#MyScout by Michael
1:18
8 ай бұрын
#MyScout by Kevin
1:29
9 ай бұрын
Why I love the SCOUT by Miroslav
5:30
Пікірлер
@wayneherron6511
@wayneherron6511 2 күн бұрын
Ive flown that 4 prop type of paramotor. It went surprisingly well considering my lack of experience, however the landing was not so hot and I damaged the frame. The design was intended to be very light, but it sacrifices strength. Openppg quit making them and has gone to single prop design as well.
@DarioushAryan
@DarioushAryan 5 күн бұрын
bravoo
@AndrewGlobus
@AndrewGlobus 6 күн бұрын
Moster EFI is the first engine in aviation history without magnetto, alternator, charging coil. After 7 hours of flying in have to look for an electrical socket and wait 1 hour until you can continue your flight. The Iphone philosophy is now in the paramotor world as well. In cold climates and in winter, the battery life is reduced to 3.5 hours. Over time, the battery degrades and its capacity decreases. For your 6000 euros Now you need to consider all these additional factors when planning your XC flight.
@dewolfeFSP
@dewolfeFSP 7 күн бұрын
The Ural Motorcycle went through this change and it reinvigorated the model.
@ahmaddarwish1175
@ahmaddarwish1175 9 күн бұрын
Thank you so much again.... i want to ask you a question Is there a mobile app you recommend to measure the reclining angle?
@SCOUTaviation
@SCOUTaviation 7 күн бұрын
I use Clinometer on iPhone
@DarioushAryan
@DarioushAryan 9 күн бұрын
great... bravoo
@DarioushAryan
@DarioushAryan 9 күн бұрын
bravoo ... great
@jonconer3701
@jonconer3701 9 күн бұрын
Hello sir my name is muhamad hasan in my rc gearbox planes i found medium size prop with medium number gear ratio is the best so i think in paramotor reduction ratio 1 to 2,5 is awesome, because air slip on blade to avoid that u need some high rpm , thanks.
@Anthony_DP
@Anthony_DP 11 күн бұрын
On day two of my paragliding instruction🎉. I'm hooked. This interests me greatly. I'm going to show my instructor this weekend.
@mattfly6102
@mattfly6102 13 күн бұрын
Hello, the project is so incredible ! Every are so enthusiasm about this new propeller. Why don't you do a croundfonfing ? Thanks
@wagner24314
@wagner24314 19 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.
@jonnomcintosh8336
@jonnomcintosh8336 20 күн бұрын
Incredible! I wish I could join, all the way from Australia. Looking forward to seeing some snippets of the adventure hopefully :) A video on how and what you carry on the adventure wingman challenge would be great and helpful?!
@Johndoe182hr
@Johndoe182hr 20 күн бұрын
I wish it was a race, the sport needs a proper adventure race series. I also believe the cost is far too high I'm young and got into paramotor flying because it was affordable I'm not an old guy with heaps of disposable income $2590 to fly my own equipment, use my own gear, buy fuel and fly in a public space? To be honest that's kind of insulting.
@milesb4231
@milesb4231 20 күн бұрын
why would you take it as an insult? just go do your own thing or find a way to pay for it.
@Robbo1966
@Robbo1966 17 күн бұрын
Seems like a great adventure, why not?
@RoofAndAMeal4UsAll
@RoofAndAMeal4UsAll 20 күн бұрын
You're a cool cat dude. Thanks for your contribution to the pursuit of the sky. Lotsa guys just do dumbass shit for clicks, pushing their karma, setting the worst example. You're the one pushing the real frontiers of performance for the sake of safety, and fun. Here's to you
@Malaysiarider
@Malaysiarider 20 күн бұрын
Interested, do you provide flying course?
@xunorus
@xunorus 20 күн бұрын
sounds amazing!
@infin81974
@infin81974 25 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.
@Bob-sk6xq
@Bob-sk6xq 25 күн бұрын
What about prop tip fences?
@Bob-sk6xq
@Bob-sk6xq 25 күн бұрын
Didn’t the Wright brothers invent and use a very efficient propellor?
@lobbyrobby
@lobbyrobby 25 күн бұрын
Thank you for making this and all of your hard work
@shaneross7428
@shaneross7428 27 күн бұрын
Great video. KZbin isnt a stand alone instructor but the hundreds of hours I watched before training made everything click into place a lot faster at the training center.
@SCOUTaviation
@SCOUTaviation 26 күн бұрын
Exactly!
@terrylutke
@terrylutke 27 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 [email protected] 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.
@MrGoMario
@MrGoMario 29 күн бұрын
I think you are confusing a ducted fan with a shrouded prop!!!!!!!
@donlawrence1428
@donlawrence1428 29 күн 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: kzbin.info/www/bejne/a4SpeJuln6ZgrKs
@GabrielDeVault
@GabrielDeVault 29 күн 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
@fabriziotieghi9342
@fabriziotieghi9342 29 күн 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.
@SCOUTaviation
@SCOUTaviation 29 күн 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
@fabriziotieghi9342
@fabriziotieghi9342 29 күн бұрын
Geek!! Cool!!
@wolframzirngibl1147
@wolframzirngibl1147 29 күн 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.
@jonnomcintosh8336
@jonnomcintosh8336 29 күн бұрын
Just here again watching this video because it’s so interesting and efficiency of our paramotors can change the way and distance we could fly! 😁🤞🏽
@richardwallinger1683
@richardwallinger1683 Ай 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 .
@Exuma_Guy
@Exuma_Guy Ай бұрын
non-planar blades...
@fabriziotieghi9342
@fabriziotieghi9342 Ай бұрын
The carabiners offset in the miniplane first example is wrong. They are moved to the left, not to the right. Cheers 😊
@SCOUTaviation
@SCOUTaviation Ай бұрын
Yes I messed up. I said the drawing stands for a paramotor torque steering to the right but in the bottom right corner it was labelled as miniplane. That label was incorrect
@fabriziotieghi9342
@fabriziotieghi9342 Ай бұрын
@@SCOUTaviation hello Miro. Thank you for your reply :)
@donlawrence1428
@donlawrence1428 Ай бұрын
I have been working with his research a few years. Id be hsppy to help you get started. I design flying wing models.
@donlawrence1428
@donlawrence1428 Ай бұрын
The aerodynamicist Al Bowers said it can be applied to props.
@donlawrence1428
@donlawrence1428 Ай бұрын
The idea is to reduce the tip vortex strength and move it inboard.
@donlawrence1428
@donlawrence1428 Ай 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.
@EllipsisAircraft
@EllipsisAircraft 26 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.
@donlawrence1428
@donlawrence1428 25 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.
@EllipsisAircraft
@EllipsisAircraft 25 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.
@StabilisingGlobalTemperature
@StabilisingGlobalTemperature Ай бұрын
This KZbinr has tested a large number of designs of boat propellers. Including a Prandtl design which performs very well: kzbin.info/www/bejne/oarNdKqvm9Oli5o
@StabilisingGlobalTemperature
@StabilisingGlobalTemperature Ай 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. kzbin.info/www/bejne/rV7HnGSEpbuBhKs
@SCOUTaviation
@SCOUTaviation Ай бұрын
I learned something new today. Thank you!
@StabilisingGlobalTemperature
@StabilisingGlobalTemperature Ай бұрын
@@SCOUTaviation Great. Al Bowers at NASA has done a lot of work on Prandtl wings. At 39 minutes he discusses Prandtl propellers: kzbin.info/www/bejne/rV7HnGSEpbuBhKs 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.
@StabilisingGlobalTemperature
@StabilisingGlobalTemperature Ай бұрын
What proportion of the annoying part of the noise is from the prop and how much from the engine?
@StabilisingGlobalTemperature
@StabilisingGlobalTemperature Ай 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?
@freecapitan1
@freecapitan1 Ай 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.
@richc.3100
@richc.3100 Ай бұрын
16:17 this is just killing me😂 of course the results don’t match. Too many uncontrolled variables.
@SCOUTaviation
@SCOUTaviation 29 күн 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).
@richc.3100
@richc.3100 Ай 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.
@SCOUTaviation
@SCOUTaviation 29 күн 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).
@richc.3100
@richc.3100 Ай бұрын
14:03 how do you factor all the variables. Pressure, temperature, humidity, pilot input, etc.? Regardless, great video.
@SCOUTaviation
@SCOUTaviation 29 күн 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).
@JohnDoe-fk6id
@JohnDoe-fk6id Ай 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.
@jonnomcintosh8336
@jonnomcintosh8336 Ай 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 👌🏽
@antrygrevok6440
@antrygrevok6440 Ай 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.
@antrygrevok6440
@antrygrevok6440 Ай 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! _ /\ _
@EridanTheEnchanter
@EridanTheEnchanter Ай 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.
@tedarcher9120
@tedarcher9120 Ай бұрын
What about prop winglets?
@SCOUTaviation
@SCOUTaviation Ай бұрын
Do you know any successful application of winglets on propellers?
@austinsmith9413
@austinsmith9413 Ай 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!
@blue_beephang-glider5417
@blue_beephang-glider5417 Ай бұрын
That quiet you enjoyed is why I fly Hang-gliders every chance I get. The powered Hang-glider (Sub 70kg using a Polini Thor130) is only for last resort flying. The new fuel injected engines will allow easy inflight restarts, Ill use the powered much more then just using the engine as a launch and relaunch tool 😎👍