Ppt Final(Amit Yadav)

8/10/2019 Ppt Final(Amit Yadav)

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H.A.L, ACCESSORIES DIVISION,

LUCKNOW

SUKHOI SU-30 MKI -FUEL SYSTEM

Presnted BY:

AMIT YADAV

Roll no.-1109040030

IEC-CET, Gr. Noida

M.E- 4th year



HAL CAME INTO EXISTENCE ON 1ST OCTOBER 1964.

THE COMPANY WAS FORMED BY THE MERGER OF HINDUSTAN

AIRCRAFT LIMITED WITH AERONAUTICS INDIA LIMITED AND

AIRCRAFT MANUFACTURING DEPOT, KANPUR. THE COMPANY

TRACES ITS ROOTS TO THE PIONEERING EFFORTS OF AN

INDUSTRIALIST WITH EXTRAORDINARY VISION, THE LATE SETH

WALCHAND HIRACHAND, WHO SET UP HINDUSTAN AIRCRAFT

LIMITED AT BANGALORE IN ASSOCIATION WITH THE ERSTWHILE

PRINCELY STATE OF MYSORE IN DECEMBER 1940.

ABOUT HAL



THE GOVERNMENT OF INDIA BECAME A SHARE HOLDER

IN MARCH 1941 AND TOOK OVER THE MANAGEMENT IN

1942.

DURING THE 1980’ HAL'S OPERATIONS SAW A RAPID

INCREASE WHICH RESULTED IN THE DEVELOPMENT OF

NEW INDIGENOUS AIRCRAFT SUCH AS HAL

TEJAS AND HAL DHRUV. HAL ALSO DEVELOPED AN

ADVANCED VERSION OF THE MIG-21, KNOWN AS MIG-

21

SON

, WHICH INCREASED ITS LIFE-SPAN BY MORE

THAN 20 YEARS.

http://en.wikipedia.org/wiki/HAL_Tejas


http://en.wikipedia.org/wiki/HAL_Dhruv

http://en.wikipedia.org/wiki/MiG-21












19 PRODUCTION UNITS AND 9 R D IN 7 LOCATIONS OVER INDIA

BANGALORE DIVISION

KANPUR DIVISION

KORAPUT DIVISION

HYDERABAD DIVISION

NASIK DIVISION

LUCKNOW DIVISION

KORWA DIVISION

HAL DIVISIONS

http://www.hal-india.com/enginedivisionkoraput.asp

http://www.hal-india.com/avionicsdivisionhyderabad.asp

http://www.hal-india.com/aircraftdivisionnasik.asp

http://www.hal-india.com/avionicsdivisionkorwa.asp

http://www.hal-india.com/transairdivision.asp

http://www.hal-india.com/helicopterdivision.asp



HAL SERVICES



Fighter Aircraft

1.Su-30 MKI2. Mig Series

3.Tejas

4.Jaguar

5.MIRAGE -2000Helicopters

1.Dhruv

2.Cheetah

3.Chetak

4.Advanced Light

Helicopters

Unmanned Aerial VehiclesEngines

1.Lakshya PTA

Passenger Aircraft

1.Dornier

2.Indian Regional Jet

Transport Aircraft

1.Saras

Light Trainer Aircraft1.Kiran

2.Basant

3.Sitara

Glider

1.HAL G-12.Ardhra

Satellite Launch Vehicles

1.PSLV2.GSLV

3.IRS

4.INSAT

PRODUCTS OF HAL



CUSTOMER PROFILE

Air force Army

Navy

Coast Guard Flying Academics & Educational

Institutions

Airlines / Air taxi / Air cargoDefence R&D Laboratories /

Department of Space



Airbus Boeing Sukhoi Aviation Corporation Israel Aircraft Industries RSK MiG BAE Systems Rolls-Royce plc Dassault Aviation Dornier Flugzeugwerke

Indian Aeronautical Development Agency Indian Space Research Organisation.

COLLABORATIONS WITH COMPANIES

http://en.wikipedia.org/wiki/Airbus

http://en.wikipedia.org/wiki/Boeing

http://en.wikipedia.org/wiki/Sukhoi_Aviation_Corporation

http://en.wikipedia.org/wiki/Israel_Aircraft_Industries

http://en.wikipedia.org/wiki/Mikoyan

http://en.wikipedia.org/wiki/BAE_Systems

http://en.wikipedia.org/wiki/Rolls-Royce_plc

http://en.wikipedia.org/wiki/Dassault_Aviation

http://en.wikipedia.org/wiki/Dornier_Flugzeugwerke

http://en.wikipedia.org/wiki/Aeronautical_Development_Agency

http://en.wikipedia.org/wiki/Indian_Space_Research_Organisation

http://en.wikipedia.org/wiki/Indian_Space_Research_Organisation

http://en.wikipedia.org/wiki/Aeronautical_Development_Agency









http://en.wikipedia.org/wiki/BAE_Systems



http://en.wikipedia.org/wiki/Israel_Aircraft_Industries




http://en.wikipedia.org/wiki/Boeing

http://en.wikipedia.org/wiki/Airbus



ABOUT H.A.L,ACCESSORIES DIVISION,

LUCKNOW

Established in 1964.

Primary Objective - To manufacture systems and accessories

for various aircrafts and engines and attain self sufficiency inthis area.

Spread over an area of 94,000 sq m.

Division Manufactures – Accessories for Aircrafts like Avro,

Dornier, Cheetah, Cheatak & Advanced Light Helicopters(ALH)

& SU-30.



DIVISIONS OF HAL LUCKNOW

LCA Division

ALH Division

Sukhoi Division

Instrument Factory

Accessories Division



SUKHOI SU-30 MKI

• The SUKHOI SU-30 MKI is a fourth generation air

superiority fighter developed by Russia’s Sukhoi and

assembled under license by India’s Hindustan Aeronautics

Limited (HAL) for the Indian Air Force (IAF).

• A variant of the Sukhoi SU-30,it is a heavy, all weather,

long range fighter.

ti l t t



GENERAL FEATURES OF SUKHOI 30

MKI

generation planes are yet to come.

Cost of single Su-30 MKI is $ 35 million or Rs 1.61billion

As per deal between Russia’s Sukhoi Corporation and

India’s HAL , in the first phase, components will beimported from Russia and only assembling will be

done

in 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.



SPECIFICATIONS

Crew: 2Length: 21.935 mWingspan : 14.7 mHeight: 6.36 m

Wing area: 62.0 m²Empty weight: 17,700 kgLoaded weight: 24,900 kgMax takeoff weight: 38,800 kg

Maximum speed: Mach 2.35(2,500 km/h) at11,000m.Range: 5,000 km with internal fuel tank.





FUEL FLOW AND METERING SYSTEM

IN SUKHOI 30 MKI

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

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

Service tank is centrally located is the most importantone.

Fuel from all other tanks pass through service tank before

consumption.

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

All the 5 tanks are so placed that the aircraft is

aerodynamically balanced.

TANK 1 TANK 2

TANK 3

SERVICETANK

TANK 4 TANK 5



FUEL TANKS

Number of fuel tanks: 6

• Name of fuel tanks: 1, 2, 3RT, 3LT,4, 5.

• Fuel Capacity: 1200 kg

• Special detail: Tank no. 2 is the

main tank and also known as

service tank having fuel capacity of

600 kg.

1



STRUCTURE

Fuel quantity & flow metering system can besubdivided into:

1. Fuel Flow Metering

> It computes the total quantity of fuel available in

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.



FUEL FLOW METERING 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



FUEL QUANTITY GAUGING Computes the quantity of fuel left in service tank.

It is an electronic system based on the principle of

variation of capacitance 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.



AUTOMATIC FUEL CONTROL SYSTEM



AUTOMATIC FUEL CONTROL SYSTEM

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 by

automatic control system.



FUEL QUANTITY &FLOWMETERING SYSTEM

FLOW METERINGPORTION

FUEL QUANTITYGAUGE PORTION

AUTOMATIC FUELCONTROL 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 Transduce2. Electronic Transducer U3. Relay Semiconductor

Control Unit

BRIEF DISCUSSION OF COMPONENTS



BRIEF DISCUSSION OF COMPONENTS

Signaling Transmitters(DSMK)

These are sensors for sensing the fuel levels in various

tanks.

Magnetic operated level switches of these probesgenerates

signal at one particular level of fuel.

Signals generated by these sensors act as an input for

automatic control portion.

6 types of such sensors are fitted in various tanks.

FUEL FLOW TRANSMITTERS



FUEL FLOW TRANSMITTERSThese 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 signalsprovided 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.

FUEL FLOW UNIT



FUEL FLOW UNIT

Computes quantity of total fuel available in aircraft basedon

signals from sensors which are impeller type fuel flowtransmitters and temperature probes.

It delivers the information to following instruments:

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

3. Complex Information Signaling System

4. Flight Data Recorder (FDR)

5. Integrated System (SOS)6. Transponder



FUEL QUANTITY UNIT

Computes quantity of fuel in service tank based on signals

from fuel quantity 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. Digital Light Indicator

It gives warning signal to pilot for residual fuel of 1500 Kgin

main tank.



DIGITAL LIGHT INDICATOR

It is an electronic display device in cockpit.

It continuously displays fuel quantity of service tank.

Semiconductor Relay Control Unit

It is a part of automatic control portion.

It works as an amplifier and a switching device for the

signals required for opening and closing of valves of

various tanks in aircraft.



COCKPIT

It has multi-function display.

Made up of special LCD.

These LCDs can withstand a temperature of -40 degree

Celsius.It can absorb repeated violent impacts of landing on aircraftcarriers.

The display is easily readable even in bright sunlight & dims

enough for the pilot to read at night without losing night vision.



CERTIFICATIONS

The ISO 9001 for entire range ofproducts and services.

ISO 14001 for EnvironmentalManagement System.

Approval for Research and DesignCenter by Department of Science and

Technology, Govt. of India. Approval of Director General

Aeronautical Quality Assurance forMilitary Aviation Products and Services.



THANK YOU!!!

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Ppt Final(Amit Yadav)