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AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs...

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Page 1: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 2: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

AEROSONDE UAVPropulsion system

A 26 Hour 45 min.Un-manned flight over the Atlantic

27-30 lbs weight

10 feet wing span

24 cc (1.5 inch3) engine180 grams/hour fuel consumption

Prepared by : CENGIZ CAMCIUAV propulsion class

DEPARTMENT OF AEROSPACE ENGINEERINGTHE PENNSYLVANIA STATE UNIVERSITY

Page 3: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

SMALL PROPULSION SYSTEMSFOR

UNMANNED AND MODEL AIRCRAFT

CONVENTIONAL INTERNAL

COMBUSTION

RUBBERPOWERED

ELECTRIC MOTOR

POWERED

GAS TURBINE/JET POWERED SYSTEMS

EXOTIC SYSTEMS

TWOSTROKEENGINES

FOUR STROKE ENGINES

CONVENTIONALFOUR CYCLE

OTTOENGINE

ROTARYENGINE

Wankel engine

ROTATING CYLINDER VALVE

ENGINE

MIGRATING COMBUSTION

CHAMBER

TURBO-JET SYSTEMSFOR

JET RPOPULSION

TURBO-SHAFT SYSTEMSFOR PROPELLER

ANDROTOR DRIVEN SYSTEMS

TURBO-SHAFT GAS TURBINE DRIVEN

A SINGLE DC ELECTRIC

GENERATOR &

DISTRIBUTED ELECTRIC MOTORS

CO2 ENGINESPULSE JETS

MICRO-ROCKET LASER DRIVEN

Page 4: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

THEAEROSONDE

UAV

The Aerosonde UAV is developed and operated globally by Aerosonde Pty Ltd (AePL) and

Aerosonde North America (AeNA).

It has been undertaking operations for about 7 years, was the first UAV to cross the Atlantic

Ocean, has flown for over 32 hrs in one stretch and has undertaken continuous operations with

relay aircraft extending over several days.

Page 5: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

The great flexibility of the Aerosonde, combined with a sophisticated command and control system,

enables deployment and command from virtually any location.

Page 6: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 7: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 8: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 9: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 10: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 11: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 12: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 13: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 14: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 15: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

Weight, wing span

27-30 lb, 10 ft

Engine 24 cc, 1.2 kw, fuel injected using premium unleaded petrol

Navigation GPS

Operation

Staff for Launch and Recovery

3 people: Controller, Technician, Pilot/Maintenance

Staff for Flight Operations

1 Person for up to 3 aircraft

Ground Equipment

Proprietary Staging Box, personal computer (laptop), GPS antenna, aviation and local communications radios

Flight Fully autonomous, under Base Command

Launch and Recovery

Launch from car roof rack (catapult option), land on belly, Autonomous

Page 16: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

Weight, wing span

27-30 lb, 10 ft

Engine 24 cc, 1.2 kw, fuel injected using premium unleaded petrol

Navigation GPS

Operation

Staff for Launch and Recovery

3 people: Controller, Technician, Pilot/Maintenance

Staff for Flight Operations

1 Person for up to 3 aircraft

Ground Equipment

Proprietary Staging Box, personal computer (laptop), GPS antenna, aviation and local communications radios

Flight Fully autonomous, under base command

Launch and Recovery

Launch from car roof rack (catapult option), land on belly, autonomous

Page 17: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

Ground & air communications

UHF or Satcoms (Iridium) to Aerosonde, VHF to field staff and other aircraft, internet to command

center and users.

Performance

Speed, Climb 18 – >32 ms-1, Climb >2.5 ms-1 at sea level

Range, Endurance with no additional payload

>1800 miles, >30 h

Altitude Range Up to 20,000 ft (medium weight)

Payload Maximum 5 lb with full fuel load

Standard Instrumentation

Temperature, Pressure, Humidity,

Wind

2 Vaisala RSS901 Sondes for temperature, pressure and

humidity, and a proprietary wind system.

Page 18: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

Ground & air communications

UHF or Satcoms (Iridium) to Aerosonde, VHF to field staff and other aircraft, internet to command

center and users.

Performance

Speed, Climb 18 – >32 ms-1, Climb >2.5 ms-1 at sea level

Range, Endurance with no additional payload

>1800 miles, >30 h

Altitude Range Up to 20,000 ft (medium weight)

Payload Maximum 5 lb with full fuel load

Standard Instrumentation

Temperature, Pressure, Humidity,

Wind

2 Vaisala RSS901 Sondes for temperature, pressure and

humidity, and a proprietary wind system.

Page 19: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

Weight, wing span

27-30 lb, 10 ft

Engine 24 cc, 1.2 kw, fuel injected using premium unleaded petrol

Navigation GPS

Operation

Staff for Launch and Recovery

3 people: Controller, Technician, Pilot/Maintenance

Staff for Flight Operations

1 Person for up to 3 aircraft

Ground Equipment

Proprietary Staging Box, personal computer (laptop), GPS antenna, aviation and local communications radios

Flight Fully autonomous, under Base Command

Launch and Recovery

Launch from car roof rack (catapult option), land on belly, Autonomous

Page 20: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 21: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 22: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 23: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 24: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 25: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 26: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 27: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 28: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 29: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 30: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 31: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 32: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 33: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 34: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 35: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 36: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 37: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 38: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 39: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 40: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 41: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 42: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 43: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

400 gm/[KWh]180 gm/hour level flight 0.45 KW

400gm/[KWh] @ 5500 rpm

MAX Fuel capacity 7000 gm

5000/180= 27.8 hours

Transatlantic flight took 26 H 45 min

FIRST GENERATION ENYA PROPULSION SYSTEM

Page 44: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

400 gm/[KW.h] Enya four cycle IC engineFirst generation Enya

0.454 gm-f = 1 lb-f1KW=0.75 HP1 LB/(HP.h)=610 gm/[Kw-h]

TF-53 helicopter engine HUEY1400 HP (30 min.)SFC= 0.58 LB/[HP.h] = 0.58*610=353 gm/[KW.h]

Second generation ENYA 245-300 gm/[KW.h]

SFC comparison

Page 45: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

SPECIFIC FUEL CONSUMPTION OF VARIOUS PROPULSION SYSTEMS

Page 46: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 47: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 48: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 49: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 50: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 51: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 52: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 53: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

ALTITUDE AND FLIGHT MACH NUMBER DEPENDENCY

OF VARIOUS PROPULSION SYSTEMS

Page 54: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

VSC001 VSC001-SC

Page 55: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

VANE PUMP DRIVEN SUPERCHARGING FOR 36,000 + feet OPERATION

Page 56: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 57: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 58: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 59: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 60: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 61: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 62: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 63: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 64: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.
Page 65: AEROSONDE UAV Propulsion system A 26 Hour 45 min. Un-manned flight over the Atlantic 27-30 lbs weight 10 feet wing span 24 cc (1.5 inch 3 ) engine 180.

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