X Prize Clean Aviation: $10 million

In summary: I seem to have with you, turns into a conversation about energy storage.In summary, an MIT collaboration with the X Prize foundation has proposed a $10 million prize for a race from California to New York in which competing planes must be powered entirely by electricity and produce no emissions. The winning plane would receive $7.5 million, with an additional $2.5 million prize for the longest distance covered on a single leg of the flight. The proposal has been met with skepticism due to the challenges of energy storage and the potential limitations of using electric motors to power ducted fans. However, the goal of spurring innovation remains a driving force behind the proposal.
  • #106
mheslep said:

Okay, better, but still not enough! :tongue:

Note: (I will, rather reluctantly, admit that the more I read about this I am warming up to it). :wink:

There is also the problem that you could go 20 minutes. But you would have to leave the wife, kids, dog, and luggage at home...though that may not necessarily be a bad thing! :tongue2:
 
Last edited by a moderator:
Physics news on Phys.org
  • #107
Here is a simple solution for motor weight and is cheap compared to HTS motors. Use 400 Hertz 3-phase AC induction motors. Remember people that like a transformer, higher frequencies reduce size and weight. Four-hundred hertz motors have been used in the aviation industry for years for the hydraulics or anything else that needed actuation. With 400 hertz motors you also gain insanely high RPMs. A two pole, 400HZ motor turns at about 24,000 RPM.

So I would give AC propulsion a call and ask for their AC induction motor with variable frequency speed drive package. Or talk with the engineers at 400hertz.net if you want a custom horsepower motor other than 268 HP from AC propulsion.
 
  • #108
Altrepair said:
Here is a simple solution for motor weight and is cheap compared to HTS motors. Use 400 Hertz 3-phase AC induction motors. Remember people that like a transformer, higher frequencies reduce size and weight. Four-hundred hertz motors have been used in the aviation industry for years for the hydraulics or anything else that needed actuation. With 400 hertz motors you also gain insanely high RPMs. A two pole, 400HZ motor turns at about 24,000 RPM.

So I would give AC propulsion a call and ask for their AC induction motor with variable frequency speed drive package. Or talk with the engineers at 400hertz.net if you want a custom horsepower motor other than 268 HP from AC propulsion.
The main loss component in normal electric motors is resistive, ie. IR loss in the windings. Along with the advantages of increasing frequency comes the disadvantage of increased resistive losses due to the frequency dependent http://en.wikipedia.org/wiki/Skin_effect" [Broken]. Skin depth is proportional to 1/sqrt(frequency), so increasing the frequency from 60Hz to 400Hz decreases the skin depth 62%.

Windage is another loss secondary to IR, but at some high enough RPM windage will become dominant.

BTW, AC propulsion's motor ( i.e. Tesla's motor) is indeed a three phase induction design, though I don't know about frequency. At ~4KW/kg, I am not aware of any non-HTS electric motor at this scale (<500KW) with a greater power density.
 
Last edited by a moderator:
  • #109
mheslep said:
The main loss component in normal electric motors is resistive, ie. IR loss in the windings. Along with the advantages of increasing frequency comes the disadvantage of increased resistive losses due to the frequency dependent http://en.wikipedia.org/wiki/Skin_effect" [Broken]. Skin depth is proportional to 1/sqrt(frequency), so increasing the frequency from 60Hz to 400Hz decreases the skin depth 62%.

Four hundred hertz 3-phase AC induction motors have been around since before a lot people where even born that are members of this forum. All the issues of going higher frequency have been solved a long time ago when the aviation industry needed a lightweight electric motor solution. That is why in the aviation industry 400 hertz is standard since the generators and motors are light weight.


mheslep said:
Windage is another loss secondary to IR, but at some high enough RPM windage will become dominant.

Turbo fan Jet engine turbines spin at insanely high rpms and thus suffer from windage losses too. I would say it is far worse since it has so many blades inside.

mheslep said:
BTW, AC propulsion's motor ( i.e. Tesla's motor) is indeed a three phase induction design, though I don't know about frequency. At ~4KW/kg, I am not aware of any non-HTS electric motor at this scale (<500KW) with a greater power density.
[/QUOTE]

It is a 400 hertz design with copper rotor bars instead of aluminum. It is 4-pole instead of two, so it will turn at about 12,000 RPM. A standard off the shelf 400 hertz, 200 HP induction motor only weighs around 80 pounds compared to the 60HZ version that is in the thousands.
 
Last edited by a moderator:
  • #110
Altrepair said:
It is a 400 hertz design with copper rotor bars instead of aluminum. It is 4-pole instead of two, so it will turn at about 12,000 RPM. A standard off the shelf 400 hertz, 200 HP induction motor only weighs around 80 pounds compared to the 60HZ version that is in the thousands.

Now way. How does power scale with frequency?
 
  • #111
Altrepair said:
Four hundred hertz 3-phase AC induction motors have been around since before a lot people where even born that are members of this forum.
Before all of the forum members were born.
All the issues of going higher frequency have been solved a long time ago when the aviation industry needed a lightweight electric motor solution. That is why in the aviation industry 400 hertz is standard since the generators and motors are light weight.
I'd say the issues are now well understood, not 'solved.' Certainly 400 Hz motors are lighter weight than similarly rated 60Hz motors. I only pointed out one known disadvantage that comes along with the other advantages (as with everything else): generally speaking a 400Hz motor will be a little less efficient than a similar 60 Hz motor because of IR winding losses. Thus on the factory floor a 400Hz motor will produce a higher electric bill per unit output than the similar 60Hz motor. For the case of a battery powered aircraft so equipped, the platform would have to carry a little more battery for a given power-time profile, even if the 400Hz motor weighs less. It's a trade off <shrug>. In a normal aircraft carrying thousands of megajoules of jet fuel, that efficiency loss doesn't matter (for auxiliary motors) so the 400 Hz weight savings dominates in traditional aviation.
 
Last edited:
  • #112
Altrepair said:
It is a 400 hertz design with copper rotor bars instead of aluminum. It is 4-pole instead of two, so it will turn at about 12,000 RPM.
I've never heard/seen a 400Hz spec for the Tesla. AC Propulsion http://www.acpropulsion.com/products-drivesystem.html" [Broken], I expect in the hundreds of hertz range. Do you have a reference for the 400 Hz claim?
 
Last edited by a moderator:
  • #113
mheslep said:
Before all of the forum members were born.

I know the low frequency design of AC induction motors have been around since the 1800's, but I did not think the 400 Hertz design has been.
 
  • #114
mheslep said:
I've never heard/seen a 400Hz spec for the Tesla. AC Propulsion http://www.acpropulsion.com/products-drivesystem.html" [Broken], I expect in the hundreds of hertz range. Do you have a reference for the 400 Hz claim?

The article says it all. The transmission is at a fixed gear ratio, so varying the frequency stands in place of shifting gears. I'm pleasantly surprised to hear about using induction motors. I'd always considered them too massive and underpowered for transportation. However, I can't say I understand the reasoning to inducing a 4 pole magnet in the rotor rather than using a 4 pole permanent magnet.
 
Last edited by a moderator:
  • #115
Tesla Motors eventually included a transmission (2 gears I think) in their Roadster - still a big improvement over the transmissions used with combustion engines.
 
  • #116
Phrak said:
The article says it all. The transmission is at a fixed gear ratio, so varying the frequency stands in place of shifting gears. I'm pleasantly surprised to hear about using induction motors. I'd always considered them too massive and underpowered for transportation.

Until today when you learned of high frequency designs. :smile:

Phrak said:
However, I can't say I understand the reasoning to inducing a 4 pole magnet in the rotor rather than using a 4 pole permanent magnet.

There would be no torque if current was not induced into the rotor bars which requires slip of the rotor relative to the rotating magnetic field of the stator. If instead magnets were used, it would be a synchronous motor which have no starting torque. So it would sit there buzzing with a very angry 60 HZ hum until damage occurs or some safety device trips. The large industrial synchronous motors start up as asynchronous induction motors since they also have rotor bars embedded into the rotor, till about 75% speed, at which point the DC field circuit is energized which causes the rotor to lock up in sync with the rotating magnetic field of the stator. Before they made them this way, a "pony motor" which is synonymous with a starter motor used for ICE's was used to bring up the speed of the synchronous motor.


mheslep said:
I've never heard/seen a 400Hz spec for the Tesla. AC Propulsion http://www.acpropulsion.com/products-drivesystem.html" [Broken], I expect in the hundreds of hertz range. Do you have a reference for the 400 Hz claim?

If you look at the specs you see it says four pole, and if you know the formula to find the frequency of an ac induction motor when the poles and RPM are known then you can get a general idea of the frequency it is designed for. Another factor is also weight.

The Tesla uses AC propulsion's designs. The motor from AC propulsion weighs in at 110 pounds where as the 400 HZ, 200 HP motor from: http://www.400hertz.net/Products/ME-400-200-416.htm" [Broken] weighs in at 85 pounds. The weight differences are due to more HP likely in the AC propulsion design and/or the frame the motor is in maybe weighs more, but both of them are are at least 12,000 RPM or greater and have about the same weight.
 
Last edited by a moderator:
  • #117
Altrepair said:
Until today when you learned of high frequency designs. :smile:

I'm an electronics products design engineer in instrumentation, controls, and power conversion (and I don't push papers, I engineer). I know a little about DC motors and haven't done anything with AC induction motors beyond turning them on and off and advising against unreliable speed control using triacs.

There would be no torque if current was not induced into the rotor bars which requires slip of the rotor relative to the rotating magnetic field of the stator. If instead magnets were used, it would be a synchronous motor which have no starting torque.

Not really. An induction motor requires slip to generate a field on the rotor. No slip, no rotor field, no torque. For a permanent magnet rotor, no slip is required, and the torque is maximal at stall. DC motors that have permanent magnets are not driven by a constant AC frequency and neither is the tesla motor. DC motors are supplied with their own alternating potential mechanically or electronically.
 
Last edited:
  • #118
mheslep said:
Tesla Motors eventually included a transmission (2 gears I think) in their Roadster - still a big improvement over the transmissions used with combustion engines.

Interesting. I was curious about how they managed one gear. The power and torque curves of an electric motor are OK, but not wonderful. I think another alternative is to vary the field winding current (where both stator and field are electromagnets), but I haven't looked into it. It could have drawbacks.
 
Last edited:
  • #119
Phrak said:
Not really. An induction motor requires slip to generate a field on the rotor. No slip, no rotor field, no torque. For a permanent magnet rotor, no slip is required, and the torque is maximal at stall. DC motors that have permanent magnets are not driven by a constant AC frequency and neither is the tesla motor. DC motors are supplied with their own alternating potential mechanically or electronically.


If you read the text of mine you quoted (There would be no torque if current was not induced into the rotor bars which requires slip of the rotor relative to the rotating magnetic field of the stator.) you would see I said it required slip. No slip means no current will be induced into the rotor bars. It is that simple. If the rotor followed exactly with the rotating magnetic field, no current will be induced since no magnetic flux lines will be passed through by the rotor bar conductors meaning no current could ever flow in the conductors, thus no magnetic field will set up on the rotor, meaning NO torque.



I did not say anything of PM DC brushless motors which have a feed back loop either by hall effect sensors or by back EMF, in which case the controller knows the position of the rotor to correctly time when to energize the next set of windings (the electronic version of the commutator).

Synchronous AC motors, though, have no starting torque and have totally a different torque curve and work differently, PERIOD, compared to PM brushless DC motors. You can argue that till the cows come home, but it is a fact. Either a pony motor is needed or it must be the type that has rotor bars embedded into the rotor such that it starts up as an asynchronous induction motor till sufficient speed is reached for the rotor to lock in step with the rotating magnetic field when the DC power source is supplied to the slip rings of the rotor that powers the electromagnets.

If I am not considered a credible source by you, then have a look here that backs up my claim of pure AC synchronous motors having no starting torque at all:

http://www.engineersedge.com/motors/synchronous_motor.htm" [Broken]

http://www.electricmotors.machinedesign.com/guiEdits/Content/bdeee11/bdeee11_8.aspx" [Broken]

http://www.tpub.com/content/neets/14177/css/14177_92.htm"

I did make one honest mistake by saying 75% synchronous speed, when it is actually 95% of synchronous speed before the DC circuit is energized to power the rotor electromagnets to lock the motor in step with the rotating magnetic field.

Finally, the AC induction motor in the Tesla roadster works on the same principle as your typical AC induction motor which requires sinusoidal current to work. The voltage feed to it from the vector-variable-voltage/frequency drive is variable length square waveform that has the on/off ratios such that it makes the current flowing through the motor windings sinusoidal due to its inductance.

Have a look: http://oee.nrcan.gc.ca/industrial/equipment/vfd-ref/images/figure-08.jpg" [Broken]

Anyways, I think we are stirring the topic off course and so I shall refrain from posting about motor characteristics.
 
Last edited by a moderator:
  • #120
Altrepair said:
If you look at the specs you see it says four pole, and if you know the formula to find the frequency of an ac induction motor when the poles and RPM are known then you can get a general idea of the frequency it is designed for.
Yes for a synchronous AC motor rpm = 120 x frequency / # poles. This motor can not be synchronous. Phrac noted the design is in fact variable frequency.
 
  • #121
mheslep said:
Yes for a synchronous AC motor rpm = 120 x frequency / # poles. This motor can not be synchronous. Phrac noted the design is in fact variable frequency.

It also applies to asynchronous motors, but their will be slip obviously when a load is applied so the full load RPM will be less than synchronous. Even a 60HZ motor can have its frequency increased by a variable frequency drive. There is no "design" difference as you state. Some motor manufactures will sale "inverter duty" which the only difference is the motor's insulation is able to withstand the voltage spikes caused by the controller without insulation breakdown.

Anyways I have a feeling you only wrote this because I said I was not going to talk about motor characteristics any longer. You are causing this topic to go off course. If you wish to learn more then either PM or go to the Electrical Engineering forum to post more about electric motors. We need to get back to talking about this X-prize...
 
  • #122
Note I started the thread on "X Prize Clean Aviation". A discussion of the power density and / or efficiency of electric motors along with their possible energy sources is extremely relevant in my view.
 
  • #123
Then the alternative would be brushless DC motors which are also cheaper than High temperature super conducting motors. Surely you want to make this clean flying airplane within practical budget. The other benefit is brushless DC motors are also more efficient than asynchronous induction motors.
 
  • #124
Altrepair said:
Anyways, I think we are stirring the topic off course and so I shall refrain from posting about motor characteristics.

Long restatements of common knowledge aren't interesting to read. On topic interests are those you have avoided or misunderstood or don't understand: 1) How does an induction motor scale with frequency? 2) What are the advantages for electric flight, if any, in inducing a magnetic field in a rotor rather than having it supplied for free?
 
  • #125
Phrak said:
2) What are the advantages for electric flight, if any, in inducing a magnetic field in a rotor rather than having it supplied for free?

Asynchronous induction motors traditionally weigh less than synchronous motors with the same power (torque x speed) capability since light weight windings can be made lighter than permanent magnets. Honestly, though, this is only true at very high torque and power values. Probably in excess of 150kW total motive power.

I don't plan to get involved in this discussion, though...
 
  • #126
mheslep said:
Note I started the thread on "X Prize Clean Aviation". A discussion of the power density and / or efficiency of electric motors along with their possible energy sources is extremely relevant in my view.

Agreed.

RonL's spinning battery packs and your SC motor mated in my brain and I ran across something close to the child product:

Brunvoll.rdp.jpg

Brunvoll presents a ”Rim driven thruster” (RDT)

Rather than having the electric motor positioned along the central axis, move it out to the periphery.

I can't imagine a bearing that size being efficient at aircraft speeds, so I would position a conventional core axial bearing support.

Basically, the electric motor and ducted fan become one integral unit.
 
  • #127
OmCheeto, like the idea, and would probably reduce cost even more so.
FlexGunship, I sent that person a PM on what he wanted to know, but what you say is also true.
 
  • #128
Updated narrated version of the Puffin VTOL video.
https://www.youtube.com/watch?v=GV0qBU_u3tQ

Summary:

  • Blades don't counter rotate, but left and right sides run in opposite directions to counter torque
  • On start, trailing edge control surfaces split to deflect thrust, keeping aircraft on the ground until pilot is ready
  • Carbon fiber construction for body, provides 300 lb airframe (empty)
  • 14' wing span,
  • 7' rotors
  • cruise 150 mph, sprint 300 mph
  • Much quieter than conventional craft due to e-motors
  • No turbo charge at high altitude
  • Ceiling 30k' feet w/ environmental auxiliaries for pilot
  • 50 mile range at cruise w/ 100 lbs of batteries, NASA aiming for 175 miles in 7 years
 
  • #129
50 miles, eek...why not take a car. Even 175 miles is not all that attractive a decade later.
 
  • #130
I would prefer something a little more. . . comfortable. As a to and from work device, it seems plausible, but quite frankly traveling long distances in that thing would be absolutely horrible.
 
  • #131
Cyrus said:
50 miles, eek...why not take a car. Even 175 miles is not all that attractive a decade later.
Have fun:
picture-5.jpg
 
  • #132
KalamMekhar said:
I would prefer something a little more. . . comfortable. As a to and from work device, it seems plausible, but quite frankly traveling long distances in that thing would be absolutely horrible.

I'll take a 2 minute uncomfortable flight to work vs a comfortable but maddening 45 minute snail crawl to work any day.

But then, I always was a double black diamond kind of person.

(Emphasis on "was". I'd break a hip if I tried that now.)
 
  • #133
mheslep said:
Have fun:
picture-5.jpg

I would think that is in a foreign country, not America.:rolleyes:
 
  • #134
mheslep said:
Have fun:
picture-5.jpg

Is this suppose to constutite a valid argument? :confused: You don't even know what the average distance those cars in that picture travel and if this vehicle would even begin to address the issue in that photo.
 
  • #135
Cyrus said:
Is this suppose to constutite a valid argument? :confused: You don't even know what the average distance those cars in that picture travel and if this vehicle would even begin to address the issue in that photo.
Valid argument? Cyrus, please. My casual response to
Cyrus said:
50 miles, eek...why not take a car.
Was completely appropriate.
 
  • #138
mheslep said:
Valid argument? Cyrus, please. My casual response to Was completely appropriate.

No, I had a legitimate gripe. 50 miles is what a car is used for, and this is what NASA said this vehicle would not compete against.
 
  • #140
mheslep said:

I drove back home from Seattle a few years back on a Sunday afternoon.
The 60 mile stretch to Olympia took me 4 hours.

There was no construction.

There were no accidents.

Just a slew of cars out for a Sunday drive.

I will never drive to Seattle again.

Next time, I'm flying.

And back to the topic:
Those little Schubeler electric ducted fans are only $314 each.(298eur-19%vat)
Generating 20lbs of thrust each, it would only require 8 to lift me off the ground.
Another 8 to lift a smaller Puffin style vehicle.
Another 8 to lift the 160lb battery pack.
That's only $7500 bucks for motors.
100 wh/kg * 73 kg batteries = 7.3 kwh
each fan consumes 7 kw
7*24 fans = 168 kw
7.3 kwh / 168 kw = 2.6 minutes
...

hmmm...

I'll have to do some scaling.




I was coming back from a 3 day regional conference. So no, I was not out for just a Sunday drive.
 
<h2>1. What is the purpose of the X Prize Clean Aviation?</h2><p>The X Prize Clean Aviation is a competition that aims to accelerate the development of clean and sustainable aviation technologies. It offers a $10 million prize to the team that successfully demonstrates a clean aviation technology that can significantly reduce carbon emissions and other environmental impacts of the aviation industry.</p><h2>2. Who can participate in the X Prize Clean Aviation?</h2><p>The competition is open to teams from around the world, including individuals, universities, and companies. The team must have a pilot and a technical lead, and can also include other members such as engineers, scientists, and business experts.</p><h2>3. What are the criteria for winning the X Prize Clean Aviation?</h2><p>The winning team must demonstrate a clean aviation technology that meets the following criteria: it must be able to reduce carbon emissions by at least 50%, have a range of at least 100 miles, and be able to carry at least two passengers. The technology must also be affordable, scalable, and have the potential for commercialization.</p><h2>4. How will the winner of the X Prize Clean Aviation be selected?</h2><p>The winning team will be selected by a panel of judges based on the performance and feasibility of their technology, as well as their business plan and potential for commercialization. The judges will also consider the team's ability to meet the criteria of the competition and their overall impact on the aviation industry.</p><h2>5. What is the timeline for the X Prize Clean Aviation?</h2><p>The competition was launched in 2018 and the deadline for team registration is in early 2022. The final competition and winner announcement is expected to take place in late 2022. However, due to the ongoing COVID-19 pandemic, the timeline may be subject to change. Updates will be provided on the X Prize website.</p>

1. What is the purpose of the X Prize Clean Aviation?

The X Prize Clean Aviation is a competition that aims to accelerate the development of clean and sustainable aviation technologies. It offers a $10 million prize to the team that successfully demonstrates a clean aviation technology that can significantly reduce carbon emissions and other environmental impacts of the aviation industry.

2. Who can participate in the X Prize Clean Aviation?

The competition is open to teams from around the world, including individuals, universities, and companies. The team must have a pilot and a technical lead, and can also include other members such as engineers, scientists, and business experts.

3. What are the criteria for winning the X Prize Clean Aviation?

The winning team must demonstrate a clean aviation technology that meets the following criteria: it must be able to reduce carbon emissions by at least 50%, have a range of at least 100 miles, and be able to carry at least two passengers. The technology must also be affordable, scalable, and have the potential for commercialization.

4. How will the winner of the X Prize Clean Aviation be selected?

The winning team will be selected by a panel of judges based on the performance and feasibility of their technology, as well as their business plan and potential for commercialization. The judges will also consider the team's ability to meet the criteria of the competition and their overall impact on the aviation industry.

5. What is the timeline for the X Prize Clean Aviation?

The competition was launched in 2018 and the deadline for team registration is in early 2022. The final competition and winner announcement is expected to take place in late 2022. However, due to the ongoing COVID-19 pandemic, the timeline may be subject to change. Updates will be provided on the X Prize website.

Similar threads

  • General Discussion
Replies
2
Views
2K
Replies
19
Views
4K
Replies
1
Views
727
  • Beyond the Standard Models
Replies
8
Views
4K
  • STEM Academic Advising
Replies
5
Views
1K
  • General Discussion
Replies
10
Views
3K
  • Mechanical Engineering
Replies
1
Views
2K
Replies
8
Views
2K
Replies
10
Views
2K
  • Beyond the Standard Models
2
Replies
39
Views
4K
Back
Top