The main technical progress directions in air-jet engine design branch, which are worked out by the “Single theory of continuous flow propulsions”
DOI:
https://doi.org/10.15587/2313-8416.2016.63913Keywords:
gas-dynamic work steady, thrust, regulation lawAbstract
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
References
Shljahtenko, S. M. (Ed.) (1987). Teorija i raschet vozdushno-reaktivnyh dvigatelej. Moscow: Mashinostroenie, 568.
Mamedov, B. Sh. (2013). Edinaja teorija dvizhitelej na nepreryvnyh potokah. Kharkiv: Tehnologicheskij centr, 296.
Mamedov, B. Sh. (2014). Edinaja teorija dvizhitelej. Prichiny generirovanija neustojchivoj raboty turboreaktivnyh dvigatelej pri vzlete v uslovijah zharkogo klimata. Aviacionno-kosmicheskaja tehnika i tehnologija, 9, 56–62.
Mamedov, B. Sh. (2014). Edinaja teorija dvizhitelej. Novoe naznachenie i princip raboty "nulevoj" stupeni kompressora nizkogo davlenija. Aviacionno-kosmicheskaja tehnika i tehnologija, 8, 55–60.
Mamedov, B. Sh. (2009). Pat. 86788. MPK F02K 1/00, F02K 3/00, F02C 7/00. Turboreaktivnij dvokonturnij dvigun. № U200607941; zajav. 14.07.2006; opubl. 25.05.2009; Bjul. № 10, 24.
Mamedov, B. Sh. (2009). Pat. 46407. MPK F04D 27/00, F02K 1/00, F02K 3/00, F02C 7/00. Sposib pidvyshhennja gazodynamichnoi' stijkosti roboty povitrja-reaktyvnyh dvyguniv. № U200905152; zajavl. 25.05.2009; opubl. 25.12.2009; Bjul. № 24, 26.
Mamedov, B. Sh. (2012). Pat. 66619. MPK F02K 1/00, F02K 3/08, F02K 7/00, F02K 3/11 Turboreaktyvnyj dvokonturnyj dvygun. № U201107779; zajav. 20.06.2011; opubl. 10.01.2012; Bjul. № 1, 12.
Mamedov, B. Sh. (2012). Pat. 66620. MPK F02S 7/04, F04D 27/02, F02K 1/00, F02K 3/00. Turboreaktyvnyj dvokonturnyj dvygun. № U201107780; zajav. 20.06.2011; opubl. 10.01.2012; Bjul. № 1, 12.
Mamedov, B. Sh. (2012). Pat. 66621. MPK F02S 7/04, F04D 27/02, F02K 1/00, F02K 3/00. Turboreaktyvnyj dvokonturnyj dvygun. № 201107781; zajav. 20.06.2011; opubl. 10.01.2012; Bjul. № 1, 10.
Mamedov, B. Sh. (2012). Pat. 66622. MPK F02S 7/04, F04D 27/02, F02K 1/00, F02K 3/00. Turboreaktyvnyj dvokonturnyj dvygun. № 201107782; zajav. 20.06.2011; opubl. 10.01.2012; Bjul. № 1, 10.
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Copyright (c) 2016 Борис Шамшадович Мамедов, Петр Константинович Штанько
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