Challenge

Project-1: Powertrain for aircraft in runways

Question 1

list of Weight Of Different aircrat has been attach in tbe Exel file report (Project 1)

Question 2

Is there any difference between ground speed and air speed?

Airspeed and ground speed are completely different when it comes to determining how fast an airplane flies.

Ground speed is that speed how fast the airplane is travelling on the ground relative to fixed point.

Air speed is that speed ,under his own engine power how fast airplane is travelling

In general ,If there no wind Ground speed=Air speed.

but as there is wind present

ground spped - Wind speed = Air speed.

NASA Explains,

On a perfectly still day, the airspeed is equal to the ground speed. But if the wind is blowing in the same direction that the aircraft is moving, the airspeed will be less than the ground speed.

This is because that Drag is require for the lift of the airplane ,and its only generated from the Wind coming From the Opposite Side.

Question 3

Why is it not recommended to use aircraft engine power to move it on the ground at Airport?

Air craft Engine Power are Very much High ,as they are used to produced thrust.

Its works on sucking the wind and throwing backwards direction ,this way it Moved forward.

But the Wind Generating due to enhine power are high as Hurricane wind .

This types of wind can Damage the Buildings near air ports ,small houses, and the ROOF of Airports Buildings which are Prone to small forces.

Risk factor is high While using the aircfrat engine power At airport..

Question 4

How an aircraft is pushed to runway when its ready to take off?

A truck Called pushback truck Is used to push and pull the Aircraft,pushing it with a towbar attached to the nose-wheel or you can say Front Single wheel.

A Pushback Vehicle is shown in the Image.

(this the new versions of push back late where used a TOW bar attchteach to airplane and Truck)

By Lookinf this picture you may be wondering that ,How a little truck and pull this heavy airplane?

actuclly This they dont have to lift the heavy weight of the airplane ,airplane itself is mounted on high pressure tyre, thney Only have to use the Firction thing here to get Reduced.

This truck are slow speed but produce very large amount of torque ,used to pull or push aircraft.

IMPOTANT Terms When the Aircraft is Landing.

Tafe Off Power

The amount of power that an engine is allowed to produce for a limited period of time for takeoff.

The use of takeoff power is usually limited to 5 min for reciprocating engines and up to 2½ min for gas turbine engines.

tyre design

An aircraft tyre is designed to withstand extremely heavy loads while landing, take off, taxing, and parking. The number of wheels required for aircraft increases with the weight of the aircraft, as the weight of the aeroplane needs to be distributed more evenly.

The degisn of airplane tyre is not similar to truck or car tyre beacuse they have to with stand heavy load ,friction,pressure.
You can observe from the image How the Contruction of aircraft tyre.

Load Rating – Load rating is the maximum permissible load at a inflation pressure.

Ply Rating – Ply Rating is used to identify the maximum load rating and inflation pressure for a specified tyre.

Speed Rating – The speed rating is the maximum takeoff speed to which the tyre has been tested.

Skid Depth – Skid depth is the distance between the tread surface and the deepest groove as measured in the mould.

Tyre pressure

Tyre of an air craft is fas different from the tyre used in cars and trucks.,

generally car needs a 30 to 40 psi tyre pressure in it But airplane have a tyre pressure of 200 psi,to with stand on heavy loads, diffreent temperatures etc.

Rather than a normal air as used in the car or truck ,Nitrogen gas used in the tyre of airplane.

nitrogen is a inert gas, it does not change its structure in high and Low temperature, this is reason they used in airplane tyres.

brake forces.

From below example you can get Which forces are needed to calculate a brake power for airplane.

some assumptions

Landing weight = takeoff weight in case of aborted takeoff =20000 lbf

Landing distance = 1000 ft

Speed (assume aborted takeoff) = 120 kt (200 ft/sec)

We will use Newton’s second law to determine force due to deceleration:

Deceleration: from simple kinematics, acceleration = velocity^2 / distance

= (200 ft/s)^2 / 1000 ft = 40 ft / s^2

Mass of aircraft = (weight) / g = 20000/32.2 = 621.11 lbf*s^2 / ft

Force = mass * acceleration (621.11 lbf*s^2/ft) * (40 ft / s^2) = 24844.4 lbf

So in this example, the braking (deceleration) force is 24844.4 lbf

Notice that in the English foot-pound-second units the mass unit is
pound-second^2 per foot, called a slug in order for the units to work out.

Question 6

A. With necessary assumptions, calculate the force and power required to push / pull an aircraft by a towing vehicle.

Airplane Value

Gross weight = 35,000 kg

Width = 3400 mm = 3.4 m
Height = 4400 mm = 4.4 m
Values of the Pushback Truck
Length (excluding coupler) = 8470 mm = 8.47 m
Tyre size = R 22.5 = 571.5 mm = 0.5715 m
Maximum vehicle speed = 32 kmph
= (32*5/18)
Velocity of the truck = 8.89 m/s
gross weight = 164000 kg
Height = 15.80 m
Width= 43.90 m
Drag coefficient (Cd)=0.0265

Now

Total Tractive froce = Rolling resistence +Arodynamic drag

Rolling resistance force
urr*mg
Drag force=Fa=01/2*p*A*Cd*V^2.
To find rolling resistance force
Rolling resistance force- Fir- urr-mg
(m) mass of the towing vehicle+mass of the airbus
(m)=35000+164000
m-199000kg
Substitute mass (m) value in rolling resistance formula
Rolling resistance force=-0.02*199000 *9.81
Frr=39043.8 N
To find the air drag force
Drag force Fad=1/2* row* A* Cd* v^2
row= 1.225 kg/m^3 (standard)
Frontal area A = Height of the airbus * Width of the airbus
A =15.80* 43.90= 693.62 m^2
Substituting the row and A values in drag force formula,
Assume that vehicle running at the speed of 20 kmph
V= (20 5/18) = 5.56 m/s
Fad = 0.5 *1.225* 693.62* 0.0265*(5.56)^2
Fad=347.58 N
Now find the total force Fte = Frr+Fad
Fte-39043.8+347.58
Fte=39391.38 N
Now Find the power require in KW
Power =all foreces *velocity
39391.38*5.56=217431.550 W =219.431 KW
Now find total torqure of truck =Total force * radius of the wheel R
39391.38*0.5715=
22512.17 Nm
Question 6 B
Simple model develop using simulin blocks
BLOCKS USED
constant blocks for input values
products blocks for multiplication
ADD blocks for ADDing.
DISPLAY for values.
Here the formulas used in above question are converted into simulink model.
Question 7
Now will calculate the the Energy
Energy = Power output*time (considering time as 30min=1800 sec)
219.431*(1800/3600)=109.71 kilo watt hour
NOw find the Duty Cycle for the truck
WE know D>C =power output/power input
(we dont know the input power of truck therfore assuming it,
Power =VOLTAGE*CURRENT=440V*600A=264000watts=264KW)
Duty cycle = 219.431/264=0.83
83% is the duty cycle of the truck.
Block DIagram of electic Vehicle Power Train(front wheel drive)
DEsign of power train in sumulink
Result of the model
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