It’s not a failure when you learn something from it.
@PDWhiteАй бұрын
I've noticed it's very difficult to get accurate flight data for comparing different props, power systems, torque fins, etc., and their effects on efficiency. Even with the electric setup and the instant feedback in power consumption it provides, the weather variable makes getting useful data hard and confirming results that much harder, as there are only so many zero-wind days and even on the zero wing days with the sun set so there is seemingly no effect from thermals there is still a surprising amount of variability. I have found that day-to-day weather changes efficiency around 5-10%, and most changes in props and power systems, etc., only have around a 5% effect, so it can get lost in the noise. I've found myself on nice days testing something and getting a surprising result, then landing and running back to the shop to quickly swap out a part or grab a completely new setup with just the one variable different, and taking off again because at least the weather can't change too much in the 10 minutes between the two tests. So by the time the evening's over, I'll have 2 or 3 units out in the field that I have to take back to the shop. The point being, it's really hard to make the incremental changes of that 5% improvement here and there when weather changes make the noise floor so high.
@SCOUTaviationАй бұрын
With all my measurements I always did two flights 15 minutes apart. First with our standard prop and then immediately after with the prototype. Same engine, same glider, same conditions
@AndrewGlobus20 күн бұрын
It depends on the area you're flying in.
@nevillecreativitymentorАй бұрын
WOW.... All your knowledge shared ... tons of money and time poured in ... and SHARED to the world. TRUE AVIATOR.
@blue_beepblue_beep6358Ай бұрын
Zip-line drones use a 3 bladed prop of different diameters to spectacularly reduce noise. I think this is the most important thing to grow paramotoring and the most likely end or reduction to the business. A sound test of a 2 blade prop with a 2 to 3cm radius difference should make balancing manageable.
@paramotorheadАй бұрын
Very interesting. I worked in R&D the cycling industry and love that Scout keep pushing the boundaries in efficiency through experimentation. The mk x prop with the softer elastomer is great for someone like myself who likes beach flying.
@aaronhorn6849Ай бұрын
I wouldn't call all that research a failer. You successfully discovered what didn't work!
@portnuefflyerАй бұрын
After flying 3 bladers for year, I flew 2 blades for the last 14 years, now my new 80" 3 blade E prop is SO much smoother....., on a plane but props are props.
@freecapitan1Ай бұрын
Dji made something interesting with their props years ago, take a look at them. It’s a long blended winglet, Boeing 787 like… it even ends with a sharp tip. Those props are way quieter.
@michrozАй бұрын
I heard aircraft engineer said: winglet does really improve the wing efficiency, but only as well as a wing itself would do if it would be longer by half of the winglet length...
@EllipsisAircraft28 күн бұрын
One-third of the length. Actually. Span has the greatest effect in reducing downwash. Because it acts on a larger volume of air. Picture a cylinder, diameter equal to span. Now imagine a longer span. How does the volume of the larger cylinder compare? A small change in span results in a large change in air mass deflected downward/a direction. Air mass being deflected generates the force that is lift/thrust. The more mass, the less velocity is required. Less change in velocity equals less angular deflection. So the wing does not generate as much downwash.
@infin8197428 күн бұрын
Solid development effort. An exotic design I would like to see tested would be a hollow blade that has a port at the root that sucks messy air from there and ejects it at the tip in a way that will negate tip vortices or allow higher tip speeds.
@AndyRRR0791Ай бұрын
The loss of engine RPM with heat during climb with the fat chord blades would be caused by the exhaust heating up. The tuning of the exhaust on a two-stroke is dependent on the exhaust gas temperature because the speed of sound increases with increasing temperature, so the resonant frequency will probably increase. The other problem with operating right on the peak power point is that it is an unstable point because any increased load pushes you down the power curve rather than up which would be the case if you were operating beyond the peak power point. It's a negative feedback slope which generates the engine speed stability.
@Hyperious_in_the_airАй бұрын
I really, REALLY want a 140cm+ scout some day.
@SCOUTaviationАй бұрын
You can have the 140 prop with enduro cage. No problem at all
@jayeshchhari5539Ай бұрын
Hi Miro, I love your videos they are always very insightful. You are doing an amazing job of R N D in Paramotor. Keep up the great work. 😊. Hopefully one day we share the sky together. 🪂🛩️
@verticallines212Ай бұрын
determination, wins over Skill! nyc
@austinsmith9413Ай бұрын
I wonder if its different in the US and Europe. Here in the US, 140cm props are the standard and probably 70% of new paramotors run it. 130 was the standard up until about 3 years ago and has been replacing the 125cm with a slow phase out starting ~15 years ago. Great work on the prop! I hope to try one some day!
@mattfly610215 күн бұрын
Hello, the project is so incredible ! Every are so enthusiasm about this new propeller. Why don't you do a croundfonfing ? Thanks
@lobbyrobby28 күн бұрын
Thank you for making this and all of your hard work
@fabriziotieghi9342Ай бұрын
Geek!! Cool!!
@alexrands2580Ай бұрын
Thank you for your exhaustive research!
@ivonakisАй бұрын
I am glad you landed on design you are happy with, and thanks for sharing.
@MrMartin0815Ай бұрын
I love to see what you tested/tried for our hobby and share with us all! Thank you so much!!! One question: Why not run full throttle at let's say 6800rpm instead of 8600? Same power, less rpm, less consumption, less heat, less stress on all parts?
@SCOUTaviationАй бұрын
I we have tried. t was actually more heat!
@MrMartin0815Ай бұрын
@@SCOUTaviation ok... So maybe less rpm = less cooling from the prop...
@jonnomcintosh8336Ай бұрын
Amazing Miro, truly amazing! You and your team just keep trying to make these incredible machines more efficient and fun. Thankyou for “failing 5 times to set scene 1” 😄 this is why I chose Scout! You guys are unreal 👌🏽
@GabrielDeVaultАй бұрын
Use an electric drive system to help you evaluate props. You will be able to see extremely subtle variations and performance with high accuracy. Especially if the system will let you log volts, amps, RPMs, etc
@donlawrence1428Ай бұрын
NASA found 15% efficiency increase by using much more washout in the tip region. About 4 times the normal washout for a typical wing.
@EllipsisAircraft28 күн бұрын
No. They gained slightly less than 15% lower INDUCED drag by increasing the wingspan 30%. (They would have 41% greater efficiency from the same span increase, with a traditional elliptical lift distribution). What is remarkable, is their increased span (used inefficiently). does not increase the wing root (cantilever beam) bending-moment. Therefore the structural weight remains the same. So it's 15% better at the same weight. Not 15% better outright. Propellers cannot be made 30% larger in diameter. Diameter bogs down the engine and reduces power output. It also pushes the propeller tip speed supersonic. Which is loud. And relatively inefficient as well. The diameter is fixed at some ratio, or fraction, of mach 1.
@donlawrence142827 күн бұрын
@@EllipsisAircraft Dude, u have been reading too much technical literature. Decrease the induced drag of the prop and u can use that extra torque to create more thrust. Same diameter but greater pitch or chord. Noise will b reduced also, another energy gain. It is all about induced drag reduction, which is proportional to the lift coefficient. Those paramotor props operate at high alpha ie high lift coefficient. The induced drag is a big chunk of total prop drag, so the gains are greater. Redesign the prop, apply the Prandtl-D twist schedule and see what happens. Caveat: I did not design a prop or fly a paramotor.
@EllipsisAircraft27 күн бұрын
@@donlawrence1428 At the same diameter, twisting the blade with additional washout INCREASES induced drag from the optimal. You have to increase diameter to attain any induced drag reduction. The (second, revised) Prandtl lift distribution is substantially LESS efficient at the same span.
@iKenFlyPPGАй бұрын
2 blades is a beautiful compromise, balancing out the 1 blade prop most efficiently.
@johncpescodАй бұрын
Again, another great educative video from Scout! It's Milo's dedication to teach people all about paramotor design that made me buy a Scout Enduro with Atom 80 engine. It's a pity that his vario-prop is not available for the Atom 80 😢
@williamwalker39Ай бұрын
You can use the large prop if you reverse the engine by placing it behind the prop so that the prop thrust blows on the engine. This will provide a lot more cooling. This is what we do in drones. This could be done by mounting the motor in front of the vehicle, or it could be mounted in back with the proper mounting structure, which would also reduce the sound for the pilot, since the thrust blows the sound away from the pilot. We are developing a full scale electric Blade Runner style flying car called the Sky Chaser. See our icon for project details.
@SCOUTaviationАй бұрын
There are more considerations to it. You don’t want the heavy engine behind the prop because it would place the centre of gravity too far back.
@williamwalker39Ай бұрын
@@SCOUTaviation so just move the pilot forward relative the wing CG to balance the motor moving backward.
@donlawrence1428Ай бұрын
I forgot to mention, Bowers says it will reduce noise. The washout formula is used to reduce computer fan noise on the International Space station. It can be found here: kzfaq.info/get/bejne/a7l2esugz6eRpn0.html
@NavidSalekiАй бұрын
Looking forward to the EFI+ variable pitch prop , and always thanks for sharing! thank you
@tango_sierra8608Ай бұрын
This was a fun watch. Love how easily you made it to absorb this info and your thought processes
@snakeveraАй бұрын
From the sounds of things as long as you have good temps and your rpm is running within a nominal range that's as good as it gets. Great video!
@terrylutke29 күн бұрын
Interesting video, goes to show that there's still prop re-thinking associated with very low speed flight. Almost no propeller expert has done exhaustive repeatable prop design work to fly at 25/30mph, perhaps RC prop design offers useful correlation. Experience leads me to state the following re powered para props; - longer props are more efficient than shorter props, almost w/o limit or exception - persistent prop tip speeds above .4 Mach, is annoyingly noisy - prop blade pitch exceeding 14deg@.75r results in thrust/drag tail chasing (under 12deg is preferable) - 3+ prop blades are theoretically advantageous in pusher apps where prop blade shading is significant; also more blades at finer pitch is preferable to more pitch on fewer blades.
@donlawrence1428Ай бұрын
I have been working with his research a few years. Id be hsppy to help you get started. I design flying wing models.
@sr71afanАй бұрын
Awesome presentation! Thank You for all the great information!!!
@DontPanicTeamАй бұрын
epic info
@donlawrence1428Ай бұрын
The idea is to reduce the tip vortex strength and move it inboard.
@mikemartin6165Ай бұрын
I love your auto-pitch prop design. I bet it would work well with electric too since electric has more torque for acceleration.
@krzysztofbartnikАй бұрын
Great video as always.But I am still waitnig for variomatic propeler for Polini Thor 202 😞. Maybe someday.
@leodovooАй бұрын
Sensacional
@iKenFlyPPGАй бұрын
You don't actually know much until you see for yourself...says a real engineer.
@JohnDoe-fk6idАй бұрын
You are going to NEED a variable pitch prop, to maintain full power, for maximum climb rate. Anything else is window dressing. As the engine heats up, and starts to lose power, the prop would de-pitch, and maintain peak power RPM. Having the pitch increase from there, as you reduce throttle, will get you SIGNIFICANT gains in fuel economy. You can use electronic systems which are similar to RC variable pitch system, or you could use an aerodynamically controlled system, like the Aeromatic prop, from decades past. The only thing it's REALLY missing, is altitude compensation. Ah. there it is. You're talking about your variomatic. That is only RPM dependent pitch, and it needs to have an aerodynamic (load) dependence, in order to hold the engine at peak power, instead of having to set the rpm above peak power rpm, to account for heat sag.
@wagner2431421 күн бұрын
I make props for FLPHG and i have found that a prop prop that has a pitch that is higher at the root and lower at the tip gives great performance. props i make are 54"dia root 23" and tip of 20" one thing i have noticed is that my prop pull air in from the tips and act like flat winglets.
@ncsufan01Ай бұрын
Have you tested adding stators or flow straighteners behind the propeller? They are used in some hovercraft and airboat designs and claim increased thrust and efficiency. I could see how they could also help with paramotor frame rigidity. A con being increased weight but that may be offset with the gas savings.
@arnaudmerat4452Ай бұрын
Nice and informative as usual 👍👍
@pittsjohn57Ай бұрын
Excellent!!!!
@donlawrence1428Ай бұрын
The aerodynamicist Al Bowers said it can be applied to props.
@adibabiАй бұрын
Looking forward to the 140 vario coming to market
@FireDFPVАй бұрын
I tried to have more efficiency on small quadcopters, only fixed pitch props available. Given the same diameter and number of blades, the only night and day factors seem to be the weight and the rigidity of the props. The lighter and more rigid it is the better. But first of all, the props must provide proper amount of lift for the weight.
@patrickmckowen2999Ай бұрын
When is the Variomatic going to be for sale? Cheers
@johntenhave1Ай бұрын
Look at p tips on Prince propellors.
@EridanTheEnchanterАй бұрын
Tried it all? But did you try the Prandtl washout twist? The claims are: less drag/torque, lower power consumption, and less noise. If you're still experimenting it would be interesting to see the results.
@jamesperet9499Ай бұрын
Have you thought about tubercles? I’ve seen some work with wind turbine blades replicating the tubercle structures on the forefins of a humpback whale…. Reduced noise and increased efficiency… I think it is something about reducing span wise flow and increasing vorticity to promote attachment. Could this be a number 11?
@jonmarchello5760Ай бұрын
Forgive my noviceness in the ultra light aviation space, but has anyone tried designing a CRP(Contra Rotating Prop) for any of these motor variants?
@wardified8566Ай бұрын
Also looks like it has not been tried yet...
@receopadajoАй бұрын
It has already been tried, and the effect is not worth the complications.
@Arturo4586Ай бұрын
@@receopadajoWhat complications? The mechanism providing contra rotating propellers? They are substantially more efficient.
@fredfrancis5221Ай бұрын
Look at the the work of Al Bowers (ret. NASA Armstrong Chief Scientist) on Pradtl wing; instead of elliptical lift, look at the bell-shaped lift profile of the 1933 Prandtl wing. kzfaq.info/get/bejne/mKmnp8Z1s6iVZXk.html The whole video is worthwhile, but this URL goes directly to his application of this work to propellers.
@brandesadventures2155Ай бұрын
Excelent! I love to test one . Is the propeller in produccion?
@prabhakaranbalasundaramАй бұрын
Out of curiosity, in the classical props any reason why winglets design for propeller was not studied in your experiments? Technically there is a considerable noise and drag reduction. Checkout eVTOL propeller designs.
@turkeyphantАй бұрын
He said he didn't think there are any benefits
@cmtetaboacoАй бұрын
Ducted fan is only better for higher speeds
@toetbakkerАй бұрын
I fly an e-prop 3 blade 155 cm at 2000/2100 rpm, with an old hirth engine. many times quieter than the Polini with 150 prop and the Cosmos with 160 prop
@AvtodomUSAАй бұрын
What about "many blades" prop with tin blades. Like in some helicopter tail rotor.
@Resteasy8686Ай бұрын
What about some AI designed props like the innovations in the marine prop industry?
@Bob-sk6xq28 күн бұрын
Didn’t the Wright brothers invent and use a very efficient propellor?
@tedarcher9120Ай бұрын
What about prop winglets?
@SCOUTaviationАй бұрын
Do you know any successful application of winglets on propellers?
@richc.3100Ай бұрын
14:03 how do you factor all the variables. Pressure, temperature, humidity, pilot input, etc.? Regardless, great video.
@SCOUTaviationАй бұрын
Very simply. Every time I did two measurements: new prototype and our standard prop as reference. Two flight 15 minutes apart. All variables the same (temperature, pressure, humidity, weight, same engine, same glider).
@richc.3100Ай бұрын
16:17 this is just killing me😂 of course the results don’t match. Too many uncontrolled variables.
@SCOUTaviationАй бұрын
Every time I did two measurements: new prototype and our standard prop as reference. Two flight 15 minutes apart. All variables the same (temperature, pressure, humidity, weight, same engine, same glider).
@StabilisingGlobalTemperatureАй бұрын
What proportion of the annoying part of the noise is from the prop and how much from the engine?
@StabilisingGlobalTemperatureАй бұрын
By annoying part I mean the typical 2 stroke engine sound of high and monotonous pitch. Most people do not mind white noise - it is similar to wind blowing trees. If you record the sound and do a spectral analysis maybe?
@guymazor8945Ай бұрын
So if I squeeze my gas in full throttle it gives me less power than when I'm in almost full throttle In my moster?
@SCOUTaviationАй бұрын
We have used an aerodynamically heavier propeller that stopped the fully open engine at 7500 rpm. With your prop at 7500 rpm the throttle is not fully open, that’s a different scenario
@patrickmckowen2999Ай бұрын
👍👍 Your prop engineers were wrong when they were optimistic about their design calculations, maybe they are wrong about prop tip winglets? Best wishes
@SCOUTaviationАй бұрын
Nah, you cannot trust the engineers these days!
@michrozАй бұрын
Dusan and Milos must be getting worried: most of their theoretical predictions have basically failed... :)
@richc.3100Ай бұрын
14:29 bro there are so many uncontrolled variables in your experiment that it could be 20%+ better and your data might show a 20% decrease. I urge you to consider static testing, it’s at least a good starting point.
@SCOUTaviationАй бұрын
Every time I did two measurements: new prototype and our standard prop as reference. Two flight 15 minutes apart. All variables the same (temperature, pressure, humidity, weight, same engine, same glider).
@MrGoMarioАй бұрын
I think you are confusing a ducted fan with a shrouded prop!!!!!!!
@Exuma_GuyАй бұрын
non-planar blades...
@StabilisingGlobalTemperatureАй бұрын
This KZfaqr has tested a large number of designs of boat propellers. Including a Prandtl design which performs very well: kzfaq.info/get/bejne/od-adtqqy9TWhWw.html
@williamloveless5644Ай бұрын
33% fuel efficiency bro. Shut up and take my money.
@antrygrevok6440Ай бұрын
2 comments, thus-far: 1. WHEN switching from a 2-blade prop to a 3-blade design, THEN one should be reducing the chord significantly, to keep the wetted-area similar? Also, at higher-altitudes, more-blades is apparently better, resisting loss-of-thrust as the air-density drops ( I don't know if you'd find that at 8,000' altitude, which is the safety-ceiling for no-supplemental-oxygen, ttbomk ) 2. the Darth Wader should have altered only 1 thing: 7800rpm max-power operating duration. It *should* have extended that. Nothing else that I can think-of.. --- Back to watching the video.. ( : --- "seconds to climb 100m" depends entirely on air-density, air-temperature, AND humidity! --- I don't understand why you weren't using a genetic-algorithm in OpenFOAM? Let IT find the optimal thickness/chord/pitch/distribution-of-force ( which should be elliptical? ) --- Ah, you've got the "toroidal propeller".. Please go watch videos on the Sharrow propeller: *nearly all* the noise from the normal prop is from cavitation! The Sharrow isn't cavitating: it's silent.
@antrygrevok6440Ай бұрын
I just realized: The optimal-prop-diameter, in that context, is ergonomic: a 7' tall Dutch person could use a larger-diameter prop on their back than could a dwarf, right? Therefore, there ought be multiple prop-solutions, using a diameter powerlaw, so you fit the tallest people, the 5'9" average-men, the 5'4" average-women, & the 4'11" short women, & then each of them has a prop that works *for them*, & all get to fly with efficient props! _ /\ _
@StabilisingGlobalTemperatureАй бұрын
Have you tried specifically a Prandtl foil? The Sikorsky looks by eye to be similar. But Prandtl propellers are known to be high efficient and low noise. kzfaq.info/get/bejne/rZOUnpR_1byyfn0.html
@SCOUTaviationАй бұрын
I learned something new today. Thank you!
@StabilisingGlobalTemperatureАй бұрын
@@SCOUTaviation Great. Al Bowers at NASA has done a lot of work on Prandtl wings. At 39 minutes he discusses Prandtl propellers: kzfaq.info/get/bejne/rZOUnpR_1byyfn0.html He points out that most of the noise comes from the tip. And if you unload the tip it reduces the noise. And reduces the torque required for a given thrust. He quotes a 15.4% improvement, see the slide showing the graph.
@richardwallinger1683Ай бұрын
dumb idea that fan would need quite a few HP at 8,600 rpm . Make up a dummy hub / model aeroplane electric motor and you will see that the guy who recommended the extra cooling fan . obviously hasnt a clue .
@Bob-sk6xq28 күн бұрын
What about prop tip fences?
@wolframzirngibl1147Ай бұрын
Hmmm. Sounds like you did not take into account the bad laminar flow, a Paramotor Prop is facing. You may not optimize prop design by conventional means. Rather, build a prop more robust against vortices. But I am afraid, that was impossible. Anyhow. You did nop see big improbevements with any of your designs. What did you expect? Conventional props work quite well in measn of efficiency, so any improvement must stay in the few per cent range. And that's what you did measure.
@fabriziotieghi9342Ай бұрын
Dear Miro. I love your approach. You have refused to copy all other messing manufacturers, which copy one anothers, all doing the same gross mistakes. One only note about this video. I have introduced on my belt reduced nanotrike engine a customized increased reduction ratio matched with higher pitch. And my prop is spinning at max 2500 revs Min. I have achieved a level flight at a consistent lower rpms. You have mentioned the same test with 3.45 reduction ratio, and you have had no significant improvements in noise or fuel consumption. But you didn't say anything about climb ratio. Why?? According to my experience, you should have improved it. Isn't it? Kindly.
@SCOUTaviationАй бұрын
With every prop I measure max climb rate and cruise consumption. With the 3.45 I measured noise levels as well. Unfortunately, it did not perform better in any of these parameters
@fgbhrl4907Ай бұрын
have you considered a clutched (say) 2 meter diameter propeller along with a more regular size? The large propeller would be locked in the horizontal position during takeoff / landing, and the clutch would engage the larger prop at altitude.
@turkeyphantАй бұрын
What?
@fgbhrl4907Ай бұрын
@@turkeyphant two propellers. One clutched so that it does not spin during takeoff. You engage this while in the air (and potentially disengage the smaller one).
@turkeyphantАй бұрын
@@fgbhrl4907 Are they mounted in the same plane?
@fgbhrl4907Ай бұрын
@@turkeyphant They'd be offset the depth of a prop. Basically two independent props, on the same driveshaft.
@SoloRenegadeАй бұрын
toroidal props have been around for decades, nothing new, they are a gimmick. the "efficiency" gains are not what people claim. people take the data from the paper out of context and make claims the paper does not support.
@GabrielDeVaultАй бұрын
Thank you! People are so freaking gullible just because they look cool and they haven't seen it before. They think it must be new and amazing. No, all of these designs were explored heavily in the '40s and '50s and discarded because they were inferior to traditional designs