Single theory of movers. Turbo-jet engines thermodynamic cycle in co-ordinate P-V, T-S calculation
DOI:
https://doi.org/10.15587/1729-4061.2013.12382Keywords:
Thermodynamic cycle, zone of the slow down flowAbstract
The drawbacks of modern turbo-jet engines theory are considered that lead to mistaken turbo-jet engines work principle description on the basis of mistaken thermodynamic cycle.
Turbo-jet engines thermodynamic cycle in co-ordinate P-V, T-S is the strategical foundation not only for turbo-jet engines work principal description but also for any kind of physical processes taking place on turbo-jet engines working. turbo-jet engines thermodynamic cycle which is worked out with the modern theory of air-jet engines is deeply mistaken since it absolutely has not reflected actual current of gas flow in H-B zone of turbo-jet engines violating with this all the laws of gases and fluid flow mechanics hence the point B can never be above the point H.
This mistake lead to mistaken turbo-jet working principle description as well as to mistaken description of such a strategical notion as turbo-jet engines thrust generation and initiated on mistaken description of theoretical and physical basis of blades flow tear off generation on the last working wheels of high pressure compressor and then on the blades of the first working wheel of low pressure compressor that lead to mistaken description of full pressure preservation coefficient and etc.
Thermodynamic cycle in co-ordinate P-V, T-S investigations considered with single theory of movers on the continuous flows show that the air-engines flight speed can not exceed with the temperature increasing in combustion chamber. To increase the flight speed of movers above of for example up to it is necessary to develop the movers which generate the thrust on gravitation field besis.References
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