STEM Aviation Lesson 2-3: Helicopter Flight Controls and Surfaces
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- čas přidán 8. 06. 2024
- As a helicopter is a very different type of flying machine, this lesson examines the forces (and torques) inherent in flying. It also discusses how the unwanted torque is balanced by a counter-torque system and how the main rotor provides for both vertical and horizontal motion. Basic helicopter control mechanisms are also introduced.
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This video really needs to cover the phase lag aspect pf the rotor assembly. Because of the gyroscopic effect, a pitch change in the cyclic produces a force that occurs 90° later in the rotation. If you wanted to tilt the rotors forward, you would move the cyclic forward but the blades would pitch up 90° before the rear or 6 O'clock position (pitch up occurs at the 9 O'clock position or left side relative to the pilot). This causes the rotors to tilt up at the 6 O'clock position or 90° after the pitch change occurs. This may cause confusion as it isn't very intuitive, but it's still a critical aspect for flight in a rotary wing aircraft.
Awesome explanation and graphics
This is not 100% accurate. Because of the phase lag of the rotor blade.
Thank you a lot
Excellent. I love being in a chopper but I'd never want to fly one (maybe, okay, if I was 20 and had faster reaction time and more coordination. My math would stop me cold, however.)
Thank you bro
Damn!! now i wanna build one😅😅...
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ought to use 3-dimensional illustrations