Presentation On Electronics

Control System In Aircrafts

PREPARED BY: SADDAM HUSSAIN

EC(4th

Year)

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ABSTRACT

Electronic control system is used to

install and maintain the sensors which

measure and report flight and engine

parameters.

1-SU-30.

2-Electronic flight instrumentation system.

3-Full Authority Digital Electronics Control

(FADEC).

4-Limited Authority Spark Advance Regulator.

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ABOUT HINDUSTAN AERONAUTICS LIMITED (HAL)

HAL was established as Hindustan Aircraft Limited in Bangalore in 1940 by the late Seth Walchand Hirachand to produce military aircraft for the Royal Indian Air Force.

Hindustan Aeronautics Limited came into existence on 1st October 1964 by the merger of Hindustan Aircraft Limited with Aeronautics India Limited and Aircraft Manufacturing Depot, Kanpur.

The Gov. of India became a share holder in March 1941 and took over the management in 1942.

Today H.A.L has 19 production units and 10 Research and Design Centers in 8 location of India.

HAL is one of the largest aerospace companies in Asia with its annual turnover to be running above US$ 2 billion.

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SUKHOI-30

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SUKHOI SU-30

The Sukhoi Su-30 is an air superiority

fighter jointly developed by Russia's Sukhoi

Aviation Corporation and India's Hindustan

Aeronautics Limited (HAL).

Sukhoi Su-30 is a heavy, all-weather, long-

range fighter.

The Su-30 is a highly integrated twin-finned

aircraft.

The Su-30 is a multirole fighter.

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SUKHOI SU-30 The aircraft is fitted with a satellite

navigation system (GPS compatible),

which permits it to make flights in all

weather, day and night.

SU-30 is equipped with a modern digital

weapons control system as well as anti-

jamming features.

The Su-30 is capable of accomplishing a

wide variety of combat mission at

significant distance from the home base, in

any weather conditions.

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Electronic Flight Instrument System

An electronic flight instrument system is a flight deck instrument display system in aircrafts.

Which the display technology used in electronic rather thatn electromechanical.

EFIS consists of PFD,MFD,EICAS.

An EFIS installation will have the following components:

1-Display

2-Controls

3-Data Processors A basic EFIS might have all these facilities in the one unit.

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Electronic Flight Instrument System

Two Primary Flight Displays

(PFD) for EFIS functions

(EADI/EHSI)

Two Primary Flight Displays

(PFD) for EFIS functions

(EADI/EHSI)

Two Multi Function

Displays

(MFD) for Navigation and

aircraft system synoptic.

Control panels for system settings

One Engine & Warning

Display

(EWD) for Engine

Instruments and

Crew Alerting System,

Checklists/

Procedures management

and

permanent data.

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DISPLAY UNITS:

1-Primary Flight Display

* On the flight deck, the display units are the most obvious parts of an EFIS

system.

* The PFD displays all information critical to flight, including calibrated

airspeed, altitude, heading, attitude, vertical speed and yaw.

* The PFD is designed to improve a pilot's situational awareness by

integrating this information into a single display instead of six different analog

instruments.

* LCD units generate less heat than CRTs; an advantage in a congested

instrument panel. They are also lighter, and occupy a lower volume.

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The Multi Function Display (MFD)-

1-The MFD (multi-function display) displays navigational and weather

information from multiple systems.

2- . MFDs are most frequently designed as "chart-centric", where the aircrew

can overlay different information over a map or chart.

3- MFDs can also display information about aircraft systems, such as fuel and

electrical systems (see EICAS, below).

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Engine indications and crew alerting system (EICAS) / electronic centralized aircraft monitoring (ECAM):

1- EICAS (Engine Indications and Crew Alerting System) displays information

about the aircraft's systems, including its fuel, electrical and propulsion

systems (engines).

2- EICAS improves situational awareness by allowing the aircrew to view

complex information in a graphical format and also by alerting the crew to

unusual or hazardous situations.

Control Panels :

The pilots are provided with controls, with which they select display range

and mode (for example, map or compass rose) and enter data (such as

selected heading).

Where inputs by the pilot are used by other equipment, data

buses broadcast the pilot's selections so that the pilot only

needs to enter the selection once.

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Advantages Of EFIS- 1-Offers versatality.

2- Flexibility afforded by software modifications.

3- Minimizes costs.

4- EFIS system can be updated with new software to

extend its capabilities.

5- Degree of redundancy is available.

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Full Authority Digital Engine Control (FADEC):

Full Authority Digital Engine (or Electronics) Control

(FADEC) is a system consisting of a digital computer, called

an electronic engine controller (EEC) or engine control unit(ECU),

and its related accessories that control all aspects

of aircraft engine performance

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~ Provides optimum engine efficiency.

~ Provides efficient engine operation.

~ Controls engine starting & restarting.

~ Controls fuel flow.

~ Manages the power efficiently.

~ Manages the wind conditions, runway length.

FUNCTIONS OF FADEC:

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Advantages of FADEC: ~ Better fuel efficiency. ~ Automatic engine protection against out-of-tolerance operations. ~ Safer as the multiple channel FADEC computer provides redundancy in case of failure. ~ Provides semi-automatic engine starting. ~ Better systems integration with engine and aircraft systems. ~ Can provide engine long-term health monitoring and diagnostics.

Disadvantages of FADEC:

~ If a total FADEC failure occurs, the engine fails. ~ High system development and validation effort due to the complexity.

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Limited Authority Spark Advance Regulator: ~ FIRST microprocessor based engine control system approved the FAA for general aviation piston aircraft. ~ To establish and command the optimum ignition timing and spark energy to produce maximum torque from the engine. ~ LASAR has an inherent mechanical magneto backup system.

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Benefits Of LASAR: ~Better engine starting with three times more spark energy and higher output voltage. ~Smoother transition in ignition timing from engine start to idle . ~Faster Rate of Climb. ~Increased spark plug life. ~EGT reduced by 150°F on average. ~Up to 12% Reduced Fuel Consumption. ~Up to 8% Increased Horsepower.

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THANK YOU

..

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Any Query !!

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