Why are we not seeing more variable-pitch quadcopters?

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The discussion centers on the efficiency of variable-pitch propellers for quadcopters compared to conventional constant-speed propellers. It concludes that while variable-pitch propellers can enhance efficiency by reducing air-drag at low RPMs, they face significant mechanical challenges, particularly slow response times and added complexity. Current electronic speed controllers (ESCs) operate at 400Hz, while mechanical systems struggle to achieve the necessary responsiveness. The conversation highlights that while some variable-pitch quadcopters are in development, widespread adoption is hindered by cost, complexity, and mechanical limitations.

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Jarfi
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Been doing some research on propeller-pitch. And it seems that a variable-pitch-propeller seems superior, with a constant-speed-propeller(adjusting pitch for constant RPM) seems the most efficient of all.

A quadcopter with a low RPM will generally spend less energy on air-drag so we have more efficiency. The problem is once you accelerate the RPM increases and efficiency is lost due to airdrag, similar to a car in a low gear driving fast, causing a too high RPM of the engine itself, which wastes energy.

I've seen a few variable pitch-quads, most seem to be in the development stage, there are even petrolium variable-quads being researched.

My question is, are there(other than added weight) some big mechanical drawbacks to having a variable-pitch propellers over a conventional propeller?

Also will all the professional high-speed quads be using variable-pitch like helicopters in the future?
 
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russ_watters said:
Cost and complexity.
Already got answers on another forum, cost and complexity is an extra factor but this one seemed convincing:

the big issue is slow response time to change, The ESC can change at 400Hz, and go from 0 to 100% in close to the same time,I don't see a mechanical system or servo system getting close to 20Hz and staying in one piece long enough to fly.
 

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