Fuselage, Wings, Empennage or Tail, Powerplant, Landing Gear
Components of an aircraft
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Fuselage
The main body of an airplane
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Wings
Airfoils attached to each side of the fuselage
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Empennage
Known as the tail section
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Vertical Stabilizer, Rudder, Horizontal Stabilizer, Elevator
Empennage is consisted of
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Powerplant
The heart of the aircraft
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Powerplant
A unit or machine that converts chemical energy contains in the fuel to thrust force
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Thrust Force
Essential for moving the airplane forward and producing lift force.
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Propeller
With the piston engine it is used to convert torque at engine shaft to be thrust.
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Jet engine Output
It is the thrust force in the jet engine.
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Landing Gear
Located underneath of the fuselage with shock strut
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High strength to weight ratio
Light weight
Corrosion resistant
Should be non-flammable
High-quality
Airframe materials properties
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Composite material
Most used material now in airframe construction
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Wood
Steel & its alloys
Aluminum & its alloys
Titanium alloys
Magnesium alloys
Plastics and composite materials
Example of materials used in airframe construction
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Truss Type
Monocoque
Semi-monocoque
Basic Fuselage Structure Types
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Pratt Truss
Warren Truss
Two types of truss structure
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Truss Type
Most early aircraft used this technique with wood and wire trusses and this type of structure is still used in many lightweight aircraft using welded steel tube trusses.
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Monocoque
In this method, the exterior surface of the fuselage is also the primary structure.
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Semi-monocoque
This is the preferred method of constructing an all aluminum fuselage.
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Formers
Frame
Ring
Bulkhead
The basic structure vertical members
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Longerons
Stringers
The basic structure longitudinal members
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Semi-cantilever
Type of wing structure where the wing struts are usually attached approximately halfway out on the wing
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Spars
Ribs
Stringers
The principal structural parts of the wing
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Wing ribs
Determine the shape and thickness of the wing (airfoil)
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Fuel tanks
They are either an integral part of the wing structure or consist of flexible containers mounted inside of the wing in most modern airplanes
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Ailerons
Flaps
Two types of control surfaces attached to the rear or trailing edges of the wings
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Ailerons
Extend from about the midpoint of each wing outward toward the tip and move in opposite directions to create aerodynamic forces that causes the airplane to roll
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Flaps
Extend outward from the fuselage to near the midpoint of each and move simultaneously downward to increase the lifting force of the wing for takeoffs and landings
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Empennage
The correct name for the tail section of an airplane
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Rudder
Elevator
One or more trim tabs
The movable surfaces include
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Stabilator
Incorporates a one-piece horizontal stabilizer that pivots from a central hinge point and is moved using the control stick
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Rudder
Attached to the back of the vertical stabilizer and is used to move the airplane’s nose left and right
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Elevator
Attached at the back of the horizontal stabilizer, and is used to move the nose of the airplane up and down during flight
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Trim tabs
Small, movable portions of the trailing edge of the control surface
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Landing Gear
The principle support of the airplane when parked, taxiing, taking off, or when landing
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Convential landing gear
Landing gear employing a nearmounted wheel
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Tail wheel airplanes
Referred to airplanes with conventional landing gear
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Nose wheel
When the third wheel is located on the nose
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Tricycle gear
The design of the nose wheel
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Steerable nose wheel or tail wheel
Permits the airplane to be controlled throughout all operations while on the ground
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Powerplant
Includes both the engine and the propeller
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Engine
Its primary function is to provide power to turn the propeller
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Cowling or Nacelle
The purpose is to streamline the flow of air around the engine and to help cool the engine by ducting air around the cylinders
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Propeller
Mounted on the front of the engine, translates the rotating force of the engine into a forward acting force called thrust that helps move the airplane through the air.
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Wing Pod Mount
Commonly use on commercial airplane since fuel is carry on wing
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Fuselage Mount
Has no ground clearance limitation
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1. Long live 2. Repairable / Less maintenance 3. Requirement for graceful degradation
Spacecraft operational characteristics
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Payload fairing
Payload / Spacecraft
Payload adaptor
Stage structure
Thrust structure
Typical spacecraft structures
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Strutted structure
Central cylindrical shell structures
Two categories of spacecraft structures
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Payload fairing
It protects the payload; the frontliner
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Heat engine
Converts chemical energy into heat energy
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Reciprocating engine
A type of heat engine that derives its name from back-and-forth
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Sputnik I
The first satellite that operated until January 3, 1958.
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October 4, 1957
When did Sputnik I first operated?
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Opposed engine
Most popular reciprocating engine used on light aircraft, 36 hp to 400 hp, has even number of cylinders, high power-to-weight ratios and vibrates less than other engines.
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In-line engines
Has an even number of cylinders, aligned in a single row parallel with the crankshaft, liquid-cooled or air-cooled, small frontal area and allows for better streamlining least drag, and limited to four or six cylinders.
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V Type engines
Arranged around a single crankshaft in two in-line banks that are 45, 60, 90 degrees apart; had two rows of cylinders, and 8 or 12 cylinders
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Radial engines
Consists of a row or rows; greatest drag, lowest weight for horsepower ratios and problems in cooling.
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Pratt and Whitney R-4360
The largest multiple-row radial engines
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Crankcase
The foundation of reciprocating engine
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Cylinders
The powerhouse of the engine/ head and barrel
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Pistons
Cylindrical plunger / 4000 F
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Connecting rods
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Valves
Regulates the flow of gases
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Poppet valve
The most common valve.
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In-Line and V
Opposed
Radial
Types of engine crankcases
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Spark plugs
Ignites air fuel mixtures
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Piston Head
Ring Grooves
Ring Land
Piston Pin Boss
Piston Skirt
Piston parts
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Plain Type
Master and Articulated
Fork and Blade
Types of connecting rods
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Crankshaft
The backbone of a reciprocating engine
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Valve Operating Mechanism
Consists of a cam ring or camshaft equipped with lobes that work against a cam roller or a cam follower.
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Gas turbine engine (turbo jet)
Sucks in air and compresses or squeezes it. The gases flow through the turbine and make it spin. These gases bounce back and shoot out of the rear of the exhaust, pushing the plane forward.
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External Combustion Engine
Internal Combustion Engine
Types of combustion engine
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Reciprocating engine
Jet engines
Types of internal combustion engine
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Aeolipile
Was invented by Hero, a mathematician in 250 BC.
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Dr. Sanford Moss (1900)
Engr. for the General Electri Company who invented turbosupercharger
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Sir Frank Whittle
A Royal Airforce Officer and is considered the father of Jet Propulsion. He received the first patent for the Jet Engine (1930)
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Hans Von Ohain
The designer of the first operational turbojet engine, a German Engr., Physicist, and Aerodynamicist
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Heinkel He-178 Aircraft
World’s first aircraft to fly using the thrust from a turbojet engine. August 27, 1939 was the first successful flight
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Jet Propulsion
Propelling force generated in the direction opposite to the flow of mass of gas or liquid under the pressure which is escaping through a hole or opening called jet nozzle.
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* Increase the speed of exhaust gases * Increase the quantity of exhaust gases
Two ways on how to increase jet engine thrust
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* Air density * Air speed * Air Temperature * Air Pressure * RAM Pressure
Environmental factors affecting thrust
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* Non-air breathing ( closed) * Air breathing (open)