Why Use Contra-Rotating Propellers in Aircraft Design?

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Discussion Overview

The discussion revolves around the use of contra-rotating propellers in aircraft design, particularly in the context of the fictional Scorpion Gunship from the film Avatar. Participants explore the advantages and implications of this design choice, including torque cancellation and structural considerations. The conversation touches on both theoretical aspects and practical applications in aviation.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested

Main Points Raised

  • Some participants propose that the primary purpose of contra-rotating propellers is to cancel engine torque, preventing the aircraft from pulling to one side.
  • Others argue that even in symmetrical designs, the torque is canceled, suggesting there may be no advantage to using contra-rotating props.
  • A later reply suggests that contra-rotating propellers provide a larger effective disk area in a smaller package.
  • One participant notes that while counter-rotation cancels torque, it does not prevent slip or side-to-side movement, and raises concerns about yaw control in designs with only two fans.
  • Another participant questions the necessity of adding a second rotor for structural integrity, suggesting it complicates the design unnecessarily.
  • Some participants discuss potential methods for achieving yaw control, such as asymmetrically slowing down rotors or tilting rotor pods.
  • There is a technical correction regarding the effects of counter-rotation, indicating it cancels more than just spinning, including gyroscopic couplings due to angular momentum.

Areas of Agreement / Disagreement

The discussion remains unresolved, with multiple competing views on the advantages of contra-rotating propellers and their implications for aircraft design. Participants express differing opinions on the necessity and effectiveness of this design choice.

Contextual Notes

Participants express uncertainty regarding the technical aspects of yaw control and the structural implications of rotor design. Some statements reflect assumptions about the design's engineering that are not fully explored.

DaveC426913
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Upon exiting Avatar I was discussing with my biologist sister some of the flubbs in the film - she biology, me technology. I made a joke about the helicopters but now it's become a topic of discussion and I thought I'd check my facts.

I noticed while watching Avatar that the http://james-camerons-avatar.wikia.com/wiki/Scorpion_Gunship" . So, the copters have one prop pod per side AND each prop pod has two rotors (for a total of 4 rotors). The rotors in a pod rotate on the same axis but in opposite directions.

IIRC, some carrier-based craft used this prop design in WWII. Funny, Wiki doesn't pull up ones that have familair names, but here's the http://en.wikipedia.org/wiki/Fairey_Gannet" .

Anyway, it is my understanding that the primary purpose for using contra-rotating propellors is that the engine torque is cancelled, i.e. it does not pull to one side.

So, it seems to me, on a craft that is symmetrical and therefore can use two http://en.wikipedia.org/wiki/Counter-rotating_propellers" , the torque is canceled anyway, meannig there's no advantage to using contra-rotating props.
 
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:sigh: Further research (read: Wiki surfing) turns up an airplane with exactly the configuration as the Scorpions - the http://en.wikipedia.org/wiki/A2J_Super_Savage" .

So, yes, I guess there is an advantage, else they would not have built this craft at all...
 
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DaveC426913 said:
Upon exiting Avatar I was discussing with my biologist sister some of the flubbs in the film - she biology, me technology. I made a joke about the helicopters but now it's become a topic of discussion and I thought I'd check my facts.

I noticed while watching Avatar that the http://james-camerons-avatar.wikia.com/wiki/Scorpion_Gunship" . So, the copters have one prop pod per side AND each prop pod has two rotors (for a total of 4 rotors). The rotors in a pod rotate on the same axis but in opposite directions.

IIRC, some carrier-based craft used this prop design in WWII. Funny, Wiki doesn't pull up ones that have familair names, but here's the http://en.wikipedia.org/wiki/Fairey_Gannet" .

Anyway, it is my understanding that the primary purpose for using contra-rotating propellors is that the engine torque is cancelled, i.e. it does not pull to one side.

So, it seems to me, on a craft that is symmetrical and therefore can use two http://en.wikipedia.org/wiki/Counter-rotating_propellers" , the torque is canceled anyway, meannig there's no advantage to using contra-rotating props.

Yep, that's right. The real difference between the two is that a contra-rotating propeller has a larger effective disk area in a smaller package.
 
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It amuses me that this was the first thing you thought about upon leaving the film Dave. :-p

Not to bump it off topic buuuuuut, but did you feel slightly motion sick until you get used to the 3D? Saw Avatar about a week ago and, I don't know if it's becuse it was my first time watching 3D or because I wear glasses (I do need my prescription updating) but about 15 mins I felt a bit groggy.
 
xxChrisxx said:
but about 15 mins I felt a bit groggy.

Me too. I don't wear glasses and I never suffer from motion sickness, but during the first 10-15 minutes I did feel sick. I watched it in Xpand3D theater. Some of my friends who saw it later in Dolby3D told me it was a lot easier, both on the eyes and the brain.

As for the science of Avatar, the first thing I noted immediately is that the Na'vi feel somewhat out of place on Pandora when wildlife is accounted. They are anatomically too different from the rest of the animals on the planet yet they still share that LAN-kinda connector.
 
DaveC426913 said:
Anyway, it is my understanding that the primary purpose for using contra-rotating propellors is that the engine torque is cancelled, i.e. it does not pull to one side.

So, it seems to me, on a craft that is symmetrical and therefore can use two http://en.wikipedia.org/wiki/Counter-rotating_propellers" , the torque is canceled anyway, meannig there's no advantage to using contra-rotating props.
The counter rotation cancels torque which prevents the SPINNING of the aircraft, i.e. about the yaw axis. It does not prevent slip or side-to-side. Looking at the picture, if you had a single rotor on each wing and they were counter rotating, they would cancel out, but there would be some serious bending (about the vertical axis) stresses on the wings themselves. With two rotors on each pod, they cancel each other out and eliminate the bending moment on the wings.

I can't tell but it looks like they are lacking some form of yaw control. If they have just the two fans, then there is no way to yaw the aircraft without rolling as well.
 
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xxChrisxx said:
It amuses me that this was the first thing you thought about upon leaving the film Dave. :-p
Well, not the first thing. I was half kidding around. My sister was being a biology nerd, so I played the tech nerd.

xxChrisxx said:
Not to bump it off topic buuuuuut, but did you feel slightly motion sick until you get used to the 3D? Saw Avatar about a week ago and, I don't know if it's becuse it was my first time watching 3D or because I wear glasses (I do need my prescription updating) but about 15 mins I felt a bit groggy.
I did not experience any difficulties at all. I was sitting in the third row and I wear glasses too.

tomkeus said:
As for the science of Avatar, the first thing I noted immediately is that the Na'vi feel somewhat out of place on Pandora when wildlife is accounted. They are anatomically too different from the rest of the animals on the planet yet they still share that LAN-kinda connector.
Yes, this was my sister's complaint.

Elsewhere on the web, there is a hypothesis that the Na'vi are not native to Pandora. The pony-LAN is a carry-over from an ancient bio-engineering mod.

FredGarvin said:
The counter rotation cancels torque which prevents the SPINNING of the aircraft, i.e. about the yaw axis. It does not prevent slip or side-to-side.
Yes, I was being sloppy with my words.

FredGarvin said:
Looking at the picture, if you had a single rotor on each wing and they were counter rotating, they would cancel out, but there would be some serious bending (about the vertical axis) stresses on the wings themselves. With two rotors on each pod, they cancel each other out and eliminate the bending moment on the wings.
I find it implausible that they would add a whole second rotor to the design, vastly complicating its workings, for the sake of an under-engineered wing.

FredGarvin said:
I can't tell but it looks like they are lacking some form of yaw control. If they have just the two fans, then there is no way to yaw the aircraft without rolling as well.
The rotor pods pivot along a common transverse axis. Easy yaw control.
 
FredGarvin said:
I can't tell but it looks like they are lacking some form of yaw control. If they have just the two fans, then there is no way to yaw the aircraft without rolling as well.
Perhaps, asymmetrically slowing down rotors on one or both sides of the aircraft to produce net torque, while adjusting the pitch of the blades at the same time to compensate for the lost lift.
 
tomkeus said:
Perhaps, asymmetrically slowing down rotors on one or both sides of the aircraft to produce net torque, while adjusting the pitch of the blades at the same time to compensate for the lost lift.
Or just tilting the rotor pods.
 
  • #10
The only thing with the tilting pads is that there would have to be an associated change in pitch to accommodate the lower lift due to the tilting of the lift vector. Still...nice and easy.
 
  • #11
FredGarvin said:
The counter rotation cancels torque which prevents the SPINNING of the aircraft, i.e. about the yaw axis.

Errr...that's not true. It cancels out a lot more than just spinning, it cancels out all gyroscopic couplings due to angular momentum of the rotors:

[tex]M_T = [0, I_p \Omega_p r, -I_p \Omega_p q][/tex]

It does not prevent slip or side-to-side.

I don't know what this means.

With two rotors on each pod, they cancel each other out and eliminate the bending moment on the wings.

Good point!

I can't tell but it looks like they are lacking some form of yaw control. If they have just the two fans, then there is no way to yaw the aircraft without rolling as well.

Why? Adverse/proverse yaw behavior will happen contra-rotating propellers or not. Its an effect of variational freestream velocity along the span wise direction due to yaw rate.
 
  • #12
Cyrus said:
I don't know what this means.
He was interpreting my original use of the phrase "pulling to one side"; he was thinking I meant side-slip.

So: torque doesn't prevent side-slip; it prevents yaw.
 
  • #13
DaveC426913 said:
So: torque doesn't prevent side-slip; it prevents yaw.

If you have asymmetric thrust, yes. Typically, the tail fin prevents side slip by weathercocking the airplane into the wind.
 
  • #14
Cyrus said:
If you have asymmetric thrust, yes. Typically, the tail fin prevents side slip by weathercocking the airplane into the wind.
Tell that to the poor slobs trying to outmaneuver a Sopwith Camel in a hard right turn... :-p
 
  • #15
DaveC426913 said:
Tell that to the poor slobs trying to outmaneuver a Sopwith Camel in a hard right turn... :-p

That's because of gyroscopic coupling in the equation I gave earlier.
 
  • #16
Cyrus said:
That's because of gyroscopic coupling in the equation I gave earlier.

Well ... yes. But weren't you just suggesting that the tail fin will prevent this side-slip?
 
  • #17
DaveC426913 said:
Well ... yes. But weren't you just suggesting that the tail fin will prevent this side-slip?

Well, I said a tail provides weathercock stability. But I did not say that it necessarily has enough counter torque if there is a high inertia engine spinning at the nose. I made no claims about the overall aircraft performance, only the contributions of each.

Edit: Going back to your original question and tails for a moment (no pun), the size of the tail is usually design to specifically provide stability in an engine-out scenario for a twin engine aircraft.
 
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