The main technical progress directions in air-jet engine design branch, which are worked out by the “Single theory of continuous flow propulsions”

Authors

  • Борис Шамшадович Мамедов Zaporizhzhya National Technical University 64 Zhukovsky str., Zaporozhye, Ukraine, 69063, Ukraine
  • Петр Константинович Штанько Zaporizhzhya National Technical University 64 Zhukovsky str., Zaporozhye, Ukraine, 69063, Ukraine

DOI:

https://doi.org/10.15587/2313-8416.2016.63913

Keywords:

gas-dynamic work steady, thrust, regulation law

Abstract

The main technical progress directions in air-jet engine design branch, which are worked out by the “Single theory of continuous flow propulsions” are highlighted. They are connected with providing the fly security by air-jet engines gas-dynamic work steady increasing with full elimination zone of rigid (spring) stroke in the cross section B-B of the air-jet engines, with bypass turbojet engine’s thrust increasing with simultaneously fuel consumption lowering, with inlet and outlet decibel characteristic and radial dementias lowering, with high pressure compressor’s last working wheels blades increasing, with regulating law air-jet engine’s introduction to provide maximum thrust with the purpose of flying (thrust) efficiency increasing

Author Biographies

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

PhD, Associate Professor

Department "Descriptive geometry, engineering and computer graphics"

Петр Константинович Штанько, Zaporizhzhya National Technical University 64 Zhukovsky str., Zaporozhye, Ukraine, 69063

PhD, Associate Professor

Department of "Mechanics"

References

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Published

2016-03-27

Issue

Section

Technical Sciences