Íàöèîíàëüíûé àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé èíñòèòóò”

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2015. – ¹ 10 (127). – 167 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2015. – ¹ 10 (127). – 167 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2015. – ¹ 10 (127). – 167 ñ.

 

 

Ìàòåðèàëû, ñîäåðæàùèåñÿ â æóðíàëå, îïóáëèêîâàíû
ïî ðåøåíèþ XX ìåæäóíàðîäíîãî êîíãðåññà äâèãàòåëåñòðîèòåëåé

 

ÑÒÀÒÜè (articleS)

 

Àâòîðû
(ÿçûê
îðèãèíàëà)

Íàçâàíèå ñòàòüè (article title)

Ñòðàíèöû

(pages)

English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Ñîòíèêîâ Å. Ã.,
Ëåõîâèöåð Ç. Â.,
Ãðåøòà Â. Ë.,
Êëèìîâ À. Â.,
Òêà÷ Ä. Â.

DEVELOPMENT OF A THERMAL BARRIER COATING FOR DETAILS TURBINE ENGINE, WORKERS AT HIGH TEMPERATURES

ÐÎÇÐÎÁÊÀ ÑÊËÀÄÓ ÒÅÏËÎÇÀÕÈÑÍÎÃÎ ÏÎÊÐÈÒÒß ÍÀ ÄÅÒÀ˲ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲÂ, ÙÎ ÏÐÀÖÞÞÒÜ Â ÓÌÎÂÀÕ ÂÈÑÎÊÈÕ ÒÅÌÏÅÐÀÒÓÐ

ÐÀÇÐÀÁÎÒÊÀ ÑÎÑÒÀÂÀ ÒÅÏËÎÇÀÙÈÒÍÎÃÎ ÏÎÊÐÛÒÈß ÍÀ ÄÅÒÀËÈ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ, ÐÀÁÎÒÀÞÙÈÕ Â ÓÑËÎÂÈßÕ ÂÛÑÎÊÈÕ ÒÅÌÏÅÐÀÒÓÐ

6–10
(5)

Äàíîâ À. Ñ.

SETTING THE PARAMETRES OF HIGH RESOURCE JOINTS BY HIGHLY DURABLE RIVETS WITH COMPENSATORS AND RESTRICTIVE ELEMENTS

ÂÈÁ²Ð ÏÀÐÀÌÅÒв ÂÈÑÎÊÎÐÅÑÓÐÑÍÈÕ Ç'ªÄÍÀÍÜ ÂÈÑÎÊÎ̲ÖÍÈÌÈ ÇÀÊËÅÏÊÀÌÈ Ç ÎÁÌÅÆÓÂÀËÜÍÈÌÈ ÅËÅÌÅÍÒÀÌÈ ÒÀ ÊÎÌÏÅÍÑÀÒÎÐÀÌÈ

ÂÛÁÎÐ ÏÀÐÀÌÅÒÐΠÂÛÑÎÊÎÐÅÑÓÐÑÍÛÕ ÑÎÅÄÈÍÅÍÈÉ ÂÛÑÎÊÎÏÐÎ×ÍÛÌÈ ÇÀÊ˨ÏÊÀÌÈ Ñ ÊÎÌÏÅÍÑÀÒÎÐÀÌÈ È ÎÃÐÀÍÈ×ÈÒÅËÜÍÛÌÈ ÝËÅÌÅÍÒÀÌÈ

11–14
(4)

Êàëèíèíà Í. Å.,
Þõèìåíêî À.
 Å.,
Êàëèíèí À.
 Â.,
Ïàâëîâ Ä.
 Ð.,
Ãðåêîâà Ì.
 Â. 

INFLUENCE OF MODIFICATION ON MECHANICAL PROPERTIES SUPERALLOYS

ÂÏËÈ ÌÎÄÈÔ²ÊÓÂÀÍÍß ÍÀ ÌÅÕÀͲ×Ͳ ÂËÀÑÒÈÂÎÑÒ² ÆÀÐÎ̲ÖÍÈÕ ÑÏËÀ²Â

ÂËÈßÍÈÅ ÌÎÄÈÔÈÖÈÐÎÂÀÍÈß ÍÀ ÌÅÕÀÍÈ×ÅÑÊÈÅ ÑÂÎÉÑÒÂÀ ÆÀÐÎÏÐÎ×ÍÛÕ ÑÏËÀÂÎÂ

15–18
(4)

Ëûñåíêî Í. À.,
Êëî÷èõèí Â. Â.,
Íàóìèê Â. Â.

THE STRUCTURE AND PROPERTIES OF HOLLOW CASTINGS OF NICKEL ALLOY TURBINE BLADES AFTER HOT ISOSTATIC PRESSING

ÑÒÐÓÊÒÓÐÀ ÒÀ ÂËÀÑÒÈÂÎÑÒ² ÏÓÑÒÎÒ²ËÈÕ Â²ÄËÈÂÎÊ ËÎÏÀÒÎÊ ÒÓÐÁ²ÍÈ ²Ç ͲÊÅËÅÂÈÕ ÑÏËÀ² ϲÑËß ÃÀÐß×ÎÃÎ ²ÇÎÑÒÀÒÈ×ÍÎÃÎ ÏÐÅÑÓÂÀÍÍß

ÑÒÐÓÊÒÓÐÀ È ÑÂÎÉÑÒÂÀ ÏÓÑÒÎÒÅËÛÕ ÎÒËÈÂÎÊ ËÎÏÀÒÎÊ ÒÓÐÁÈÍÛ ÈÇ ÍÈÊÅËÅÂÛÕ ÑÏËÀÂΠÏÎÑËÅ ÃÎÐß×ÅÃÎ ÈÇÎÑÒÀÒÈ×ÅÑÊÎÃÎ ÏÐÅÑÑÎÂÀÍÈß

19–27
(9)

Íåñòåðåíêîâ Â. Ì.,
Êðàâ÷óê Ë. À.,
Àðõàíãåëüñêèé Þ. À.,
Ïåòðèê È. À.,
Ìàð÷åíêî Þ. À.

DEVELOPMENT OF THE ADVANCED MANUFACTURING PROCESS FOR LARGE CASE-SHAPED PARTS BY METHOD OF ELECTRON BEAM WELDING (CASE STUDY: MPC FRONT CASING SHELL)

ÐÎÇÐÎÁÊÀ ÏÐÎÃÐÅÑÈÂÍί ÒÅÕÍÎËÎò¯ ÂÈÃÎÒÎÂËÅÍÍß ÊÐÓÏÍÎÃÀÁÀÐÈÒÍÈÕ ÊÎÐÏÓÑÍÈÕ ÄÅÒÀËÅÉ ÌÅÒÎÄÎÌ ÅËÅÊÒÐÎÍÍÎ-ÏÐÎÌÅÍÅÂÎÃÎ ÇÂÀÐÞÂÀÍÍß, ÍÀ ÏÐÈÊËÀIJ ÇÎÂͲØÍÜί ×ÀÑÒÈÍÈ ÊÎÐÏÓÑÓ ÏÅÐÅÄÍÜÎÃÎ ÊÑÄ

ÐÀÇÐÀÁÎÒÊÀ ÏÐÎÃÐÅÑÑÈÂÍÎÉ ÒÅÕÍÎËÎÃÈÈ ÈÇÃÎÒÎÂËÅÍÈß ÊÐÓÏÍÎÃÀÁÀÐÈÒÍÛÕ ÊÎÐÏÓÑÍÛÕ ÄÅÒÀËÅÉ ÌÅÒÎÄÎÌ ÝËÅÊÒÐÎÍÍÎ-ËÓ×ÅÂÎÉ ÑÂÀÐÊÈ, ÍÀ ÏÐÈÌÅÐÅ ÍÀÐÓÆÍÎÉ ×ÀÑÒÈ ÊÎÐÏÓÑÀ ÏÅÐÅÄÍÅÃÎ ÊÑÄ

28–32
(5)

Ïàâëåíêî Ä. Â.,
Êîöþáà Â. Þ.,
Ïàõîëêà Ñ. Í.

THE FORMATION OF THE SUBMICROCRYSTALLINE STRUCTURE IN THE SERIAL AND PERSPECTIVE OF MATERIALS FOR THE COMPRESSOR BLADE OF GAS TURBINE ENGINE

ÔÎÐÌÓÂÀÍÍß ÑÓÁ̲ÊÐÎÊÐÈÑÒÀ˲×Íί ÑÒÐÓÊÒÓÐÈ Â ÑÅвÉÍÈÕ ÒÀ ÏÅÐÑÏÅÊÒÈÂÍÈÕ ÌÀÒÅвÀËÀÕ ËÎÏÀÒÎÊ ÊÎÌÏÐÅÑÎÐÀ ÃÒÄ

ÔÎÐÌÈÐÎÂÀÍÈÅ ÑÓÁÌÈÊÐÎÊÐÈÑÒÀËËÈ×ÅÑÊÎÉ ÑÒÐÓÊÒÓÐÛ Â ÑÅÐÈÉÍÛÕ È ÏÅÐÑÏÅÊÒÈÂÍÛÕ ÌÀÒÅÐÈÀËÀÕ ËÎÏÀÒÎÊ ÊÎÌÏÐÅÑÑÎÐÀ ÃÒÄ

33–39
(7)

Ïåäàø À. À.,
Áÿëèê Ã. À.,
Öèâèðêî Ý. È.

INCREASING OF THE CERAMIC CASTING MOULD THERMAL CONDUCTIVITY WITH COBALT ALUMINATE

ϲÄÂÈÙÅÍÍß ÒÅÏËÎÏÐβÄÍÎÑÒ² ÊÅÐÀ̲×Íί ËÈÂÀÐÍί ÔÎÐÌÈ ÀËÞ̲ÍÀÒÎÌ ÊÎÁÀËÜÒÓ

ÏÎÂÛØÅÍÈÅ ÒÅÏËÎÏÐÎÂÎÄÍÎÑÒÈ ËÈÒÅÉÍÎÉ ÊÅÐÀÌÈ×ÅÑÊÎÉ ÔÎÐÌÛ ÀËÞÌÈÍÀÒÎÌ ÊÎÁÀËÜÒÀ

40–44
(5)

Òèõîìèðîâà Ò. Â.,
Ãàéäóê Ñ. Â.,
Áåëèêîâ Ñ. Á.

RESEARCH OF THE INFLUENCE NIKEL ON PHASE STRUCTURE AND CHARACTERISTIC TEMPERATURES OF THE COBALT ALLOY BY METHOD CALPHAD

ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ Â̲ÑÒÓ ÍÈÊÅËß ÍÀ ÔÀÇÎÂÈÉ ÑÎÑÒÀ ÒÀ ÕÀÐÀÊÒÅÐÈÑÒÈ×Ͳ ÒÅÌÏÅÐÀÒÓÐÈ ÊÎÁÀËÜÒÎÂÎÃÎ ÑÏËÀÂÓ ÌÅÒÎÄÎÌ CALPHAD

ÈÑÑËÅÄÎÂÀÍÈÅ ÂËÈßÍÈß ÑÎÄÅÐÆÀÍÈß ÍÈÊÅËß ÍÀ ÔÀÇÎÂÛÉ ÑÎÑÒÀÂ È ÕÀÐÀÊÒÅÐÈÑÒÈ×ÅÑÊÈÅ ÒÅÌÏÅÐÀÒÓÐÛ ÊÎÁÀËÜÒÎÂÎÃÎ ÑÏËÀÂÀ ÌÅÒÎÄÎÌ CALPHAD

45–48
(4)

Áàñîâ Þ.Ô.,
Îâ÷èííèêîâ À. Â.,
Ìèõàéëþòåíêî À. Â.,
Ãëîòêà Ò. À.

DEVELOPMENT OF INTEGRATED IMPORT-SUBSTITUTING TECHNOLOGY OF GETTING COMPRESSOR BLADE BLANKS

ÐÎÇÐÎÁÊÀ ²ÍÒÅÃÐÎÂÀÍÍί ²ÌÏÎÐÒÎÇÀ̲ÙÓÞ×ί ÒÅÕÍÎËÎò¯ ÎÒÐÈÌÀÍÍß ÇÀÃÎÒÎÂÎÊ ËÎÏÀÒÎÊ ÊÎÌÏÐÅÑÎÐÓ

ÐÀÇÐÀÁÎÒÊÀ ÈÍÒÅÃÐÈÐÎÂÀÍÍÎÉ ÈÌÏÎÐÒÎÇÀÌÅÙÀÞÙÅÉ ÒÅÕÍÎËÎÃÈÈ ÏÎËÓ×ÅÍÈß ÇÀÃÎÒÎÂÎÊ ËÎÏÀÒÎÊ ÊÎÌÏÐÅÑÑÎÐÀ

49–53
(5)

Ïëàíêîâñêèé Ñ. È.,
Öåãåëüíèê Å. Â.,
Ãîëîâèí È. È.,
Ìåëüíè÷óê Ï. È.

PROSPECTS FOR LASER CLEANING DURING REPAIR GTE

ÏÅÐÑÏÅÊÒÈÂÈ ËÀÇÅÐÍί Î×ÈÑÒÊÈ ÏÐÈ ÐÅÌÎÍÒ² ÃÒÄ

ÏÅÐÑÏÅÊÒÈÂÛ ËÀÇÅÐÍÎÉ Î×ÈÑÒÊÈ ÏÐÈ ÐÅÌÎÍÒÅ ÃÒÄ

54–57
(4)

Êîìáàðîâ Â. Â.,
Ñîðîêèí Â. Ô.,
Êðèæèâåö Å. À.

STUDY OF CNC SYSTEM CONTROL CYCLE STABILITY INFLUENCE ON SHAPE-GENERATING ACCURACY

ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ ÑÒÀÁ²ËÜÍÎÑÒ² ÖÈÊËÓ ÓÏÐÀÂ˲ÍÍß ÑÈÑÒÅÌÈ ×ÏÓ ÍÀ ÒÎ×ͲÑÒÜ ÔÎÐÌÎÓÒÂÎÐÞÞ×ÈÕ ÐÓÕ²Â

ÈÑÑËÅÄÎÂÀÍÈÅ ÂËÈßÍÈß ÑÒÀÁÈËÜÍÎÑÒÈ ÖÈÊËÀ ÓÏÐÀÂËÅÍÈß ÑÈÑÒÅÌÛ ×ÏÓ ÍÀ ÒÎ×ÍÎÑÒÜ ÔÎÐÌÎÎÁÐÀÇÓÞÙÈÕ ÄÂÈÆÅÍÈÉ

58–64
(7)

Êîìáàðîâà Å. Â.

FEEDRATES PLANNING METHOD FOR CNC SYSTEM WITH USING S-SHAPED ACCELERATION/DECELERATION LAWS

ÌÅÒÎÄ ÏËÀÍÓÂÀÍÍß ÏÎÄÀ× ÄËß ÑÈÑÒÅÌÈ ×ÏÊ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ S-ÏÎÄIÁÍÈÕ ÇÀÊÎÍI ÐÎÇÃIÍÓ/ÃÀËÜÌÓÂÀÍÍß

ÌÅÒÎÄ ÏËÀÍÈÐÎÂÀÍÈß ÏÎÄÀ× ÄËß ÑÈÑÒÅÌÛ ×ÏÓ Ñ ÏÐÈÌÅÍÅÍÈÅÌ S-ÎÁÐÀÇÍÛÕ ÇÀÊÎÍΠÐÀÇÃÎÍÀ/ÒÎÐÌÎÆÅÍÈß

65–71
(7)

Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Íàçèí Â. È.

EFFECT OF SETTING STIFFNESS OF RINGS ON DISK THE DYNAMIC CHARACTERISTICS HYDROSTATODINAMIC TYPE DOUBLE BEARING

ÂÏËÈ ÆÎÐÑÒÊÎÑÒ² ÏÐÓÆÍÎÃÎ ÂÑÒÀÍÎÂËÅÍÍß Ê²ËÅÖÜ ÍÀ ÄÈÑÊÓ ÍÀ ÄÈÍÀ̲×Ͳ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ Ã²ÄÐÎÑÒÀÒÎÄÈÍÀ̲×ÍÎÃÎ Ï²ÄØÈÏÍÈÊÀ ÇÄÂΪÍÎÃÎ ÒÈÏÓ

ÂËÈßÍÈÅ ÆÅÑÒÊÎÑÒÈ ÓÏÐÓÃÎÉ ÓÑÒÀÍÎÂÊÈ ÊÎËÅÖ ÍÀ ÄÈÑÊÅ ÍÀ ÄÈÍÀÌÈ×ÅÑÊÈÅ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÃÈÄÐÎÑÒÀÒÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÏÎÄØÈÏÍÈÊÀ ÑÄÂÎÅÍÍÎÃÎ ÒÈÏÀ

72–76
(5)

Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ

Ñóááîòîâè÷ Â. Ï.,
Þäèí À. Þ.,
Òåì÷åíêî Ñ. À.

APPLICATION OF INVERSE AERODYNAMIC PROBLEM FOR ANNULAR DIFFUSER DUCTS OPTIMIZATION

ÇÀÑÒÎÑÓÂÀÍÍß ÎÁÅÐÍÅÍί ÀÅÐÎÄÈÍÀ̲×Íί ÇÀÄÀײ ÄËß ÎÏÒÈ̲ÇÀÖ²¯ ʲËÜÖÅÂÈÕ ÄÈÔÓÇÎÐÍÈÕ ÊÀÍÀ˲Â

ÏÐÈÌÅÍÅÍÈÅ ÎÁÐÀÒÍÎÉ ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÎÉ ÇÀÄÀ×È ÄËß ÎÏÒÈÌÈÇÀÖÈÈ ÊÎËÜÖÅÂÛÕ ÄÈÔÔÓÇÎÐÍÛÕ ÊÀÍÀËÎÂ

77–80
(4)

Ãîëüöîâ À. Ñ.

ANALYSIS OF THE POWER CONTROL ALGORITHM AND METHOD OF COMBINATORIAL DEPENDENCE OF KAPLAN TURBINE

ÀÍÀË²Ç ÅÔÅÊÒÈÂÍÎÑÒ² ÀÄÀÏÒÈÂÍÎÃÎ ÊÅÐÓÂÀÍÍß ÏÎÂÎÐÎÒÍÎ-ËÎÏÀÒÍÎÞ Ã²ÄÐÎÒÓÐÁ²ÍÎÞ

ÀÍÀËÈÇ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÀÄÀÏÒÈÂÍÎÃÎ ÓÏÐÀÂËÅÍÈß ÏÎÂÎÐÎÒÍÎ-ËÎÏÀÑÒÍÎÉ ÃÈÄÐÎÒÓÐÁÈÍÎÉ

81–85
(5)

Èãóìåíöåâ Å. À.,
Ïðîêîïåíêî Å. À.

MAGNETIC ENERGY AND ELECTRIC POWER GYRO WITH CHARGE

ÌÀÃͲÒÍÀ ÒÀ ÅËÅÊÒÐÈ×ÍÀ ÅÍÅÐÃ²ß Ã²ÐÎÑÊÎÏÓ, ÙÎ ÌÀª ÇÀÐßÄ

ÌÀÃÍÈÒÍÀß È ÝËÅÊÒÐÈ×ÅÑÊÀß ÝÍÅÐÃÈß ÇÀÐ߯ÅÍÍÎÃÎ ÃÈÐÎÑÊÎÏÀ

86–90
(5)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Áðóíàê À. À.,
Ñèìáèðñêèé Ä. Ô.

ISSUES OF VIBRATIONS IN CYCLIC DURABILITY OF THE AIRCRAFT GTE PARTS

ÄÎ ÏÈÒÀÍÍß ÎÁ˲ÊÓ ÂÏËÈÂÓ Â²ÁÐÀÖ²É ÍÀ ÖÈÊ˲×ÍÓ ÄÎÂÃβ×ͲÑÒÜ ÄÅÒÀËÅÉ À²ÀÖ²ÉÍÈÕ ÃÒÄ

Ê ÂÎÏÐÎÑÓ Ó×ÅÒÀ ÂËÈßÍÈß ÂÈÁÐÀÖÈÉ ÍÀ ÖÈÊËÈ×ÅÑÊÓÞ ÄÎËÃÎÂÅ×ÍÎÑÒÜ ÄÅÒÀËÅÉ ÀÂÈÀÖÈÎÍÍÛÕ ÃÒÄ

91–95
(5)

Íåõîðîøåâ Á. Ã.

ROTARY-PISTON ELECTRICAL COMPRESSOR ÝÂÊ 0,4/0,8

ÐÎÒÎÐÍÎ-ÏÎÐØÍÅÂÈÉ ÅËÅÊÒÐÎÊÎÌÏÐÅÑÎÐ ÅÂÊ 0,4/0,8

ÐÎÒÎÐÍÎ-ÏÎÐØÍÅÂÎÉ ÝËÅÊÒÐÎÊÎÌÏÐÅÑÑÎÐ ÝÂÊ 0,4/0,8

96–101
(6)

Õàóñòîâà À. Í.

INVESTIGATION OF SPT-70 PLUME BY MEANS OF OPTICAL EMISSION SPECTROSCOPY MEATHOD WITH THE SCANNING OF PLASMA THROUGH COLLIMATOR

ÄÎÑË²ÄÆÅÍÍß ÑÒÐÓ¯ ÑÏÄ-70 ÌÅÒÎÄÎÌ ÎÏÒÈ×Íί ªÌ²ÑѲÉÍί ÑÏÅÊÒÐÎÑÊÎϲ¯ ÑÎ ÑÊÓÂÀÂÀÍÍßÌ ÑÒÐÓ¯ ×ÅÐÅÇ ÊÎ˲ÌÀÒÎÐ

ÈÑÑËÅÄÎÂÀÍÈÅ ÑÒÐÓÈ ÑÏÄ-70 ÌÅÒÎÄÎÌ ÎÏÒÈ×ÅÑÊÎÉ ÝÌÈÑÑÈÎÍÍÎÉ ÑÏÅÊÒÐÎÑÊÎÏÈÈ ÑÎ ÑÊÀÍÈÐÎÂÀÍÈÅÌ ÏËÀÇÌÛ ×ÅÐÅÇ ÊÎËËÈÌÀÒÎÐ

102–105
(4)

Òêà÷ Ì. Ð.,
Òèìîøåâñêèé Á. Ã.,
Äîöåíêî Ñ. Ì.,
Ãàëûíêèí Þ. Í.

SPECIFIC POWER THE METAL HYDRIDE UTILIZATION CONTINUOUS POWER PLANTS

ÏÈÒÎÌÀ ÏÎÒÓÆÍ²ÑÒÜ ÌÅÒÀËÎòÄÐÈÄÍÈÕ ÓÒÈ˲ÇÀÖ²ÉÍÈÕ ÓÑÒÀÍÎÂÎÊ ÁÅÇÏÅÐÅÐÂÍί IJ¯

ÓÄÅËÜÍÀß ÌÎÙÍÎÑÒÜ ÌÅÒÀËËÎÃÈÄÐÈÄÍÛÕ ÓÒÈËÈÇÀÖÈÎÍÍÛÕ ÓÑÒÀÍÎÂÎÊ ÍÅÏÐÅÐÛÂÍÎÃÎ ÄÅÉÑÒÂÈß

106–110
(5)

Ìàðêóøèí À. Í.,
Áàêëàíîâ À. Â.,
Ñàëèìçÿíîâà Ã. Ô.

THE ANALYSIS OF THE COMBUSTION CHAMBER PRESSURE LOSS CALCULATION METHOD ON THE EXAMPLE OF NK-8 AIRCRAFT ENGINE

ÎÖ²ÍÊÀ ÌÅÒÎÄÈÊÈ ÐÎÇÐÀÕÓÍÊÓ Ã²ÄÐÀÂ˲×ÍÈÕ ÂÒÐÀÒ Â ÊÀÌÅв ÇÃÎÐßÍÍß ÍÀ ÏÐÈÊËÀIJ ÃÒÄ ÍÊ-8

ÎÖÅÍÊÀ ÌÅÒÎÄÈÊÈ ÐÀÑ×ÅÒÀ ÃÈÄÐÀÂËÈ×ÅÑÊÈÕ ÏÎÒÅÐÜ Â ÊÀÌÅÐÅ ÑÃÎÐÀÍÈß ÍÀ ÏÐÈÌÅÐÅ ÃÒÄ ÍÊ-8

111–114
(4)

Òàðàñåíêî À. È.

"ICE" FLYWHEEL IN SHIP PROPULSION SYSTEMS WITH LOW-SPEED DIESEL ENGINE IN ICE NAVIGATION

«ÊÐÈÆÀͲ» ÌÀÕÎÂÈÊÈ Â ÑÓÄÍÎÂÎÌ ÏÐÎÏÓËÜÑÈÂÍÎÌÓ ÊÎÌÏËÅÊѲ Ç ÌÀËÎÎÁÅÐÒÎÂÈÌÈ ÄÂÇ Â ÓÌÎÂÀÕ ÀÐÊÒÈ×ÍÎÃÎ ÏËÀÂÀÍÍß

«ËÅÄÎÂÛÅ» ÌÀÕÎÂÈÊÈ Â ÑÓÄÎÂÎÌ ÏÐÎÏÓËÜÑÈÂÍÎÌ ÊÎÌÏËÅÊÑÅ Ñ ÌÀËÎÎÁÎÐÎÒÍÛÌÈ ÄÂÑ Â ÓÑËÎÂÈßÕ ËÅÄÎÂÎÃÎ ÏËÀÂÀÍÈß

115–118
(4)

Êîíîíûõèí Å. À.,
Åïèôàíîâ Ñ. Â.,
Ïàâëþê Å. Â.

AIRCRAFT ENGINE ACTUATORS CONTROL SYSTEM BASED ON FUZZY LOGIC

ÑÈÑÒÅÌÀ ÓÏÐÀÂ˲ÍÍß ÂÈÊÎÍÀÂ×ÈÌ ÌÅÕÀͲÇÌÎÌ À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ ÍÀ ÁÀDz ÍÅײÒÊί ËÎòÊÈ

ÑÈÑÒÅÌÀ ÓÏÐÀÂËÅÍÈß ÈÑÏÎËÍÈÒÅËÜÍÛÌ ÌÅÕÀÍÈÇÌÎÌ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß ÍÀ ÁÀÇÅ ÍÅ×ÅÒÊÎÉ ËÎÃÈÊÈ

119–123
(5)

Èíôîðìàöèîííûå òåõíîëîãèè

Áàáåíêî Þ. Â. 

TARIFFS FORMATION FOR AIR TRANSPORTATION TAKING INTO ECOUNT UNIT COST DURING LIFE CYCLE OF HEAVY TRANSPORT AIRCRAFT MODIFICATIONS

ÔÎÐÌÓÂÀÍÍß ÒÀÐÈԲ ÍÀ À²ÀÏÅÐÅÂÅÇÅÍÍß Ç ÓÐÀÕÓÂÀÍÍßÌ ÏÈÒÎÌÈÕ ÂÈÒÐÀÒ ÇÀ ÆÈÒÒªÂÈÉ ÖÈÊË ÌÎÄÈÔ²ÊÀÖ²É ÂÀÆÊÈÕ ÒÐÀÍÑÏÎÐÒÍÈÕ Ë²ÒÀʲÂ

ÔÎÐÌÈÐÎÂÀÍÈÅ ÒÀÐÈÔΠÍÀ ÀÂÈÀÏÅÐÅÂÎÇÊÈ Ñ Ó×ÅÒÎÌ ÓÄÅËÜÍÛÕ ÇÀÒÐÀÒ ÇÀ ÆÈÇÍÅÍÍÛÉ ÖÈÊË ÌÎÄÈÔÈÊÀÖÈÉ Ò߯ÅËÎÃÎ ÒÐÀÍÑÏÎÐÒÍÎÃÎ ÑÀÌÎËÅÒÀ

124–128
(5)

Áàõìåò Ã. Ê.,
Ãóëÿåâà Å. Â.,
Íåñòåðåíêî Ñ. Þ.

THE USE OF SYSTEM ANALYSIS FOR EPT COMPENSATOR-CATHODES OPERATION EFFICIENCY INCREASE

ÂÈÊÎÐÈÑÒÀÍÍß ÑÈÑÒÅÌÍÎÃÎ ÀÍÀ˲ÇÓ ÄËß Ï²ÄÂÈÙÅÍÍß ÅÔÅÊÒÈÂÍÎÑÒ² ÐÎÁÎÒÈ ÊÀÒÎIJÂ-ÊÎÌÏÅÍÑÀÒÎв ÅÐÄ

ÈÑÏÎËÜÇÎÂÀÍÈÅ ÑÈÑÒÅÌÍÎÃÎ ÀÍÀËÈÇÀ ÄËß ÏÎÂÛØÅÍÈß ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÐÀÁÎÒÛ ÊÀÒÎÄÎÂ-ÊÎÌÏÅÍÑÀÒÎÐÎÂ ÝÐÄ

129–135
(7)

Ìèõàéëåíêî Â. Ñ.,
Âàðáàíåö Ð. À.

IDENTIFICATION OF THERMAL OBJECTS IN ADAPTIVE CONTROL SYSTEM USING NEURO-FUZZY NETWORKS

²ÄÅÍÒÈÔ²ÊÀÖ²ß ÒÅÏËÎÂÈÕ ÎÁ'ªÊҲ  ÑÈÑÒÅÌÀÕ ÀÄÀÏÒÈÂÍÎÃÎ ÓÏÐÀÂ˲ÍÍß ÇÀ ÄÎÏÎÌÎÃÎÞ ÍÅÉÐÎ-ÍÅײÒÊÈÕ ÌÅÐÅÆ

ÈÄÅÍÒÈÔÈÊÀÖÈß ÒÅÏËÎÂÛÕ ÎÁÚÅÊÒΠ ÑÈÑÒÅÌÀÕ ÀÄÀÏÒÈÂÍÎÃÎ ÓÏÐÀÂËÅÍÈß Ñ ÏÎÌÎÙÜÞ ÍÅÉÐÎ-ÍÅ×ÅÒÊÈÕ ÑÅÒÅÉ

136–144
(9)

Ðåâà À. Í.,
Óñòèìåíêî È. Ì.,
Ïëÿñîâñêèõ À. Ï.

SYNTHESIS OF ACTIVITY AND CYBERNETIC ANALYSIS OF INFORMATION LOAD OF THE AIR TRAFFIC CONTROLLER IN CONDITIONS OF HIGH AIR TRAFFIC INTENSITY

ÑÈÍÒÅÇ Ä²ßËÜÍÎÑÒ² ² ʲÁÅÐÍÅÒÈ×ÍÈÉ ÀÍÀË²Ç ²ÍÔÎÐÌÀÖ²ÉÍÎÃÎ ÍÀÂÀÍÒÀÆÅÍÍß À²ÀÄÈÑÏÅÒ×ÅÐÀ ÏÐÈ ÂÈÑÎÊ²É ²ÍÒÅÍÑÈÂÍÎÑÒ² ÏβÒÐßÍÎÃÎ ÐÓÕÓ

ÑÈÍÒÅÇ ÄÅßÒÅËÜÍÎÑÒÈ È ÊÈÁÅÐÍÅÒÈ×ÅÑÊÈÉ ÀÍÀËÈÇ ÈÍÔÎÐÌÀÖÈÎÍÍÎÉ ÍÀÃÐÓÇÊÈ ÀÂÈÀÄÈÑÏÅÒ×ÅÐÀ ÏÐÈ ÂÛÑÎÊÎÉ ÈÍÒÅÍÑÈÂÍÎÑÒÈ ÂÎÇÄÓØÍÎÃÎ ÄÂÈÆÅÍÈß

145–157
(13)

Òêà÷åíêî Þ. Ì.

DEVELOPMENT OF TOOLS FOR SUPPORT OF DECISION-MAKING ACCORDING TO THE ANALYSIS OF ACTIVITY OF TRAINEES IN TECHNICAL COLLEGE

ÐÎÇÐÎÁÊÀ ²ÍÑÒÐÓÌÅÍÒÀËÜÍÈÕ ÇÀÑÎÁ²Â ÄËß Ï²ÄÒÐÈÌÊÈ ÏÐÈÉÍßÒÒß Ð²ØÅÍÜ ÏÎ ÀÍÀ˲ÇÓ Ä²ßËÜÍÎÑÒ² Ó×Ͳ  ÒÅÕÍÈ×ÍÎÌÓ ÂÍÇ

ÐÀÇÐÀÁÎÒÊÀ ÈÍÑÒÐÓÌÅÍÒÀËÜÍÛÕ ÑÐÅÄÑÒ ÄËß ÏÎÄÄÅÐÆÊÈ ÏÐÈÍßÒÈß ÐÅØÅÍÈÉ ÏÎ ÀÍÀËÈÇÓ ÄÅßÒÅËÜÍÎÑÒÈ ÎÁÓ×ÀÅÌÛÕ Â ÒÅÕÍÈ×ÅÑÊÎÌ ÂÓÇÅ

158–165
(8)

ÀËÔÀÂÈÒÍÛÉ ÓÊÀÇÀÒÅËÜ

166

 

 

 

Óâàæàåìûå ÷èòàòåëè!

Íàó÷íî-òåõíè÷åñêèé æóðíàë «Àâèàöèîííî-êîñìè÷åñêàÿ òåõíèêà è òåõíîëîãèÿ»

– âõîäèò â óòâåðæäåííûé ÃÀÊ Ïåðå÷åíü íàó÷íûõ ïðîôåññèîíàëüíûõ èçäàíèé Óêðàèíû, â êîòîðûõ ìîãóò ïóáëèêîâàòüñÿ ðåçóëüòàòû äèññåðòàöèîííûõ ðàáîò íà ñîèñêàíèå ó÷åíûõ ñòåïåíåé äîêòîðà è êàíäèäàòà íàóê (ïðèêàç ÌÎÍ Óêðàèíû ¹1279 îò 6.11.2014 ã.);

– ñîõðàíÿåòñÿ â îáùåãîñóäàðñòâåííîé ðåôåðàòèâíîé áàçå äàííûõ «Óêðà¿í³êà íàóêîâà» è ïóáëèêóåòñÿ â ñîîòâåòñòâóþùèõ òåìàòè÷åñêèõ ñåðèÿõ óêðàèíñêîãî ðåôåðàòèâíîãî æóðíàëà «Äæåðåëî» (ñâîáîäíûé îí-ëàéíîâûé äîñòóï ê ðåñóðñàì íà Web-ñåðâåðå http://www.nbuv.gov.ua) (Óêðàèíà),

– ñîõðàíÿåòñÿ â ðåôåðàòèâíîé áàçå äàííûõ Âñåðîññèéñêîãî èíñòèòóòà íàó÷íîé è òåõíè÷åñêîé èíôîðìàöèè (ÂÈÍÈÒÈ) Ðîññèéñêîé àêàäåìèè íàóê è ïóáëèêóåòñÿ â ñîîòâåòñòâóþùèõ òåìàòè÷åñêèõ ñåðèÿõ ÐÆ (ñâîáîäíûé îí-ëàéíîâûé äîñòóï ê ðåñóðñàì íà Web-ñåðâåðå http://www.viniti.ru) (Ðîññèéñêàÿ Ôåäåðàöèÿ),

– âêëþ÷åí â ìåæäóíàðîäíûå áèáëèîìåòðè÷åñêèå è íàóêîìåòðè÷åñêèå áàçû äàííûõ: íàó÷íîé ýëåêòðîííîé áèáëèîòåêè eLIBRARY.RU (Ðîññèéñêàÿ Ôåäåðàöèÿ); Index Copernicus (ICV 2013: 4,83) (Ïîëüøà); Google Scholar (áèáëèîìåòðè÷åñêèå ïîêàçàòåëè – quot.=2094 / h = 10 / i10 = 15).