such fantastic work and attention to detail; cheers my friend
@Mister_G4 ай бұрын
Thank you very much indeed!
@holidayryu94072 жыл бұрын
You have finshied everthing that I have dreamed. I wated to make by hand every thing related with rc jet engine. You alomost showed that except electronics like control unit. But I love it. Great!!
@Mister_G2 жыл бұрын
Thank you very much! At the moment there is no electronics, but I'm trying to make a better RPM sensor which might mean an Arduino, so I may as well have that display EGT as well... And if it knows about those things, it may a well control the fuel, too... (You see how these things snowball :D ). Thanks for the comment, and thanks for watching. :)
@modelaircraft6576 Жыл бұрын
Very detailed and well understood simple assembly video. Is cheaper building kit turbine than buying fully built one great work mate
@Mister_G Жыл бұрын
Thank you very much indeed for the kind words. 🙂
@reedy932 жыл бұрын
really nice job on machining and finish.
@Mister_G2 жыл бұрын
Thanks very much! 😊 (I still haven't tried it on kerosene yet, but it's close.)
@cytron87872 жыл бұрын
Nice job , love your work.
@Mister_G2 жыл бұрын
Thank you very much, indeed! 😀
@yousefashry2897 Жыл бұрын
What will happen if a used pla for making that compressor inlet and the cover of this inlet?
@Mister_G Жыл бұрын
The actual inlet (before the compressor wheel) would probably be OK. The compressor wheel / diffuser cover would probably get too hot for PLA - the theoretical temperature rise across the compressor is ~~100°C, so the compressor exit temperatures could be pushing 120°C - it is on the limit for the epoxy used to glue in the diffuser vanes. From what I understand, PLA will start to soften at 50-60°C
@yousefashry2897 Жыл бұрын
Thank you so much 🌸
@yousefashry2897 Жыл бұрын
@@Mister_G i found a compressor wheel for kj66 which is has the same excducer and height but differs in inducer diameter, instead of 46.1mm it became 39.7mm what do i need to change in the inlet bell dimensions ? kkk 2038 dimensions K26 Turbo parts compressor wheel Inducer "ØA"=46.1mm Tip Height "B"=5.9mm Exducer "ØC"=66mm Hub Length "D"=33.5mm Bore "ØE"=7mm No. of blades:6/6 kkk 2036 dimensions Nose diameter:13.53mm Inducer:39.71mm Exducer:65.94mm Tapered tip exducer:69.92mm Tip height:4.47mm Superback:0.00mm Overall height:30.88mm Blades height:26.47mm Trailing angle:55 degree Bore size:7.02mm bore type:through Cutback:0.0 Splitter height:18.50mm Sp height angle:-7.00 6+6 blades Forward rotation Tapered tip angle:30 degree
@Mister_G Жыл бұрын
@@yousefashry2897 You'd need to make the intake diameter smaller to suit the inducer diameter of your wheel, and also you'd need to figure out what the profile of your wheel is, and adjust the radius of the intake profile to suit (not easy to measure this).
@yousefashry2897 Жыл бұрын
@@Mister_G i will use car's fuel pump because i can't find any suitable pump here but this, how can i adjust it to suit this engine ?
@wjstk1725 Жыл бұрын
Hello I'm enjoying the video Is the bearing lubrication in the shaft housing on the compressor side by drilling a hole in the intake cover and connecting the copper pipe? Don't you need to lubricate the bearings on the turbine side?
@Mister_G Жыл бұрын
Hi, and thanks, glad you are enjoying it. If you pause the video at 3:20 you can see that the small pipe fits into one of three slots in the front of the engine. A small amount of air from the compressor flows through these slots into the bearing tube, through both bearings and out of the back of the engine. A small amount of fuel/oil mix is pumped into the small tube and this forms an oil mist with the air that lubricates both bearings before being burned off as it comes out the back of the engine.
@wjstk1725 Жыл бұрын
@@Mister_G thank you for your answer. I have one more question As far as I understand, 1spool consists of an impeller, a shaft, and a turbine After securing the bearing to the housing, the outer diameter of the bearing is fixed with the shaft passing through the inner diameter of the bearing, and the shaft rotates as the bearing rotates the inner wheel. In the video, the inner diameter and axis of the bearing don't fit tightly and there's plenty of room Does the axis spin without tight tolerance between the axes of the bearing?
@Mister_G Жыл бұрын
@@wjstk1725 The inner diameter of the bearing is supposed to be a very close sliding fit on the shaft (it could probably be tighter than shown at 15:50). The inner race of the rear bearing is clamped to the shaft when the nut holding the turbine is tightened, and the front bearing when the nut holding the impeller is tightened - the shaft can move at 15:50 because the impeller (and the spacer behind it) have yet to be fitted and tightened down. Does that answer your question? If not, please ask again 🙂 There's a cross section of the engine on my website which may help things make more sense.
@wjstk1725 Жыл бұрын
@@Mister_G Thank you for your explanation😉
@lunakendallthebabyfingermo7524 Жыл бұрын
Any way I can get a parts and measurements list
@Mister_G Жыл бұрын
Hi, the design is all described in Thomas Kamps' book (details in description). Cute monkey, btw! :)
@مجيبالقباطي-ج9ح Жыл бұрын
You are amazing and wonderful
@Mister_G Жыл бұрын
Thank you very much. I feel warm and fuzzy inside now, ☺
@MrCzarnm Жыл бұрын
This engine was build using mini lathe ? In terms of turning operations ?
@Mister_G Жыл бұрын
Hi - yes, it was. (The compressor wheel was bought in though).
@MrCzarnm Жыл бұрын
@@Mister_G For KJ-66 did you recommend mini lathe or bigger lathe for project or mini lathe is fine ?
@Mister_G Жыл бұрын
@@MrCzarnm KJ66 is roughly the same size as this engine so it should be possible on a mini lathe, but a bigger lathe is always better! The diffuser on the KJ66 is usually milled from solid (as far as I know) which would require access to a milling machine of some sort. (The diffuser on the Kamps is made with sheet metal blades, so only turning is required). Also, I think the KJ66 uses a cast inconel turbine - I'm not sure if they are still available and at what cost.
@markrix2 жыл бұрын
Im quite confused how you created a good oil seal, it seemed like that feed tube just kinda is pancaked in the mating for the center shaft housing, does it leak oil?
@Mister_G2 жыл бұрын
Hi. Yes, you are correct in your observations - The lubrication system is a "total loss" oil mist - A small amount of pressurised air from inside the engine blows through the slots between the diffuser and the shaft tunnel and into to the inside of the shaft tunnel (which is open at the rear end). The pipe is just clamped in one of the slots (not tightly enough to close the pipe off though) and any oil that comes out of it is carried away by the stream of air. This produces a stream of air and oil droplets flowing down the inside of the shaft tunnel and through the bearings which cools and lubricates them. When this stream comes out of the rear bearing, the oil just gets burnt up with the exhaust from the engine (a bit like how a 2 stroke petrol engine is lubricated). Thanks for asking!
@Telyron2 ай бұрын
It seemed to make a lot of friction when you manually span it…
@Mister_G2 ай бұрын
Yes, it's trying to pump air all the time, so it won't spin for long, even with "frictionless" bearings. It does sound awful here - the cage-less bearings are very noisy when they're dry and the balls don't really space out properly until the bearing is running. Everything is OK though.
@yousefashry2897 Жыл бұрын
Did you scale up the size of the kj66 Turbine?
@Mister_G Жыл бұрын
Hi - No, this is a slightly different design, although very similar to the KJ66. The turbine is the same, 66mm diameter.
@yousefashry2897 Жыл бұрын
What is the name of this design please?
@Mister_G Жыл бұрын
@@yousefashry2897 It's usually called the 'Kamps' engine because it comes from the book by Thomas Kamps. (Link in description, I think.)
@demoaccount23922 жыл бұрын
How about the bearing lubrication system
@Mister_G Жыл бұрын
Hi - it is a total loss system using a small amount of fuel/oil mix that is bled into the front of the shaft tunnel from the main fuel supply.
@demoaccount2392 Жыл бұрын
@@Mister_G Oh, nice. Actually does it have a negative effect on the fuel economy and what if I use a full hybrid bearing, thanks
@Mister_G Жыл бұрын
@@demoaccount2392 The feed to the bearings is only about 1% of the main fuel flow. (have a look here for more details: misterg.org.uk/runing-on-kerosene/ ). Fuel economy is not high on the list of priorities for this engine :) I am using hybrid bearings.
@demoaccount2392 Жыл бұрын
@@Mister_G Thanks
@Fabioaw2 жыл бұрын
Good job MisterG. I saw your test run video. The engine runs very smooth and looks well balanced. I appreciate if you could share the brand of the hybrid bearings that you are using? I'm also developing a small turbine but I'm facing high level of noise and vibrations.
@Mister_G2 жыл бұрын
Hi, Thank you very much for the kind words :) The bearings are full complement hybrid bearings - I could not find any ready made at a price that I could stomach, so ended up buying some generic, caged, hybrid bearings (from ebay / Alibaba). I took the balls out of these and machined away one side of the inner race so they could be reassembled with a full complement of balls (the extra balls taken from another bearing of the same type). This is not my original idea, but it works well because the bearings are pre-loaded against the un-machined side of the race. There are some photos here: misterg.org.uk/turbine-html-10/ Others suggested doing the same thing, but buying Si3N4 balls of the identical size to the originals but every type of bearing I took apart seemed to have very slightly different ball diameter. I am no expert on turbines, bit I would say to check that the shaft is straight after fitting the turbine - I was very, very surprised how easy it was to send the shaft out of true when the turbine nut was tightened - just a slight burr or speck of dirt on the mating faces will cause a runout on the shaft. A sensitive indicator will tell you. Runout on my assembled shaft was ~0.004 mm TIR. (Feel free to contact me via my website if you want to discuss further). Good luck! 🙂
@Fabioaw2 жыл бұрын
Dear MisterG, Thank you for your attention. I agree with you that the shaft parts concentricity is critical for turbojet engines. I need to improve the machining process of my shaft and shaft tunnel to achieve better alignment. I found some misalignments in the shaft and due to this the balancing of rotor parts assembled is affected too. After that I will check the quality of the bearings too, if necessary. Congratulations to your website. There is a lot of good information. Thanks
@Mister_G2 жыл бұрын
@@Fabioaw No problem - let me know i I can help.
@كثيرالطيب Жыл бұрын
مدهش 👋🇰🇼
@dakumangalsingh138411 ай бұрын
If i want to make it from scratch, do you have 3d printing files of these ???? Pls can u share me everything. Btw i looked the description yet i want a direct way to achieve what you have Pls share if u have any🙏🏻
@Mister_G11 ай бұрын
Sorry, I don't have 3D printer files. The design belongs to Thomas Kamps, and the drawings are in the book.
@dakumangalsingh138411 ай бұрын
@@Mister_G oh, thanks alot for the guidence
@dakumangalsingh138411 ай бұрын
@@Mister_GThe book that you mentioned in the description does not ship to India and the only option i have is to search on Amazon cuz Amazon had this book but it costs ₹42.8k INR that is £406 ($517 USD)💀💀💀, No way i can afford it Do u have the pdf of the book😶🌫️ any chance?
@Mister_G11 ай бұрын
@@dakumangalsingh1384 I don't but I believe you may be able to find one on the internet...
@lawahanglimbu6220 Жыл бұрын
Wow, I never saw a combustion chamber built with thick steel plates, usually builder builds with thin steel plates, which i'm familiar with. Is a thick or thin steel sheet compatible for sustainable performance ?
@Mister_G Жыл бұрын
Hi - the combustion chamber is made from 0.5mm thick 304 stainless steel. I suspect that commercial engines might use 0.3mm, but 0.5mm was quite thin enough for me to work with!🙂. Thanks for watching and commenting.
@markrix2 жыл бұрын
How many pieces of this started as cookware?
@Mister_G2 жыл бұрын
Ha ha! None of it in this case, but I did prowl the stainless steel aisle with a tape measure,,, Just couldn't find anything suitable :)
@markrix2 жыл бұрын
Either way very pretty, looking forward to preformance figures and personal evaluation.
@johnkelly72642 жыл бұрын
Ohh Ohh.. This is brilliant! Could you tell us the ISBN of the Thomas Kamps book that you used to build this engine pls?
@Mister_G2 жыл бұрын
Thank you very much! 😊 The book is "Model Jet Engines (3rd Edition)" by Thomas Kamps. ISBN 978-1900371933 www.sarikhobbies.com/product/model-jet-engines-3rd-edition-by-thomas-kamps/?page&post_type=product&product=model-jet-engines-3rd-edition-by-thomas-kamps There's a build diary on my website: misterg.org.uk/turbine-html/ (I've added these details to the description now - thanks)
@praggiram2645 Жыл бұрын
Love the way it looks,feels and Also , Can you tell me the reason you did this 😮😮😮😊😊😊
@Mister_G Жыл бұрын
Thank you very much! 🙂 Why? - I don't know, really. I saw Kurt Schreckling's original design in the 1990s, and have had a hankering to build a jet engine for myself ever since. Only recently have I had the necessary equipment & time.
@shewagdhanush13912 жыл бұрын
How much does it costs, to make all of these?
@Mister_G2 жыл бұрын
Hi, I do this as a hobby, so my costs are just the raw materials.
@shewagdhanush13912 жыл бұрын
@@Mister_G What about the machining cost of the blade? Is that a single piece?
@Mister_G2 жыл бұрын
@@shewagdhanush1391 The compressor wheel (at the inlet) is a turbo-charger part from a car (cost 30GBP from ebay). The turbine wheel was made from an offcut of Hastelloy X sheet - see misterg.org.uk/turbine-html-7/
@shewagdhanush13912 жыл бұрын
@@Mister_G What was the max RPM and efficiency? Thank you.
@Mister_G2 жыл бұрын
@@shewagdhanush1391 I don't have a reliable way of measuring RPM yet (I am working on it! :D ). Design maximum is ~100,000RPM. I will measure thrust, etc. once I have a reliable RPM reading.
@aleksandrkargin1978 Жыл бұрын
Осталось отбалансировать и проверить.👍🏻🤓😎
@Mister_G Жыл бұрын
Thank you - the rotor was balanced before assembly 🙂
@aleksandrkargin1978 Жыл бұрын
@@Mister_G я и не сомневался, что все вращающиеся детали, были отбалансированы перед сборкой, но после сборки, они должны быть отбалансированы совместно. Поэтому купленные двигатели, нельзя разбирать, если не хочешь потерять балансировку.
@Mister_G Жыл бұрын
@@aleksandrkargin1978 True - I am relying on the compressor wheel being well balanced from the factory. This engine only runs up to 100k RPM so not quite as critical as commercial engines. Thank for the kind comments 🙂
@bruhannyanzi16605 ай бұрын
❤🎉 thnx bro
@Mister_G5 ай бұрын
Thank you
@yousefashry28972 жыл бұрын
Sir, may I get the cad drawings please?
@Mister_G2 жыл бұрын
Hi, the drawings are all in Kamps' book :) See misterg.org.uk/turbine-html/ for the link.
@Jan_Seidel2 жыл бұрын
This is a reeaaally good looking engine. Nice work mate 🙂 I have been reading much into micro turbine jets as I want to build one myself, and you are setting standards with your build. Some remarks though. You shouldn't oil up the ID and OD of the bearings. The are suppose to stay put and if snug it won't really improve the assembly. The other thing: I also been reading dissertations and scientific stuff to this topic. And I recall I've read somewhere the wave washers or springs should be locate at the front to the compressor not at the turbine. Unfortunately I do not recall if it was because of thermal issues or for another reason. But your build is made in a way that a preload in the front makes no sense. I would love to see more from you and the engine
@Mister_G2 жыл бұрын
Thank you very, very much for your kind comments. I hope to post another video with some thrust measurements soon (another project got in the way - a desktop CNC 🙂). Re: the bearings - the inner races of both bearings and the outer race of the front bearing (in this design) are held tightly. The outer race of the rear bearing floats inside the shaft tunnel and must be able to slide freely enough to accomodate differences in thermal expansion between the (steel) turbine shaft and the (aluminium) tunnel whilst maintaining bearing preload, but not so freely that it spins in its housing (it's a bit of a kludge, but it's a well used one!). The direction of the preload depends on the direction of any axial force that builds up on the rotor as the engine speeds up. The important thing is that the preload is in the same direction as the axial force. If it isn't, the bearings can become unloaded (due to the axial force overcoming the preload) resulting in vibration / scuffing and potential damage. The direction and magnitude of axial forces seem to be design dependent, and (from what I can gather) are not easy to predict. I just followed the design in the book 😄. From what I have read, KJ66 derived designs benefit from the bearings being preloaded forwards (rather than backwards as in this design), but this is by no means universal. If you're thinking about alternative preload arrangements, bear in mind that it's also beneficial to be able to hold a tight tolerance on the clearance between the compressor wheel impeller and its housing, so whether backwards or forwards, it's better (IMHO) to apply preload to the rear bearing - can be difficult to achieve a forward preload in practice, though. Thanks again for your interest, and for taking the time and trouble to comment.
@FirstLast-tx3yj Жыл бұрын
@@Mister_G do you have a video of how you made the exhaust stators?
@Mister_G Жыл бұрын
@@FirstLast-tx3yj Thanks for watching - I don't have a video for the exhaust stator (NGV) but there is a description and photos on my website - misterg.org.uk/turbine-html-5/ misterg.org.uk/turbine-html-6/ Happy to help if you have questions (either here, or get in touch via the website)
@FirstLast-tx3yj Жыл бұрын
@@Mister_G thank you for the response The links did not work but i navigated in the site. So the only parts one is obliged to buy are the compressor and the turbine wheel the rest can be made!! With enough skill Did you have a custom pcb made for control or how did you control the rpm and whatnot?
@Mister_G Жыл бұрын
@@FirstLast-tx3yj No worries! Glad you found the info. I only bought the compressor wheel - the turbine was also home made. The main reason I went with the Kamps design is that it is mild enough to use a DIY turbine wheel. It you can get hold of a commercial cast inconel turbine, then the KJ66 would probably be a better design - more powerful for the same size. Some waffle on how I made the turbine wheel on another video: kzbin.info/www/bejne/kKfSe2ShqLmFotE The only control is the speed of the fuel pump at the moment (which is just an ebay PWM motor controller). I've had difficulty getting a reliable RPM measurement, but I hope that is now sorted, and another run (video) will be coming soon. Thanks for the interest 🙂
@Joseph-hp7gt2 жыл бұрын
could you remake this video some time with the changes you made please you are a verry talented engineer i dont mind how you do it i subscribed btw :D
@Mister_G2 жыл бұрын
Thanks very much - The engine is pretty much as per the book, so no real changes.
@antoniogabriel6916 Жыл бұрын
SHOWWWW!!!!
@eddieklevin86202 жыл бұрын
I like to buy how much for that engine uncle
@Mister_G2 жыл бұрын
Not for sale yet, sorry!
@Rudakhs_ging_4739 Жыл бұрын
Hi
@Mister_G Жыл бұрын
Hi - Thanks for the comment 🙂
@KasnazanM Жыл бұрын
I think its made by a company, not a home made. Sorry
@Mister_G Жыл бұрын
Thank you! that is a very high complement 😂 You can check out the build here: misterg.org.uk/turbine-html-2/
@nurmogati64142 жыл бұрын
Please watching my new rotary engine.... Advise me...!!!???!!! 🙁🙁🙁
@Mister_G2 жыл бұрын
I have watched the last 2 videos, but I can't understand what you're trying to make, sorry!
@MarvelStudios-bf4cm11 ай бұрын
Absolutely bad perspective of the assembly to be able to see the details, small and out of frame image.
@Mister_G11 ай бұрын
I did try and warn you in the introduction! 😅 Thanks for watching and commenting, anyway,
@eddieklevin86202 жыл бұрын
You can send an email to me
@yousefashry2897 Жыл бұрын
How did you balance the turbine wheel dynamically because usually the hand work has a lot of errors
@Mister_G Жыл бұрын
I only did a static balance - the compressor wheel should be balanced as supplied and is a shrink-fit on the shaft. I worked hard to keep the shaft true when everything was assembled (keeping the spacers parallel and the dirt out), so the only part that should be out of balance is the turbine wheel itself. After assembling it to the shaft, I did the initial balancing by 'rocking' the shaft in its bearings to find the heavy point and grinding metal off the wheel. Final balancing was done by touch - you can feel the out of balance forces if you hold the back bearing between finger and thumb and spin the turbine gently with compressed air. if you stick a small piece of tape (e.g. 3 x 3 mm) to the wheel it will make the vibrations feel better or worse. Find the place where the vibrations are the least, then remove a small amount of metal from the opposite side of the wheel and try again. You eventually get to a place where you can't feel any vibraton at all - it is really noticeable! Then you can call it done :) Some more description on my website :misterg.org.uk/turbine-html-20/