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

• Main Authors: Борис Шамшадович Мамедов, Петр Константинович Штанько
• Format: Article
• Language: English
• Published: PC Technology Center 2016-03-01
• Series: ScienceRise
• Subjects: gas-dynamic work steady; thrust; regulation law
• Online Access: http://journals.uran.ua/sciencerise/article/view/63913

<p>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<em></em></p>