Attempting to Build my first Turbojet & have a few Questions
Nov 10, 2023 17:44:11 GMT -5
Johansson and thehazard like this
Post by thehazard on Nov 10, 2023 17:44:11 GMT -5
Hi there,
I have decided to build my first turbojet and am beginning to start searching for parts. I just bought a turbo with a 60 mm inducer, but it comes with a few glaring problems. As shown in the pictures below it is a twin scroll turbo with the intakes to the turbine on the same side as the exducer. I bought it for 100 dollars Canadian, and because of how cheap it was I would prefer see if I could get some use out of it. I am aware that twin scroll turbos are not ideal for this application, but again it was cheap and the bearings seem to be in good condition. I aware of the program Jetspecs and will use its measurements in the construction of my combustion chamber. My turbo is the ITI LB7 Turbo, and I intend to use propane as my fuel. I have seen many great examples and resources on this forum of how the systems of a turbojet work (such as the diy turbines thread) but of course I have some specific questions.
My questions:
Do I need to do anything differently with the exhaust gases because it is a twin scroll turbo or would I just simply route the exhaust to both the turbine intakes?
Due to the fact the turbine intakes are on the same side as the exducer I know I would need many bends in the exhaust gas tubing from the combustion chamber to the turbine inlets. Would this put such a massive hamper on efficiency that it would not be worth building with the given turbo?
Is the openable thing I will call a "door" near the exducer important? What do I need to do about it?
I also have some questions regarding the construction of the flame tube and combustion chamber, specifically regarding how air should flow through the chamber and flame tube. Should all the air from the turbine compressor be forced through the flame tube by providing the only exit from the combustion chamber to the turbine inlet through the flame tube? Or is their supposed to be a gap around the flame tube at the exit of the combustion chamber?
I have heard of people using fire extinguishers as the combustion chambers outer shell. Can I use any fire extinguisher that is wide enough and long enough as the combustion chamber?
Thank you for the time! And if I'm an idiot for buying this turbo just tell me.
I have decided to build my first turbojet and am beginning to start searching for parts. I just bought a turbo with a 60 mm inducer, but it comes with a few glaring problems. As shown in the pictures below it is a twin scroll turbo with the intakes to the turbine on the same side as the exducer. I bought it for 100 dollars Canadian, and because of how cheap it was I would prefer see if I could get some use out of it. I am aware that twin scroll turbos are not ideal for this application, but again it was cheap and the bearings seem to be in good condition. I aware of the program Jetspecs and will use its measurements in the construction of my combustion chamber. My turbo is the ITI LB7 Turbo, and I intend to use propane as my fuel. I have seen many great examples and resources on this forum of how the systems of a turbojet work (such as the diy turbines thread) but of course I have some specific questions.
My questions:
Do I need to do anything differently with the exhaust gases because it is a twin scroll turbo or would I just simply route the exhaust to both the turbine intakes?
Due to the fact the turbine intakes are on the same side as the exducer I know I would need many bends in the exhaust gas tubing from the combustion chamber to the turbine inlets. Would this put such a massive hamper on efficiency that it would not be worth building with the given turbo?
Is the openable thing I will call a "door" near the exducer important? What do I need to do about it?
I also have some questions regarding the construction of the flame tube and combustion chamber, specifically regarding how air should flow through the chamber and flame tube. Should all the air from the turbine compressor be forced through the flame tube by providing the only exit from the combustion chamber to the turbine inlet through the flame tube? Or is their supposed to be a gap around the flame tube at the exit of the combustion chamber?
I have heard of people using fire extinguishers as the combustion chambers outer shell. Can I use any fire extinguisher that is wide enough and long enough as the combustion chamber?
Thank you for the time! And if I'm an idiot for buying this turbo just tell me.