Nobody downloaded yet

Engine system for the Airbus A3200 - Assignment Example

Comments (0) Cite this document
Summary
Response to Task: Engine System for the Airbus A3200 Name Institution FADEC SYSTEM FITTED TO THE V2500 ENGINE AIRBUS A3200 The modern aircraft has two types of electronic engine management system. These are the Full Authority Digital Electronic control system (FADEC) and the hydro mechanically controls system…
Download full paperFile format: .doc, available for editing
GRAB THE BEST PAPER98% of users find it useful
Engine system for the Airbus A3200
Read TextPreview

Extract of sample "Engine system for the Airbus A3200"

Download file to see previous pages The FADEC controls the fuel injection and timing; hence, optimize engine power. This adds the considerable amount of wiring to the system due to the needed separate power supply for backup from the alternator. The extra weight of parts of FADEC system has to be checked and recalculated for adjustment. FADEC has cockpit controls and other extra switches added to this system to control the fuel pump. These systems are protected by the FADEC power supply (Gunston, 1990)). The ECU has a 3D memory map, which controls fuel injection under varied circumstances for instance, air pressure density and the air temperature, with respect to throttle settings and the RPM. The Electronic Control Unit can sense barometric pressure and respond by injecting fuel. The spark plug ignition timing is controlled depending on load for each throttle settings. The ignition timing variations yields faster engine starting and smoother operations with the variable loads. The FADEC engine does not need chocking during starting since the ECU controls fuel for every cylinder and assists in retarding the ignition. FADEC system does not use the carburettor and the ignition and does not also depend on aircraft electrical system (Guttman, 2009). On the other hand, in the hydromechanical control system, the driver is in control of the aircraft power plant using an internal combustion engine. The sensors and control are the alternator and the battery masters. The battery master activates the battery contractor that connects the battery to the electrical bus aircraft. Alternator master applies power to the field circuit of the alternator to activate the circuit. The two switches provide power to the aircraft systems. The throttle sets up the required power level and controls the massive air-flow rate in the carburetted engines that are delivered to the cylinder. Pitch control adjust the speed unit, which then adjusts the propeller pitch and controls the load required by the engine in maintaining the RPM. The mixture control will in turn set the needed fuel to add to the airflow intake. At high altitudes, the oxygen levels reduce and, therefore, volume of the fuel must readjust to the required air-fuel mixture. The ignition switch opens the ‘P’’lead circuit by activating the magnetos. The magnetron maintains the process of sending the output voltage to spark plugs and connects the engine through the gearing. Movement in the crankshaft causes the magnetrons to generate voltage for sparking (Hispano-Suiza, 2001). TASK 1: FADEC SYSTEM OF THE V2500-A5 ON THE AIRBUS A320 SYSTEM LAYEROUT DIAGRAM FIG1: The AIRBUS A320 FADEC system layout for the V2500 engine The FADEC system for V2500 is designed with EEC, the HMU and the sensors as the components that form the core of the engine system. The other component that is assigned to systems is the ignition system (Ian, 1990). Forces necessary for movement of startar vanes are brought about by the use of air pressure. Control valves from the hydraulic part is arranged centrally in HMU or decentralized around the actuators with FMU fixed in fuel distribution system. The alternator that is located at the accessory gear box is the main power supply. The aircraft electrical system provides alternative power supply and is used in case of FADEC alternator fails. The FADEC system requires relatively low power since this power is only used for EEC operation, the servo valves and also the sensors. All the components controlled by FADEC systems ...Download file to see next pagesRead More
Cite this document
  • APA
  • MLA
  • CHICAGO
(“Engine system for the Airbus A3200 Assignment Example | Topics and Well Written Essays - 1250 words”, n.d.)
Engine system for the Airbus A3200 Assignment Example | Topics and Well Written Essays - 1250 words. Retrieved from https://studentshare.org/engineering-and-construction/1446507-airbus
(Engine System for the Airbus A3200 Assignment Example | Topics and Well Written Essays - 1250 Words)
Engine System for the Airbus A3200 Assignment Example | Topics and Well Written Essays - 1250 Words. https://studentshare.org/engineering-and-construction/1446507-airbus.
“Engine System for the Airbus A3200 Assignment Example | Topics and Well Written Essays - 1250 Words”, n.d. https://studentshare.org/engineering-and-construction/1446507-airbus.
  • Cited: 0 times
Comments (0)
Click to create a comment or rate a document

CHECK THESE SAMPLES OF Engine system for the Airbus A3200

Engine Management Systems

...digitalize discrete inputs from the engine controls. This input value is switch position for engine controls, which includes; the start switch, anti ice engine switch as well as the master switch. Digitalized inputs from aircraft systems are transmitted through the interface computer into the EEC’s data buses. The power supply emanating from the ignition system and the EEC is also transferred through the EIU. Diagram02 below shows the interfacing unit of a FADE system (Anderson, 2002).Diagram02: Interfacing unit of an FADE system TASK 3: FADEC SYSTEM OF THE V2500-A5 ON THE AIRBUS A320...
7 Pages(1750 words)Coursework

Steam Engine

...?Steam Engine: The time period between 1750 and 1850 is considered to be the period of industrial revolution and which laid the foundation for many technological advancements in myriad fields like agriculture, transportation, mining, electricity, healthcare, and communication. It actually began in Great Britain and passing through Europe and America eventually prevailed throughout the world. This industrial revolution is said to have made a critically important turning point in the history of the world as it played a gigantic role in beginning to improve the life standards of masses of people everywhere in the world. Due to myriad technological inventions and discoveries, employment opportunities expanded, average per...
12 Pages(3000 words)Research Paper

The Airbus Way

...of software which was considered as the older version of Computer Aided Design (CAD) by the French and English engineers which created delays while transferring data from one system to another. Due to these circumstances, the company had to face huge losses in terms of its profitability over a certain period of time. Furthermore, another instance of cultural difference has also been observed within Airbus’ working environment. It was when the organisation’s Human Resource department attempted to provide training and development sessions to the employees, the French employees were found to be unresponsive deciphering high degree of IDV, where they depicted their preference for choosing...
8 Pages(2000 words)Essay

Search Engine Advertising

...? Advertisement Number: Lecturer: Question one Intermittent advertising should be applied in our advertising. This is because of the fact that we will have to satisfy the clients that we have before getting other clients. It is important that an e-commerce site satisfies the clients that they have before getting new ones. It is important to understand the needs of the new clients before getting new ones whose needs we are not aware. This way, we will be able to have high rating from the clients. Jupiter communications consumer survey data observes that 81 % of people who are regular internet users locate websites through the use of search engines. The article further indicates that 54% of online shoppers who are...
4 Pages(1000 words)Essay

Airbus Business Plan

...? Joint Venture Number: Lecturer: Joint venture Literature review As the Board of Directors of Airbus, we are planning a joint venture with General Electric (GE), an engine manufacturing company based in the United States. This has been informed by the industry forecast of growth in passenger numbers over the next two decades. Over the period, an extra 27,300 passenger airlines with a seating capacity of 100 and above passengers will be needed, besides 900 new cargo carriers. The industry forecasts growth in passenger planes from the current 15,500 to more than 32,500 by the year 2031. GE is one of the major engine framers in the world and more so geographically it is located across the...
8 Pages(2000 words)Essay

Engine Crankshaft System

...Running Head: Engine Crankshaft System Engine Crankshaft System Originally the v8 engines used a crankshaft arrangement (a) similar to the one used in the in-line four-cylinder engine. However, a new design (b) was later adopted to give it better balance. (Fundamentals of Motor Vehicle Design, 4th Edition by V.A.W Hillier Page 69) Both the arrangements allow for the power strokes to occur at intervals of 90 degrees and both of them allow for eight possible firing orders. Knowledge of the firing order enables the spark plug leads being connected correctly. The Engine Balance is very important in ensuring minimum vibrations. Factors which determine the number of vibrations are primary balance, component balance, firing interval... and...
4 Pages(1000 words)Essay

Recommendation report for Airbus

...output closely approximates the output from the centralized supply chain. BAE Systems has been a sleeping partner in Airbus since 2001 and owns a 20% share in the Company. BAE is a partner in America’s Joint Strike Fighter programme, however since Congress has been blocking the access to the software codes that are required, this has limited industrial participation by British companies in a large procurement project (The Economist, 2006: “A flurry of deals….”). Recommendations for the next five years: One of the major problems Airbus needs to overcome is its factory overload, which delayed the period for delivery of aircraft, i.e., about six years. Since there is also an...
14 Pages(3500 words)Essay

Industrial & Org Psychology MODULE 6; Communication

3 Pages(750 words)Essay

Diesel engine and Petrol engine ( Comparison )

...seventeen percent more hydrogen and carbon atoms therefore allowing diesel engines to be extra fuel efficient. Diesel engines are heavier and take more time to accelerate as compared to petrol engines. Thus, diesel engines take more time to get warmed up and starting up diesel engines can be very difficult during the winters. And to tackle this problem, now many diesel powered engines come along with glow plugs that can help to heat up the engine and along with that comes an engine heating system. Cost Structure When people go to buy new cars, the diesel engine cars cost...
6 Pages(1500 words)Essay

Boeing and airbus

...to the existing problem (Harress). The competitors of the Boeing include the airbus and Lockheed martin. The airbus is one of the biggest passenger airplanes known worldwide. However, it has some issues that need to be dealt with. For instance, one major problem of the airbus is its sensitive warning system. The software is not able to handle manageable tolerances and, therefore, the system can be set off even with very minor problems in the aircraft. The warnings and alarms can set off an alert and even shut down a well-functioning plane (Flight Global). There is a need for the algorithm to be set straight so that it is less sensitive and to prevent...
2 Pages(500 words)Research Paper
sponsored ads
We use cookies to create the best experience for you. Keep on browsing if you are OK with that, or find out how to manage cookies.

Let us find you another Assignment on topic Engine system for the Airbus A3200 for FREE!

Contact Us