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Uncontrolled copy not subject to amendment

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Presentation on theme: "Uncontrolled copy not subject to amendment"— Presentation transcript:

1 Uncontrolled copy not subject to amendment
Principles of Flight

2 Principles of Flight Learning Outcome 2: Understand how the stability of an aeroplane is maintained in flight and how manoeuvrability is controlled Part 2

3 Principles of Flight Revision

4 Questions What are the 3 planes of an aircraft’s movement?
a. Pitching, Lateral and Rolling. b. Pitching, Rolling and Yawing. c. Yawing, Longitudinal and Rolling. d. Longitudinal, Lateral and Normal.

5 Which one of the following will REDUCE Lateral Stability?
Questions Which one of the following will REDUCE Lateral Stability? Dihedral. A Large Fin. Sweepback. Anhedral.

6 Questions What are the 3 Axes about which an Aircraft can move?
a. Pitching, Lateral and Longitudinal. b. Pitching, Rolling and Yawing. c. Yawing, Longitudinal and Normal. d. Longitudinal, Lateral and Normal.

7 Questions Which 3 Terms describe Static Stability?
a. Stable, Neutral and Unstable. b. Stable, Rolling and Unstable. c. Yawing, Neutral and Stable. d. Neutral, Unstable and Pitching.

8 Primary Flying Controls & Trimming Devices
Objectives: List the Pilot’s Primary Flying Controls. Describe Pitching Rolling and Yawing Movements. Understand how Pitching, Yawing and Rolling are all related to the Pilot. Identify and State the Purpose of Trimming Tabs. Describe how Trimming Devices work. Explain the use of Elevators, Ailerons and Rudder.

9 We know how an aircraft flies, but how do we
Flying Controls We know how an aircraft flies, but how do we CONTROL it?

10 Flying Controls There are 3 Primary Flying Controls: Elevators
Ailerons Rudder Pitch Roll Yaw Nose Up/Down Wings One Up/One Down Nose Left/Right Note: ALL Control inputs are relative to the PILOT, regardless of the Aircraft’s Attitude or Position

11 Flying Controls Elevators Rudder Ailerons

12 Elevators Flight Path LONGITUDINAL STABILITY
longitudinal static stability the tailplane contribution must overcome the unstable wing Therefore, start with the assumption that C.G and Cp are coincident For simplicity assume stick fixed ie elevators locked

13 Elevators

14

15 Ailerons Big Fin / Diehedral / Anhedral Sweepback Wing Fuselage Interference

16 Ailerons

17

18 Rudder Flight Path DIRECTIONAL STABILITY
CofG, Stabilising, destabilising, moment arm Keel ahead/behind CofG destabilising and stabilising respectively Now on slide fin is at AOA therefore lift is generated. What about the CofP ahead of the CofG??? What about fin?

19 Rudder

20

21 Trimming We are flying straight and Level, but something changes:
We have: Increased or Decreased Speed Used our Fuel Dropped Bombs Fired Our Guns (Eaten all of the Rations!)

22 TRIM THE AIRCRAFT HOW? Trimming
Our Aircraft is now out of balance and we may be holding a “Stick Force” to fly the Aircraft. This will be tiring and prevent the pilot from carrying out other tasks such as navigation, etc. What can we do? TRIM THE AIRCRAFT HOW?

23 Trim Tabs Tabs/Explain moment arms  smaller trim tab

24 Trim Tabs Tabs/Explain moment arms  smaller trim tab

25 Trim Tabs Pull Force Stick Force Remains + + + + +
Tabs/Explain moment arms  smaller trim tab Pull Force + + + + + Stick Force Remains

26 Trim Tabs Larger Moment Arm Pull Force Stick Force Removed
+ Tabs/Explain moment arms  smaller trim tab Pull Force + + + + + Stick Force Removed Stick Force Remains

27 Trim Tabs TO CONTROL COLUMN FIXED TAB Fixed tabs/Examples

28 To reduce the pilot’s physical workload
Fixed Tabs To reduce the pilot’s physical workload Fixed tabs/Examples

29 Can be adjusted in the air
Trim Tabs TO TRIM WHEEL TO CONTROL COLUMN TRIM TAB Various ways of achieving tab balance Can be adjusted in the air

30 To reduce the pilot’s physical workload
Trim Tabs To reduce the pilot’s physical workload Various ways of achieving tab balance

31 To reduce the pilot’s physical workload
Trim Tabs To reduce the pilot’s physical workload Various ways of achieving tab balance

32 Aerodynamic Balancing - Tabs
Geared tab GEARED TAB

33 REMEMBER: Trim Tabs Trim Tabs “Work” in the Natural Sense ie
If you are pulling back on the control column to control the aircraft, then you TRIM BACK on the trimmer.

34 Any Questions?

35 Primary Flying Controls & Trimming Devices
Objectives: List the Pilot’s Primary Flying Controls. Describe Pitching Rolling and Yawing Movements. Understand how Pitching, Yawing and Rolling are all related to the Pilot. Identify and State the Purpose of Trimming Tabs. Describe how Trimming Devices work. Explain the use of Elevators, Ailerons and Rudder.

36 Which surfaces control an aircraft in the Rolling Plane?
Questions Which surfaces control an aircraft in the Rolling Plane? Elevators. Ailerons. Rudder. Tabs.

37 How do we “Pitch” an Aircraft?
Questions How do we “Pitch” an Aircraft? By using: Elevators. Ailerons. Rudder. Tabs.

38 What may cause an imbalance in Roll?
Questions What may cause an imbalance in Roll? Tyre Pressures uneven. Rudder Not Central. Wing Fuel Imbalance. A heavy co-pilot!

39 Questions On an aircraft with 2 wing mounted engines,
which control would be used to keep straight if one engine failed? Elevators. Ailerons Rudder Tabs

40

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