A method of serial production turbojet and turbofan engine configured in this way

1. A method for mass production of the turbojet (TRD), characterized in that the produced parts and subassemblies are completed, elements and assemblies of modules and systems of the engine; modules was collected in an amount of at least eight - of the low pressure compressor (LPC) to a variable speed rotary nozzle; during manufacture CPV collected stator, wherein the set input, is not more than three intermediate guide vanes and output straightener and collected rotor including a shaft, which sets and fixedly connected discs are not more than four impellers with blades system, thus forming annular portions of the inner surface of the air intake duct portion running from the CPV profiled in the air flow direction vane impellers elements and guide devices CPV; collected, preferably modulo style engine which operate two-shaft, wherein mounted on the slipway technological intermediate casing; gas generator including a high pressure compressor (HPC) having a stator including an input, at most eight intermediate guide vanes and output straightener, and the rotor shaft and the system equipped with the impeller blades, whose number is not less than twice the number of said impellers CPV main combustion chamber and a high pressure turbine (HPT); then to an intermediate body mounted CPV, and a gas generator for successively mounted coaxially low pressure turbine (LPT), a mixer, front device, augmentor combustion chamber and rotatable reagent