Propeller Mechanics and Dynamics Quiz
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Questions and Answers

What effect does fluttering have on a propeller blade?

  • It causes constant vibration leading to blade weakening and potential failure. (correct)
  • It improves the fuel efficiency of the engine.
  • It reduces the noise produced by the propeller.
  • It enhances the aerodynamic efficiency of the blade.
  • Which characteristic of a propeller blade helps prevent fluttering?

  • Increased weight of the blade.
  • Curved shape to minimize drag.
  • Flexible design to absorb vibrations.
  • Rigidity to maintain structural integrity. (correct)
  • When analyzing a propeller's action, what are the two types of motion to consider?

  • Vertical and horizontal.
  • Static and dynamic.
  • Rotational and forward. (correct)
  • Backward and lateral.
  • What does the angle at which the air strikes the propeller blade refer to?

    <p>Angle of attack (AOA). (D)</p> Signup and view all the answers

    What is the outcome of the air deflection caused by the angle of attack on a propeller blade?

    <p>Dynamic pressure greater than atmospheric pressure creating thrust. (D)</p> Signup and view all the answers

    What is a distinguishing feature of a bronze bushing in a propeller hub?

    <p>It may require a puller for removal from the shaft. (D)</p> Signup and view all the answers

    Which type of propeller allows for adjustment of blade pitch while in the air?

    <p>Controllable-Pitch Propeller (C)</p> Signup and view all the answers

    What is the purpose of ice control systems in propellers?

    <p>To prevent or remove ice from propeller blades (D)</p> Signup and view all the answers

    Which type of propeller is specifically designed to operate at constant speeds?

    <p>Constant-Speed Propeller (A)</p> Signup and view all the answers

    What does the term 'unfeathering' refer to in propeller systems?

    <p>Restoring propeller pitch to allow engine restart. (D)</p> Signup and view all the answers

    What role does the governor play in maintaining constant engine RPM in a constant-speed feathering propeller?

    <p>It allows for variation in propeller pitch using oil pressure adjustments. (A)</p> Signup and view all the answers

    How does the governor reduce propeller RPM when required?

    <p>By decreasing the volume of oil supplied to the propeller. (D)</p> Signup and view all the answers

    What initiates the feathering process in a feathering propeller?

    <p>Pulling the condition lever to its maximum travel. (B)</p> Signup and view all the answers

    What is the function of the feathering spring in the feathering propeller system?

    <p>It assists the counterweights to increase the pitch of the blades. (D)</p> Signup and view all the answers

    Which of the following statements is true regarding the feathering action of the propeller?

    <p>Feathering occurs when oil pressure in the governor is released. (D)</p> Signup and view all the answers

    What is the effect of torque bending on propeller blades?

    <p>It bends the blades backward. (C)</p> Signup and view all the answers

    Which type of bending causes the blades to move forward as the aircraft is pulled through the air?

    <p>Thrust bending (D)</p> Signup and view all the answers

    What is the primary result of aerodynamic twisting on a propeller blade?

    <p>It causes the blades to turn to a high blade angle. (A)</p> Signup and view all the answers

    Which force is greater than aerodynamic twisting and tends to force the blades toward a low blade angle?

    <p>Centrifugal twisting (D)</p> Signup and view all the answers

    What should propellers be capable of withstanding due to the stresses they encounter?

    <p>Severe stresses (D)</p> Signup and view all the answers

    What could be a serious consequence of nicks or scratches on a propeller blade?

    <p>Cracks and blade failure (D)</p> Signup and view all the answers

    As the rpm increases, what happens to the stresses on a propeller?

    <p>They increase in proportion to the rpm. (A)</p> Signup and view all the answers

    What type of propeller is affected by both aerodynamic twisting and centrifugal twisting in its operation?

    <p>Controllable pitch propeller (B)</p> Signup and view all the answers

    What is the primary function of propeller controls in aircraft?

    <p>To control the tension on the governor speeder spring (D)</p> Signup and view all the answers

    Which instrument receives input from the throttle to measure performance?

    <p>Manifold pressure gauge (D)</p> Signup and view all the answers

    What does a tachometer generator measure?

    <p>Rotational rate of a shaft (C)</p> Signup and view all the answers

    Which type of propeller can be adjusted after installation?

    <p>Controllable-Pitch Propeller (D)</p> Signup and view all the answers

    Which type of propeller is primarily used to improve fuel efficiency and performance under varying conditions?

    <p>Constant-Speed Propellers (D)</p> Signup and view all the answers

    What is the purpose of feathering a propeller?

    <p>To minimize drag during engine failure (C)</p> Signup and view all the answers

    How is the reference signal generated in a tachometer generator?

    <p>By rotating the generator's internal mechanism (A)</p> Signup and view all the answers

    Which of the following types of propellers cannot be adjusted after installation?

    <p>Fixed-Pitch Propeller (A)</p> Signup and view all the answers

    What happens when the engine speed exceeds the set rpm of the governor?

    <p>The flyweights move outward and raise the pilot valve. (A)</p> Signup and view all the answers

    In what condition is the propeller governor considered to be operating effectively?

    <p>When the engine is at the rpm set by the pilot. (B)</p> Signup and view all the answers

    What occurs in the on-speed condition of the governor?

    <p>The pilot valve neither directs oil to nor from the hydraulic cylinder. (B)</p> Signup and view all the answers

    What can cause the governor to lose the on-speed condition?

    <p>Climbing or diving of the aircraft. (D)</p> Signup and view all the answers

    What role do the counterweights on the blades serve when the governor system is activated?

    <p>They increase pitch to slow the engine. (D)</p> Signup and view all the answers

    What achieves balance in the on-speed condition of the governor?

    <p>The centrifugal force on the flyweights and the tension of the speeder spring. (B)</p> Signup and view all the answers

    What mechanism allows oil to flow from the propeller piston when the engine exceeds the set rpm?

    <p>The raising of the pilot valve. (B)</p> Signup and view all the answers

    Which statement accurately describes the pilot valve in the on-speed condition?

    <p>It remains neutral with no oil movement. (C)</p> Signup and view all the answers

    Study Notes

    Week 1 Complete

    • AVIA-1052 course confirmed as week 1 complete
    • Contact Matt C for corrections/improvements

    Week 1 of 1 Day 1

    • AVIA-1052 course, week 1, day 1

    Previously On AVIA-1052

    • First class together
    • Now in first class

    Today On AVIA-1052

    • Discussion of propellers
    • General propeller stuff
    • Aircraft propeller theory
    • Basic propeller controls

    Where are we?

    • Powerplant (Vol. 2) 7-2 to 7-6
    • Start at general
    • Stop at propeller location
    • FAA-H-8083-30A, Aviation Maintenance Technician Handbook-General
    • FAA-H-8083-31A, Aviation Maintenance Technician Handbook-Airframe Volume 1
    • FAA-H-8083-31A, Aviation Maintenance Technician Handbook-Airframe Volume 2
    • FAA-H-8083-32A, Aviation Maintenance Technician Handbook-Powerplant Volume 1
    • FAA-H-8083-32A, Aviation Maintenance Technician Handbook-Powerplant Volume 2

    Propellers

    • Unit that absorbs engine power output
    • Propeller development stages
    • First propellers were fabric-covered sticks
    • Designed to force air rearward
    • Advanced from simple designs to complex systems
    • Variable-pitch, constant-speed feathering, and reversing systems
    • Increase flying efficiency
    • Different propeller types
    • Two, four, and six-bladed propellers
    • Propeller-driven aircraft speed limitations related to propeller rpm

    Constant-speed systems

    • Flyweight-equipped governor unit
    • Controls pitch angle of blades to maintain constant engine speed

    Forces acting on a rotating propeller

    • Centrifugal force
    • Blade weight is important for propeller design
    • Excessive blade tip speed results in poor efficiency,fluttering, and vibration

    Propeller speed limitations

    • Aircraft speed limitations relate to the propeller rpm
    • Turbofan engines used for higher speed aircraft

    Propeller advantages

    • Shorter takeoff and landing times
    • Less expensive to maintain
    • Increased efficiency from new blade materials and manufacturing techniques
    • Widely used in turboprops and reciprocating engine installations
    • Many smaller aircraft will continue to use propellers

    Propeller systems (different types)

    • Many have been designed for specific aircraft, speed, and type of operation

    Propeller diagrams

    • Basic nomenclature of the parts of a simple fixed-pitch, two-bladed wood propeller
    • Aerodynamic cross-section of a blade

    Aerodynamic cross-section of a blade

    • Angle of attack
    • Chord line
    • Blade face
    • Blade back (relative wind)

    Aircraft Propeller Theory

    • The aircraft propeller is composed of two or more blades.
    • Each blade is a rotating wing.
    • The blades create thrust (force) to move the aircraft through the air.
    • The power needed to rotate propeller blades is furnished by the engine
    • A central hub is used to attach the blades.

    Basic Propeller Principles

    • Mounted on a shaft
    • Low-horsepower engines, which is an extension of the crankshaft
    • High-horsepower engines, which is mounted on a propeller shaft
    • The engine rotates the airfoils
    • The propeller transforms the rotary power of the engine to thrust

    Propeller Aerodynamic Process

    • Airplane moving through the air
    • Creates drag force opposing its forward motion
    • There must be equal force in the opposite direction to prevent the aircraft from stopping.
    • This force is called thrust
    • Work done by thrust is equal to thrust times distance
    • Power expended by thrust is equal to thrust times velocity

    Propeller Efficiency

    • Ratio of thrust horsepower to brake horsepower
    • Ratio of the useful power output to the power input
    • Generally, 50-87% depending on the amount of slip

    Propeller Pitch

    • Angle between chord/chord line of a blade section and the plane in which the propeller rotates
    • Usually measured in degrees

    Geometric pitch

    • Distance a propeller advances in one revolution with no slippage
    • Usually expressed in pitch inches
    • Calculated using a formula

    Effective pitch

    • Distance a propeller advances in one revolution with slippage
    • Difference between geometric pitch and effective pitch

    Chord line of a propeller blade

    • Determined similarly to an airfoil
    • A propeller blade can be considered as an infinite number of thin blade elements
    • Each element has an airfoil section whose chord is the propeller blade width
    • Drawn along the face of the propeller blade to identify specific areas

    Typical propeller blade

    • Describes characteristics such as a twisted airfoil, differing segments, and location from the hub as station numbers

    Forces acting on rotating propellers

    • Centrifugal force pulling the propeller blades away from the hub
    • Torque bending force causes propeller blade bending in the direction opposite of rotation.
    • Thrust bending force caused by the thrust acting on the aircraft.

    Excessive blade speed

    • Poor blade efficiency
    • Vibration
    • Flutter

    Propeller speed limitation

    • Maximum speed of propeller-driven aircraft limited to about 400mph (644km/h)
    • turbofan engines used for higher speed Aircraft

    Propeller advantages

    • Takes off and landing can be shorter, and less expensive to maintain
    • New blade materials/ manufacturing techniques have increased efficiency.
    • Propellers widely used in applications such as turboprops and reciprocating engine installations
    • Many smaller aircraft will use propellers into the future

    Propeller systems

    • Many different types of propeller systems have been developed for specific aircraft, speed, and operation type

    Propeller diagrams

    • Basic nomenclature of the parts of a simple fixed-pitch, two-bladed wood propeller
    • Aerodynamic cross-section of a blade (next slide)
    • Includes terminology to describe areas shown (e.g., trailing edge, leading edge, chord line, hub)

    Aerodynamic cross-section of a blade

    • Includes terms like angle of attack, chord line, blade back, and blade face

    Basic propeller controls and instruments (various videos and explanations available)

    • Video resources available, see resources pages for links.

    Propeller controls and instruments (various explanations available)

    • Video resources available, see resources pages for links.

    Propeller controls

    • fixed and constant

    Specific propeller control components

    • Control Lever, etc

    Propeller Governor

    • Engine and propeller rpm-sensing device
    • High pressure oil pump
    • Directs oil under pressure or releases oil from the hydraulic cylinder.
    • In constant-speed propeller system
    • Changes in oil volume in the hydraulic cylinder changes blade angle.
    • Maintains specific rpm via the cockpit propeller control.

    Propeller Governor Mechanism

    • Constant speed controls consist of a gear pump, a pilot valve and flyweights.
    • Governor flyweights to control flow of oil through governor to and from the propeller.
    • The position of the pilot valve regulates the quantity of oil.
    • Relief valve regulates the governor oil pressure.

    Propeller Governor Mechanism - ON-SPEED

    • When operating at the set rpm. governor flyweights are balanced by the speeder spring.
    • Pilot valve does not direct oil.

    Propeller Governor Mechanism - OVERSPEED

    • When engine speed is above the set rpm. the centrifugal force causes flyweights to move out.
    • Pilot valve releases oil, increasing blade pitch, and slowing the engine.

    Propeller Governor Mechanism - UNDERSPEED

    • When engine speed is below the set rpm. The centrifugal force decreases, and the flyweights move inward, towards the speeder spring.
    • The pilot valve is forced down, increasing oil flow, decreasing propeller pitch, increasing engine speed.

    Feathering Propellers

    • Used on multi-engine aircraft to reduce drag during one or more engine failure conditions
    • Blade angle changed to approximately 90° to the line of flight.
    • This greatly reduces drag.
    • Propeller stops turning when blades are parallel to the airstream.

    Feathering Propeller Mechanism

    • Uses oil pressure to move blades to low pitch position during shutdown and to high pitch during operation.
    • Latches lock the blade to the low pitch position during startup and shutdown.
    • Most small feathering props use oil pressure.

    Reverse-Pitch Propellers

    • Used to change blade angle of propellers in flight.
    • Allows the blade angle to be changed to a negative value.
    • Useful to slow the aircraft down during landing.

    Reverse-Pitch Propeller Operation

    • When the aircraft lands, the propellers blades can be moved to negative pitch.
    • Increased airframe drag slows the aircraft down.
    • Allows fast maneuvering with little to no engine power change

    Propeller Auxiliary Systems: Ice Control Systems

    • Ice formation during flight causes loss in propeller efficiency.
    • Ice formation also causes vibration and increases the weight on the blades.
    • Fluid Anti-Ice Systems is used for ice prevention.

    Propeller Auxiliary Systems: Fluid Anti-Ice System

    • Fluid Anti-ice system consists of a tank with a pump to force fluid to each propeller and a control system.
    • The system permits variation of the pumping rate to properly de-ice the propeller based on the ice conditions.

    Propeller Auxiliary Systems: Fluid Types

    • Isopropyl alcohol, phosphate composites
    • High Availability and low cost
    • Not widely used.

    Propeller Auxiliary Systems: Feed Shoes

    • Rubber strips that extend from the blade shank to the propeller radius.
    • Installed on the blades' leading edges
    • The airflow disperses the fluid to areas where ice does not develop

    Propeller Auxiliary Systems: Slinger Rings

    • Fluid transfer is transferred through nozzles from a stationary nozzle, to a U-shaped channel on the rear of the propeller assembly.

    Propeller Auxiliary Systems: Electric Deicing Systems

    • An electric propeller-icing control system consists of an electrical energy source, a resistance heating element mounted on the propeller spinner and blades.
    • The system can be controlled internally or externally and the necessary wiring.
    • The system has a master switch, toggle, selector switch, light, and timer to control the blade sequence when deicing.
    • A cycling unit energizes the heating elements in sequence and a brush block transfers electricity to the slip ring.
    • Control circuitry should reflect operation of timers and contain protective devices such as current limiters or circuit breakers.

    Propeller Synchronization and Synchrophasing

    • Synchronization systems are used on most multi-engine aircraft to provide a method to control and synchronize rpm
    • Reduces vibrations and eliminates the unpleasant beat from unsynchronized propeller operation.

    Autofeathering System

    • Automatic propeller system
    • Used for takeoff, approach, and landing
    • Automatically feathers the propeller if there is a loss of engine power.

    Propeller Governor

    • Engine rpm-sensing device
    • High-pressure oil pump
    • Responds to engine speed changes by either directing or releasing oil to the propeller hydraulic cylinder to change blade angle to maintain specific rpm.

    Wood Propeller Inspection

    • Wood propellers should be inspected frequently to ensure airworthiness
    • Inspect for defects such as cracks, dents, warpage, and glue failure
    • Inspect the blade tips, leading edge, trailing edge, and grooves to identify any defects or damage.

    Metal Propeller Inspection

    • Metal propellers and blades are generally prone to fatigue failure resulting from the concentration of stresses.
    • Inspect the full length of the leading and trailing edges, grooves, shoulders, dents, and scars with a magnifying glass to decide if the defects are scratches or cracks.
    • Tachometer inspection accuracy must be verified. This is critical because inaccurate reading may cause damage to the propeller and engine.

    Aluminum Propeller Inspection

    • Carefully inspect aluminum propellers and blades for cracks and other flaws.
    • Multiple deep nicks or gouges on the blade's leading edge may be cause for rejection.
    • Use dye penetrant or fluorescent dye penetrant to confirm suspected cracks.
    • Refer any unusual conditions or appearance to the manufacturer.

    Composite Propeller Inspection

    • Visual inspection for nicks, gouges, loose material, erosion, cracks, delaminations, and lightning strike.
    • Check for delamination and debonds by tapping the blade or cuff with a metal coin.

    Propeller Vibration

    • Vibration can be caused by propeller imbalance, blade angle variations, or problems with the track.
    • A propeller that vibrates at specific rpm ranges may indicate a problem with the engine-propeller match
    • Possible issues to check for include the centrifugal force, improper settings or parts, and engine vibration.

    Blade Tracking

    • The process of determining the blade tips' position relative to each other.
    • Blades should track each other closely, and any difference exceeding the manufacturer's tolerance may indicate a problem.

    Checking and Adjusting Propeller Blade Angles

    • Obtain the blade angle settings from the manufacturer's instructions and check the blade position at the specified station.
    • Metal scribes or other sharp instruments should not be used to mark blade stations.

    Universal and Digital Propeller Protractor

    • The universal propeller protractor can be used to check blade angles on a balancing stand or the aircraft engine.

    Propeller Balancing

    • Propeller unbalance is a source of aircraft vibration that may result from static or dynamic imbalances.
    • Static unbalance occurs when the center of gravity of the propeller does not coincide with the rotational axis.
    • Dynamic unbalance is when the components such as blades or weights do not rotate in the same plane.

    Static Balancing

    • The standard method for checking propeller assembly balance.
    • Involves several steps (e.g., checking blade angle, inserting bushings, and placing the propeller on specific locations on a specific balance check device) to determine if the propeller is properly balanced staticaly.

    Dynamic Balancing

    • Propellers are balanced by using special kits with vibration sensors and analyzers to calculate and adjust the weights.

    Propeller Removal and Installation

    • The spinner dome is removed
    • The safety wires are removed if necessary
    • The propeller mounting studs are unscrewed
    • The propeller is then supported by a sling, and carefully removed from the mounting flange and place on a cart for transportation
    • The appropriate procedures are followed for installation.

    Setting the Propeller Governor

    • The propeller governor regulates the maximum speed at which the engine runs.
    • The governor's adjustable stop will move the propeller to the low-pitch position once the takeoff rpm is reached which increases engine load and maintains the maximum engine speed

    Servicing Propellers 

    • Cleaning: washing with suitable cleaning solvents or use of a noncorrosive soap solution
    • Lubrication: propeller lubrication procedures are usually published in the manufacturer's instructions.
    • Replenishing: if a propeller has been subjected to salt water, it should be washed until all traces of salt have been removed, then dried out, and coated with fresh oil or similar.

    Cleaning Propeller Blades

    • Propeller blades should be cleaned with a suitable cleaning solvent, brush, or cloth
    • Any tool or substances that may scratch or mar the blade should be avoided.
    • For wood propellers use warm water and mild soap.

    Charging the Propeller Air Dome

    • Examine the propeller, ensure it's in the start locks, and use the proper control
    • Charge the cylinder with dry air, Nitrogen is preferred, using the proper temperature and pressure chart.

    Propeller Lubrication

    • Some propellers do not require lubrication. Proper lubrication procedures must be followed to avoid corrosion and ensure the smooth operation of moving parts.

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    Description

    Test your knowledge on the mechanics of propeller blades. This quiz covers various aspects including fluttering effects, angle of attack, and propeller types. Understand the characteristics and functionalities that enhance propeller performance.

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