what is an aircraft

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What is an aircr aft? vehicle which flies by gaining support from the air in gene ral, the atmospher e of a planet counters the force of gravity by either static lift or by usi ng the dyna mic lift or downward thrust from jet engines.

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Page 1: What is an Aircraft

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What is an aircraft?

vehicle which flies by gaining support from

the air in general, the atmosphere of a planet

counters the force of gravity by either staticlift or by using the dynamic lift or downward

thrust from jet engines.

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Classification

� Lighter-than-air aircraft called Aerostats,

examples balloons and blimps.

Heavier-than-air aircrafts called Aerodynesinclude autogyros, helicopters and fixed

winged aircrafts.

� Fixed winged aircrafts use IC engines or

Turbine engine( jet or turbo prop)

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Parts of an Airframe

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� Fuselage: portion contains the crew and

payload, either passengers, cargo.

� they are long, cylindrical tubes or sometimes

rectangular box shapes.

� wing: produces the lift that allows a plane to

fly.

� The wing is made up of two halves, left and

right, connected to each other by means of 

the fuselage

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�A wing produces lift because of its special

shape, a shape called an airfoil

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Engine

� Can be classified in two major categories

� propeller-driven piston engines and jet

engines.� larger planes, have engines mounted in

separate pods hanging below the wing or

attached to the fuselage. These pods are

called nacelles.

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Turboprop engine

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� uses most of the energy from the hot exhaust

gases to drive a propeller

�  jet core produces about 15 percent of the

thrust while the propeller generates the

remaining 85 percent.

� the turboprop engine employs as large aturbine as possible, for this is its main source

of power

�more efficient than turbojets on designed tofly at speeds below about 800 km/h

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Jet engine

Schematic of a simple jet engine

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� obtains its oxidizer from the external

atmosphere

� compressed air is then mixed with fuel,

typically a petroleum-based liquid similar to

kerosene, and burned.

� The high-pressure gas is exhausted through anozzle to generate thrust.

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Horizontal stabilizer

� aircraft consisting of only a wing or a wing andfuselage is inherently unstable.

� also known as the horizontal tail, acts as astabilizer when aircraft is disturbed in pitch.

� horizontal tail is a miniature wing of an airfoilcross-section.

� produces a force pointed downward, aquantity called downforce to maintainequilibrium

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Vertical stabilizer

� functions in the same way as the horizontaltail but provides stability for a disturbance inyaw.

� if a disturbance causes the nose to deflect toone side, the vertical tail produces acounteracting force that pushes the nose inthe opposite direction to restore equilibrium.

� vertical tail produces a force pointed to oneside of the aircraft called side-force.

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Basic Control Surfaces

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Elevator

� located on the horizontal stabilizer.

� can be deflected up or down to produce achange in the downforce produced by the

horizontal tail.

� The angle of deflection is considered positivewhen the trailing edge of the elevator is

deflected upward.� the downforce produced by the horizontal tail

increases causing the nose to pitch upward.

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Rudder

� located on the vertical stabilizer.

� can be deflected to either side to produce achange in the side-force produced by the

vertical tail.

� angle of deflection is positive when thetrailing edge of the rudder is deflected

towards the right wing.� This creates a side-force to the left which

causes the nose to yaw to the right.

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Aileron

� located on the tips of each wing.

� deflected in opposite directions to produce a

change in the lift produced by each wing.� The wing with more lift rolls upward causing

the aircraft to go into a bank.

angle of deflection is positive when theaileron on the left wing deflects downward

and that on the right wing deflects upward.

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Aircraft control surfaces and positive deflection angles

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Additional Components

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� Flap: usually located along the trailing edge of 

wings, typically inboard of the ailerons and

close to the fuselage.

� only deflect downward to increase the lift

produced by both wings simultaneously.

� often used during takeoff and landing toincrease the lift the wings generate at a given

speed.

�Slats: leading-edge flaps, more often calledslats, are also used to increase lift

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� cabin & cockpit: cockpit is a compartment at

the front of the fuselage where the pilots and

flight crew sit.

� contains the control yolks (or sticks) and

equipment the crew use to send commands to

the control surfaces and engines as well as tomonitor the operation of the vehicle.

� cabin is typically a compartment within the

fuselage where passengers are seated

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� Nose & main gear:

The landing gear is used during takeoff,landing, and to taxi on the ground

� Most planes today use a tricycle landing gear

arrangement.

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Flight control systems

Consists of control surfaces, respective cockpit

controls and necessary operating mechanisms

to control the aircraft in flight.

Primary Control surfaces

Fly-by-wire

Digital Fly-by-wire

FADEC (Full Authority Digital Engine control)

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Flight Management System

It is composed of four major components

FMC (Flight Management Computers)

AFS (auto Flight Systems)Navigation system including IRS and GPS

EFIS (Electronic Flight Instrument System)

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Electrical systems

� Primary function is to generate, regulate and

distribute power throughout the system

Used to operate aircraft flight instruments,essential systems and passenger services

� Different sources of power include engine

driven AC generators and APUs (Auxiliary

Power Units)