This document provides information about Abhishek Maurya's practical training at Hindustan Aeronautics Limited (HAL) from June 1-30, 2015. It discusses HAL's mission to become a global aerospace leader, its divisions and key products including fighter jets, helicopters, engines, satellites, and more. Specific details are given about the Sukhoi Su-30MKI jet such as its dimensions, performance specifications, and fuel system. Components like the flight data recorder, soldering techniques, and electrical systems including the transformer rectification unit and flight instruments are also outlined.

1. A PRESENTATION ON
PRACTICAL TRAINING AT
FROM 01/06/2015 TO 30/06/2015
ABHISHEK MAURYA
1201431004
SRMSCET
LUCKNOW
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2. “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 in Asia with its
annual turnover to be running above US$ 2 billion.
> It has several facilities throughout India including
Nasik, Korwa, Kanpur, Koraput, Lucknow, Bangalore
and Hyderabad.
THE MISSION
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3. DIVISIONS OF HAL
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4. Fighter Aircraft
1.Su-30 MKI
2. Mig Series
3.Tejas
4.Jaguar
5.MIRAGE -2000
Helicopters
1.Dhruv
2.Cheetah
3.Chetak
4.Advanced Light Helicopters
Unmanned Aerial Vehicles
Engines
1.Lakshya PTA
Passenger Aircraft
1.Dornier
2.Indian Regional Jet
Transport Aircraft
1.Saras
Light Trainer Aircraft
1.Kiran
2.Basant
3.Sitara
Glider
1.HAL G-1
2.Ardhra
Satellite Launch Vehicles
1.PSLV
2.GSLV
3.IRS
4.INSAT
PRODUCTS OF HAL
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5. SUKHOI-30 MKI 5

6. General characteristics of Su-30
• Length: 21.935 m (72.97 ft)
• Wingspan: 14.7 m (48.2 ft)
• Height: 6.36 m (20.85 ft)
• Wing area: 62.0 m2 (667 ft2)
• Empty weight: 17,700 kg
(39,021 lb)
• Loaded weight: 24,900 kg
(54,900 lb) with 56% fuel
• Max. takeoff weight:
34,500 kg (76,060 lb)
• Fuel capacity: 9,400 kg
(20,724 lb) internally
• Performance
• Maximum speed: Mach 2.0
(2,120 km/h, 1,320 mph)
• Range: 3,000 km (1,620 nmi)
at altitude.
• Service ceiling: 17,300 m
(56,800 ft)
• Rate of climb: 230 m/s
(45,275 ft/min)
• Wing loading: 401 kg/m2 with
56% fuel (468.3 kg/m2 with
full internal fuel) (82.3 lb/ft2
with 56% fuel)

7. FDR(BLACK BOX)
• The Black Box was first
invented by a young
Australian scientist
named Dr. David
Warren working at the
Aeronautical Research
Laboratory in
Melbourne in the mid-
1950s.

8. Flight Data Recorder(Black Box)
• All recorders undergo countless tests. For
example, one Black Box recorder, the L-3 FA
2100 underwent testing that includes
exposure to a 1,110°C fire for an hour and
260°C heat for 10 hours. It is also able to
operate between -55° to +70°C and it can
carries a minimum 25 hours of flight data

10. Under water locator beacon
• A 37.5 kHz
(160.5 dB re 1 μPa)
ping can be
detectable 1–2
kilometres (0.62–
1.24 mi) from the
surface in normal
conditions and 4–5
kilometres (2.5–
3.1 mi) in good
conditions

11. 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 main tank.
 Service tank is centrally located is the most important one.
 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
SERVICE
TANK
TANK 4 TANK 5
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12.  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 is connected
to the sensing box by means of cable assembly.
 Depending on the fuel level in the tank , the capacitance
formed is sensed and amplified by the amplifier box and
the data is sent to the electronic display in the cockpit.
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FUEL QUANTITY GAUGING

13. Fuel measuring probes
• C={(permittivity x
area)/distance}
Capacitance
Based
Gauging
probe
Cable
assembly
Amplifier
box
Electronic
Display in
cockpit
display

14. Fuel gauging system
Capacitive Probes
Temperature
Sensor
EElectronic
Block
Cockpit Display
Device
32 bit code

15. Soldering of components
• Step 1: Warm Up The
Iron
• Step 2: Prepare A Little
Space
• Step 3: Thoroughly
Coat The Tip In Solder
• Step 4: Clean The
Soldering Tip

16. • Step 1:
Surface
Preparation
• Step 2:
Component
Placement
• Step 3: Apply
Heat
• Step 4: Apply
Solder To The
Joint

17. Transformer Rectification Unit
• Input Voltage
Three Phase WYE
115/200VAC L-L Nominal
190 to 210 VAC L–L
Normal
173 to 216 VAC L–L
Abnormal Input
Frequency
400 Hz Nominal
• Output Voltage
Unregulated
28 VDC Nominal
24.0-31.5 VDC Normal
Regulated
28VDC +/-1%
• Output Power
50 to 500 Amps
1400 to14000 Watts
• Overload
125% for 5 Minutes
150% for 2 Minutes
200% for 1 Minute
1200% for 1 Second
• Ripple
1.5V p-p Efficiency

18. TTransformer Rectification Unit

19. Flight Instruments
• Altimeter
• ROCI

20. Altimeter
It measures the altitude of an aircraft

21. Variometer(ROCI)
It is the rate of climb indicator.
Thermistors are
used for
measuring voltage
difference

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