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ELEMENT OF AERONAUTICS

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INTERCEPTORS FLIGHT CONTROL SURFACE PRIMARY GROUP AILERON ELEVATOR RUDDER ... Servo-assisted Hydraulic pressure transmitted to servo actuator which assists ... – PowerPoint PPT presentation

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Title: ELEMENT OF AERONAUTICS


1
ELEMENT OF AERONAUTICS 111305
2
PARTS OF AEROPLANE
  • THE IMPORTANT PARTS OF AN AROPLANE
  • WINGS
  • FUSELAGE
  • EMPENNAGE
  • LANDING GEARS
  • CONTROL SURFACE
  • ENGINES

3
PARTS OF AEROPLANE
4
AIRCRAFT CLASSIFICATION AND PARTS
  • 1. CLASSIFICATION BY CONFIGURATION
  • POSITION OF THE WING
  • LOW WING
  • MID WING
  • HIGH WING
  • NUMBER OF WINGS
  • MONO PLANE
  • BI PLANE
  • TRI PLANE
  • SHAPE OF THE WINGS
  • DELTA WING
  • DIAMOND WING
  • SWEPT WING
  • GULL SHAPED WING
  • POSITION OF THE WINGS
  • CONVENTIONAL WING
  • NO TAIL OR TAILESS
  • HORIZONTAL TAIL LOCATED AOVE THE VERTICAL TAIL

5
AIRCRAFT CLASSIFICATION AND PARTS
  • LOCATION AND TYPE OF LANDING GEAR
  • RETRACTABLE
  • NON RETRACTABLE
  • TAIL WHEEL
  • NOSE WHEEL

6
AIRCRAFT CLASSIFICATION AND PARTS
  • CLASSIFICATION BY POWER PLANTS
  • POWER PLANT TYPES
  • PISTON ENGINE
  • TURBO PROP
  • TURBO SHAFT
  • TURBO JET
  • TURBO FAN
  • ROCKET
  • NUMBER OF ENGINES
  • SINGLE ENGINE
  • TWO ENGINE
  • MULTI ENGINE
  • LOCATION OF THE ENGINES
  • NOSE
  • FUSELAGE
  • JET ENGINE SUBMERGED IN WING
  • PYLON MOUNTING

7
AIRCRAFT CLASSIFICATION AND PARTS
  • TYPES OF FUSELAGE
  • ROUND
  • SQUARE
  • OVAL

8
AIRCRAFT CLASSIFICATION AND PARTS
  • 5. CLASSIFICATION BY PURPOSE
  • A. CIVIL
  • B. CARGO
  • C. MILITARY
  • I. BOMBERS
  • II. FIGHTERS
  • III. INTERCEPTORS

9
FLIGHT CONTROL SURFACE
  • PRIMARY GROUP
  • AILERON
  • ELEVATOR
  • RUDDER
  • SECONDARY GROUP
  • TRIM TAB
  • SPRING TAB
  • AUXILIARY GROUP
  • WING FLAPS
  • SPOILERS
  • SPEED BRAKES
  • LEADING EDGE FLAP
  • SLOTS

10
AILERON
  • Longitudinal axis extends lengthwise from the
    nose through the tail. Movement about the
    longitudinal axis is called roll.  Roll is
    controlled by the ailerons.

11
ELEVATOR
  • Lateral axis extends crosswise from wingtip
    through wingtip. Movement about the lateral axis
    is called pitch. Pitch  is controlled by the
    elevator.

12
RUDDER
  • Vertical axis passes vertically through the
    center of gravity (when the aircraft is in level
    flight). Movement about the vertical axis is
    called yaw. Yaw is controlled by the rudder.

13
AIRCRAFT ENGINES
  • DIFFERENT TYPES OF AIRCRAFT ENGINES ARE
  • PROPELLER WITH PISTON ENGINE
  • JET ENGINE
  • TURBOPROP
  • TURBOFAN
  • TURBOJET
  • RAMJET
  • ROCKET ENGINE

14
TURBOPROP
15
PUSHER
16
TURBOFAN
17
TURBOJET
18
TURBOJET WITH AFTERBURNER
19
ROCKET ENGINE
LIQUID FUEL
SOLID FUEL
20
AIRFOIL
  • AN AIRFOIL IS A SURFACE DESIGNED TO OBTAIN A
    DESIRABLE REACTION FROM THE AIR THROUGH WHICH IT
    MOVES
  • AIRFOIL GEOMETRY
  • CHORD LINE
  • MEAN CAMBER LINE
  • ANGLE OF ATTACK
  • ANGLE OF INCIDENCE

21
FOUR FORCES OF FLIGHT
22
DRAG
  • DRAG IS THE RESOLVED COMPONENT OF THE COMPLETE
    AERODYNAMIC FORCE WHICH IS PARALLEL TO THE FLIGHT
    DIRECTION (OR RELATIVE ONCOMING AIRFLOW).
  • IT MUST ALWAYS ACT TO OPPOSE THE DIRECTION OF
    MOTION.
  • IT IS THE UNDESIRABLE COMPONENT OF THE
    AERODYNAMIC FORCE WHILE LIFT IS THE DESIRABLE
    COMPONENT

23
TYPES OF DRAG
24
DRAG POLAR
25
TOPICS TO BE COVERED
  • Why should we study properties of
  • atmosphere?
  • Variation of Temperature with Altitude
  • Variation of Pressure with Altitude
  • Variation of Density with Altitude
  • Tables of Standard Atmosphere

26
Why should we study Atmospheric Properties
  • Engineers design flight vehicles, turbine engines
    and rockets that will operate at various
    altitudes.
  • They can not design these unless the atmospheric
    characteristics are not known.
  • For example,

27
What is a standard atmosphere?
  • Weather conditions vary around the globe, from
    day to day.
  • Taking all these variations into design is
    impractical.
  • A standard atmosphere is therefore defined, that
    relates fight tests, wind tunnel tests and
    general airplane design to a common reference.
  • This common reference is called a standard
    atmosphere.

28
Powered Controls
  • May take one of two basic forms
  • Servo-assisted
  • Hydraulic pressure transmitted to servo actuator
    which assists mechanical linkage to move surface.
  • Linkage still available if power is lost but
    system then very heavy to operate.
  • Fully power-operated
  • Control signals transmitted hydraulically,
    electrically (fly-by-wire) or optically
    (fly-by-light).

29
AIRCRAFT INSTRUMENTS
30
INTRODUCTION
  • HISTORY
  • THE VERY FIRST AIRCRAFT HAD LITTLE TO NO FLIGHT
    INSTRUMENTS
  • ALL WEATHER FLYING WAS RISKY
  • NAVIGATION DEPENDED ON PILOTS ABILITY TO USE
    LANDMARKS

31
AIRCRAFT INSTRUMENTS
  • FLIGHT INSTRUMENTS
  • ENGINE INSTRUMENTS
  • NAVIGATION AND COMMUNICATION INSTRUMENTS

32
  • THE COMMON FLIGHT INSTRUMENTS
  • ALTIMETER
  • AIRSPEED INDICATOR
  • VERTICAL SPEED INDICATOR
  • HEADING INDICATOR
  • ATTITUDE INDICATOR (ARTIFICIAL HORIZON)
  • TURN COORDINATOR

33
AIRCRAFT CONSTRUCTION
34
TRUSS
35
MONOCOQUE
36
SEMI MONOCOQUE
37
THANK YOU
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