ÍÀÖ²ÎÍÀËÜÍÈÉ ÀÅÐÎÊÎÑ̲×ÍÈÉ
ÓͲÂÅÐÑÈÒÅÒ ²Ì. Ì. ª. ÆÓÊÎÂÑÜÊÎÃÎ "ÕÀÐʲÂÑÜÊÈÉ À²ÀÖ²ÉÍÈÉ ²ÍÑÒÈÒÓÒ"
ISSN: 1727-7337 (Print), 2663-2217 (Online). À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ
² ÒÅÕÍÎËÎòß. – 2020. – ¹ 7(167). – 160 ñ.
ISSN: 1727-7337 (Print), 2663-2217 (Online). ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß
ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2020. – ¹ 7(167). – 160 ñ.
ISSN: 1727-7337 (Print), 2663-2217 (Online). AEROSPACE
TECHNIC AND TECHNOLOGY. – 2020. – No. 7(167). – 160 p.
Òåìàòè÷íèé âèïóñê «Ïðîáëåìè äâèãóíîáóäóâàííÿ»
ÑÒÀÒÒ² (articleS)
Àâòîðè |
Íàçâà ñòàòò³ (article title) |
Ñòîð³íêè (pages) |
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English |
Óêðà¿íñüêà ìîâà |
Ðîñ³éñüêà ìîâà |
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Ïðîåêòóâàííÿ ë³òàëüíèõ
àïàðàò³â |
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Ëîñü
À. Â., |
PROBLEMS OF CREATION OF AIRCRAFT
CATEGORY PLANES ACCORDING TO ENVIRONMENTAL LIMITATIONS |
ÏÐÎÁËÅÌÈ ÑÒÂÎÐÅÍÍß Ë²ÒÀʲÂ
ÒÐÀÍÑÏÎÐÒÍί ÊÀÒÅÃÎв¯ Ç ÓÐÀÕÓÂÀÍÍßÌ ÅÊÎËÎò×ÍÈÕ ÎÁÌÅÆÅÍÜ |
ÏÐÎÁËÅÌÛ
ÑÎÇÄÀÍÈß ÑÀÌÎËÅÒΠÒÐÀÍÑÏÎÐÒÍÎÉ ÊÀÒÅÃÎÐÈÈ Ñ Ó×ÅÒÎÌ ÝÊÎËÎÃÈ×ÅÑÊÈÕ ÎÃÐÀÍÈ×ÅÍÈÉ |
5–11 |
Òåîð³ÿ ³ ðîáî÷³
ïðîöåñè àâ³àö³éíèõ äâèãóí³â ³ åíåðãîóñòàíîâîê |
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Òêà÷
Ì. Ð., |
INCREASING THE EFFICIENCY OF HYDROGEN
PRODUCTION TECHNOLOGY BY USING A REGENERATION CIRCUIT WITH A ROTARY-PISTON
EXPANDER MACHINE |
ÏÎÂÛØÅÍÈÅ ÝÔÔÅÊÒÈÂÍÎÑÒÈ
ÒÅÕÍÎËÎÃÈÈ ÏÎËÓ×ÅÍÈß ÂÎÄÎÐÎÄÀ ÏÓÒÅÌ ÈÑÏÎËÜÇÎÂÀÍÈß ÐÅÃÅÍÅÐÀÖÈÎÍÍÎÃÎ ÊÎÍÒÓÐÀ Ñ
ÐÎÒÎÐÍÎ-ÏÎÐØÍÅÂÎÉ ÐÀÑØÈÐÈÒÅËÜÍÎÉ ÌÀØÈÍÎÉ |
12–18 |
|
Óñåíêî
Â. Þ., |
EFFECT OF THE CLEARANCE BETWEEN
ROWS OF COAXIAL PROPFAN ON THRUST |
ÂÏËÈÂ ÇÀÇÎÐÓ
Ì²Æ ÐßÄÀÌÈ Ñϲ²ÑÍÎÃÎ ÏβÒÐßÍÎÃÎ ÃÂÈÍÒÀ ÍÀ ÒßÃÓ |
ÂËÈßÍÈÅ ÇÀÇÎÐÀ ÌÅÆÄÓ ÐßÄÀÌÈ
ÑÎÎÑÍÎÃÎ ÂÎÇÄÓØÍÎÃÎ ÂÈÍÒÀ ÍÀ ÒßÃÓ |
19–23 |
Ðîìàíåíêî
È. Ñ., |
FUEL GEAR PUMP OF GAS TURBINE
ENGINE OPERATING PROCESSES SIMULATION ISSUES ANALYSIS |
ÀÍÀ˲Ç
ÎÑÎÁËÈÂÎÑÒÅÉ ÌÎÄÅËÞÂÀÍÍß ÏÐÎÖÅѲ  ÏÀËÈÂÍÈÕ ØÅÑÒÅÐÅÍÍÈÕ ÍÀÑÎÑÀÕ ÃÒÄ |
ÀÍÀËÈÇ
ÎÑÎÁÅÍÍÎÑÒÅÉ ÌÎÄÅËÈÐÎÂÀÍÈß ÏÐÎÖÅÑÑÎÂ Â ÒÎÏËÈÂÍÛÕ ØÅÑÒÅÐÅÍÍÛÕ ÍÀÑÎÑÀÕ ÃÒÄ |
24–30 |
Åïèôàíîâ
Ñ. Â., |
ERROR ANALYSIS OF THERMOCOUPLE
DYNAMIC PERFORMANCES EXPERIMENTAL DETERMINING IN ENGINE CONDITIONS USING STEP
RESPONCE |
ÀÍÀË²Ç ÏÎÕÈÁÎÊ ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÃÎ
ÂÈÇÍÀ×ÅÍÍß ÄÈÍÀ̲×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÒÅÐÌÎÏÀÐÈ Â ÓÌÎÂÀÕ ÄÂÈÃÓÍÀ Ç
ÂÈÊÎÐÈÑÒÀÍÍßÌ ÑÒÐÈÁÊÎÏÎIJÁÍÎÃÎ
ÂÏËÈÂÓ |
ÀÍÀËÈÇ
ÏÎÃÐÅØÍÎÑÒÅÉ ÎÏÐÅÄÅËÅÍÈß ÄÈÍÀÌÈ×ÅÑÊÈÕ ÏÀÐÀÌÅÒÐΠÒÅÐÌÎÏÀÐÛ
ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎ-ÐÀÑ×ÅÒÍÛÌ ÌÅÒÎÄÎÌ |
31-40 |
Êîíñòðóêö³ÿ ³ ì³öí³ñòü
àâ³àö³éíèõ äâèãóí³â ³ åíåðãîóñòàíîâîê |
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Ïðèäîðîæíûé Ð. Ï., |
INFLUENCE OF CREEP OF MATERIAL OF
A HIGH PRESSURE NOZZLEVANES ON THEIR OPERABILITY |
ÂÏËÈ ÏÎÂÇÓ×ÎÑÒ²
ÌÀÒÅвÀËÓ ÍÀ ÐÎÁÎÒÎÇÄÀÒͲÑÒÜ ËÎÏÀÒÎÊ ÑÎÏËÎÂÎÃÎ ÀÏÀÐÀÒÓ ÒÓÐÁ²ÍÈ ÂÈÑÎÊÎÃÎ ÒÈÑÊÓ
|
41–46 |
|
Ñíåæíîé Ã. Â., |
MAGNETOMETRIC METHOD FOR
INVESTIGATION THE EFFECT OF CARBON AND NITROGEN ON THE CORROSION RESISTANCE
OF AUSTENITIC CHROMIUM-NICKEL STEELS |
ÌÀÃͲÒÎÌÅÒÐÈ×ÍÈÉ Ï²ÄÕ²Ä ÄÎ
ÂÈÂ×ÅÍÍß ÂÏËÈÂÓ ÂÓÃËÅÖÞ ² ÀÇÎÒÓ ÍÀ ÊÎÐÎDzÉÍÓ ÒÐÈÂʲÑÒÜ ÀÓÑÒÅͲÒÍÈÕ
ÕÐÎÌÎͲÊÅËÅÂÈÕ ÑÒÀËÅÉ |
47–51 |
|
Êóõòèí Þ. Ï., |
REDUCING VIBRATION TENSION OF
PAIRWISE SHROUDED BLADES OF TURBINE |
ÇÍÈÆÅÍÍß
²ÁÐÎÍÀÏÐÓÆÅÍÎÑÒ² ÏÎÏÀÐÍÎ ÁÀÍÄÀÆÎÂÀÍÈÕ ÐÎÁÎ×ÈÕ ËÎÏÀÒÎÊ ÒÓÐÁ²ÍÈ |
ÑÍÈÆÅÍÈÅ
ÂÈÁÐÎÍÀÏÐ߯ÅÍÍÎÑÒÈ ÏÎÏÀÐÍÎ ÁÀÍÄÀÆÈÐÎÂÀÍÍÛÕ ÐÀÁÎ×ÈÕ ËÎÏÀÒÎÊ ÒÓÐÁÈÍÛ |
52–58 |
Òåõíîëî㳿 âèðîáíèöòâà
îá'ºêò³â àâ³àö³éíî-êîñì³÷íî¿
òåõí³êè |
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Àäæàìñêèé Ñ. Â., |
ÐROSPECTS FOR THE APPLICATION OF ADDITIVE
TECHNOLOGIES IN AIRCRAFT AND ROCKET ENGINEERING |
ÏÅÐÑÏÅÊÒÈÂÈ ÇÀÑÒÎÑÓÂÀÍÍß ÀÄÄÈÒÈÂÍÈÕ ÒÅÕÍÎËÎÃ²É Ó À²À-ÒÀ ÐÀÊÅÒÎÁÓÄÓÂÀÍÍß |
ÏÅÐÑÏÅÊÒÈÂÛ ÏÐÈÌÅÍÅÍÈß ÀÄÄÈÒÈÂÍÛÕ ÒÅÕÍÎËÎÃÈÉ Â ÀÂÈÀ- È ÐÀÊÅÒÎÑÒÐÎÅÍÈÈ |
59–65 |
Ïåäàø À. À., |
STRUCTURE AND PROPERTIES OF SLM-MANUFACTURED
PARTS AFTER LCF-TESTING |
ÑÒÐÓÊÒÓÐÀ É ÂËÀÑÒÈÂÎÑÒ² ÄÅÒÀËÅÉ, ÙÎ ÎÒÐÈÌÀͲ ÑÅËÅÊÒÈÂÍÛÌ ËÀÇÅÐÍÈÌ ÑÏËÀÂËÅÍÍßÌ Ï²ÑËß ÂÈÏÐÎÁÓÂÀÍÍß ÍÀ ÌÀËÎÖÈÊËÎÂÓ ÂÒÎÌÓ |
66–72 |
|
Âèøíåïîëüñêèé Å. Â., |
PREDICTED EFFECTS OF STRENGTHENING BY DIAMOND
IRONING OF DETAILS OBTAINED BY SELECTIVE LASER SINTERING |
ÏÐÎÃÍÎÇÎÂÀͲ ÅÔÅÊÒÈ Ç̲ÖÍÅÍÍß
ÀËÌÀÇÍÈÌ ÂÈÏÐÀÑÎÂÓÂÀÍÍßÌ ÄÅÒÀËÅÉ ÎÒÐÈÌÀÍÈÕ ÇÀ ÄÎÏÎÌÎÃÎÞ ÑÅËÅÊÒÈÂÍÎÃÎ
ËÀÇÅÐÍÎÃÎ ÑϲÊÀÍÍß |
73–82 |
|
²íôîðìàö³éí³ òåõíîëî㳿 |
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Áóðÿ÷åíêî À. Ã., |
STAND IMITATOR OF THE ENGINE AS A UNIVERSAL
MEANS OF ENSURING THE DEVELOPMENT AND TESTING OF REGULATORS |
ÑÒÅÍÄ-IÌIÒÀÒÎÐ ÀÂÈÀÄÂÈÃÓÍÀ ßÊ ÓÍÈÂÅÐÑÀËÜÍÈÉ ÇÀÑIÁ ÇÀÁÅÇÏÅ×ÅÍÍß ÐÎÇÐÎÁÊÈ ÒÀ ÂÈÏÐÎÁÓÂÀÍÜ ÐÅÃÓËßÒÎÐI |
83–88 |
|
Åïèôàíîâ
Ñ. Â., |
RESEARCHING OF RELATIONS FORMING
BETWEEN PARAMETERS OF TWO-SPOOL TURBOFAN DYNAMIC MODEL AND OPERATION MODE |
ÄÎÑË²ÄÆÅÍÍß ÏÐÎÁËÅÌÈ ÔÎÐÌÓÂÀÍÍß
ÇÀËÅÆÍÎÑÒ² ÏÀÐÀÌÅÒв ÄÈÍÀ̲×Íί ÌÎÄÅ˲ ÄÂÎÂÀËÜÍÎÃÎ ÒÐÄÄ Â²Ä ÐÅÆÈÌÓ ÐÎÁÎÒÈ |
89–97 |
|
Tamargazin À., |
NEURAL NETWORK
INTERPOLATION PARAMETERS OF A MULTI-MODE DYNAMIC MODEL OF THE AIRCRAFT ENGINE |
ÍÅÉÐÎÌÅÐÅÆÅÂÀ ²ÍÒÅÐÏÎËßÖ²ß ÏÀÐÀÌÅÒв ÁÀÃÀÒÎÐÅÆÈÌÍί ÄÈÍÀ̲×Íί ÌÎÄÅ˲ À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ |
ÍÅÉÐÎÑÅÒÅÂÀß ÈÍÒÅÐÏÎËßÖÈß ÏÀÐÀÌÅÒÐΠÌÍÎÃÎÐÅÆÈÌÍÎÉ ÄÈÍÀÌÈ×ÅÑÊÎÉ ÌÎÄÅËÈ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß |
98–104 |
Îãàíÿí È. Â. |
MATHEMATICAL MODEL OF FUEL PUMP-REGULATOR OF
HELICOPTER TURBO-SHAFT ENGINE |
ÌÀÒÅÌÀÒÈ×ÍÀ ÌÎÄÅËÜ ÏÀËÈÂÍÎÃÎ ÍÀÑÎÑÀ-ÐÅÃÓËßÒÎÐÀ ÒÓÐÁÎÂÀËÜÍÎÃÎ ÄÂÈÃÓÍÀ ÂÅÐÒÎËÜÎÒÀ |
ÌÀÒÅÌÀÒÈ×ÅÑÊÀß ÌÎÄÅËÜ ÒÎÏËÈÂÍÎÃÎ ÍÀÑÎÑÀ-ÐÅÃÓËßÒÎÐÀ ÒÓÐÁÎÂÀËÜÍÎÃÎ ÄÂÈÃÀÒÅËß ÂÅÐÒÎËÅÒÀ |
105–112 |
Òîâêà÷
Ñ. Ñ. |
APPROACH OF FUZZY CLUSTERING IN DISTRIBUTED
INFORMATION SYSTEMS OF AVIATION ENGINES |
ϲÄÕ²Ä ÍÅײÒÊί ÊËÀÑÒÅÐÈÇÀÖ²¯  ÐÎÇÏÎIJËÅÍÈÕ ²ÍÔÎÐÌÀÖ²ÉÍÈÕ ÑÈÑÒÅÌÀÕ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲ |
ÏÎÄÕÎÄ ÍÅ×ÅÒÊÎÉ ÊËÀÑÒÅÐÈÇÀÖÈÈ Â ÐÀÑÏÐÅÄÅËÅÍÍÛÕ ÈÍÔÎÐÌÀÖÈÎÍÍÛÕ ÑÈÑÒÅÌÀÕ
ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ |
113–117 |
Âàðáàíåö Ð. À., |
THE METHOD OF ANALYTICAL SYNCHRONIZATION OF
THE WORKING PROCESS DATA MONITORING IN TRANSPORT DIESEL ENGINES OPERATING |
ÌÅÒÎÄ ÀÍÀ˲ÒÈ×Íί ÑÈÍÕÐÎͲÇÀÖ²¯ ÄÀÍÈÕ ÌÎͲÒÎÐÈÍÃÓ
ÐÎÁÎ×ÎÃÎ ÏÐÎÖÅÑÓ ÒÐÀÍÑÏÎÐÒÍÈÕ ÄÈÇÅ˲  ÅÊÑÏËÓÀÒÀÖ²¯ |
118–128 |
|
Ìèðãîðîä
Â. Ô., |
ESTIMATION OF POWER OF TREND CRITERIA |
ÎÖÅÍÊÀ ÌÎÙÍÎÑÒÈ ÊÐÈÒÅÐÈÅÂ ÒÐÅÍÄÀ |
129–136 |
|
ʳÿíîâñüêèé Ì. Â., |
CHOICE OF MODELS FOR ADAPTIVE CONTROL BY
RELIABILITY OF INDUSTRIAL EQUIPMENT «ON STATE» |
ÂÈÁ²Ð ÌÎÄÅËÅÉ ÄËß ÀÄÀÏÒÈÂÍÎÃÎ ÊÅÐÓÂÀÍÍß ÍÀIJÉͲÑÒÞ ÏÐÎÌÈÑËÎÂÎÃÎ ÎÁËÀÄÍÀÍÍß «ÇÀ ÑÒÀÍÎÌ» |
ÂÛÁÎÐ ÌÎÄÅËÅÉ ÄËß
ÀÄÀÏÒÈÂÍÎÃÎ ÓÏÐÀÂËÅÍÈß ÍÀÄÅÆÍÎÑÒÜÞ ÏÐÎÌÛØËÅÍÍÎÃÎ ÎÁÎÐÓÄÎÂÀÍÈß «ÏÎ ÑÎÑÒÎßÍÈÞ» |
137–145 |
Õðóëåâ À. Ý., |
FEATURES OF COMPOSING AND APPLICATION OF
LOGICAL METHODS FOR SEARCHING OF FAILURE CAUSES OF INTERNAL COMBUSTION PISTON
ENGINES IN OPERATION |
ÎÑÎÁËÈÂÎÑÒ² ÏÎÁÓÄÎÂÈ ÒÀ ÇÀÑÒÎÑÓÂÀÍÍß ËÎò×ÍÈÕ ÌÅÒÎIJ ÏÎØÓÊÓ ÏÐÈ×ÈÍ Â²ÄÌΠÏÎÐØÍÅÂÈÕ ÄÂÈÃÓͲ ÂÍÓÒвØÍÜÎÃÎ ÇÃÎÐÀÍÍß Â ÅÊÑÏËÓÀÒÀÖ²¯ |
146–157 |
|
158 |
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159 |
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