Turbine Engine Combustor Design
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- เผยแพร่เมื่อ 25 ก.ค. 2024
- Operation and inspection of turbine engine combustors. A combustor is a component or area of a gas turbine, ramjet, or scramjet engine where combustion takes place. It is also known as a burner, combustion chamber or flame holder. In a gas turbine engine, the combustor or combustion chamber is fed high pressure air by the compression system.
We called that one part a sombrero. Obvious
congratulations from Brazil!!!!
very interesting video. Thank you for sharing.
Very interesting!
Nossa que canal que achei. Muito bom.
Great!!
The way the holes on the combustion liner is a black ark.
I like it
Thanks for the video. I am. Inventor and mechanical and software engineer. Your place full of educational resource. Can I know where are you? I wish to learn from you or your place for few months.
what about using high temp materials
Enggine boing apa itu mas broo,??..
my dad made me do this
Why do they have reverse flow combustor why do they reverse the flow ? Is there some advantage to doing that ? Is that a helicopter engine ? Big airline engine doesn't have reverse flow just some turboprop.
In short, it saves space, regular axial flow jer engine Is sometimes too long, so this design saves space, you also see this space saving in centrifugal compressor, which replaces few regular stages with one centrifugal stage. Keep in mind that some helis still use engines with standard axial flow, like Mi 8/17 with its klimov tv117.
Reverse flow is also used when propulsion isnt delivered derrectly by thrust of jet, instead it transfers its kinetic energy into mechanical by so called "free turbine", which drives propeller, rotor, or on tank sprocket, of course in all of them there is transmission to adjust rpm and torque.
🍎🍎🍎🍎🍎🍎🍎
You know that combustor with your hand print will have to be scrapped now...hydrogen embrittlement from the oils in your skin and all. 😏🇦🇺
Copied russian vervion of this engine called as ГТД-350
Awesome, thanks for the info.