Fuel System (PDF)
Document Details
Tags
Summary
This document provides a comprehensive overview of different fuel systems used in aircraft. It describes the components of the system like tanks, pumps, filters, and control units, emphasizing their function and differing types like the gravity feed, pump feed, and fuel injection system. This information is ideal for professionals working in the aviation or engineering field.
Full Transcript
Fuel system - stores and delivers fuel from the tanks to the engine, ensuring that the engine operates efficiently and reliably. Fuel Tanks - are storage containers for the fuel used by the aircraft. Fuel pumps - move the fuel from the tanks to the engine. Fuel Filters - remove...
Fuel system - stores and delivers fuel from the tanks to the engine, ensuring that the engine operates efficiently and reliably. Fuel Tanks - are storage containers for the fuel used by the aircraft. Fuel pumps - move the fuel from the tanks to the engine. Fuel Filters - remove contaminants from the fuel to prevent clogging and damage to the engine components. Fuel Lines - are the pipelines that carry fuel from the tanks through the system to the engine. Fuel Control Unit (FCU) - regulates the amount of fuel delivered to the engine, ensuring the correct air-fuel mixture for efficient combustion. Fuel Injectors/Carburetors - responsible for delivering fuel into the engine's combustion chamber. Vents and Drains: - equalize pressure as the fuel is consumed, and drains to remove water or other contaminants that might accumulate at the bottom of the tank Most common location of fuel tanks: 1. Wings 2. Fuselage 3. Center tank 4. Auxiliary tank Fuel system process 1. Fuel Tank - where the fuel is stored 2. Fuel Pumps - move the fuel from the tank to the engine 3. Fuel Lines - pipes that carry the fuel from the tank to the engines 4. Fuel Filters - remove contaminants that could damage the engine 5. FCU - regulates the amount of fuel delivered to the engines 6. Engines - fuel reaches the engine where it is mxied with air abd combusted o produce thrust Gravity Feed Fuel System - the fuel tanks are usually located higher than the engine, as seen in high-wing aircraft. - Fuel flows naturally from the tank to the engine by gravity. - The Fuel Selector Valve allows the pilot to choose the fuel source. - Carburetor is required - Does not require FCU fuel selector valve - allows the pilot to choose which fuel tank supplies fuel to the engine(s). Engine Primer - used to introduce a small amount of fuel directly into the engine's intake manifold or cylinders before starting the engine. Oil Dilution Solenoid - used in aircraft engines to thin the engine oil, making it easier to start the engine in extremely cold conditions. Pump Feed Fuel System - These systems have tanks equipped with electric boost pumps that push fuel toward the engine. - requires a carburetor to properly mix the fuel with air before combustion - engine-driven pump - electric pump - FCU Fuel Injection System - high pressure pumps to push fuel - FCU - the fuel is injected directly into the cylinders or intake manifold Multi-Engine Fuel System - used in two or more engines - uses multiple tanks with its own fuel pumps and cross feed valves - managed by fuel selector valve and cross feed options - some multi engine use carburated engines while others use fuel injection systems Jet Engine Fuel System - have complex tanks w/ multiple high pressure pumps and scavenge pumps - floaters and probes measures fuel - fuel is pressurized by pumpls and controlled by FCU - do not use carb Rich Mixture - higher portion of fuel relative to air - more fuel, less air - used for more power and cooling Lean Mixture - lower portion of fuel relative to air - less fuel, more air - used for fuel efficiency and economy