Turbojet Engine (GM-style)

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Bounding box: 610.2 × 730.0 × 1301.4 mm
Engine: Precision B-rep
Parameters: 26
Published: August 20, 2026

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The prompt

یک عدد توربین توربوجت طراحی کن، با تمام جزییاتیی که شرکت جنرال موتورز ارائه میده

Parameters

Name	Value	Range
Intake Diameter	500 mm	200 – 800
Intake Length	200 mm	100 – 400
Intake Wall Thickness	5 mm	2 – 20
Compressor Dia (rotor tip)	450 mm	200 – 700
Compressor Length	300 mm	150 – 500
Number of Stages	3	1 – 6
Blades per Rotor Row	24	10 – 60
Combustor Outer Dia	400 mm	200 – 600
Combustor Length	200 mm	100 – 400
Wall Thickness	3 mm	2 – 10
Fuel Nozzle Count	6	3 – 12
Turbine Rotor Dia	350 mm	150 – 500
Turbine Length	150 mm	80 – 300
Number of Stages	1	1 – 3
Blades per Rotor Row	30	10 – 50
Exhaust Throat Dia	300 mm	100 – 500
Exhaust Length	250 mm	100 – 400
Wall Thickness	4 mm	2 – 10
Shaft Diameter	50 mm	20 – 100
Shaft Length	600 mm	300 – 1000
Outer Casing Dia	550 mm	300 – 800
Outer Casing Length	1200 mm	800 – 1800
Casing Wall Thickness	5 mm	2 – 20
Gearbox Width	200 mm	100 – 300
Gearbox Depth	150 mm	80 – 250
Gearbox Height	100 mm	50 – 200

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.

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