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Questions and Answers

What is the main purpose of a propeller?

To convert the rotary power of the engine into thrust, which propels the aircraft through the air.

What are the two main types of propeller installations?

  • Tractor and Pusher (correct)
  • Fixed Pitch and Variable Pitch
  • Constant Speed and Variable Speed
  • Feathering and Non-Feathering
  • What is the primary function of a constant-speed propeller system?

    To maintain a constant engine speed regardless of changes in aircraft attitude or power settings.

    What is the purpose of blade feathering in a propeller?

    <p>To reduce propeller drag to a minimum during an engine failure, preventing the propeller from windmilling and causing excessive drag.</p> Signup and view all the answers

    A ground-adjustable propeller can be adjusted while in flight.

    <p>False</p> Signup and view all the answers

    What are the primary factors that influence the efficiency of a propeller?

    <p>Blade angle, propeller pitch, and propeller slip.</p> Signup and view all the answers

    What is the primary purpose of the slip ring system in a propeller deicing system?

    <p>The slip ring provides a pathway for electrical current to flow from the engine to the propeller deice boots.</p> Signup and view all the answers

    What is the purpose of a propeller synchronization system?

    <p>To control and synchronize the engine rpm of multi-engine aircraft to reduce vibration and ensure smooth, harmonious operation.</p> Signup and view all the answers

    An autofeathering system is typically used during an emergency landing.

    <p>True</p> Signup and view all the answers

    During the inspection of a wooden propeller, what are some of the key areas that require careful attention?

    <p>Inspect for cracks, dents, warpage, glue failure, delaminations, charring, and separation between the metal leading edge and the cap.</p> Signup and view all the answers

    What are some of the crucial aspects to consider when inspecting a metal propeller?

    <p>Look for sharp nicks, cuts, scratches, and any signs of corrosion or fatigue failure.</p> Signup and view all the answers

    How often should a propeller tachometer be inspected?

    <p>Every 100 hours or annually, whichever occurs first.</p> Signup and view all the answers

    What is the purpose of blade tracking in propeller maintenance?

    <p>Blade tracking ensures that all propeller blades rotate in the same plane, preventing vibration and stress on the aircraft structure.</p> Signup and view all the answers

    What are some of the crucial steps involved in propeller removal and installation?

    <p>Remove the spinner dome, safety wire, and mounting bolts. Support the propeller with a sling and mark it for proper orientation when reinstalling. Clean the engine flange and propeller flange before installing the propeller.</p> Signup and view all the answers

    What is the purpose of propeller balancing?

    <p>To ensure that the propeller assembly is balanced, preventing vibration caused by uneven weight distribution.</p> Signup and view all the answers

    What is the common method for addressing propeller hunting?

    <p>Consult a qualified propeller repair facility to inspect and adjust the governor, fuel control system, synchrophaser, or synchronizer.</p> Signup and view all the answers

    What is the purpose of a propeller governor?

    <p>To control the pitch of the propeller blades, ensuring a constant engine speed regardless of load or flight conditions.</p> Signup and view all the answers

    What is the purpose of an autofeathering system?

    <p>To automatically feather the propeller in case of an engine failure, reducing drag and minimizing damage to the engine.</p> Signup and view all the answers

    What is the purpose of a propeller deicing system?

    <p>To prevent ice accumulation on the propeller blades, which can disrupt airflow, reduce propeller efficiency, and lead to vibration and structural damage.</p> Signup and view all the answers

    Electric propeller deicing systems should only be operated when the propellers are rotating.

    <p>True</p> Signup and view all the answers

    Study Notes

    Week 1 Complete

    • Week 1 of AVIA-1052 is complete.
    • Contact Matt C with any errors or improvements needed.

    Previously On AVIA-1052

    • This is the first class.
    • Topics covered include propellers, propeller theory, and basic propeller controls.

    Today On AVIA-1052

    • Topics include propeller location, different types of propellers, including fixed-pitch, test club, ground-adjustable, controllable-pitch, constant-speed, feathering, reverse-pitch propellers, and propeller governor.
    • FAA handbooks are relevant for this topic.

    Where are we?

    • Powerplant (Vol. 2).
    • Start at section 7-2 to 7-6
    • Topics include propeller location.
    • Stop at section 7-6
    • Relevant FAA handbooks are mentioned.

    Propellers

    • The unit that must absorb the power output of the engine.

    • Propeller development has gone through many stages of development.

    • The first propellers were fabric-covered sticks designed to force air in a rearward direction.

    • Propellers have evolved from simple two-bladed wood propellers to complex turboprop aircraft systems.

    • More complex propeller systems have constant-speed and variable-pitch, feathering, and reversing systems. This allows the engine's rpm to be changed slightly for different flight conditions.

    • Constant-speed systems have a flyweight-equipped governor unit that controls the blade pitch angle to maintain constant engine speed.

    • Propeller efficiency ratios are often used in evaluation (thrust horsepower to brake horsepower).

    • The usual symbol for propeller efficiency use is the Greek letter "n" (eta).

    • Propeller efficiency varies widely depending on how much the propeller slips.

    • Pitch is not the same as blade angle; an increase or decrease in either is usually accompanied by an increase or decrease in the other.

    • Geometric pitch is the distance a propeller should advance in one revolution (with no slippage).

    • Effective pitch is the distance a propeller advances in one revolution (with slippage).

    • Geometric pitch - effective pitch = slip.

    • The chord line is an imaginary line drawn through the blade from the leading edge to the trailing edge.

    • The blade back is the cambered or curved side of the blade, similar to the upper surface of an aircraft wing

    • The blade face is the flat side of the propeller blade.

    • Most propellers are two-bladed.

    • Great increases in power output have resulted in the development of four- and six-bladed propellers.

    • Forces acting on propellers include centrifugal force, which tends to pull the blades out of the hub at high rpm.

    • Blade weight is important to propeller design.

    • Excessive blade tip speed can result in poor blade efficiency, fluttering, and vibration.

    • Aircraft speed is limited by propeller speed.

    • Propeller-driven aircraft have advantages, such as takeoff and landing being relatively short and less expensive to maintain.

    Aircraft Propeller Theory

    • The aircraft propeller consists of two or more blades; each blade is essentially a rotating wing.
    • Propeller blades produce forces to create thrust.
    • Engine power is needed to rotate the propeller blades.

    Basic Propeller Principles

    • Low- and high-horsepower engines are mounted on the shaft.

    Propeller Aerodynamic Process

    • Airplane movement generates a drag force.
    • Thrust is needed to counteract the drag force for an airplane to move forward.
    • The work performed by thrust is equivalent to multiplying the thrust by the distance the airplane moves.
    • The power expended by thrust is the product of thrust and the velocity of the aircraft.
    • Power = Thrust x Velocity
    • Thrust horsepower is the expression for power expended when used in horsepower units.
    • The engine produces brake horsepower for the propeller through a rotating shaft.
    • The propeller converts brake horsepower into thrust horsepower.
    • Some propeller power is lost in the conversion process.
    • The propeller needs to be designed to reduce wasted power for maximum efficiency.
    • Propeller efficiency is the ratio of thrust horsepower to brake horsepower.
    • Propeller efficiency uses the Greek letter "n" (eta) as its symbol.
    • Propeller efficiency varies from 50-87%.
    • Pitch of the propeller is not the same as the blade angle, the blade angle is a part of determining the pitch.
    • Geometric pitch is the distance the propeller advances during one full rotation, with no slippage.
    • Slip is the difference between geometric and effective pitch.
    • The chord line is an imaginary line extending from the propeller blade's leading edge to the trailing edge.
    • The propeller blade's chord line is also how the blade element's chord thickness is determined.

    Propeller Governor

    • Constant-speed control consists of a gear pump, a pilot valve.
    • The pump increases the pressure of the engine oil.
    • Flyweights control the flow of oil.
    • The position of the pilot valve controls the quantity of oil flowing from and to the propeller.
    • A relief valve regulates the operating oil pressures in the governor.

    Types of Propellers

    • Types:
      • Fixed-pitch
      • Ground-adjustable
      • Controllable-pitch
      • Constant-speed
      • Feathering
      • Reverse-pitch

    Propeller Location

    • Propeller types are mounted on the upstream end of a drive shaft in front of the supporting structure. (tractor propeller)
    • Propeller types are mounted on the downstream end of a drive shaft behind the supporting structure. (pusher propeller).
    • Pusher propellers are more susceptible to damage than tractor propellers.

    Wood Propeller Inspection

    • Wood propellers should be inspected regularly.
    • Inspect for cracks, dents, warpage, and glue failure.
    • Inspect the trailing edge for delamination defects, and charring between the propeller and the flange.
    • Check for cracks near the metal sleeve and the tightness of the lag screws.

    Metal Propeller Inspection

    • Inspect metal propellers for nicks, cuts, scratches, and other defects.
    • Use a magnifying glass during the inspection.
    • Inspect for the full length of the leading edge, especially near the tip.
    • Inspect the full length of the trailing edge.
    • Inspect the grooves and shoulders on the shank or other areas as needed.

    Tachometer Inspection

    • Ensure the engine tachometer is accurate.
    • Accuracy should be measured every 100 hours or annually to avoid engine damage.

    Aluminum Propeller Inspection

    • Carefully inspect aluminum propellers for cracks or other flaws.
    • Multiple deep nicks or gouges are cause for rejection.

    Composite Propeller Inspection

    • Visually inspect for nicks, gouges, loose material, erosion, cracks, debonds, and lightning strikes.
    • Inspect for possible delamination and debonds.
    • Use a metal coin to tap the composite blade (and cuff) to listen for an audible change that might indicate delamination.

    Blade Tracking

    • Blade tracking is the process of determining the positions of the propeller blades relative to each other.

    Blade Angle Checking

    • Obtain the blade angle setting and the blade station from the manufacturer's instructions.
    • Do not use metal scribes to add markings to propeller blades, this can lead to blade failure.
    • Use a bench-top protractor if the propeller is removed from the aircraft.
    • Use a handheld protractor for on-aircraft propeller inspections.

    Propeller Balancing

    • Propeller unbalance can be either static or dynamic.
    • Static unbalance occurs when the center of gravity does not coincide with the rotation axis.
    • Dynamic unbalance occurs when the centers of gravity of the blades or counterweights do not lie in the same plane of rotation.
    • Dynamic unbalance can be mitigated through inspection and correction.

    Propeller Removal and Installation

    • Remove the spinner dome and safety wire (if necessary).
    • Support the assembly with a sling and make sure to check the engine and airframe manuals.
    • Install the propeller, making sure to align the dowel studs with the corresponding engine mounting flange holes.
    • Tighten the mounting nuts according to manufacturer's specifications.

    Setting the Propeller Governor

    • At the time of propeller, propeller governor, or engine installation, take the following steps:
      • During ground run-up, adjust the throttle to the takeoff position, and note the resultant rpm and manifold pressure.
      • If the obtained rpm is higher or lower than the prescribed takeoff rpm, reset the adjustable stop on the governor.

    Servicing Propellers

    • Propeller servicing involves cleaning, lubrication, and replenishing the operating parts.

    Cleaning Propeller Blades

    • Cleaning propeller blades should use a clean film of engine oil.
    • Clean metal parts with clean engine oil or a suitable equivalent.

    Charging the Propeller Air Dome

    • Inspect the propeller to make sure it is positioned on the start locks and the proper control is used.
    • Charge the piston with dry air or nitrogen.
    • Use a temperature-based chart to determine the correct air pressure to charge.

    Propeller Lubrication

    • Some propeller types do not need lubrication, but others do.
    • Follow the manufacturer's procedures, but use caution with any method to avoid damage.

    Propeller Overhaul

    • A work order must be prepared.
    • A process document should be created to record each step of the process
    • The records should include applicable ADs, current specifications, and manufacturer's sBs.
    • Double-check the serial number and other details for proper accuracy.

    Miscellaneous

    • Autofeathering System, Unfeathering, and Propeller Auxiliary Systems are mentioned.

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