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Cat Hatter
Oct 24, 2006

Hatters gonna hat.

goatsestretchgoals posted:

Someone touch the poop and tell him to put a box of used washers on his store.

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azflyboy
Nov 9, 2005
How do you install install turbochargers backwards?

Did he plumb it so they're dumping the compressed air out the exhaust or something?

jammyozzy
Dec 7, 2006
<img src="https://fi.somethingawful.com/customtitles/title-jammyozzy.gif"><br>Is that a challenge?
I keep staring at diagrams and still can't make heads or tails of it. I think it's a combo sequential/twin turbo setup, with a pressure operated valve that allows turbo 1 to either feed or bypass turbo 2 on the cold side. Then on the hot side turbo 2 has some variable geometry turbine that does roughly the same thing.

It's like someone at Audi was doing rails of coke off that RX-7 vacuum hose diagram when they came up with this.

Sagebrush
Feb 26, 2012

ERM... Actually I have stellar scores on the surveys, and every year students tell me that my classes are the best ones they’ve ever taken.

azflyboy posted:

How do you install install turbochargers backwards?

Did he plumb it so they're dumping the compressed air out the exhaust or something?

I guess a better way of putting it is "out of order." He has a sequential twin-turbo setup with the goal of boosting more than a single turbo (rather than, say, feeding each bank of cylinders separately as in a parallel setup, or reducing lag as in the RX-7). One turbo feeds the next directly as a multi-stage compressor. This is how he plans to keep his car engine developing 300 horsepower at 25,000 feet, where there is only one-third as much air as at sea level.

For his application the first turbocharger needs to be bigger than the second one. The big turbo moves a high volume of air at relatively low pressure and feeds the small one, which works on a small volume at high pressure. He has them installed the other way around. For a good explanation of why this sucks, we go to the aforementioned Audi engineer:

quote:

Hi Peter!

I am a fan of the Raptor project and big respect for you that you pulled it through up to this point! Please let me help with a single quick fix advice which will help your temperature problem by a lot.

As said before in another comment, I was developer for BMW/Audi/VW/Renault Diesel engines.

In your setup, the turbos are staged for boost pressure (at altitude). This means, that the first turbo (low pressure) needs to be the bigger one than the second one, MUCH bigger. Why? While mass flow is constant, the volume changes. The first stage squeezes the air to a smaller volume, but you are interested in the mass. This means, that the second turbo has to be much smaller by the ratio of the pressure rise of the first turbo. The way it is set up in the Raptor, you are experiencing a surging second stage.

OK, this explains why your boost pressure is not much better than for a single turbo setup, but your problem is on the opposite side: the exhaust.

The exhaust gases expand in the high pressure (second stage turbo) and expect a much larger turbo as the second (low pressure). Now, your turbos are almost equal sized, but the second smaller than the first. So you create a lot of backpressure, which rises the EGT to values that I don't consider safe in an aircraft anymore. Why the high EGT? Because the heat cannot leave the engine over the exhaust. Normally, the turbos would let the air expand, recovering the energy that way. But here, due to the backpressure it stays in the cylinders and the turbos are not doing what you want them to.

What is the quick fix? Get rid of the low pressure turbo and only use the high pressure turbo. You will notice that power goes up to 300hp instead of 230hp you currently have and in addition that temperature will go down A LOT! You won't need the twin turbo setup with your current hull (no pressurization and high empty weight).

Hope I could help you and that you take this advice serious. Keep up the good work and wish you much energy to continue your dream!

BR, Andreas

quote:

I first advised Peter to do this a year ago. My comment and subsequent ones by several other knowledgeable people were not just ignored, many were deleted. Peter is sure he has designed the turbos correctly and will not be swayed. Even by people who have been there and got the t-shirt.

I do not know why he thinks the small turbocharger has to go first, but I would be interested to hear his justification. :allears:

Sagebrush fucked around with this message at 23:16 on Aug 9, 2021

Midjack
Dec 24, 2007



gently caress, if you have any idea how forced induction works that's obvious. I didn't realize Raptor man was that dumb.

azflyboy
Nov 9, 2005
Thanks for the explanation. I figured it was something like that, but the level of dumb with the project is high enough that I wouldn't have been surprised if he had plumbed them backwards somehow.

Nebakenezzer
Sep 13, 2005

The Mote in God's Eye

Now I sorta understand how forced induction in cars work, do you not need an intercooler to keep the heat of compressing the air from creeping into the cylinders? I get why the hot side is failing (gas doesn't expand enough to shed heat of compression) but this is a twin turbo diesel that somebody had built poorly and used it in an airplane

MrYenko
Jun 18, 2012

#2 isn't ALWAYS bad...

The kicker is that it’s going in an airplane where you don’t really care about low-RPM boost or turbo lag, so you can just stick the biggest turbo the engine can spin on there so you have the extra compressor capacity when ambient pressure goes down. Sequential turbocharging exists in aerospace, but it’s rare as gently caress, since a single big turbo is generally plenty until you go high enough that you’re probably using a turbine engine anyway.

Cat Hatter
Oct 24, 2006

Hatters gonna hat.

Nebakenezzer posted:

Now I sorta understand how forced induction in cars work, do you not need an intercooler to keep the heat of compressing the air from creeping into the cylinders? I get why the hot side is failing (gas doesn't expand enough to shed heat of compression) but this is a twin turbo diesel that somebody had built poorly and used it in an airplane

You don't need an intercooler, but it greatly increases efficiency for not much money or effort. The primary goal is just to get more air into the engine and hot air has less air in it than cold air at the same pressure. It helps with cooling too, but not really enough that it should cause a problem*.

*Not valid for people turbocharging things that weren't designed to be turbocharged and are already bumping up against the limits of their cooling system.

Platystemon
Feb 13, 2012

BREADS
Staged superchargers were the bee’s knees from like nineteen forty to nineteen forty‐four.

Outside of that, not so much.

Woolwich Bagnet
Apr 27, 2003



My favorite is that he thinks this thing will do 300 KTAS with that engine when in reality he probably needs 2-3x the power for that kind of performance. Of course I have no doubt the plane would rip itself apart long before that speed is reached.

MrYenko
Jun 18, 2012

#2 isn't ALWAYS bad...

300ktas up there would only be ~200kias, so it’s not completely ludicrous. The ludicrous thing is not just making the Velocity work with a GTSIO-520 or something (which would probably still be over his head.) Something where he’s JUST doing airframe integration, instead of airframe integration and an entire power plant re-engineering project.

Woolwich Bagnet
Apr 27, 2003



MrYenko posted:

300ktas up there would only be ~200kias, so it’s not completely ludicrous. The ludicrous thing is not just making the Velocity work with a GTSIO-520 or something (which would probably still be over his head.) Something where he’s JUST doing airframe integration, instead of airframe integration and an entire power plant re-engineering project.

Yeah I suppose that's fair.

When you think about it his design takes all the uncertainty about flying like you'd get with a normal plane. You know you're going to crash 100% of the time so you can always be ready for it!

azflyboy
Nov 9, 2005

MrYenko posted:

300ktas up there would only be ~200kias, so it’s not completely ludicrous. The ludicrous thing is not just making the Velocity work with a GTSIO-520 or something (which would probably still be over his head.) Something where he’s JUST doing airframe integration, instead of airframe integration and an entire power plant re-engineering project.

For what it's worth, the Mooney M20 managed a top cruise speed of about 240kts on 280hp, so I'm thinking this would need more than 300hp to hit 300kts.

Sagebrush
Feb 26, 2012

ERM... Actually I have stellar scores on the surveys, and every year students tell me that my classes are the best ones they’ve ever taken.
Ah but you're forgetting all the supersonic wave drag the Mooney has to deal with that the Raptor won't :dukedog:

Platystemon
Feb 13, 2012

BREADS

Sagebrush posted:

Ah but you're forgetting all the supersonic wave drag the Mooney has to deal with that the Raptor won't :dukedog:

“Am I a bad designer?”

“No, it is the physicists who are wrong.”

mlmp08
Jul 11, 2004

Prepare for my priapic projectile's exalted penetration
Nap Ghost
Need a raptor swag shirt of a guy holding controls as a monster made of re-used parts, overheating, and engine out lights sneaks up on him

“Clever girl”

Salami Surgeon
Jan 21, 2001

Don't close. Don't close.


Nap Ghost

MrYenko posted:

The kicker is that it’s going in an airplane where you don’t really care about low-RPM boost or turbo lag, so you can just stick the biggest turbo the engine can spin on there so you have the extra compressor capacity when ambient pressure goes down. Sequential turbocharging exists in aerospace, but it’s rare as gently caress, since a single big turbo is generally plenty until you go high enough that you’re probably using a turbine engine anyway.

But if you just use another turbo, you can turbo normalize your turbo engine. Now it's at sea level all the time. Bing bong so simple.
Here's the video where he explains his turbo setup. It really does a good job of documenting his engineering design tools: reading websites, Excel, CAD modeling.
https://www.youtube.com/watch?v=Rh-ClOSuoEc

Kia Soul Enthusias
May 9, 2004

zoom-zoom
Toilet Rascal

Platystemon posted:

“Am I a bad designer?”

“No, it is the physicists who are wrong.”



:psyduck:

Sagebrush
Feb 26, 2012

ERM... Actually I have stellar scores on the surveys, and every year students tell me that my classes are the best ones they’ve ever taken.

That's from the lawsuit regarding the kid who was decapitated on the water slide in Kansas, by the way.

Kia Soul Enthusias
May 9, 2004

zoom-zoom
Toilet Rascal

Sagebrush posted:

That's from the lawsuit regarding the kid who was decapitated on the water slide in Kansas, by the way.

Oh right. God drat

Xakura
Jan 10, 2019

A safety-conscious little mouse!
Am I remembering wrong, or is the Raptor way phatter than a Velocity XL? I remember someone made a frontal area comparison on homebuiltairplanes I think, specifically regarding claimed performance numbers and power required.

Humphreys
Jan 26, 2013

We conceived a way to use my mother as a porn mule


Xakura posted:

Am I remembering wrong, or is the Raptor way phatter than a Velocity XL? I remember someone made a frontal area comparison on homebuiltairplanes I think, specifically regarding claimed performance numbers and power required.

soon to be flatter

:v:

Zero One
Dec 30, 2004

HAIL TO THE VICTORS!
The test flight video:

https://www.youtube.com/watch?v=5gnEknj242M

Nebakenezzer
Sep 13, 2005

The Mote in God's Eye

Platystemon posted:

“Am I a bad designer?”

“No, it is the physicists who are wrong.”



:allears:

hellotoothpaste
Dec 21, 2006

I dare you to call it a perm again..


Oh man there’s an hour of this poo poo? :munch: this guy is such a ding-dong!

hellotoothpaste fucked around with this message at 14:41 on Aug 10, 2021

vessbot
Jun 17, 2005
I don't like you because you're dangerous
I finally placed something that'd been bothering me forever. He's the old version of MzeoA guy!

hellotoothpaste
Dec 21, 2006

I dare you to call it a perm again..

“Now you could tie a few knots in it…” (door lever elastic band)

“Now if you just disconnect the spring…” (control stick rebuild)

Hahaha Peter is the worst, if these two weren’t there for testing he’d be dead already.

Scam Likely
Feb 19, 2021

HookedOnChthonics posted:

Collaborate with poor, doomed tom selfridge on a series of interesting pioneer era aircraft, then mostly give up on aviation in a huff when glenn curtiss very rudely decided to start turning profit?





No drag, only lift.

*scrapes across the beach*

Zero One
Dec 30, 2004

HAIL TO THE VICTORS!
Old but YouTube just recommend this to me:

https://www.youtube.com/watch?v=sHMhClzfoi8

That's a big woopsie.

Cojawfee
May 31, 2006
I think the US is dumb for not using Celsius
That's one way to get promoted to civilian

Ola
Jul 19, 2004

Zero One posted:

Old but YouTube just recommend this to me:

https://www.youtube.com/watch?v=sHMhClzfoi8

That's a big woopsie.

How it ended:

https://www.youtube.com/watch?v=qC3zr0Ka-Ac

https://www.youtube.com/watch?v=J7SE-0tD2HE

EvenWorseOpinions
Jun 10, 2017
A guy I knew told a story about how he was ferrying a GA plane with someone. The other guy was setting up for a straight in to the airport, called runway in sight, was just about to flare, saw that the ramp was lined with fighter jets and started climbing again.

Turns out his airport's runway was on the same heading as this one, except that it was several miles further down the runway heading. They gave him a number to call

priznat
Jul 7, 2009

Let's get drunk and kiss each other all night.

Missed opportunity to bust out the RATO rockets smdh

Sagebrush
Feb 26, 2012

ERM... Actually I have stellar scores on the surveys, and every year students tell me that my classes are the best ones they’ve ever taken.

the C-17 is supposed to be able to take off from a 3,500' runway and apparently runway 22 at KTPF is 3,580 feet long. i don't see the problem. it'd be pretty loving embarrassing for boeing if the plane couldn't do it. sheesh

Ola
Jul 19, 2004

Sagebrush posted:

the C-17 is supposed to be able to take off from a 3,500' runway and apparently runway 22 at KTPF is 3,580 feet long. i don't see the problem. it'd be pretty loving embarrassing for boeing if the plane couldn't do it. sheesh

The runway isn't built to handle its weight, so the wheels could actually push the runway surface into the ground, which would lengthen your takeoff roll somewhat.

hobbesmaster
Jan 28, 2008

Ola posted:

The runway isn't built to handle its weight, so the wheels could actually push the runway surface into the ground, which would lengthen your takeoff roll somewhat.

I thought the C-17 was built for operating off weak runways but I just looked up its ACN and its actually quite high at 80, compared to roughly 40 for a C-130 or a small airliner.

slidebite
Nov 6, 2005

Good egg
:colbert:

hobbesmaster posted:

I thought the C-17 was built for operating off weak runways but I just looked up its ACN and its actually quite high at 80, compared to roughly 40 for a C-130 or a small airliner.
That's probably loaded though, right?

Godholio
Aug 28, 2002

Does a bear split in the woods near Zheleznogorsk?
Typically you fly things on a C-17 because it's better than driving/shipping them. That C-17 was loaded when it landed, and had to be unloaded to take off. In addition to transporting the cargo, you also need to send the AF cops over to guard the stupid thing. And yeah, possibly have the runway inspected for damage.

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MrYenko
Jun 18, 2012

#2 isn't ALWAYS bad...

Godholio posted:

Typically you fly things on a C-17 because it's better than driving/shipping them. That C-17 was loaded when it landed, and had to be unloaded to take off. In addition to transporting the cargo, you also need to send the AF cops over to guard the stupid thing. And yeah, possibly have the runway inspected for damage.

Wasn’t Mattis on board for that one?

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