Engine Components & Performance Quiz
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Questions and Answers

What is a key characteristic of a good combustor?

  • High combustion emergency (correct)
  • Low pressure loss
  • Compact design
  • High temperature tolerance
  • Which of the following statements about impulse turbine blade function is true?

  • They change the direction of flow without affecting velocity. (correct)
  • They convert heat energy to pressure.
  • They increase the temperature of the gases.
  • They decrease both velocity and pressure.
  • How can pressure loss be reduced in a combustion chamber?

  • By using more louvers.
  • By reducing the combustion chamber length.
  • By shortening the diameter.
  • By increasing the diameter or length of the diameter. (correct)
  • What primarily controls the active clearance in turbine cases?

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

    What is the highest temperature location in a gas turbine engine (GTE)?

    <p>Turbine nozzle</p> Signup and view all the answers

    What is the ideal air/fuel mixture ratio?

    <p>15:1</p> Signup and view all the answers

    Which device is used to check the high tension ignition system?

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

    What component is used to protect the stator in a gas turbine engine?

    <p>Labyrinth Seal</p> Signup and view all the answers

    What does the Blade Cuff do in a gas turbine engine?

    <p>Increases the flow of cooling air into the nozzle</p> Signup and view all the answers

    What are two parameters used for calculating thrust horsepower of a turboprop engine?

    <p>Thrust and Airplane Speed</p> Signup and view all the answers

    What occurs in a convergent duct regarding pressure, velocity, and temperature?

    <p>Pressure decreases while velocity increases and temperature decreases</p> Signup and view all the answers

    What is a characteristic of a Bell Mouth Inlet?

    <p>It has high aerodynamic efficiency with zero duct loss.</p> Signup and view all the answers

    Which type of compressor has a compressor ratio that is not a factor in its performance?

    <p>Centrifugal compressor</p> Signup and view all the answers

    What disadvantage is associated with a divided type intake in an aircraft?

    <p>It produces uneven distribution of airflow into the compressor.</p> Signup and view all the answers

    What does duct pressure efficiency ratio measure?

    <p>The ability to convert kinetic pressure energy into static energy.</p> Signup and view all the answers

    What role does the Variable Inlet Guide Vane (VIGV) play in an engine?

    <p>It allows changes in compressor geometry for better airflow management.</p> Signup and view all the answers

    In a centrifugal compressor, what does the centrifugal force provide?

    <p>High acceleration due to high velocity and kinetic energy.</p> Signup and view all the answers

    How does the placement and shape of the inlet duct affect aircraft performance?

    <p>It significantly influences airflow efficiency and engine performance.</p> Signup and view all the answers

    What is the typical spark rate for an ignition system?

    <p>60 to 100 sparks per minute</p> Signup and view all the answers

    What is the maximum duration for which long-term preservation of an engine is effective?

    <p>6 months</p> Signup and view all the answers

    How often should a humidity indicator be inspected if it has not turned pink?

    <p>Every 24 hours</p> Signup and view all the answers

    Which mechanism controls the propeller beta range?

    <p>Power lever position</p> Signup and view all the answers

    What happens to noise levels as the distance from the source is doubled?

    <p>Noise level decreases by 6dB</p> Signup and view all the answers

    What is used for sealing where minimal leakage is required?

    <p>Contact Seal</p> Signup and view all the answers

    What type of material is primarily used for noise suppressors in engines?

    <p>Welded stainless steel sheets</p> Signup and view all the answers

    What must be done after 3 years for an uninstalled engine stored in an envelope?

    <p>It should be represerved</p> Signup and view all the answers

    What is a primary function of the FADEC system at altitudes below 14,100 ft?

    <p>Calculate takeoff power rating</p> Signup and view all the answers

    What is the purpose of the Low Pressure Filter in the fuel system?

    <p>To prevent low filter icing</p> Signup and view all the answers

    What is one disadvantage of the water injection system used for thrust augmentation?

    <p>High weight ratio system</p> Signup and view all the answers

    What is the effect of adding methanol to the water injection system?

    <p>Decreases the freezing point of water</p> Signup and view all the answers

    Which component prevents the engine from overheating during takeoff?

    <p>Electronic control amplifier</p> Signup and view all the answers

    How is EGT measured in turbine engines?

    <p>By averaging readings from all thermocouples</p> Signup and view all the answers

    What material is used for the engine firewall bulkhead?

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

    What is a function of the APU load compressor?

    <p>Produce bleed air</p> Signup and view all the answers

    What type of thermocouple is primarily used in the gas turbine exhaust section?

    <p>Type K thermocouple</p> Signup and view all the answers

    Which safety feature is associated with the turbine starter system?

    <p>Automatic cut-off mechanism</p> Signup and view all the answers

    What purpose does the fine mesh filter serve in the fuel system?

    <p>Act as last chance filter before oil reaches bearings</p> Signup and view all the answers

    What happens to the fuel control under high-pressure conditions?

    <p>It operates through mechanical hydraulics</p> Signup and view all the answers

    Which component of the APU indicates engine speed?

    <p>N g tachometer</p> Signup and view all the answers

    What is the primary function of the inlet duct during flight operation?

    <p>To convert kinetic energy into RAM pressure</p> Signup and view all the answers

    Which statement correctly describes the efficiency of an adiabatic compressor?

    <p>It operates with 100% efficiency without heat loss</p> Signup and view all the answers

    What is a primary advantage of an axial compressor over a centrifugal compressor?

    <p>Greater pressure ratio</p> Signup and view all the answers

    What does compressor surge indicate?

    <p>Disturbance in the instantaneous flow of air</p> Signup and view all the answers

    Which of these is a characteristic of a can-type combustion chamber?

    <p>It is more maintenance-friendly</p> Signup and view all the answers

    What role do swirl vanes play in a combustion chamber?

    <p>To mix fuel and air</p> Signup and view all the answers

    In axial flow compressors, which component helps to direct the airflow efficiently?

    <p>Intake guide vanes (IGV)</p> Signup and view all the answers

    What is the purpose of the vortex reducer installed at the bottom side of the engine?

    <p>To prevent dirt particle injection into the engine</p> Signup and view all the answers

    What is indicative of a stall occurring in a compressor system?

    <p>Loud bangs and changes in compression ratio</p> Signup and view all the answers

    What material is commonly used for the impeller of a compressor?

    <p>Forged aluminum</p> Signup and view all the answers

    Study Notes

    Engine Components & Performance

    • Fuel burns to produce pressure energy. Engine performance is affected by RPM, aircraft speed, and ambient density.
    • Convergent ducts decrease pressure and increase velocity. Convergent nozzles produce momentum and thrust. Inlet duct efficiency is crucial at all altitudes. Bell-mouth inlets have high aerodynamic efficiency and eliminate duct loss.
    • Inlet systems (Rose Ram Pressure, Nose Type) produce profile and induced drag. Inlet duct efficiency converts dynamic pressure energy to static energy.
    • Divided entrance intake (single engine) aircraft unevenly distribute airflow. The design of inlets is determined by engine and aircraft placement. Induction ducts may produce normal shocks (Bow Shock)
    • Centrifugal compressors operate perpendicular to the longitudinal axis, are less prone to foreign object damage (FOD), and efficiently direct air to the combustion chamber.

    Compressor & Turbine

    • Centrifugal compressor tip speed problems reduce efficiency. Centrifugal force provides high acceleration.
    • Axial compressors have a greater pressure ratio compared to centrifugal compressors. Clearance between the rotor and case is maintained in axial compressors with abradable material for reduced friction.
    • Total pressure at a compressor's outlet is P3, T3.
    • Adiabatic compressors maintain 100% efficiency with no loss.
    • Forward-fan engine design reduces forward fan injection of foreign object debris (FOD).
    • High heat resistant ball bearings are used in turbine power plants.

    Combustion Chamber

    • Combustion chambers vary, with annular or can types being the most common. Annular combustion chambers have better structural stability and are less susceptible to warping.
    • Can-type combustion chambers are more maintenance friendly.
    • Combustion chamber design is complex, requiring precise perforation liners and aperture sizes..
    • Intake & Exhaust considerations are critical for air flow and pressure, impacting performance and efficiency

    Turbine

    • Gases must be cooled in the turbine to half their initial temperature.
    • Modern turbine blades are impulse reaction-type.
    • Turbine blades rely on heat energy to convert it into velocity. Hot spots in the tail cone can cause turbine malfunctions.
    • Turbine blades and discs are often made of cobalt-based alloys and nickel-based alloys.

    Exhaust System

    • Exhaust system materials include stainless steel and titanium.
    • Exhaust flow control is vital for reducing swirling motion of exhaust gases, increasing resultant pressure.
    • Exhaust components include the tail cone, nozzle, and exhaust duct. Temperatures of exhaust are monitored to prevent overheating.
    • Exhaust temperature is monitored to prevent overheating of turbine blades, turbine cases, and combustion chambers.

    Other Components & Systems

    • Oil flow systems, lubrication, and cooling have various implementations. The total loss system differs from the complete flow system in terms of oil scavenging.
    • Oil is critical in ensuring smooth operation and reducing friction in moving parts. Oil coolers are used to maintain optimal oil temperature.
    • Electrical, pneumatic, hydromechanical, and hydraulic components operate and control the fuel systems and other systems.
    • FADEC (Full Authority Digital Engine Control) manages operation and provides control.

    General Notes

    • Units of measurement and factors affecting performance are noted in various sections.
    • Critical components, such as bearings, are highlighted for their importance in maintenance and operation.
    • Engine types (turboshaft, turboprop) and their unique features and advantages and disadvantages are discussed.

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    Description

    Test your knowledge on engine components and their impact on performance. This quiz covers essential concepts including fuel combustion, duct efficiency, and compressor operations. Ideal for aviation students and enthusiasts looking to solidify their understanding of engine mechanics.

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