2-Fundamentals of rotor aerodynamics 2013 [Modo … / Filipe Szolnoky Cunha Fundamentals of rotor...
Transcript of 2-Fundamentals of rotor aerodynamics 2013 [Modo … / Filipe Szolnoky Cunha Fundamentals of rotor...
Helicopters / Filipe Szolnoky CunhaSlide 1Fundamentals of rotor aerodynamics
Airplane
Helicopters / Filipe Szolnoky CunhaSlide 2Fundamentals of rotor aerodynamics
Fundamentals of rotor
aerodynamics
•The rotor provides 3 basic functions
•Generation of lift
•Generation of trust
•Control the attitude and position
Helicopters / Filipe Szolnoky CunhaSlide 3Fundamentals of rotor aerodynamics
Fundamentals of rotor
aerodynamics
Azimuth
Angle
V Forward
velocity
ψ
Ψ=0
Ψ=90Advancing
Side
Ψ=180
Retreating
SideΨ=270
Helicopters / Filipe Szolnoky CunhaSlide 4Fundamentals of rotor aerodynamics
Rotor
rotation
speed Ω
Velocity
Perpendicular
to the blade
Fundamentals of rotor
aerodynamics
Velocity in
hover
Helicopters / Filipe Szolnoky CunhaSlide 5Fundamentals of rotor aerodynamics
Fundamentals of rotor
aerodynamicsVelocity in
Forward
Flight
Helicopters / Filipe Szolnoky CunhaSlide 6Fundamentals of rotor aerodynamics
Fundamentals of rotor
aerodynamics
• Velocity distribution is not
uniform
• Generation of lift is asymmetric
Helicopters / Filipe Szolnoky CunhaSlide 7Fundamentals of rotor aerodynamics
Fundamentals of rotor
aerodynamicsTo compensate de asymmetry
• It’s necessary to change the blade AOA (lower on
the advancing side, higher on the retreating side)
Helicopters / Filipe Szolnoky CunhaSlide 8Fundamentals of rotor aerodynamics
Fundamentals of rotor
aerodynamics• To avoid high moments due to the blade on
the rotor hub the blade is allowed to flap
Helicopters / Filipe Szolnoky CunhaSlide 9Fundamentals of rotor aerodynamics
Fundamentals of rotor
aerodynamics• To allow the blades movement at constant
velocity the blade is allowed to lag
Helicopters / Filipe Szolnoky CunhaSlide 10Fundamentals of rotor aerodynamics
Fundamentals of rotor
aerodynamics• The blade can have three movements:
- Flapping (β) - Feathering (θ) - Lagging (ζ)
Helicopters / Filipe Szolnoky CunhaSlide 11Fundamentals of rotor aerodynamics
Fundamentals of rotor
aerodynamicsRotor
Helicopters / Filipe Szolnoky CunhaSlide 12Fundamentals of rotor aerodynamics
Fundamentals of rotor
aerodynamicsThis changes are cyclical->The Swashplate
Helicopters / Filipe Szolnoky CunhaSlide 13Fundamentals of rotor aerodynamics
Fundamentals of rotor
aerodynamics
The rotor Hub
Helicopters / Filipe Szolnoky CunhaSlide 14Fundamentals of rotor aerodynamics
Balancing the torque
• For each action there is an equal and opposite
reaction.
• A torque is applied to the rotor to maintain it
rotating. The rotor applies an opposite torque
to the fuselage.
• To stabilize the fuselage an anti-torque is
necessary.
Helicopters / Filipe Szolnoky CunhaSlide 15Fundamentals of rotor aerodynamics
Balancing the torque
Typical configuration: Main rotor/tail rotor
Helicopters / Filipe Szolnoky CunhaSlide 16Fundamentals of rotor aerodynamics
Balancing the torque
Typical configuration: Main rotor/tail rotor
Helicopters / Filipe Szolnoky CunhaSlide 17Fundamentals of rotor aerodynamics
Balancing the torque
Co-Axial configuration: two main rotors on the
same shaft
Helicopters / Filipe Szolnoky CunhaSlide 18Fundamentals of rotor aerodynamics
Balancing the torque
Co-Axial configuration: two main rotors on the
same shaft
Helicopters / Filipe Szolnoky CunhaSlide 19Fundamentals of rotor aerodynamics
Balancing the torque
Tandem: Two main rotors fore and aft
Helicopters / Filipe Szolnoky CunhaSlide 20Fundamentals of rotor aerodynamics
Balancing the torque
Tandem: Two main rotors fore and aft
Helicopters / Filipe Szolnoky CunhaSlide 21Fundamentals of rotor aerodynamics
Controls
• Cyclic control: cyclic stick
– Changes the main rotor tilt and therefore
changes the direction of the propulsion
Helicopters / Filipe Szolnoky CunhaSlide 22Fundamentals of rotor aerodynamics
Controls
Cyclic control :
Helicopters / Filipe Szolnoky CunhaSlide 23Fundamentals of rotor aerodynamics
Controls
Cyclic control :
Helicopters / Filipe Szolnoky CunhaSlide 24Fundamentals of rotor aerodynamics
Controls
• Collective control: collective lever, ( left side)
– The collective changes the pitch angle at the same
time and independent of the position.
Helicopters / Filipe Szolnoky CunhaSlide 25Fundamentals of rotor aerodynamics
Controls
Collective control :
Helicopters / Filipe Szolnoky CunhaSlide 26Fundamentals of rotor aerodynamics
Controls
• Yaw control: Anti-torque pedals
– Changes the tail rotor propulsion
Helicopters / Filipe Szolnoky CunhaSlide 27Fundamentals of rotor aerodynamics
Controls
Yaw control:
:
Helicopters / Filipe Szolnoky CunhaSlide 28Fundamentals of rotor aerodynamics
• Motors VS rotors?
Helicopters / Filipe Szolnoky CunhaSlide 29Fundamentals of rotor aerodynamics
Manoeuvring
What you can´t (can) do with an helicopter
Helicopters / Filipe Szolnoky CunhaSlide 30Fundamentals of rotor aerodynamics
Wake
Wake velocity
Helicopters / Filipe Szolnoky CunhaSlide 31Fundamentals of rotor aerodynamics
Fundamentals of rotor
aerodynamics
The problems are many