DCO11611 Aviation Operations - PowerPoint PPT Presentation

1 / 48
About This Presentation
Title:

DCO11611 Aviation Operations

Description:

1783 First manned flight in history hot air balloon rose near Paris. 1881 Two German brothers 'flew' with a heavier-than-air machine glider from a hill ... – PowerPoint PPT presentation

Number of Views:188
Avg rating:3.0/5.0
Slides: 49
Provided by: cityuniv
Category:

less

Transcript and Presenter's Notes

Title: DCO11611 Aviation Operations


1
DCO11611Aviation Operations
2
Dr. Joseph Chan email dcjcchan_at_cityu.edu.hk
http//personal.cityu.edu.hk/dcjcchanOffice
P6821 Main Campus Phone 2788-8207
3
Consultation Hours (at Telford)Monday 330
430 pmTuesday 230 330 pm During these
hours you can call me at phone 2707-9086and I
can meet you at the counter
4
Assessments Final Exam 70 Course Work
30 Mid-term Quiz Lab Exercises
5
What is this Course About?
  • The basic structures and functions of airplane
    components
  • The aerodynamics of flying
  • Equipments of a modern plane
  • Navigation and communications processes
  • Flight regulations and laws
  • Meteorology that affects safe flying
  • Human physiology and psychology that affects safe
    flying
  • Similar to Private Pilot License (PPL) Exam

6
Cathay Pacific Aircadets Training Program
  • Structures of airplanes
  • Aerodynamics
  • Principles of aviation wireless communication
  • Aviation Navigation
  • Aviation Meteorology
  • Principles of Aviation Planning
  • (Australian) Aviation Laws and Regulations
  • Aviation Physiology

7
My academic background
  • BSc., M.Sc. and Ph.D. Candidacy in Physics
  • M.Engr. in Electrical and Computer Engineering
  • Ph.D. in Neuroscience (Physiological Psychology)

8
Flight Training Programs in HK
  • Cathay Aircadets Training Program
  • www.aircadets.org.hk/plttrg_e.html
  • Hong Kong Aviation Club
  • http//www.hkaviationclub.com.hk/
  • Dragonair
  • http//www.dragonair.com/icms/servlet/template?ser
    ies59langbig5

9
Textbooks for the course
  • Jeppesen. Private Pilot Manual. Sanderson
    Training Products.
  • (Manual for PPL License Exam, but expensive
    U.S. 80).
  • Kroes and Rardon. Aircraft Basic Science (7th
    ed.). McGraw-Hill International Edition. 1993.
  • (Good for the fundamental principles)

10
  • Lecture 1
  • Jeppesen. Chapters 1, 2

11
Human efforts to try to fly Milestones (1)
  • 1783 First manned flight in history hot air
    balloon rose near Paris
  • 1881 Two German brothers flew with a
    heavier-than-air machine glider from a
    hill
  • 1903 Wright brothers achieved the first
    powered, sustained and controlled airplane
    flight in U.S.
  • 1927 First trans-continental flight from New
    York to Paris in 33 hours, 30 minutes and
    29.8 seconds
  • 1932 First woman to pilot an airplane solo
    across the Atlantic Ocean

12
Human efforts to try to fly Milestones (2)
  • 1939 First turbojet in the world in Germany
  • 1942 First turbojet in the U.S.
  • 1947 First super-sonic flight 700 mph at
    42,000 feet
  • 1961 First manned spaceship from Russia
  • 1969 First man on the moon
  • 1986 First non-stop-without-refueling flight
    around the world. Took 9 days, 3 minutes,
    and 44 seconds. The 7,011.5 pounds of fuel was
    72.3 of the airplanes gross weight
  • 2003 Chinas first manned spaceship

13
Basic components of airplane
  • All planes basically have the same structural
    components
  • Fuselage
  • Wings
  • Power plant
  • Landing gear
  • Empennage

14
Basic components of airplane
15
Basic Components of Airplane
16
The fuselage
  • Cockpit control of the plane
  • Cabin contains seats of passengers
  • Room for cargo
  • Attachment points for other major airplane
    components
  • Fuselage in early planes used open truss
    structure. Modern planes uses stressed skin,
    known as
  • monocogue no supporting truss, for light planes
  • semi-monocoque - has truss members for support

17
The fuselage Fig 2-3 Open Truss
18
The fuselage Fig 2-4 Semi-monocoque
19
The Wings
  • When air flows around the wings of a plane it
    generates a lifting force
  • Wing are designed to maximize this lift
  • Monoplanes have one set of wings. Biplanes have
    two sets. Fig 2-4
  • Monoplanes wings can be attached to the top of
    the fuselage (high-wing), to the middle
    (mid-wing), or the lower portion (low-wing).

20
Monoplane and Biplanes Fig 2-4
21
The Wings
  • Attached to the rear edge of each wing are two
    types of control surfaces called aileron and flap
    respectfully
  • Ailerons extend from about the mid-point of the
    wings to near the tips.
  • Ailerons of the two wings moves up and down in
    opposite directions to create aerodynamic forces
    that cause the plane to turn.
  • When the wheel is turned left the left aileron
    moves up and the right moves down. The plane
    then turns left.

22
The Wings
  • The flap extends from the side of the fuselage to
    about the mid-point of each wing.
  • In normal flight the flap is parallel to the
    surface of the wings surface.
  • The flaps move simultaneously downwards to
    increase the lifting force of the wings during
    takeoffs and landing.
  • Flaps are controlled by a switch or a handle in
    the cockpit.

23
The Empennage
  • The empennage is the tail of the plane. It
    consists of the horizontal stabilizer and the
    vertical stabilizer, (the vertical stabilizer is
    also referred to as the fin).
  • These two stabilizers help the plane to maintain
    a straight path through the air
  • The empennage also consists of the rudder which
    is attached to the back of the vertical
    stabilizer
  • Also, an elevator is attached to the back of the
    horizontal stabilizer (Fig 2-7)

24
The Empennage Fig 2-7
25
The Empennage - Rudder
  • The rudder helps to move the nose of the plane to
    left or right
  • It is used together with the ailerons to turn the
    plane
  • The rudder is controlled by the pilots feet with
    pedals. The left pedal moves the rudder to the
    left and helps turn the plane to the left. The
    right pedal turns the plane to the right.

26
The Empennage - Elevator
  • An elevator is attached to the back of the
    horizontal stabilizer
  • The elevator is used to move the planes nose up
    and down during flight, directing the plane to go
    higher or lower
  • The elevator is controlled by the wheel. When
    the pilot pulls the wheel back, the elevator and
    the nose move up. When the pilot pushes the
    wheel down, the elevator and the nose move down.

27
The Empennage - Stabilator
  • Some planes combine the horizontal stabilizer and
    the elevators into one piece called the
    stabilator.
  • The stabilator is hinged up and down at a center
    point.
  • When the control wheel is pulled back, the
    stabilator and the nose move up. When the wheel
    is pushed down, the stabilator and the nose move
    down.

28
The Empennage Trim Devices
  • Some planes use small pieces of surfaces attached
    to the control surfaces mentioned above. These
    are generally called trim devices. (Fig 2-10)
  • Trim devices exploit aerodynamic force of the air
    to adjust the workload needed to move the other
    control surfaces or to maintain those surfaces at
    a desired position.

29
Trim Devices Fig 2-10
30
The Empennage Trim Devices
  • An example of trim devices is the trim tab which
    is attached at the tail edge of the elevator and
    is commonly used in many training planes. It
    lessens the air resistance the pilot feels when
    moving the elevator.
  • Another example is the trim used in a stabilator
    to provide more resistant feel so that the
    control feels more like that of an elevator.

31
Landing Gear
  • The landing gear absorbs the shock upon landing
    and supports the plane on the ground.
  • Typically the landing gear consists of three
    wheels two main wheels on either side of the
    fuselage, and a third wheel either at the front
    or at the rear. Landing gear using a rear wheel
    is called a conventional landing gear and a plane
    using conventional landing gear is called a
    tailwheel airplane. (Fig 2-11)

32
Tailwheel airplane 2-11
33
Landing Gear - Nosewheel
  • When the third wheel is located at the front it
    is called a nosewheel. Most modern plane uses
    this design. (Fig 2-12)
  • Nosewheels are either steerable or castering.
  • Steerable nosewheels are connected to the rudder
    through cables and rods while castering
    nosewheels are not.

34
Nosewheel airplane 2-12
35
Landing Gear - nosewheels
  • The pilot steers the plane using the rudder
    pedals in both types of nosewheels.
  • If the nosewheel is of the steerable type,
    pushing the left rudder forward will turn that
    wheel to the left, thus turning the plane left
    while taxiing
  • If the nosewheel is of the castering type the
    pilot may have to combine the use of the rudder
    pedals with independent use of the brakes
    (pushing the rudder downwards) on the main
    wheels, particularly on tight turns.

36
Landing Gear Fixed or Retractable
  • Landing gears can be classified as either fixed
    or retractable depending whether the landing gear
    can be retracted or not.
  • Fixed gear always remains extended.
  • The advantage is simplicity and low cost.
  • The disadvantage is having more air resistance.
  • Retractable gear is designed to streamline the
    airplane to reduce friction.
  • The disadvantage is increased weight and cost.
    It is normally used only in high performance
    planes.

37
Landing Gear Water Operation
  • Long time ago, before runways were available,
    planes took off and descended over water.
  • Nowadays many landplanes are still fitted with
    twin floats that support them on water for use in
    remote areas where runways or even long strip of
    land are not available. These type of airplanes
    are referred to as seaplanes.

38
Landing Gear Water Operation
  • Some airplanes can be operated both on land and
    on sea, and are called an amphibian.
  • Amphibian planes have the fuselage designed like
    a boat, with floats attached to the wings to
    increase support during water operations. They
    use retractable wheels for land operations.

39
Landing Gear Struts
  • The wheels are attached to the fuselage through
    struts, which reduce the sudden shocks during
    landing or taxiing on rough grounds.
  • Spring steel and bungee struts do not actually
    absorb shocks but reduce their suddenness. (Fig.
    2-14)
  • Most planes nowadays use oleo struts which are
    true shock absorbers.
  • An oleo strut uses a piston enclosed in a
    cylinder with oil and compressed air to absorb
    the shock. (Fig. 2-15)

40
Struts spring steel bungee (2-14)
41
Struts Oleo absorber (2-15)
42
Brakes
  • Typical training planes use disc brakes on the
    main wheels
  • Equal pressure can be applied to the two brakes
    simultaneously by pressing (downwards) equally on
    the top of each rudder pedal, in order to slow
    down the plane in a straight line.
  • The brakes can also be applied to varying degrees
    independent of each other. This would help steer
    the plane during ground operation. This
    technique is called differential braking.

43
The Powerplant
  • In small planes the powerplant consists of the
    engine and the propeller.
  • The engine provides the power to turn the
    propeller, which in turn, provides the thrust to
    move the plane through the air.
  • The engine is enclosed by a cowling, which, in
    addition to provide streamlining for the nose,
    helps cool the engine by ducting outside air
    around the engine cylinders. (Fig. 2-18)

44
A cowling (opening) is seen behind the propeller
(2-18)
45
POH, AFM, and PIM
  • Most of the pertinent information about a
    particular plane in contained by the Pilots
    Operation Handbook (POH) provided by the planes
    manufacturer. The format of POH for all planes
    are standardized.
  • The Federal Aviation Administration (FAA)
    requires that all planes built after March 1,
    1979 be equipped with an FAA approved airplane
    flight manual (AFM) which is specifically
    assigned to the individual airplane.
  • The FAA requires that the AFM for each plane be
    accessible by the pilot all the time when
    operating that plane.

46
POH, AFM, and PIM
  • To compile with the FAAs requirement
    manufacturers then write their POH just like the
    AFM.
  • The POH/AFM has to stay with the plane all the
    time during operation and is therefore not
    available to others to review for a lengthy
    period of time. As a result the manufacturer
    also publish a pilots information manual (PIM).
  • The PIM contains the same information as the
    POH/AFM except for precise weight and balance
    data and optional equipment specific to the
    particular plane.

47
Contents of AFM 10 Sections
  • General basic information terminology
  • Limitations includes operating limitations
  • Emergency procedures
  • Normal procedures
  • Performance
  • Weight and balance
  • Airplane and system description
  • Handling, Service and maintenance
  • Supplements
  • Safety and operational tips

48
Summary
  • An airplane generally contains the following
  • Fuselage
  • Wings
  • Empennage
  • Landing gear
  • Powerplant
  • Airplane flight manual (AFM)
Write a Comment
User Comments (0)
About PowerShow.com