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    A PRESENTATION ON

    INDUSTRIAL TRAINING AT

    FROM JUNE 27 TO JULY 23 2011

    ASHISH KUMAR MISHRAUNIVERSITY ROLLNO:0922240010B.TECH : MEYEAR : 4th yr

    LUCKNOW

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    TypeState-ownedenterprise

    Industry Aerospace anddefence

    Founded1940 (in 1964,company took oncurrent name)

    Headquarters

    Bangalore,

    Karnataka, India

    Chairman Ashok Nayar

    Products

    Aerospaceequipment

    Military aircraftCommunication &NavigationequipmentSpace systems

    RevenueUS$2.35 billion

    (FY 2007)Employees 30,000

    http://en.wikipedia.org/wiki/Types_of_business_entityhttp://en.wikipedia.org/wiki/Government-owned_corporationhttp://en.wikipedia.org/wiki/Government-owned_corporationhttp://en.wikipedia.org/wiki/Industryhttp://en.wikipedia.org/wiki/Aerospacehttp://en.wikipedia.org/wiki/Bangalorehttp://en.wikipedia.org/wiki/Karnatakahttp://en.wikipedia.org/wiki/Indiahttp://en.wikipedia.org/wiki/Revenuehttp://en.wikipedia.org/wiki/US$http://en.wikipedia.org/wiki/Fiscal_yearhttp://en.wikipedia.org/wiki/Employmenthttp://en.wikipedia.org/wiki/Employmenthttp://en.wikipedia.org/wiki/Fiscal_yearhttp://en.wikipedia.org/wiki/US$http://en.wikipedia.org/wiki/Revenuehttp://en.wikipedia.org/wiki/Indiahttp://en.wikipedia.org/wiki/Karnatakahttp://en.wikipedia.org/wiki/Bangalorehttp://en.wikipedia.org/wiki/Aerospacehttp://en.wikipedia.org/wiki/Industryhttp://en.wikipedia.org/wiki/Government-owned_corporationhttp://en.wikipedia.org/wiki/Government-owned_corporationhttp://en.wikipedia.org/wiki/Government-owned_corporationhttp://en.wikipedia.org/wiki/Government-owned_corporationhttp://en.wikipedia.org/wiki/Types_of_business_entity
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    To become a global player in the aerospace industry

    > Hindustan Aeronautics Limited is the largest PSU under the

    Department of Defence Production and is a Navaratana Company.

    > HAL is one of the largest aerospace companies inAsia with its

    annual turnover to be running above US$ 2 billion.

    > It has several facilities throughout India includingNasik, Korwa, Kanpur, Koraput, Lucknow, Bangaloreand Hyderabad.

    THE MISSION

    http://en.wikipedia.org/wiki/US$http://en.wikipedia.org/wiki/Nasikhttp://en.wikipedia.org/wiki/Korwahttp://en.wikipedia.org/wiki/Kanpurhttp://en.wikipedia.org/wiki/Koraputhttp://en.wikipedia.org/wiki/Lucknowhttp://en.wikipedia.org/wiki/Bangalorehttp://en.wikipedia.org/wiki/Hyderabad,_Indiahttp://en.wikipedia.org/wiki/Hyderabad,_Indiahttp://en.wikipedia.org/wiki/Bangalorehttp://en.wikipedia.org/wiki/Lucknowhttp://en.wikipedia.org/wiki/Lucknowhttp://en.wikipedia.org/wiki/Koraputhttp://en.wikipedia.org/wiki/Kanpurhttp://en.wikipedia.org/wiki/Korwahttp://en.wikipedia.org/wiki/Nasikhttp://en.wikipedia.org/wiki/US$
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    DIVISIONS OF HAL

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    AirbusBoeingSukhoi Aviation CorporationIsrael Aircraft IndustriesRSK MiG

    BAE SystemsRolls-Royce plcDassault AviationDornier Flugzeugwerke

    Indian Aeronautical DevelopmentAgencyIndian Space Research Organisation.

    COLLABORATIONS WITH COMPANIES

    http://en.wikipedia.org/wiki/Airbushttp://en.wikipedia.org/wiki/Boeinghttp://en.wikipedia.org/wiki/Sukhoi_Aviation_Corporationhttp://en.wikipedia.org/wiki/Israel_Aircraft_Industrieshttp://en.wikipedia.org/wiki/Mikoyanhttp://en.wikipedia.org/wiki/BAE_Systemshttp://en.wikipedia.org/wiki/Rolls-Royce_plchttp://en.wikipedia.org/wiki/Dassault_Aviationhttp://en.wikipedia.org/wiki/Dornier_Flugzeugwerkehttp://en.wikipedia.org/wiki/Aeronautical_Development_Agencyhttp://en.wikipedia.org/wiki/Aeronautical_Development_Agencyhttp://en.wikipedia.org/wiki/Indian_Space_Research_Organisationhttp://en.wikipedia.org/wiki/Indian_Space_Research_Organisationhttp://en.wikipedia.org/wiki/Aeronautical_Development_Agencyhttp://en.wikipedia.org/wiki/Aeronautical_Development_Agencyhttp://en.wikipedia.org/wiki/Dornier_Flugzeugwerkehttp://en.wikipedia.org/wiki/Dornier_Flugzeugwerkehttp://en.wikipedia.org/wiki/Dassault_Aviationhttp://en.wikipedia.org/wiki/Dassault_Aviationhttp://en.wikipedia.org/wiki/Dassault_Aviationhttp://en.wikipedia.org/wiki/Rolls-Royce_plchttp://en.wikipedia.org/wiki/Rolls-Royce_plchttp://en.wikipedia.org/wiki/Rolls-Royce_plchttp://en.wikipedia.org/wiki/BAE_Systemshttp://en.wikipedia.org/wiki/Mikoyanhttp://en.wikipedia.org/wiki/Mikoyanhttp://en.wikipedia.org/wiki/Israel_Aircraft_Industrieshttp://en.wikipedia.org/wiki/Sukhoi_Aviation_Corporationhttp://en.wikipedia.org/wiki/Sukhoi_Aviation_Corporationhttp://en.wikipedia.org/wiki/Sukhoi_Aviation_Corporationhttp://en.wikipedia.org/wiki/Boeinghttp://en.wikipedia.org/wiki/Airbus
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    Fighter Aircraft1.Su-30 MKI2. Mig Series3.Tejas4.Jaguar5.MIRAGE -2000 Helicopters

    1.Dhruv2.Cheetah3.Chetak4.Advanced LightHelicoptersUnmanned Aerial VehiclesEngines1.Lakshya PTA

    Passenger Aircraft1.Dornier2.Indian Regional Jet

    Transport Aircraft1.Saras

    Light Trainer Aircraft1.Kiran2.Basant3.SitaraGlider1.HAL G-12.Ardhra

    Satellite Launch Vehicles1.PSLV2.GSLV3.IRS4.INSAT

    PRODUCTS OF HAL

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    The Sukhoi Su-30MKI has been jointly-developed by Russia'sSukhoi Corporation and India's Hindustan Aeronautics Limited

    (HAL) for the Indian Air Force (IAF). It is a heavy class, long-range air superiority fighter aircraft.

    The Su-30 MKI is more advanced than the basic Su-30MK, the

    Chinese Su-30 MKK, and the Malaysian Su-30 MKM.

    The aircraft features state of the art avionics developed by

    Russia, India , Israel , France and South Africa which includesdisplay, navigation, targeting and electronic warfare systems.

    MKI stands for "Modernizirovannyi Kommercheskiy Indiski"

    meaning "Modernized Commercial India".

    http://en.wikipedia.org/wiki/Russiahttp://en.wikipedia.org/wiki/Sukhoihttp://en.wikipedia.org/wiki/Indiahttp://en.wikipedia.org/wiki/Hindustan_Aeronautics_Limitedhttp://en.wikipedia.org/wiki/Indian_Air_Forcehttp://en.wikipedia.org/wiki/Air_superiority_fighterhttp://en.wikipedia.org/wiki/Su-30http://en.wikipedia.org/wiki/Su-30MKKhttp://en.wikipedia.org/wiki/Su-30MKMhttp://en.wikipedia.org/wiki/Su-30MKMhttp://en.wikipedia.org/wiki/Su-30MKMhttp://en.wikipedia.org/wiki/Su-30MKMhttp://en.wikipedia.org/wiki/Su-30MKKhttp://en.wikipedia.org/wiki/Su-30MKKhttp://en.wikipedia.org/wiki/Su-30MKKhttp://en.wikipedia.org/wiki/Su-30http://en.wikipedia.org/wiki/Su-30http://en.wikipedia.org/wiki/Su-30http://en.wikipedia.org/wiki/Air_superiority_fighterhttp://en.wikipedia.org/wiki/Indian_Air_Forcehttp://en.wikipedia.org/wiki/Hindustan_Aeronautics_Limitedhttp://en.wikipedia.org/wiki/Indiahttp://en.wikipedia.org/wiki/Sukhoihttp://en.wikipedia.org/wiki/Sukhoihttp://en.wikipedia.org/wiki/Sukhoihttp://en.wikipedia.org/wiki/Russia
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    Sukhoi 30 MKI is a 4.5 generation fighter aircraft . Fifth

    generation planes are yet to come. Cost of single Su-30 MKI is $ 35 million or Rs 1.61billion As per deal between Russias Sukhoi Corporation and

    Indias HAL , in the first phase, components will be

    imported from Russia and only assembling will bedonein India.

    In the second phase , there will be transfer oftechnology

    from Russia to India , and then both manufacturing &

    assembling will be done in India. Various independent sources have claimed Su-30MKI

    to be the most superior fighter plane in presentWorld.

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    Fuel capacity of Sukhoi 30 MKI: 12 ton or 12000Kg

    There are 5 fuel tanks of which one is service tank ormain tank.

    Service tank is centrally located is the mostimportant one.

    Fuel from all other tanks pass through service tankbefore

    consumption.

    So in the end fuel remains only in the service tank.

    All the 5 tanks are so placed that the aircraft isaerodynamically balanced.

    TANK 1 TANK 2

    TANK 3

    SERVICETANK

    TANK 4 TANK 5

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    Fuel quantity & flow metering system can besubdivided into:1. Fuel Flow Metering

    > It computes the total quantity of fuel availablein aircraft.

    Uses impeller type of sensors.

    2. Fuel Quantity Gauging> It computes the quantity of fuel in the service

    tank.

    Uses capacitance type electronic sensors.

    3. Automatic Control> It manages the sequence of fuel flow to/from

    various

    tanks during refueling and consumption.

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    Computes the quantity of fuel left in aircraft.

    Based on the principle of impeller movement.

    Impeller is a device which rotates due to the movementof

    liquid(fuel) through pipe. One complete rotation of impeller is associated with a

    unique amount of fuel flow. This gives us the volumeof

    fuel consumed.

    So weight of fuel consumed:weight of fuel = volume * density

    Net fuel remaining = initial quantity of fuel fuelconsumed

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    Computes the quantity of fuel left in service tank.

    It is an electronic system based on the principle of

    variation ofcapacitance with change in dielectric medium.

    It consists of uniform cylindrical shaped capacitor withthe

    fuel acting as the dielectric. As the fuel gets consumed , the fuel is replaced by air as

    dielectric and there is a change in capacitance.

    So , the remaining fuel in the service tank can becalculated

    on the basis of variation in capacitance.

    Fuel quantity gauge is of utmost importance when

    1. Only service tank is left with fuel.

    2. Flow metering system fails.

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    The system comprises of

    1 . A capacitance based gauging probe.

    2. Cable assembly.3. Sensing amplifier box.

    The gauging probe assembly in the fuel tank isconnected

    to the sensing box by means of cable assembly. Depending on the fuel level in the tank , thecapacitance

    formed is sensed and amplified by the amplifier

    box andthe data is sent to the electronic display in the

    cockpit. Amplifierbox

    CapacitanceBasedGaugingprobe

    Cableassembly

    ElectronicDisplay incockpit

    display

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    Automatic control manages sequence of fuel flow to/from

    various tanks during refueling as well as consumption.

    The fuel from all the five tanks is taken in such a way that

    the aerodynamic balance of the plane is not disturbed.

    This is done with the help of automatic control system.

    Fuel from a certain tank is not taken all at once. After taking

    a certain quantity of fuel from one tank, the valve is closed

    and then fuel is drawn from another tank.

    So, the sequence of fuel flow from various tanks is decided byautomatic control system.

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    FUEL QUANTITY &FLOWMETERING SYSTEM

    FLOW METERINGPORTION

    FUEL QUANTITYGAUGE PORTION

    AUTOMATICCONTROL PORTION

    1. Fuel Flow Transmitter2. Refueling Fuel Flow

    Transmitter3. Two Channel Temperature

    Probes4. Fuel Flow Unit5. Fuel Control Panel

    1. Fuel Quantity Transducers2. Two Channel Temperature

    Probes3. Fuel Quantity Unit

    4. Digital Light Indicator5. Fuel Control Panel

    1. Fuel Quantity Transdu2. Electronic Transducer3. Relay Semiconductor

    Control Unit

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    Signaling Transmitters(DSMK) These are sensors for sensing the fuel levels invarious

    tanks.

    Magnetic operated level switches of these probes

    generatessignal at one particular level of fuel.

    Signals generated by these sensors act as an inputfor

    automatic control portion.

    6 types of such sensors are fitted in various tanks.

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    These are impeller type of sensors which produce electrical

    signal proportional to the rate of flow of fuel through it. Fuel consumed by aircraft is computed based on the signals

    provided by these sensors.

    FUEL QUANTITY TRANSMITTERS These are sensors for computing fuel quantity in servicetank.

    Capacitance of these probes change with variation in fuellevel

    in tank.

    Resultant capacitance acts as an input for computing fuel in

    service tank.

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    Computes quantity of total fuel available in aircraft

    based onsignals from sensors which are impeller type fuel

    flow

    transmitters and temperature probes.

    It delivers the information to following instruments:

    1. Refueling Control Panel

    2. Stand By Equipment (SBI)

    3. Complex Information Signaling System

    4. Flight Data Recorder (FDR)

    5. Integrated System (SOS)

    6. Transponder

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    Computes quantity of fuel in service tank based onsignals

    from fuel quantity transmitters and temperatureprobes.

    It delivers the information to following instruments:

    1. Refueling Control Panel2. Stand By Equipment (SBI)

    3. Complex Information Signaling System

    4. Digital Light Indicator

    It gives warning signal to pilot for residual fuel of1500 Kg in

    main tank.

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    It is an electronic display device in cockpit.

    It continuously displays fuel quantity of servicetank.

    Semiconductor Relay Control Unit

    It is a part of automatic control portion. It works as an amplifier and a switching devicefor the

    signals required for opening and closing of

    valves ofvarious tanks in aircraft.

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    Thank

    You

    Any Queries??