Single theory of movers. Turbo-jet engines thermodynamic cycle in co-ordinate P-V, T-S calculation

Authors

  • Борис Шамшадович Мамедов Zaporizhzhya National Technical University street Zhukovsky, 64, Zaporozhye, Ukraine, 69063, Ukraine

DOI:

https://doi.org/10.15587/1729-4061.2013.12382

Keywords:

Thermodynamic cycle, zone of the slow down flow

Abstract

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.

Author Biography

Борис Шамшадович Мамедов, Zaporizhzhya National Technical University street Zhukovsky, 64, Zaporozhye, Ukraine, 69063

Ph.D., Associate Professor

References

  1. Karachevsky G. Airdynamic –classical theory crisis [Text] / G.Karachevsky / Technique of youth, №10, 2005y., p.5–7.
  2. Mamedov B.S. Foundations of single theory of movers on the continuous flows. Turbo-jet engines formulas thrust, flying (thrust) efficiency calculation [Text] / B.S.Mamedov / Eastern-European Journal of Enterprise Technologies, – Kharkov: pub. Technological center. Apply mechanic, 4/7(52), 2011, p.15–20.
  3. Mamedov B.S. Chapter 2. Foundations of single theory of movers on the continuous flows. Blowing profile, as a mover, formulas of thrust, flying (thrust) efficiency, theorem of raising force calculation. [Text] / B.S.Mamedov / National technical university news, "KhPI". Scientific works collection. Topical issue: New solutions in modern technologies, – Kharkov: NTU " KhPI ", 2011y., –№33,–p.146–153.
  4. Shlyhtenko S.M. Air-jet engines theory and calculation. [Text] / S.M.Shlyhtenko /–M:Machinebuilding, 1987y., –568 p.
  5. Kazandgan P.K. Aviation engines theory [Text] / P.K.Kazandgan, N.D.Tihonov, A.K.Jnko / – M.: Machinebuilding, 1983,–223 p.
  6. Mamedov B.S. Chapter 3. Foundations of single theory of movers on the continuous flows. Air-jet engines throttle down reasons when take off, flight, landing. [Text] / B.S.Mamedov / Eastern-European Journal of Enterprise Technologies, – Kharkov: pub. Technological center. Apply mechanic, 5/7(53), 2011, p.24–28.
  7. Mamedov B.S. Foundations of single theory of movers on the continuous flows. [Text] / B.S.Mamedov / Eastern-European Journal of Enterprise Technologies, – Kharkov: pub. Technological center. Apply mechanic, 6/7(60), 2012, p.29-34.
  8. Mamedov B.S. Foundations of single theory of movers. Calculation the formulas of thrust, flying (thrust) efficiency of rocket engeines. [Text] / B.S.Mamedov / Eastern-European Journal of Enterprise Technologies, – Kharkov: pub. Technological center. Apply mechanic, 1/7(61), 2013, p.61-67.
  9. Mamedov B.S. The using of Ayler`s equation for calculation the formulas of thrust and flying (thrust) efficiency on external parameters of gas flow for air-jet engines when Vп>0. [Text] / B.S.Mamedov / National technical university news, "KhPI". Scientific works collection. Topical issue: New solutions in modern technologies, – Kharkov: NTU " KhPI ",–№4(978), 2013y., p.3-15.
  10. Mamedov B.S. Chapter 4. Foundations of single theory of movers on the continuous flows. Working out the direction of technical progress in aviaenginebulding, connected whit an increasing of gasodinamic work steady of air-jet engines when takeoff, cruise, landing. [Text] / B.S.Mamedov / National technical university news, "KhPI". Scientific works collection. Topical issue: New solutions in modern technologies, – Kharkov: NTU " KhPI ",–№34, 2011y., p.124-134.

Published

2013-04-25

How to Cite

Мамедов, Б. Ш. (2013). Single theory of movers. Turbo-jet engines thermodynamic cycle in co-ordinate P-V, T-S calculation. Eastern-European Journal of Enterprise Technologies, 2(7(62), 29–34. https://doi.org/10.15587/1729-4061.2013.12382

Issue

Section

Applied mechanics