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Easa part 66 module 15 Gas Turbine Engine CH 10/25.

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Introduction to Fuel system PDF.

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The functions of the equipment are to supply the engine with fuel during a kind appropriate for combustion and to regulate the flow to the desired amount necessary for simple beginning, acceleration and stable running, the least bit engine operational conditions. To do this, one or a lot of fuel pumps are accustomed deliver the fuel to the fuel spray nozzles, that inject it into the combustion system (Part 4) within the sort of Associate in Nursing atomized spray. as a result of the rate of flow should vary per the quantity of air passing through the engine to keep up a continuing elect engine speed or pressure quantitative relation, the dominant devices are absolutely automatic with the exception of engine power choice, that is achieved by a manual throttle or power lever. A fuel shut-off valve (cock) management lever is additionally accustomed stop the engine, though in some instances these 2 manual controls are combined for single-lever operation easa training courses.

 

The Jet Engine by Rolls Royce

Chapter 1/25 : Basic mechanics (page 1 to 10)
Chapter 2/25 : Working cycle and airflow (page 11 to 18)
Chapter 3/25 : Compressors (page 19 to 34)
Chapter 4/25 : Combustion chambers (page 35 to 44)
Chapter 5/25 : Turbines (page 45 to 58)
Chapter 6/25: Exhaust system (page 59 to 64)
Chapter 7/25 : Accessory drives (page 65 to 73)
Chapter 8/25 : Basic mechanics (page 73 to 85)
Chapter 9/25 : Lubrication (page 85 to 94)
Chapter 10/25 : Internal air system (page 95 to 120)
Chapter 11/25 : Fuel system (page 121 to 132)
Chapter 12/25 : Starting and ignition (page 133 to 146)
Chapter 13/25 : Ice protection (page 147 to 152)
Chapter 14/25 : Fire protection (page 153 to 158)
Chapter 15/25 : Thrust reversal (page 159 to 168)
Chapter 16/25 : Afterburning (page 169 to 180)
Chapter 17/25 : Water injection (page 181 to 186)
Chapter 18/25 : Vertical/short take-off and landing (page 187 to 198)
Chapter 19/25 : Noise suppression (page 199 to 206)
Chapter 20 & 21 /25 : Thrust distribution & Performance (page 207 to 214)
Chapter 22/25 : Manufacture (page 215 to 228)
Chapter 23/25 : Power Plant Installation (page 229 to 242)
Chapter 24/25 : Maintenance (page 243 to 262)
Chapter 25/25 : Overhaul (page 251 to 264)

 

Fuel system ( Chapter 7/25) PDF.

Sample Quiz        –   Gas Turbine Engine Quiz ( 60 questions 75 min),
Category AGas Turbine Engine Quiz ( 60 questions 75 min),
Category B1Gas Turbine Engine Quiz ( 92 questions 115 min),

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EASA Training Courses

2. it’s conjointly necessary to possess automatic safety controls that stop the engine gas temperature, mechanical device delivery pressure, and also the rotating assembly speed, from surpassing their most limitations easa training courses.
3. With the turbo-propeller engine, changes in mechanical device speed and pitch must be taken into consideration thanks to their result on the facility output of the engine. Thus, it’s usual to interconnect the throttle lever and mechanical device controller unit, for by therefore doing the right relationship between fuel flow and flow of air is maintained the least bit engine speeds and the pilot is given single-lever management of the engine. though the most speed of the engine is often determined by the mechanical device speed controller, overspending easa training courses is ultimately prevented by a governor within the equipment.
4. The equipment usually provides for appurtenant functions, like oil cooling (Part 8) and also the hydraulic management of varied engine control systems; for instance, mechanical device flow of air management (Part 3) easa training courses.