Easa part 66 module 15 Gas Turbine Engine CH 12/25.
Introduction to Controls and instrumentation PDF.
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The controls of the turbine engine are designed to get rid of, as way as doable, work load from the pilot whereas still permitting him final management of the engine. to realize this, the fuel flow is mechanically controlled once the pilot has created the initial power choice (Part 10).
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)
Controls and instrumentation ( Chapter 12/25 ) PDF.
EASA Part 66 Module 15 PDF Forum
Module 15: Gas Turbine Engine
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2. All engine parameters need observance and instrumentation is provided to tell the pilot of the right functioning of the varied engine systems and to warn of any imminent failure. ought to any of the automated governors fail, the engine are often manually controlled by the pilot choosing the specified thrust setting and observance the instruments to keep up the engine at intervals the relevant operational limitations part 145.
3. The multitude of dials and gauges on the pilot’s control part 145 panel is also replaced by one or variety of ray tubes to show engine parameters. These are tiny screens capable of displaying all of the data necessary to control the engine safely part 145.
4. The management of a turbine engine usually needs the utilization of only 1 control lever and also the observance of sure indicators situated on the pilot’s control panel (fig. 12-1) part 145. Operation of the management (throttle/power) lever selects a thrust level that is then maintained mechanically by the equipment (Part 10) part 145.