCREASE power
- Increase REVS
- Increase PRESSURE
- Check MIXTURE
REMEMBER: Increase R P M, throttle FORWARD RPM
–> RPM –>
CSU and Engine management
What are the 3 steps to DECREASE power
- Check MIXTURE
- Reduce PRESSURE
- Reduce REVS
REMEMBER: Decrease RPM, throttle BACK RPM
<– RPM <–
Where can a pilot find the allowable combinations of MAP and RPM for a given flight configuration
PIlot Operating Handbook
(POH)
CSU and Engine Management
During descent, what will happen to atmospheric pressure
What will happen to MAP if unchecked
- INCREASE
- INCREASE
CSU and Engine Management
During ascent, what will happen to atmospheric pressure
What will happen to MAP if unchecked
- DECREASE
- DECREASE
What are 3 possible failure scenarios of a variable pitch propeller
- Oil Pressure
- CSU
- Pilot Action