Aeroengine
A technology for aero-engines and compressors, which is applied in the directions of machines/engines, mechanical equipment, gas turbines, etc., can solve the problems of low thrust efficiency and low pressure, and achieve the effect of high thrust efficiency and simple structure.
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Embodiment 1
[0016] an aeroengine such as figure 1 As shown, it includes a compressor 1, a combustion chamber 2, a turbine 3, a nozzle 4, an auxiliary combustion chamber 5 and an auxiliary nozzle 6, and the compressor 1 communicates with the turbine 3 through the combustion chamber 2, and the The outlet of the working medium of the turbine 3 communicates with the nozzle 4, and a working medium outlet is provided on the fluid passage between the compressor 1 and the turbine 3, and the outlet of the working fluid passes through the auxiliary The combustion chamber 5 communicates with the auxiliary nozzle 6 .
[0017] As an alternative embodiment, in Embodiment 1 of the present invention, the auxiliary combustion chamber 5 and the combustion chamber 2 may be further selectively set to be set or not set together.
Embodiment 2
[0019] an aeroengine such as figure 2 As shown, it includes a compressor 1, a combustion chamber 2, a turbine 3, a nozzle 4 and an auxiliary nozzle 6, the compressor 1 communicates with the turbine 3 through the combustion chamber 2, and the turbine 3 The working medium outlet communicates with the nozzle 4 , and the combustion chamber 2 is provided with a working medium outlet, and the working medium outlet communicates with the auxiliary nozzle 6 .
[0020] As a changeable embodiment, Embodiment 1 and Embodiment 2 of the present invention and their changeable embodiments can further selectively choose to make the nozzle pipe 4 and the auxiliary nozzle pipe 6 fit or not.
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