Aircraft Fuel Systems Overview
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Questions and Answers

What type of fuel is specifically designed for use in turbine engines?

  • Propane
  • Diesel fuel
  • Aviation gasoline
  • Jet fuel (correct)
  • Which of the following subsystems is NOT part of jet transport fuel systems?

  • Vent
  • Distribution
  • Storage
  • Flotation (correct)
  • What is the primary purpose of surge tanks in jet transport fuel systems?

  • To store fuel during flight
  • To prevent fuel evaporation
  • To cool the fuel
  • To allow one-way drainage of fuel (correct)
  • Why is low volatility fuel desirable in turbine engines under normal conditions?

    <p>It prevents vapor lock and evaporation</p> Signup and view all the answers

    What is one of the key conflicting factors in choosing turbine engine fuel?

    <p>Operational temperature range</p> Signup and view all the answers

    Which component in a jet transport fuel system connects all tanks to the vent space?

    <p>Vent tubing</p> Signup and view all the answers

    What characteristic should turbine engine fuel possess to facilitate starting in cold environments?

    <p>High volatility</p> Signup and view all the answers

    What is the primary function of baffle check valves in aircraft fuel tanks?

    <p>To prevent fuel from moving outboard while allowing it to flow inboard</p> Signup and view all the answers

    What safety procedure must be followed before entering an integral fuel tank for maintenance?

    <p>All fuel must be emptied from the tank and fuel vapors purged</p> Signup and view all the answers

    What are manually-operated gate valves primarily used for in fuel systems?

    <p>To provide a means for shutting off fuel flow without electrical power</p> Signup and view all the answers

    Which component is essential for operating motor-operated valves in fuel systems?

    <p>Electric motors</p> Signup and view all the answers

    Where are baffle check valves situated in relation to fuel boost pumps?

    <p>In the bottom of the tanks to maintain fuel supply</p> Signup and view all the answers

    What must be ensured regarding the fuel venting system on an aircraft?

    <p>It must vent under all conditions of aircraft attitude and fuel quantity.</p> Signup and view all the answers

    Which component is NOT part of a transport category aircraft fuel distribution subsystem?

    <p>Crossfeeding components</p> Signup and view all the answers

    What is the role of boost pumps in the fuel system of an aircraft?

    <p>To supply engines and assist in fuel transfer or jettison.</p> Signup and view all the answers

    Where is the central pressure refueling station commonly located on a transport category aircraft?

    <p>Conveniently positioned for ramp refueling trucks.</p> Signup and view all the answers

    What happens when a boost pump fails in the aircraft's fuel system?

    <p>Fuel flow can still occur through bypasses.</p> Signup and view all the answers

    Which statement correctly describes the function of the transfer/crossfeed manifold?

    <p>It allows any tank to supply fuel to any engine and manages jettisoning.</p> Signup and view all the answers

    What is the purpose of check valves in the fuel vent system?

    <p>To prevent backflow and maintain venting regardless of aircraft attitude.</p> Signup and view all the answers

    Which of the following components is specifically involved in jettisoning fuel?

    <p>Transfer system</p> Signup and view all the answers

    What is the main benefit of single-point pressure fueling?

    <p>It reduces the number of connections needed for fueling.</p> Signup and view all the answers

    What is the primary function of a drain valve in the sump system?

    <p>To remove impurities and contaminants from the fuel</p> Signup and view all the answers

    Which type of fuel tank is described as having the highest volume with the lowest weight?

    <p>Integral fuel tank</p> Signup and view all the answers

    What role does baffling play in aircraft fuel tanks during maneuvers?

    <p>It prevents fuel from sloshing</p> Signup and view all the answers

    How are bladder fuel tanks attached to the aircraft structure?

    <p>Attached using clips or other fastening devices</p> Signup and view all the answers

    What are the possible benefits of being able to remove and repair a rigid fuel tank?

    <p>Easier leak detection and repairs</p> Signup and view all the answers

    What materials can a rigid removable fuel tank be made from?

    <p>Various metals and composites</p> Signup and view all the answers

    What characteristic of integral fuel tanks aids in reducing weight for aircraft?

    <p>Their construction as a unit within the airframe</p> Signup and view all the answers

    Which statement about bladder fuel tanks is accurate?

    <p>They often include similar components to rigid tanks</p> Signup and view all the answers

    In what way do wing ribs and box beams contribute to the fuel system in aircraft?

    <p>They serve as baffles to prevent fuel flow issues</p> Signup and view all the answers

    What is a disadvantage of using a bladder fuel tank compared to a rigid tank?

    <p>Greater susceptibility to punctures</p> Signup and view all the answers

    What is the primary function of the fuel cooled oil cooler (FCOC) in the fuel system?

    <p>To heat the fuel and cool the engine oil</p> Signup and view all the answers

    Where is the temperature sensor typically located in the fuel system of a jet transport aircraft?

    <p>In the fuel tank</p> Signup and view all the answers

    What happens when a fuel filter becomes clogged in a jet transport aircraft?

    <p>The bypass allows fuel flow to continue</p> Signup and view all the answers

    Which type of fuel quantity indication system is commonly used in transport category aircraft?

    <p>Capacitance type system</p> Signup and view all the answers

    What is the purpose of low fuel pressure warning lights in jet transport aircraft?

    <p>To alert of possible boost pump failure</p> Signup and view all the answers

    What are the three basic types of aircraft fuel tanks?

    <p>Removable tanks, bladder tanks, and integral tanks</p> Signup and view all the answers

    What design feature does a fuel tank have to manage contaminants and water?

    <p>A sump where contaminants can settle</p> Signup and view all the answers

    What is the role of true fuel flow indicators in a jet transport aircraft?

    <p>To serve as the primary means of monitoring fuel delivery to the engines</p> Signup and view all the answers

    What signals a malfunction in the fuel system related to fuel filters?

    <p>Fuel filter bypass warning lights</p> Signup and view all the answers

    What is the primary means for monitoring fuel delivery to the engines in jet transport aircraft?

    <p>Fuel flow indicators</p> Signup and view all the answers

    Which system is commonly used for indicating fuel quantity in transport category aircraft?

    <p>Capacitance type indication system</p> Signup and view all the answers

    What component in the fuel system is designed to allow fuel flow around filters if they become clogged?

    <p>Fuel filter bypass</p> Signup and view all the answers

    Where are low fuel pressure warning sensors typically located in a jet transport aircraft?

    <p>In the boost pump outlet line</p> Signup and view all the answers

    What is the function of the sump area in an aircraft fuel tank?

    <p>To collect contaminants and water</p> Signup and view all the answers

    Which statement accurately describes the construction of rigid removable fuel tanks?

    <p>They can be riveted or welded together and often include baffles.</p> Signup and view all the answers

    What is a key feature of integral fuel tanks utilized in transport category and high performance aircraft?

    <p>They integrate structural members of the aircraft to form a tank.</p> Signup and view all the answers

    In which manner are bladder fuel tanks secured to the aircraft structure?

    <p>They must be fastened using clips or other fastening devices.</p> Signup and view all the answers

    What primary advantage do baffling features provide to integrated fuel tanks during flight maneuvers?

    <p>They keep the fuel from sloshing and ensure stable fuel flow.</p> Signup and view all the answers

    What material characteristic distinguishes bladder fuel tanks from rigid removable tanks?

    <p>Bladder tanks utilize reinforced flexible material.</p> Signup and view all the answers

    What is the primary benefit of the transfer/crossfeed system in a jet transport aircraft's fuel system?

    <p>It enables any fuel tank to supply fuel to any engine.</p> Signup and view all the answers

    Which component in a transport category aircraft fuel system prevents fuel spillage during refueling?

    <p>Check valves in the vent system</p> Signup and view all the answers

    What function do the float and check valves serve in the aircraft's fuel vent system?

    <p>They prevent overflow and maintain venting during various attitudes.</p> Signup and view all the answers

    Why is a central pressure refueling station advantageous for a transport category aircraft?

    <p>It simplifies the refueling process by allowing all tanks to be filled with one connection.</p> Signup and view all the answers

    How do boost pumps contribute to the fuel management of an aircraft?

    <p>They provide pressure for fuel delivery during engine supply and jettison operations.</p> Signup and view all the answers

    Study Notes

    Aircraft Fuel Systems

    • Aircraft fuel systems are designed for uninterrupted contaminant-free fuel flow, regardless of aircraft attitude.
    • Fuel systems must accommodate varying fuel loads without negatively affecting aircraft control during maneuvers.
    • Fuel flow must be consistent and at the correct pressure and rate to ensure proper engine and auxiliary power unit (APU) function.
    • Fuel pumps must prevent drawing fuel from multiple tanks concurrently.
    • Systems must prevent air introduction into the fuel system.
    • Turbine engine-powered aircraft need fuel venting systems to prevent loss of fuel supply caused by component failure.

    Fuel Storage System

    • Fuel systems in turbine engines must withstand operational loads without failure.
    • Fuel systems must be isolated from personnel compartments and protected from hazards due to unintended temperature fluctuations.
    • Systems must provide fuel for half an hour of maximum operation and be capable of safe jettisoning for landing purposes.
    • Jettisoning systems are also referred to as fuel dump systems for transport category aircraft.

    Aircraft Fuel

    • Turbine engines use jet fuel (Jet A, Jet B), not aviation gasoline, and should not be mixed.
    • Inhibitors are added to jet fuel to control corrosion, oxidation, ice, and microbial/bacterial growth.
    • Fuel choice depends on conflicting factors. High volatility fuel is easier to start turbine engines with, but vapor lock and evaporation are undesirable.

    Jet Transport Aircraft Fuel Systems

    Storage

    • Integral fuel tanks—common design, the wing is sealed. Sections or fuselage tanks may also be sealed.
    • Main and auxiliary fuel tanks—common on jet transports, with surge tanks for overflow and fuel system venting.

    Vent

    • Fuel systems are vented via tubing and channels to the surge/vent overboard.
    • Venting is crucial for all attitudes and fuel volumes.

    Distribution

    • Pressure fueling components, transfer system, defueling components, and fuel dump systems are all part of the subsystem.
    • Fueling can be done in a single point for multiple tanks.

    Feed

    • Boost pumps move fuel to a transfer manifold.
    • Transfer/cross-feed manifolds and boost pumps are used for jettisoning fuel.
    • Fuel systems can provide secondary fuel feed for the engines if the primary fails.

    Indicating

    • Systems monitor parameters - fuel flow, pressure, and temperature.
    • Display is by instrumental panel or multifunction display (MFD).
    • Fuel flow indicators used for monitoring delivery to engines.
    • Temperature sensors are located in the tanks to alert of potentially harmful warnings.
    • Filtered fuel bypass warning light for clogged filters.
    • Low fuel pressure lights are used for boost pump failure.
    • Fuel quantity gauges for total remaining.

    Fuel System Components

    Fuel Tanks

    • Three basic types: rigid removable, bladder, and integral.
    • Integral—part of the airframe; fitted with baffling or dividers to help keep fuel from shifting excessively during maneuvers.
    • Sumps—low areas for contaminants and water.
    • Drain valves—used to remove impurities during preflight.

    Rigid Removable Fuel Tanks

    • Made of various materials and strapped to the aircraft structure.

    Bladder Fuel Tanks

    • Made of reinforced flexible material.
    • Similar function to rigid tanks, but attached with clips or other fasteners.

    Integral Fuel Tanks

    • Forged as part of the aircraft structure in the wings and fuselage.
    • High performance aircraft require baffling to prevent slosh.
    • Baffle check valves control flow.

    Fuel Valves

    • Used for fuel flow control—shut off and routing.
    • Manually—operated gate valves; commonly used for fire control functions.
    • Motor operated— use electrical motors for operating fuel valves, controlling flow, and shutoff.

    Fuel Pumps

    • Boost pumps provide fuel under pressure to the engine-driven pump during start-up or if the engine-driven pump fails.
    • Centrifugal boost pumps— used to supply and transfer fuel between tanks if the aircraft is configured for such design.

    Fuel Filters

    • Used to filter debris and water from fuel to protect the engine(s).

    Fuel System Indicators

    Fuel Quantity Probes

    • Variable capacitance transmitters are installed, with each measuring the fuel level in its assigned tank.

    Fuel Quantity Using Drip Sticks

    • Fuel quantity can be determined using calibrated drip sticks.
    • Drip sticks are checked around all tanks.

    Fuel Flowmeters

    • Aircraft using turbine-engine fuel systems use mass flow fuel flow meters to measure fuel flow.

    Fuel Temperature Gauges

    • The temperature of the fuel is monitored for ice formation or buildup in the system, by the gauges.

    Fueling

    • Two types of fueling processes: Over-the-wing and pressure refueling.
    • Over-the-wing is done by opening the tank's fill cap and placing a nozzle into it.
    • Pressure fueling—a nozzle locks onto the fueling port and the fuel is pumped into the corresponding tank.

    Fueling Safety Measures

    • Fueling must be done outside in a well ventilated area, away from flammable materials.
    • Personnel must be properly dressed and equipped to prevent static discharge.
    • Fire extinguishers, bonding cables, and ground safety equipment should be present.
    • Open flames or electrical devices must be prohibited.

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    Description

    This quiz explores the critical aspects of aircraft fuel systems, focusing on their design for uninterrupted fuel flow and performance under various conditions. Topics include fuel storage, fuel flow consistency, and safety measures against contaminants and air introduction. Test your knowledge on how these systems support turbine engines and aircraft maneuverability.

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