1. Air Craft Reciprocating Engines & Accessories detail BTEUP Diploma syllabus for Aircraft Maintenance Engineering, effective from 2017 is collected from BTEUP 2017 Syllabus official website and presented for diploma students. The course details such as exam duration, Teaching Hr/week, Practical Hr/week, Total Marks, internal marks, theory marks, duration and credits do visit complete sem subjects post given below. The syllabus PDFs can be downloaded from official website.
For all other aircraft maintenance eng 5th sem bteup diploma syllabus 2017 you can visit Aircraft Maintenance Eng 5th Sem BTEUP Diploma Syllabus 2017 Subjects. The detail syllabus for 1. air craft reciprocating engines & accessories is as follows.
Rationale:
Engine is the source of propullsive force for the of aircraft and its knowledge, principle of working is must for aircraft maintenance engineer.
DETAILED CONTENTS
1. ENGINE FUEL AND OIL SYSTEM :
Principles of operation and construction of type carburetor and Direct fuel injection Difference between down draft and updraft typical float system and . configuration.
Description and operation of throttle valves, main/idle jets, Power enrichment systems, float chamber, Discharge nozzles, accelerator pumps and mixture control system. Cause and effect performance. icing and construction of impact, throttle and fuel ice on engine Conditions for use of carburetor/induction its prevention. Principle, operation and of pressure injection carburetor and fuel injection carburetor. Function and operation of fuel/air metering forces, impact tubes, venturi.
Description of installation, removal, inspection and servicing of typical carburetor system and system components. Adjustments and functional checks required of the fuel metering control system. Determination of rectification requirements of system faults. Description of the installation, removal, inspection and servicing of typical fuel injection system and system components. Adjustments and functional checks required for the fuel constrol system. Trouble shooting and rectification requirements of fuel system faults.
Characteristics of lubricants used in piston engine of system. Contamination of oil and its identification.
Properties of lubricating oil-Purity, viscosity, viscosity index, grading, flash point, fire point, pour point, detergent and non detergent.
Description of operation principles and constructional features of wet and dry sump lubrication systems. Suitability of each for typical engine configuration. Description of the constructional features and operation of : pressure pumps, scavenger pumps, oil coolers, oil cooler regulators, oil tank/hoppers, relief valves, check valves, oil filters and oil dilution systems.
2. IGNITION AND STARTING SYSTEM :
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3. SUPERCHARGED SYSTEMS :
Description, construction and operation of typical intake and alternate air system and engine exhaust system. Purpose and principle of supercharging and the effects on volumetric efficiency, charge density and temperature, brake hourse power, manifold absolute pressure, detonation, revolution per minute and fuel consumption. Description of construction and operating principle of geared supercharger and turbo supercharger system. Construction and function of impeller, diffuser, engine gear drive, turbine and intercooler. Definition of rated altitude, criticl altitude, overboost, overshoot, boot strapping, upper deck pressure and manifold pressure. Difference between internal supercharge, external turbo supercharger, multistage and multispeed supercharger. Difference between ground boosted and altitude engines.
Operation and layout of a system consisting of absolute pressure controller, ratio controller, manifold pressure relief valve and waste gate assembly. Operation and layout of a system consisting of density controller, differential pressure controller and waste gate assembly. Operation and layout of a system consisting of variable absolute pressure controller and waste gate assembly. Operation and function of a system consisting of ground adjustable waste gate valve, mainfold pressure relief valve. Description of the operation and procedures. Resolving problem which involve with power, surging, low deck pressure, high deck pressure, low critical altitude and low oil pressure. Description of control system and adjustment procedures.
4. ENGINE INDICATING SYSTEMS OF PISTON ENGINES :
Principles of operation, installation procedures, and the conditions sensed by the following instruments : Mainfold pressure guage, oil pressure gauge, electrical and mechanical tachometers, fuel flow indicator, electrical resistance thermometers, thermocouple thermometer indicators, ratiometer electrical resistance thermometers, fule contents and pressure gauge. Identification of the causes of faults in typical aircraft system.
5. Induction, exhaust and cooling system of piston engines.
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6. Power plant installation, storage and removal:
Engine, monitoring and ground operation, safety precaution etc.Procedure for starting and ground runup, interpretation of engine power output and preservation and depreservation of engine.
List of Experiments:
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For detail syllabus of all other subjects of BE Aircraft Maintenance Eng, effective from 2017 do visit Aircraft Maintenance Eng 5th Sem BTEUP syllabus for 2017.
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