SlideShare a Scribd company logo
Principles of Flight Chapter 6 – Helicopters
Introduction A helicopter generates both lift and thrust by using its rotor blades rather than wings. Blades are just wings which spin round on a central axis.
Lift To generate more lift the blades must be pitched to increase the angle of attack. Pilots control known  as the Collective  pitch control.
Horizontal Flight The thrust is provided by tilting the disc in the direction required Pilots control called cyclic pitch control or stick.
Horizontal Flight The thrust is provided by tilting the disc in the direction required Pilots control called cyclic pitch control or stick.
Horizontal Flight The thrust is provided by tilting the disc in the direction required Pilots control called cyclic pitch control or stick.
Horizontal Flight The thrust is provided by tilting the disc in the direction required Pilots control called cyclic pitch control or stick.
Torque Reaction Is the force that tries to make the fuselage spin in the same direction as the blades. Counteracted by using a tail rotor to push the fuselage in the opposite direction. By altering the pitch of the tail rotor blades it can yaw the aircraft. Helicopters with 2 blades – each rotor spins in different directions.
Torque Reaction
Torque Reaction
Controls 4 Controls Collective Pitch – On left hand side, pulls up to increase lift and vice versa. Hand Throttle – On the collective pitch stick, twists to give more power to rotor. Cyclic Pitch – Stick between legs, left to go left, forward to go forward etc. Tail Rotor - Feet Pedals, Right to yaw right and vice versa.

More Related Content

PPT
Basic aerodynamics
PPT
Principles of flight_chapter_3
PPT
Principles Of Flight
PPT
Flight Basics
PPT
Flight basics
PPT
Project Aeroplane (Short Review)
PPTX
Basic Aerodynamics.Ppt
DOCX
Aerodynamic design of aeroplane
Basic aerodynamics
Principles of flight_chapter_3
Principles Of Flight
Flight Basics
Flight basics
Project Aeroplane (Short Review)
Basic Aerodynamics.Ppt
Aerodynamic design of aeroplane

What's hot (19)

PDF
Basics of airplanes
PPTX
EASA PART-66 MODULE 8.4 : FLIGHT STABILITY AND DYNAMICS
PDF
Aerodynamics of a_rotary_wing_type_aircraft
PPT
A basic introduction to aerodynamics
PPT
Aircraft basics
PPT
Basic Aerodynamics and Flight Controls
PPTX
EASA PART-66 MODULE 8.3 : THEORY OF FLIGHT
PPT
Why airplanes fly aerodynamics
PPT
Advanced Aerodynamics
ODT
MOTION IN AIRCRAFTS
PPTX
Aerodynamics flight force
PPT
Aerodynamics slide
PPT
Basics of Flight and Aerodynamics (Groups B/D)
PPTX
Hands on experience with primary control surfaces
PPTX
How does a plane fly?
PPT
Aerodynamic theories
PPTX
The complex and dynamic theory of flight
PPTX
flight control surfaces
PPT
Basic aircraft control system
Basics of airplanes
EASA PART-66 MODULE 8.4 : FLIGHT STABILITY AND DYNAMICS
Aerodynamics of a_rotary_wing_type_aircraft
A basic introduction to aerodynamics
Aircraft basics
Basic Aerodynamics and Flight Controls
EASA PART-66 MODULE 8.3 : THEORY OF FLIGHT
Why airplanes fly aerodynamics
Advanced Aerodynamics
MOTION IN AIRCRAFTS
Aerodynamics flight force
Aerodynamics slide
Basics of Flight and Aerodynamics (Groups B/D)
Hands on experience with primary control surfaces
How does a plane fly?
Aerodynamic theories
The complex and dynamic theory of flight
flight control surfaces
Basic aircraft control system
Ad

Viewers also liked (20)

PDF
Principles of flight
PPT
Po f lo5 p1
PPT
Principles of flight_chapter_4
PPT
Principles of flight_chapter_1
PPT
Principles of flight_chapter_2
PPT
Principles of flight_chapter_5
PPT
Basic Aerodynamics Ii Stability Large
PPTX
Forces acting in an airplane edwin pitty s.
PPT
Basic Aerodynamics To Stability
DOCX
Stability
PPTX
PDF
Aerodynamics Chapter 4
PPTX
Cg location
PPT
Introduction to flight 1
PDF
3 longitudinal static stability 6
PPTX
Magnetic flux
PPTX
Fixed wing aircrafts
PPT
Subsonic Airplane Design
PDF
Star review jeopardy final 4 25-11
PPT
Conning
Principles of flight
Po f lo5 p1
Principles of flight_chapter_4
Principles of flight_chapter_1
Principles of flight_chapter_2
Principles of flight_chapter_5
Basic Aerodynamics Ii Stability Large
Forces acting in an airplane edwin pitty s.
Basic Aerodynamics To Stability
Stability
Aerodynamics Chapter 4
Cg location
Introduction to flight 1
3 longitudinal static stability 6
Magnetic flux
Fixed wing aircrafts
Subsonic Airplane Design
Star review jeopardy final 4 25-11
Conning
Ad

Similar to Principles of flight_chapter_6 (20)

PPTX
Flight controls translift
PPT
直升机飞行力学 Helicopter dynamics chapter 2
DOCX
How Helicopter work
PPT
Physics Presentation Final
PPTX
Intro to helicopters translift
DOCX
Rotorcraft (11 16 09)
PPTX
helicopter dynamics
KEY
Physics Presentation Final 1
PPT
Helicopter_Presentation.ppt
PPT
直升机飞行力学 Helicopter dynamics chapter 1
DOCX
Flight Conditions
PPTX
BSS AEROdynamics lecture including helicopter
PDF
Apache Helicopter
PPT
Robinson Helicopter Private Lesson 1
PPTX
How helicopters fly
PPTX
Rc helicopter
PPTX
Helicopters
DOC
helicopter-aerodynamics
PDF
Quadcopter Dynamics, Stability and Control
PPT
Helecopter
Flight controls translift
直升机飞行力学 Helicopter dynamics chapter 2
How Helicopter work
Physics Presentation Final
Intro to helicopters translift
Rotorcraft (11 16 09)
helicopter dynamics
Physics Presentation Final 1
Helicopter_Presentation.ppt
直升机飞行力学 Helicopter dynamics chapter 1
Flight Conditions
BSS AEROdynamics lecture including helicopter
Apache Helicopter
Robinson Helicopter Private Lesson 1
How helicopters fly
Rc helicopter
Helicopters
helicopter-aerodynamics
Quadcopter Dynamics, Stability and Control
Helecopter

Principles of flight_chapter_6

  • 1. Principles of Flight Chapter 6 – Helicopters
  • 2. Introduction A helicopter generates both lift and thrust by using its rotor blades rather than wings. Blades are just wings which spin round on a central axis.
  • 3. Lift To generate more lift the blades must be pitched to increase the angle of attack. Pilots control known as the Collective pitch control.
  • 4. Horizontal Flight The thrust is provided by tilting the disc in the direction required Pilots control called cyclic pitch control or stick.
  • 5. Horizontal Flight The thrust is provided by tilting the disc in the direction required Pilots control called cyclic pitch control or stick.
  • 6. Horizontal Flight The thrust is provided by tilting the disc in the direction required Pilots control called cyclic pitch control or stick.
  • 7. Horizontal Flight The thrust is provided by tilting the disc in the direction required Pilots control called cyclic pitch control or stick.
  • 8. Torque Reaction Is the force that tries to make the fuselage spin in the same direction as the blades. Counteracted by using a tail rotor to push the fuselage in the opposite direction. By altering the pitch of the tail rotor blades it can yaw the aircraft. Helicopters with 2 blades – each rotor spins in different directions.
  • 11. Controls 4 Controls Collective Pitch – On left hand side, pulls up to increase lift and vice versa. Hand Throttle – On the collective pitch stick, twists to give more power to rotor. Cyclic Pitch – Stick between legs, left to go left, forward to go forward etc. Tail Rotor - Feet Pedals, Right to yaw right and vice versa.