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Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
American ultralights can have retractable wheels if they're amphibious. Or a glider. They can also be heavier if you have a parachute. I think 17lbs is allocated to a parachute. But most are under 10.

Oh, and an important note. Most ultralights "aren't." The affordaplane builds up almost 50lbs heavy. The legal eagle doesn't easily make it under weight. And a variety of others are just barely scraping by.

Nerobro fucked around with this message at 23:02 on Apr 3, 2012

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Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
What's the lifespan of a canopy?

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
Slight cub infestation? That is massive. I'd call an exterminator. Or at least a Bearcat to clean the joint up.

On plane news... I bought a house. It will be about a month before it's totally "in my hands." (203k HUD stuff...)

I'm excited. I"m also seeking opinions on the KR-1.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
I own a house now. :-) And I am negotiating some aircraft materials. woohoo!

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

hayden. posted:

How safe are these ultralights? They look awesome as hell and I've always wanted to get my PPL, but maybe this would be a cheaper alternative.

In a large part pretty safe. The idea is that they're draggy enough to never get going that fast, and in full stall they're falling at a non lethal airspeed.

Really, they're as safe as you want to be. If you treat them as a "real airplane" they're as safe as a real airplane. If you treat it like a lawnmower... well you can expect some lawnmower ish things to happen.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
I've always said that there are model airplanes that could carry a person. Now you're using model parts to carry you. :-)

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
It would seem money is starting to go my way. I think I can order aluminum this week. that means I also need to build some work tables and start doing an ever loving butt-load of layout.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

babyeatingpsychopath posted:

Here's a question I haven't seen addressed at all:

Why not use motorcycle engine units for light aircraft? You can very easily find a whole motor kit that's the same size and weight, and has all the accessories strapped in. The shipping weight of a hayabusa motor with EVERYTHING bolted on (including battery) in a crate is 175lb. Add a few pounds for oil. They're also designed to run near redline for a long time. The "needs reduction gearing" is moot because the transmissions are built in. You could easily run a chain drive to a thrust bearing and not worry about modifying the engine cases at all.

It may also be beneficial for cruising to leave the transmission in and just upshift to put yourself in a more efficient engine range, then downshift back into the powerband for TO/GA.

Is this crazy talk?

It's only "sorta" crazy talk. There's a lot to consider though.

Piston speed directly relates to engine life. Most motorcycles (the Hayabusa included) run with some fairly high piston speeds. While the base motor might make the power, and do it light enough, it's durability is in question.

Second, sustained power levels. Motorcycle engines, for the most part, are designed for intermittent power. You'd need to look at adding an oil cooler, and potentially piston squirters.

You'd also need to consider cylinder head heat soak. If the cylinder head can't extract the heat, you'll end up melting exhaust valves.

Changing the gears isn't a very useful trick. At most you'd need two. changing prop pitch is the air going equivalent. To give an idea of why it's not so useful. If an airplane is sitting still, on the ground, and at full throttle, you can expect only a 200rpm drop versus cruise rpm.

Also, with changing gears, pilot workload is an issue. So you don't want to do anything that's gonna stress a guy out while flying. More features is not more better!

Propellers are heavy. And they're springy. This means the forces that come back from the propeller are difficult to manage. (This is also why wood props are popular. They self dampen somewhat.) Each gear interface, is a place where all the loads of the engine are placed on some very small gear teeth. This leads to a catastrophic failure mode. Namely munched gearbox!

The single plug ignition is "something" of a concern. But there are plenty of airplanes out there there fly with single plugs. Including all auto conversions. You can set up redundant ignitions without redundant plugs. It wouldn't bother me much.

The fuel injection system is a problem. The Hayabusa computer doesn't know what to do with changing altitude. Put in a new controller. Older bikes, with CV carbs are at an advantage there. CV carbs are altitude compensating! Which means you remove a control for the pilot. The Rotax 912 has CV carbs, so that's even certifiable.

After a lot of thought on the subject. I concluded that the only way to use a motorcycle engine in an airplane, was to cut off the gearbox. You get several advantages there. First, lower base weight. (though you'll need to add a reduction gear...) Second, you can use a belt type reduction unit, which addresses the resonance issues. Third, you end up with an excuse to build a proper sump, potentially with a lot of cooling area, removing the need for separate oil cooler piping and the associated points of failure.

The motors from motorcycles that most easily convert to airplane use are the bmw boxer twins, the honda flat fours and sixes, and harleys. All of those motors are separate crank and gearbox engines. And most of them run conventional car speeds. So you're not really finding more power.

I suppose you could fly on a MotoGuzzi... but I have something deeply against using italian motors for anything that's life dependent.

All of that said..... You have the same concerns with a car engine. And car engines fly all the time too.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

Ferris Bueller posted:

*Which is kinda funny that so many experimental builders are not actually experimenting, but I understand where they are coming from. Yes I realize that many guys are experimenting as well, and I'm not trying to dig anyone at all who has the balls/whatever to build their own airplane, tried and true design or drawing it up yourself.

I have had this argument with myself a few times. And.. after hanging out on enough builder forums, I've determined that even though you fly a "RV6" or "A Hummelbird" or whatever.. the chances of your plane matching the performance of another plane are so slim that you might as well be flying a one off.

That's what makes a certified plane so expensive. Building the planes to the EXACT SAME STANDARD so that the same numbers can be used from plane to plane. the RV's get close... But most homebuilts tend to be different in some significant fashion from the plans, or even the kit. Sadly, most builders don't thoroughly test their planes to properly determine what their flight envelope really is.

I'm currently on the KRnet, and the DA-2 mailing lists. I was kicked off the Affordaplane mailing list. ;-)

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
so.. I'm trying to buy 2024 t3 aluminum from somewhere OTHER than aircraft spruce. .025 and .040

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

zharmad posted:

I've had affordaplane plans for a while, and plan on building one once I get back in the US. My wife has concerns about my safety while flying, even though I plan on taking flying lessons before I ever try flying on my own. Does anyone have a whole-aircraft parachute or have any experience and recomendations for one?

You just stopped my heart. My recomendation, is buy a parachute, but don't build an affordaplane.

The Affordaplane is a flawed design. The design is more so flawed because nobody has actually characterized it's flight. Built to plans, it will be more than 75lbs overweight. That's 30%! Your wife SHOULD have concerns. Balistic parachutes are a good plan in general.

There's no reason you can't build a plane that's "affordaplane shaped." But you should spend some time with a calculator and re-do all of the dimensioning. You can save THIRTY POUNDS of fuselage weight, and still retain strength to support 10g's of loading. ... After accounting for the 60% derating for aluminum in high vibration environments.

I made and maintain (heh) http://theaffordaplaneresource.blogspot.com/ Lets say I put a lot of thought into my opinion.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
And here we are a few hours later. So.. If you are set on the affordaplane, I can send you my notes on it. The changes are .. extensive.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

zharmad posted:

Well, I haven't bought any material yet, but was looking for a project to start over this winter. I'm not married to the affordaplane at all, but I expect to have about 90 days that I'm not working to devote to the project. Is it worth the time to re-work the plans or is there a better plan out there I could get?

Well, to be really silly. You can buy an off the shelf ultralight. Brand new, for $10k.

The legal eagle is a better plane. And it can be built under weight. The ultra baby can be done as well, and it shows the designers work, so you know the math is right. The Sky Pup is definitely 90 day able, but it's not a 3 axis ship.

I really like the fischer flying products airplanes.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
http://www.n56ml.com/n981jf/

Please tell me not to build a KR? Please?

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

helno posted:

Changing your mind about the DA2A?

Not really. Just that KR-2 is pretty as hell, and makes almost everything on the market look bad.

Getting my hands on .025 and .040 alclad 2024 t3 seems to be harder than I was expecting. Any suggestions that don't have spruce in the name?

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
First off, since you're getting your license, why limit yourself to a ultralight? There are a lot of small, easy to build airplanes out there. Which opens your options to all sorts of "normal" engines.

Is the engine the only thing that is really keeping you on the legal eagle?

My only "problem" with the legal eagle, is that you need to learn to weld, as well as woodwork. A texas parasol is a very similar rig, but is all wood, simplifying life quite a bit.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

charliemonster42 posted:

My biggest concerns with doing a full scale airplane is time and money. I don't know how readily I'd be able to commit 3 years to a project like that. I've looked at a few full size kits, like Sonexes and RVs and the like, and would love to do one, but the level of involvement with a kit like that is orders of magnitude bigger.

The Legal Eagle is stuck in my head because it's the first one I've really looked into is all. I'm comfortable with welding and need an excuse to improve my skills. I suppose the 4 stroke aspect of it made it stick more than the others because it sounds more enjoyable. The weight penalty of the 4 stroke really is a pain in the rear end though.

What are the odds of getting caught with an overweight ultralight? How would they even know? Ramp check you?

Ultralights, and "full scale" airplanes are very close in size. In fact, for single seaters, ultralights tend to be much, much bigger than "full scale" airplanes.

For example, a KR-1
Length 12' 9"
Wing Span 17' 0"
Total Wing Area 62 sq. ft.
Cruise 180mph

Lets compare that to a Lazair:
Length: 13 ft (3.96 m)
Wingspan: 36 ft 4 in (11.1 m)
Wing area: 143 sq ft (13.3 mē)
Cruise 40mph

The lazair is almost twice as big!

Lets try another. The Legal Eagle:
Length: 13 ft 0 in (3.96 m)
Wingspan: 23 ft 6 in (7.16 m)
Wing area: 107 sq ft (9.9 m2)
Cruise speed: 50mph

Lets get back to "conventional" aircraft. Those that don't have the ultralight tag. I'm going to stick wtih single seaters to keep things even.

Rutan Q1 "Quickie"
Wingspan 17 ft 9 in
Length 17 ft 5 in
Cruise 120mph

FRED
Wing span: 22 ft 6 in (6.86 m)
Wing area: 111 sq ft (10.32 sq m)
Length: 16 ft (4.88 m)
Cruise: 71mph

RV3
Length: 19 ft 0 in (5.85 m)
Wingspan: 19 ft 11in (6.12 m)
Cruise 170-190mph

So, why a "legal" plane versus an ultralight? Ultralights live in a very narrow range of airspeeds. And in a very narrow range of weight loading. Ultralights can't fly around populated areas. Ultralights aren't really welcome in controlled airspace. Ultralights have quite short durations.

Building a plane that fits into the narrow little corner of the law that is "ultralight" is just that. A plane that exists in a narrow little corner of the law. If you don't need to live in that little corner, don't.

Building an ultralight means leaving a lot of the fun stuff at home. A decent guage cluster. Comforts, and even some safety systems. You don't see carb heat on ultralights, nor cabin heat. You also almost never see flaps, and things that you should want to use to keep your skills up.

"Real" airplanes give you more room to fudge. You can leave things a little heavier and you will still get a decent plane. "Real" planes also are smaller, which means there's less material to buy, and usually cheaper materials to buy. They also tend to use normal covering techniques, and normal materials, so you can get normal advice from normal airplane people.

Not that I'd personally use normal materials or covering... I'm just saying.. you can. :-)

Now, you asked about the plane getting checked. As far as I know, nobody gets checked. But, if you crash, and there are legal proceedings, your rig WILL get checked, and then you could be up the creek. Operating an unregistered aircraft, that sort of thing. And no insurance will want to touch you ever again.

Why do you think an airplane will take you three years to build? why do you think a Legal Eagle will take much less time than say.. a Cub clone? (they are of about equal complexity.)

Something like a FRED assembles very quickly. So can a KR-1.

I went through the same thing. I didn't think I could afford to actually get a pilots license. when I discovered that it was going to be a reality, I did a careful check of myself and what my desires were. Building a ultralight just didn't make any sense once I knew a real license was in reach.

Recently I read through all of bob hoovers blog. I picked up all the really choice stuff on building an airplane on the cheap. http://realtinker.blogspot.com/2013/04/cheap-aircraft-building-techniques.html

Helo: no offence eh? :-)

Ninja Edit: And somehow i got through a post without mentioning a DA-2 or a Hummelbird. Amazing.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

Sagebrush posted:

My understanding of why rotary engines seemed to be a good idea in planes is that it came down to two things: (1) the inherent smoothness of the design, and (2) with iron rotors in an aluminum housing (vs. aluminum pistons in an aluminum or iron housing) they can't seize from overheating. You can also run a rotary engine with pre-mixed oil like a two-stroke, which saves you from having the oiling system as a point of failure.

Not sure why they fell out of favor, though. Just too strange a design for people to get used to?

That's because nobody "really" seems to understand wankels. (I avoid the term rotary because that can mean a different kind of engine. See: Gnome rotary)

Wankels really don't seize. (Modern cylinders and piston rings don't either..) But they do start detonating. Instead of seizing, the hot cylinder walls start to bulge, and you lose compression. And you lose apex seals. Or, if you manage to keep the seals around, then they start detonating, and really bad things happen. Like busted center section bearings, and more, blown out seals.

The big advantage with a wankel, is it's size. They're downright tiny. However, they aren't a light as people seem to think they are.

The need to have oil in the fuel is a sign of a design FAULT, not a design advantage. You can run a little oil in normal piston engines and it helps with ring life. Much as it helps with apex seal lift.

The fundamental problem with Wankels is cooling. Piston engines have several methods for cooling pistons. There's the incoming air charge, there's air under the piston, there's contact with the cylinder walls, there's heat conduction through the rings, there's oil squirters to cool the bottoms of the pistons...

There's NOTHING to cool apex seals, other than contact with the cylinder wall. And then they don't get any oil.

The only way to carry significant heat from the rotor, is through oil. (or, in the case of the Hercules motorcycle, intake air... It ran the intake air through the rotor.) Oil management within the rotor isn't easy.

There's also no easy way to increase the displacement of a Wankel. Rebuilding one is not far removed from building a new engine, because you can't refinish the cases.

And, from what I've seen of installed weights, the weight of a Wankel is comparable to whatever horsepower engine you intended to run in the first place.

... I am a fan of these motors.... I've got several books on their history, and the math involved in them is inspiring. So is the story of making them survive. And the different engine case arrangements. (thing spinning block, with a straight crankshaft...)

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
When did you leave? I was there on saturday.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

kastein posted:

What are people using for PSRUs on Subaru engines?

First off, what plane do you have in mind?

I would recommend avoiding PSRU's. And that horsepower level for a subaru seems.. very, very high. I strongly suspect you'll run into head cooling issues at that sort of power level. I can go into the whole explanation of why "romp all day at 250hp" isn't the same as "flying at 200hp" if you'd like.

So, to avoid the PSRU issue, feel free to run boost. Build for torque. Spin a multi blade propellor a little faster, and keep the blades shorter. You can find a lot of usable power without going to 6000rpm. Take a look at the people flying Corvairs.

If you're dead set on trying to get 250hp from a subaru for any useful length of time, and require the PSRU, building your own is not an insurmountable task. I'd look at this guys documentation, http://www.zenith.aero/profile/Ben He's got a v8 engine driving a (mostly homemade) PSRU.

We can also discuss what causes crank, and PSRU failure. :-)

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
1900 foot pounds isn't enough. At least not without some very, very, very, serious torsional damping in place. Hardening has it's own share of issues, beacause with hardening, comes brittlenss.

Propellers are big springs. They resonate. If you reach the right rpm, where the power impulses are anywhere near the same frequency as the prop is rotating, you can build some massive forces in fractions of a second. The big advantage of having a zero lash drivetrain, is as those forces build up, they never unload the mechanical bits. The hammering action of teeth on each other causes even mild resonances to weaken and remove teeth rather quickly.

Piston sprayers shouldn't be left on the table, don't add those as an upgrade, do them the first time. I can't say it enough, the sort of operation that airplane engines sustain, isn't equaled anywhere else that most people have experience with.

Another thing to look at, is the Subaru engines aren't all that light. A good PSRU isn't going to be light either. If you really want 200hp, there are other engines that can do 200hp, without needing a massive array of associated support devices. For example, the ford SHO v8, is making 210hp at 4800rpm. And is a mere 390lbs. And then there's the classic inverted oldsmobile V8 in the wittman planes.

You can check this for installed weights of subarus.
http://www.sdsefi.com/air51.htm

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

MrYenko posted:

That thing looks like what you'd get if you asked a scale modeler with zero engineering knowledge to build an airplane.

I read this as if you were talking about someone who builds flying model planes. Instead of scale models that sit in dioramas. The first interpretation borders on insulting. :-)

A lot of r/c people don't understand engineering, but somehow do grasp "what seems right" and they make planes that fly very well.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
well.. I'm sure there's a lot of good wood there. "aircraft quality" wood is a matter of selection, more than "as delivered" state. But geeze, that pile doesn't look good.

I love how he thinks his 1/10 model which was 800g, will be 750kg once scaled up.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
You need to buy that thing just to fix everything that's wrong with it. :-) What's it's useful load?

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
Yes.

Many of the first and even second generation of ultralights only had (or have) elevator and rudder control. Anything controlled by weight shifting realistically only has two axis of control as well.

Unless you mean "rudder and throttle" control, which is another story entirely. You're giving up a lot of control at that point. The ability to "get in to trouble" also means the "ability to get out of trouble" While I'll happily fly a free flight glider that has no control, I wouldn't ride a free flight glider with no control.

Even powered parachutes have elevator control of a sort. By pulling on both control straps you can chose to slow down and descend more quickly.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

edmund745 posted:

So what control problems do powered parachutes have?
Wind gust caused collapse of the canopy is a big control problem.

quote:

Because a powered parachute proves that you can have an aircraft that is entirely flyable yet never inverts, never stalls and never spins.
I think I've seen a parachute looped. And you can get into a spin with a parachute that you can't get out of.

Most important with powered parachutes, is that their speed range is very very small. You've got just a few miles per hour between the fastest you can go level, and the slowest you can go level.

quote:

Is fly-by-wire even a realistic option for homebuilt aircraft yet? What is the cheapest factory-built aircraft that has it?
(I know enough about electronics and programming to say that it can certainly be done DIY--but what is the legal climate like for such an aircraft? Is anybody actually flying anything like that?)
I do not believe fly by wire will be a "thing" for GA aircraft in our lifetimes. So long as the existing legal precedents are still standing. And what's the point? GA will always be positively or at least neutrally stable aircraft. Fly by wire doesn't really show it's advtanages until an airplane is on the wrong side of the stability curve.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

edmund745 posted:

Yea, and losing the parachute canopy and switching to a canard/fixed wing arrangement would totally fix that problem. This is what surprises me about the observation that such aircraft don't already exist.

Yes, it would essentially be a single-speed aircraft. So (for example) it would climb at 55 mph, cruise at 50 mph and descend at anything less than 50 mph.
You wouldn't be able to fly acrobatics with it, but it would be an enclosed cabin, much higher speed than a powered parachute, much less noise and much better fuel economy/longer range.
You fall down the hole of "might as well". By the time you have an "airplane" that flys, you might as well give it controls that are effective. And you go from being single speed, to a competent airplane. I don't see where the niche could grab a foothold. To do what you want, you just need to fix the controls, and set the CG of a "normal airplane" to a fixed, stable, configuration.

quote:

That would not work for all purposes--but I would bet that for a lot of small aircraft/recreational flying a lot of people wouldn't have a problem with it.
Choosing a specialty airframe that limits your learning and experience with other airplanes? I think it would be a problem... It's like choosing to drive an electric trollycar to learn how to drive a stickshift car.

The people who flew single control airplanes the most, were RC people. They were able to weasel out a lot of control from a single surface, but those lessons don't translate well to flying a fully controlled airframe.

quote:

Well,,, I did not suggest the fly-by-wire option.
But even so--how would a fly-by-wire system help anything at all? It would help by limiting what you could do with the controls of the plane.

It would seem to be safer to design an aircraft to totally prevent unsafe maneuvers than to install a fly-by-wire system to prevent them, or to just use mechanical controls and hope the pilot never makes any such mistakes.
Airbus uses fly by wire to save airframes. Using controls that are limited to stop airframe overstressing is a design feature of the Ercoupe and the Skypup. Some other planes uses aerodynamic weighting of surfaces to overcome the strength of the pilot.

As has been mentioned, stall speed is the single biggest factor in safety. This discussion starts to hinge on "who you plan to have flying." A 3 year old could fly a throttle + rudder plane. With no training. (also note I'm not talking canard, the "can't stall" stability can be built into other layouts as well)

In that case, your crash speed, will be essentially your cruise speed. ... Unless you have an adjustable tailplane to act as speed trim. but at that point, you might as well give the pilot control of the elevator.

This discussion has me thinking about flying cars. If you can treat a plane like a gokart, why shouldn't everyone fly? The factors that answer that, also indicate why a dumbed down airplane probally isn't ideal.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

edmund745 posted:

It's not my pet theory; powered parachutes have been flying around on single-axis control for ~33 years.

PPG's are not as simple as you think they are. They have at least two, if not four controls. By pulling on the two drag lines at once, you can slow down the PPG, and convert some forward speed to lift. IIRC they also have "speed" lines too.. or that may just be paragliders. Those give you elements of control that a throttle and rudder airplane just won't have... unless it's very marginal.

Using just rudder, people were able to climb, dive, and even loop single channel r/c airplanes. That said, nobody does that anymore, because more control is better.

At some point here, you need to explain what you think the killer application of a two control airplane is. What would be the niche you'd sell into?

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

edmund745 posted:

I asked about any examples of fixed-wing-single-axis control aircraft, and there appear to be none. At least, not known to anyone here.
I find it odd that single-axis-control is entirely acceptable for powered parachutes, yet it is presumed to be wholly inadequate for fixed-wing aircraft.

You keep saying it, but PPGs are NOT single axis control. The ONLY example of single axis control are r/c airplanes, they work. You've still not pointed out what the "killer app" for this would be.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

edmund745 posted:

Why do you insist they are not?

This page:
http://buckeyedragonfly.com/
says in the FAQ:

It has a throttle (that is not counted as a control axis on other aircraft) and it has foot controls to turn left or right--which is only one control axis. That is one-axis control.

It would be for people who liked how easy PPGs are to fly, but didn't like how slow/noisy/open they are?
Also it would be for people who don't ever want to stall or perform uncoordinated turns, since doing either of those things would not be possible (even intentionally).

I insist they're not, because the people who seriously use parachutes don't use single control canopies.

You need to take a close look at why people fly PPGs. Because you're really missing why people fly PPGs.

By giving up elevator control, you're giving up the ability to positively touch down, or take off. That's a huge risk factor.

Stalls aren't scary. Uncoordinated turns is what happens in a "classically" designed airplane. You can make planes auto coordinate. Though that ends up only working right for certian airspeeds.

You've still not convinced me that there's any significant group of people who'd want to fly a crippled airplane.

You also seem to think PPG canopies are foolproof. A good gust at the wrong time will collapse the canopy and you're in deep doo-doo unless it decides it wants to re-inflate.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

helno posted:

Met some interesting people. Got to chat with Burt Rutan and a couple of his buddies while flying r/c aircraft.

My jealousy is unending. I was up there on saturday, it was a good day.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

helno posted:

Parked.

Happened last week. We never took the cover off afterwards and I went out today to take it flying and found the broken window.

That doesn't ground you does it? Expensive, demoralizing, but does it stop you flying?

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

MrYenko posted:

Finally, a fuel tank that makes your wedding tackle part of the crash structure!

(I'm jealous, and redirecting my jealousy to sarcasm.)

Never looked at a CriCri or Quickie eh? :-)

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!
He... is better prepared than most people who've dove into that. His plane is already better than some plans you can pay for. He is a very, very, good TLAR engineer, and doesn't often get it very wrong.

Each episode shows a lot of learning. While he didn't discuss it, between the night fligth, and yesterdays flight, he taped the wing gaps That alone took the plane from barely flying to solid flying.

... He has had lots of hours training for his PPL. He's got his ultralight, that's actually less than 254lbs. (which can't be said about a lot of them..)

If he did math, he'd knock 10lbs off the plane...

I wouldn't worry much. Peter is safe (mostly) and will provide entertainment for years to come. Just... dont' do what he's doing.

Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

MrYenko posted:

All the problems of multiple engines, with none of the power reserve!

It's probably ok though, because I don't think he has the power even with both motors to leave ground effect.

He's been out of ground effect. He was out of ground effect before fixing the leaking wing panels. The wing gaps are EXTREMELY important. For a long time GWS sold a plane called the slow stick. It had two wing panels attached at the center, with a gap between them. If you closed the gap, you got something like double the flight time, and a 50% better glide ratio.

It's also worth mentioning, he's running on only 80% of the voltage his motors are designed for. So that's going to get "fixed" too.

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Nerobro
Nov 4, 2005

Rider now with 100% more titanium!

helno posted:

Even in the latest video it looks pretty marginal power wise.

I bet he could have saved a lot of weight in the fuselage design.

The places weight could be saved are numerous. He's still a totally legal ultralight. Wtih none of the "funny business" that many of the other ultralights do. LIke.. Belite and the removable fairings. Or the other electric ultralights having 5 gallons (volume) of battery...

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