Simple Question to do with TORQUE on a helicopter

In summary, the conversation discussed the force and torque applied to helicopter blades from the pivot point, where the force is actually transferred through a cylindrical shaft. The blades create an equal and opposite torque on the shaft, and for the purposes of analysis, the rotor can be treated like the spokes on a rigid wheel. Some helicopters have a lead-lag hinge in the blades, but this does not affect the overall torque on the shaft.
  • #1
06mangro
20
0

Homework Statement



If the force pushing the helicopter blades from the pivot point surely r is 0... therefore T (torque) is 0 also...

Homework Equations


r is the Length from pivot point to force
F is force
τ= r × F ×sin(θ)

The Attempt at a Solution

 
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  • #2
welcome to pf!

hi 06mangro! welcome to pf! :smile:
If the force pushing the helicopter blades from the pivot point surely r is 0... therefore T (torque) is 0 also...

ah, but the force actually comes from the outside of a shaft …

so r is the radius of that shaft :wink:
 
  • #3


tiny-tim said:
hi 06mangro! welcome to pf! :smile:ah, but the force actually comes from the outside of a shaft …

so r is the radius of that shaft :wink:

would it be possible to elaborate on what you mean... and where this shaft would be on the chopper
 
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  • #4
i'm not knowledgeable on helicopter construction,

but clearly the engine is attached to a cylindrical shaft that goes up to the centre of the blades …

exactly like the axle going to the centre of a wheel​

the outside of the shaft turns the blades, in the same way that the outside of the axle turns the wheel
 
  • #5
thank you very much :)
 
  • #6
one more thing...
so does that mean the blades do not create torque...
only the shaft does?

or does it mean that that the torque is transferred into the blades in a sense...?
 
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  • #7
06mangro said:
one more thing...
so does that mean the blades do not create torque...
only the shaft does?

the shaft creates a torque on the blades

by good ol' Newton's third law, there's an equal and opposite reaction …

the blades create an equal and opposite torque on the shaft :wink:
 
  • #8
For your purposes you can probably treat the rotor like the spokes on a rigid wheel.

The blades on some helicopters are (in effect) rigidly connected to the shaft. Others have a lead-lag hinge that allows the blade to swing back and forth (normally only a little) for quite technical reasons.

Even if it had a big floppy hinge the hinge is outboard from the shaft so it's a bit like swinging buckets around your head. Having a hinged handle on the bucket isn't a problem.
 

1. What is torque on a helicopter?

Torque on a helicopter is the force that causes the helicopter to rotate around its axis. It is created by the rotation of the helicopter's main rotor blades and is counteracted by the tail rotor to keep the helicopter stable.

2. How does torque affect a helicopter's flight?

Torque can affect a helicopter's flight by causing it to rotate in the opposite direction of the main rotor's rotation. This can affect the helicopter's stability and require constant adjustments from the pilot to maintain control.

3. How is torque controlled on a helicopter?

Torque is controlled on a helicopter through the use of a tail rotor. The tail rotor produces a force in the opposite direction of the main rotor's rotation, which helps to counteract the torque and keep the helicopter stable.

4. What are some factors that can affect torque on a helicopter?

Some factors that can affect torque on a helicopter include the weight distribution of the aircraft, the size and speed of the main rotor, and external forces such as wind.

5. How do helicopter pilots compensate for torque?

Helicopter pilots compensate for torque by using the helicopter's controls to adjust the tail rotor's angle and power. They may also use other techniques such as tilting the main rotor blades or adjusting the collective pitch to help counteract the torque.

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