Gas Turbine | Gas Turbine Working | Gas Turbine Components | Gas Turbine Overhauling

Better than my university professor’s teaching

It's 1am... how did I get here?

Excellent description and detail by the commentator. My hearty congratulations. I do feel that the modern jet engine must be classified as one of the modern wonders of engineers. The combined engineering logic of the jet engine took a lot of time to be put together and if one had to put an initiation spark on the human mind, it was Charles parson who combined the high pressure in a boiler to spin the turbine in a steam layout. I was lucky enough to have lived at Newcastle-upon -Tyne where I went on many visits to see the Turbina the first steam turbine ship which surprised the Royal Navy at Spithead. I worked on the first jet turbines on a naval ship and it was the HMS Exmouth when I worked at Chatham Dockyard. Again Congratulations to Oil Gas World for providing such detailed information about the thermodynamic stages and the cooling methods on every unit. When I built a model engine with one compressor stage and one turbine stage, the diffuser right after the compressor was a tricky unit where the air had to be slowed down to sustain the flame and then the flame diluted with colder air along the burner to isolate the flame from the metal. Well done to the commentator, HIs English accent is what I aimed for when I spoke that language, but I could never get rid of my mother's tongue diluting the English language I spoke at Chatham and Newcastle.

Best educational video can ever be found on Gas Turbines. I spent hours upon hours looking at GE technical sheets and explaination, but bro this is much eaiser.

I used to be an 14CFR Part 147 instructor for an A&P school. I taught turbine engine theory, and helicopters. A lot this is the same as a standard aircraft engine but there are some terms that are used here that aren't used on aircraft. Like spark plugs. We don't all them that since they are not used at all times. They are called igniters on aircraft engines, we simply call them flame propagation tubes, and what they call a labyrinth seal we call knife edge seals or knife seals, and we usually describe the intake separately from the compressor but for the most part they are pretty much the same.

YouTube is great at reading my mind...I'm learning about gas power cycles in my thermo course and now I'm getting this video recommended..I never searched anything related to thermodynamics ..this is exciting and horrifying at the same time

Whoever did the cadd modeling was very good. Lighting and animation all work very well and appear realistic. Thanks for sharing!

7:24 man I’m glad I watched this videos. I have been making honey comb seals for years and just found out where they go. 😎

I worked for the UK admiralty Material Laboratory as a Toolmaker/Welding specialist 1977 to 1981. One of the projects I was involved in was a high temperature wind tunnel for gas turbine blades. They were initially interested in the front and rear blades. The for the front blade the conditions surrounding the blade were easily met. The rear blade was another thing. We spent over a year getting the Air pressures correct flowing over the blade. The tool shop made up test blades out of different materials to see their corrosion resistance as the hot gases flowed over the test blade. Gas pressure was monitored around the blade by spark eroding very small holes in the blade then welding 1mm dia stainless steel pipes on to the end of the test blade where the hole came out of the blade which was then connected to pressure gages. After a year of development and spending 1 million pounds it was announced everything was good. The customer turned around a stated they were only interested in the front blade high temperature corrosion resistance. Whoops.

keren...asli keren penjelasannya dan visualisasinya...trm ksh banyak ya Om Bule yang ganteng dan baik hati mau berbagi ilmu...🙏

Love this video's level of detail. It should be required viewing for new GE Power engineers. I've been one for 10 years now in combustion and compressor design, and I still learned a lot, especially about how the systems I work on interface with other components.

The amount of metal machining and specific metal production is wild. Every time I fly I cant help but think I’m flying on mans ultimate invention. Mechanical and computer technology combined. At least for an average person. That’s why I like sitting just behind the wings.

Holy crap. 56 minutes with zero fluff. I don't think this aspect can be comprehended without watching it, like how it can be 0% entertaining and 100% interesting at the same time.

Literally the best video I’ve seen (on this subject).

Amazing job! Well done! Thank you very much.

Bjour,merci pour votre travail,magnifique j'aime beaucoup

Very Cool and also amazing how these things such as high speed gas jets work and last as long as they do with not just it's speeds in RPMs but the amount of continuous heat saturation of all the internal parts without melting down or seizing by welding themselves together, to me that's mind blowing. Working with Turbos on gas engine's is challenging enough when you are dealing with exhaust temps and heat saturation into the drive shaft and Journal bushings or ball bearings, but I also assume with the amount of continuous volumes of fresh air always coming into the intakes and the lower compression ratios of the turbine the BTUs aren't nearly as hot as it coming out of an exhaust port of a V8 cylinder head, of a hot Blue flame upwards of 2k degrees Fahrenheit? But it's a different story when you add a afterburner to a jet or turbine combustion which is under much higher atmospheres of pressure when extra air and fuel are pumped into the afterburners, those parts have to be some sort of super metals used by NASA it not melt or erode away if not some sort of ceramic coatings on the metal parts to protect these parts from the intense heat being funneled throw a adjustable nozzle at the tail ends of these modern jet engines. I understand they are slightly different than a Gas turbine is but they share a lot of the same mentioned above parts and temps I'm sure.

Thanks for these,only ever worked on Westinghouse,and seeing the differences in them and GE,as well as a real explanation of the purpose of all parts is very helpful information..thank you

Gas Turbine | Gas Turbine Working | Gas Turbine Components | Gas Turbine Overhauling. Good video, thank you for the information. Always success "Oil Gas....."....Pekalongan, Central Java, Indonesia On

Absolutely amazing ! It's a must watch over and over. Many ideas are provoked in me brain. Keep up the good work.