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Natural Gas Turbojet Assembly

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Bounding box
705.2 × 340.1 × 340.0 mm
Engine
Precision B-rep
Parameters
29
Published
October 20, 2026

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Natural Gas Turbojet Assembly

Parameters

NameValueRange
Main Shaft Diameter40 mm10 – 100
Main Shaft Length500 mm100 – 1000
Inlet Casing Outer Diameter300 mm100 – 500
Inlet Casing Wall Thickness5 mm1 – 20
Inlet Casing Length250 mm50 – 500
Compressor Rotor Diameter220 mm50 – 400
Compressor Hub Diameter60 mm20 – 200
Compressor Rotor Length180 mm20 – 500
Combustor Liner Outer Diameter260 mm50 – 400
Combustor Liner Wall Thickness3 mm0.5 – 15
Combustor Liner Length140 mm20 – 300
Fuel Manifold Ring Diameter240 mm50 – 400
Fuel Manifold Inner Diameter200 mm20 – 300
Fuel Manifold Ring Width20 mm5 – 50
Number of Injectors82 – 24
Injector Tube Length30 mm5 – 60
Injector Tube Diameter8 mm2 – 20
Turbine Rotor Diameter240 mm50 – 400
Turbine Hub Diameter80 mm20 – 200
Turbine Rotor Length120 mm20 – 300
Exhaust Nozzle Inlet Diameter200 mm50 – 400
Exhaust Nozzle Exit Diameter150 mm20 – 300
Exhaust Nozzle Length180 mm20 – 400
Exhaust Nozzle Wall Thickness3 mm0.5 – 15
Bearing Strut Outer Diameter260 mm100 – 400
Bearing Strut Hub Diameter80 mm20 – 150
Number of Struts63 – 12
Strut Width (Tangential)20 mm5 – 40
Strut Thickness (Axial)10 mm2 – 30

Every value above is a live dimension. Open a model like this in the editor and each one becomes a slider you can drag before exporting.

Natural Gas Turbojet Assembly - Free CAD Model (STEP, STL) | TextoCAD