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

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2015. – ¹ 8 (125). – 143 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2015. – ¹ 8 (125). – 143 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2015. – ¹ 8 (125). – 143 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

Ìîçãîâîé Â. Ô.,
Áàëóøîê Ê. Á.,
Ïàíàñåíêî Â. À.,
Áèðóê Ì. Ê.

MODERN METHODES OF PRELIMINERY PROCESSING MONOWHEELS OF TURBINE ENGINS ON MACHIN CNC

ÑÓ×ÀÑͲ ÌÅÒÎÄÈ ÏÎÏÅÐÅÄÍÜί ÎÁÐÎÁÊÈ ÌÎÍÎÊÎËÅÑ ÃÒÄ ÍÀ ÂÅÐÑÒÀÒÀÕ Ç ×ÏÊ

ÑÎÂÐÅÌÅÍÍÛÅ ÌÅÒÎÄÛ ÏÐÅÄÂÀÐÈÒÅËÜÍÎÉ ÎÁÐÀÁÎÒÊÈ ÌÎÍÎÊÎ謄 ÃÒÄ ÍÀ ÑÒÀÍÊÀÕ Ñ ×ÏÓ

5–10
(6)

Ïåòðèê È. À.,
Îâ÷èííèêîâ À. Â.,
Ñåëèâåðñòîâ À. Ã.

DEVELOPING POWDERS OF TITANIUM ALLOYS FOR ADDITIVE TECHNOLOGIES AS APPLIED TO GAS TURBINE ENGINE PARTS

ÐÎÇÐÎÁÊÀ ÏÎÐÎØÊ²Â ÒÈÒÀÍÎÂÈÕ ÑÏËÀ² ÄËß ÀÄÈÒÈÂÍÈÕ ÒÅÕÍÎËÎÃ²É ÑÒÎÑÎÂÍÎ ÄÎ ÄÅÒÀËÅÉ ÃÒÄ

ÐÀÇÐÀÁÎÒÊÀ ÏÎÐÎØÊΠÒÈÒÀÍÎÂÛÕ ÑÏËÀÂΠÄËß ÀÄÄÈÒÈÂÍÛÕ ÒÅÕÍÎËÎÃÈÉ ÏÐÈÌÅÍÈÒÅËÜÍÎ Ê ÄÅÒÀËßÌ ÃÒÄ

11–16
(6)

Ñèíÿºâà Í. Ï.

DETERMINATION OF ALLOYING ELEMENTS IN THE SUPERALLOYS ON THE BASIS OF NICKEL BY ATOMIC-ABSORPTION METHOD

ÂÈÇÍÀ×ÅÍÍß ËÅÃÓÞ×ÈÕ ÅËÅÌÅÍÒ²Â Ó ÆÀÐÎ̲ÖÍÈÕ ÑÏËÀÂÀÕ ÍÀ ÎÑÍβ ͲÊÅËÞ ÀÒÎÌÍÎ-ÀÁÑÎÐÁÖ²ÉÍÈÌ ÌÅÒÎÄÎÌ

ÎÏÐÅÄÅËÅÍÈÅ ËÅÃÈÐÓÞÙÈÕ ÝËÅÌÅÍÒΠ ÆÀÐÎÏÐÎ×ÍÛÕ ÑÏËÀÂÀÕ ÍÀ ÎÑÍΊͲÊÅËß ÀÒÎÌÍÎ-ÀÁÑÎÐÁÖÈÎÍÍÛÌ ÌÅÒÎÄÎÌ

17–21
(5)

Ñíåæíîé Ã. Â.,
Ñàæíåâ Â. Í.,
Îëüøàíåöêèé Â. Å.

INFLUENCE OF CHEMICAL COMPONENTS ON MECHANICAL AND MAGNETIC PROPERTIES MANGANESE STEELS

ÂÏËÈ ղ̲×ÍÈÕ ÊÎÌÏÎÍÅÍҲ ÍÀ ÌÅÕÀͲ×Ͳ ² ÌÀÃͲÒͲ ÂËÀÑÒÈÂÎÑÒ² ÂÈÑÎÊÎÌÀÐÃÀÍÖÅÂÈÕ ÑÒÀËÅÉ

ÂËÈßÍÈÅ ÕÈÌÈ×ÅÑÊÈÕ ÊÎÌÏÎÍÅÍÒΠÍÀ ÌÅÕÀÍÈ×ÅÑÊÈÅ È ÌÀÃÍÈÒÍÛÅ ÑÂÎÉÑÒÂÀ ÂÛÑÎÊÎÌÀÐÃÀÍÖÅÂÛÕ ÑÒÀËÅÉ

22–26
(5)

Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ

Forghany F.,
Taiebi-Rahni M.,
Asdollahi-Ghohieh A.

NUMERICAL STUDY OF THE AERODYNAMIC EFFECTS ON FLUIDIC THRUST VECTORING

×ÈÑÅËÜÍÅ ÄÎÑË²ÄÆÅÍÍß ÀÅÐÎÄÈÍÀ̲×ÍÈÕ ÌÅÒÎIJ ÊÅÐÓÂÍÍß ÂÅÊÒÎÐÎÌ ÒßÃÈ

×ÈÑËÅÍÍÎÅ ÈÑÑËÅÄÎÂÀÍÈÅ ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÌÅÒÎÄΠÓÏÐÀÂËÅÍÈß ÂÅÊÒÎÐÎÌ ÒßÃÈ

27–34
(8)

Ïðèõîäüêî À. À.,
Àëåêñååíêî Ñ. Â.

ICING OF AIRFOILS: METHODOLOGY OF ICE ACCRETION

ÎÁÌÅÐÇÀÍÍß ÀÅÐÎÄÈÍÀ̲×ÍÈÕ ÏÎÂÅÐÕÎÍÜ: ÌÅÒÎÄÈÊÀ ÌÎÄÅËÞÂÀÍÍß ÍÀÐÎÑÒÀÍÍß ÊÐÈÃÈ

ÎÁËÅÄÅÍÅÍÈÅ ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÏÎÂÅÐÕÍÎÑÒÅÉ: ÌÅÒÎÄÈÊÀ ÌÎÄÅËÈÐÎÂÀÍÈß ÍÀÐÀÑÒÀÍÈß ËÜÄÀ

35–45
(11)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Ðóñàíîâ À. Â.,
Ïàùåíêî Í.
 Â.,
Ðóñàíîâ Ð.
 À.

MODELING OF VISCOUS FLOWS IN FLOW PARTS OF POWER TURBINES USING THE DIFFERENT EQUATIONS OF STATE

ÌÎÄÅËÞÂÀÍÍß ÏÐÎÑÒÎÐÎÂÈÕ Â'ßÇÊÈÕ ÒÅײ¯ Ó ÏÐÎÒÎ×ÍÈÕ ×ÀÑÒÈÍÀÕ ÅÍÅÐÃÅÒÈ×ÍÈÕ ÒÓÐÁ²Í ²Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ Ð²ÇÍÈÕ Ð²ÂÍßÍÜ ÑÒÀÍÓ

ÌÎÄÅËÈÐÎÂÀÍÈÅ ÏÐÎÑÒÐÀÍÑÒÂÅÍÍÛÕ ÂßÇÊÈÕ ÒÅ×ÅÍÈÉ Â ÏÐÎÒÎ×ÍÛÕ ×ÀÑÒßÕ ÝÍÅÐÃÅÒÈ×ÅÑÊÈÕ ÒÓÐÁÈÍ Ñ ÈÑÏÎËÜÇÎÂÀÍÈÅÌ ÐÀÇËÈ×ÍÛÕ ÓÐÀÂÍÅÍÈÉ ÑÎÑÒÎßÍÈß

46–51
(6)

Êîðîáêî Â. Â.

ANALYSIS OF OPPORTUNITIES FOR IMPROVEMENTS OF THERMOACOUSTIC HEAT ENGINES THROUGH THE HEAT EXCHANGE PROCESSES RATIONALIZATION

ÀÍÀË²Ç ÌÎÆËÈÂÎÑÒÅÉ ÂÄÎÑÊÎÍÀËÅÍÍß ÒÅÐÌÎÀÊÓÑÒÈ×ÍÈÕ ÒÅÏËÎÂÈÕ ÌÀØÈÍ ØËßÕÎÌ ÐÀÖ²ÎÍÀËÜÍί ÎÐÃÀͲÇÀÖ²¯ ÏÐÎÖÅѲ ÒÅÏËÎÎÁ̲ÍÓ

ÀÍÀËÈÇ ÂÎÇÌÎÆÍÎÑÒÅÉ ÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈß ÒÅÐÌÎÀÊÓÑÒÈ×ÅÑÊÈÕ ÒÅÏËÎÂÛÕ ÌÀØÈÍ ÏÓÒÅÌ ÐÀÖÈÎÍÀËÜÍÎÉ ÎÐÃÀÍÈÇÀÖÈÈ ÏÐÎÖÅÑÑÀ ÒÅÏËÎÎÁÌÅÍÀ

52–57
(6)

Æóëàé Þ. À.

THEORETICAL EVALUTATION OF EFFICIENCY FACTOR OF VORTEX HEAT GENERATOR

ÒÅÎÐÅÒÈ×ÍÀ ÎÖ²ÍÊÀ ÅÔÅÊÒÈÂÍÎÑÒ² ÊÀ²ÒÀÖ²ÉÍÎÃÎ ÒÅÏËÎÃÅÍÅÐÀÒÎÐÀ

ÒÅÎÐÅÒÈ×ÅÑÊÀß ÎÖÅÍÊÀ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÊÀÂÈÒÀÖÈÎÍÍÎÃÎ ÒÅÏËÎÃÅÍÅÐÀÒÎÐÀ

58–64
(7)

Ëîÿí À. Â.,
Öàãëîâ À. È.

RESULTS OF MIRCRO MASS FLOW CATHODE-NEUTRALIZER WITH OPERATING CURRENT UP TO 300 MA DEVELOPMENT AND TESTING

ÐÅÇÓËÜÒÀÒÈ ÐÎÇÐÎÁÊÈ É ÂÈÏÐÎÁÓÂÀÍÜ Ì²ÊÐÎ ÂÈÒÐÀÒÍÎÃÎ ÊÀÒÎÄÓ-ÍÅÉÒÐÀ˲ÇÀÒÎÐÓ ÍÀ ÐÎÁÎײ ÑÒÐÓÌÈ ÄÎ 300 ÌÀ

ÐÅÇÓËÜÒÀÒÛ ÐÀÇÐÀÁÎÒÊÈ È ÈÑÏÛÒÀÍÈÉ ÌÈÊÐÎ ÐÀÑÕÎÄÍÎÃÎ ÊÀÒÎÄÀ-ÍÅÉÒÐÀËÈÇÀÒÎÐÀ ÍÀ ÐÀÁÎ×ÈÅ ÒÎÊÈ ÄÎ 300 ÌÀ

65–69
 (5)

Ñîðîãèí Ô. Ã.,
Æåìàíþê Ï. Ä.,
Òðîôèìîâ Â. Ï.,
Øàõîâ Þ. Â.,
Ïåòóõîâ È. È.,
Ìèíÿ÷èõèí À. Â.

EXPERIMENTAL INVESTIGATION OF THE GAS TURBINE UNIT CYCLIC AIR SPRAY COOLING SYSTEM

ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ ÄÎÑËIÄÆÅÍÍß ÐÎÇÏÈËÞÂÀËÜÍί ÑÈÑÒÅÌÈ ÎÕÎËÎÄÆÅÍÍß ÖÈÊËÎÂÎÃÎ ÏβÒÐß ÃÒÏ

ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÅ ÈÑÑËÅÄÎÂÀÍÈÅ ÐÀÑÏÛËÈÒÅËÜÍÎÉ ÑÈÑÒÅÌÛ ÎÕËÀÆÄÅÍÈß ÖÈÊËÎÂÎÃÎ ÂÎÇÄÓÕÀ ÃÒÏ

70–74
(5)

Òèìîøåíêî Â. È.,
Äåøêî À.
 Å. 

ON THE RATIONAL IMPLEMENTATION OF PROCESSES OF MIXING AND COMBUSTION WITHIN RAMJET COMBUSTION CHAMBER

ÄÎ ÏÈÒÀÍÍß ÐÀÖ²ÎÍÀËÜÍί ÎÐÃÀͲÇÀÖ²¯ ÏÐÎÖÅѲ Ç̲ØÓÂÀÍÍß ² ÃÎвÍÍß Â ÊÀÌÅв ÇÃÎÐßÍÍß ÏÏÐÄ

Ê ÂÎÏÐÎÑÓ Î ÐÀÖÈÎÍÀËÜÍÎÉ ÎÐÃÀÍÈÇÀÖÈÈ ÏÐÎÖÅÑÑÎÂ ÑÌÅØÅÍÈß È ÃÎÐÅÍÈß Â ÊÀÌÅÐÅ ÑÃÎÐÀÍÈß ÏÂÐÄ

75–81
(7)

Òèòîâ Ì. Þ.,
Ëîÿí À. Â.

MEASUREMENTS OF PROBE CHARACTERISTICS IN THE DISCHARGE CHANNEL OF STATIONARY PLASMA THRUSTER

ÂÈ̲ÐÞÂÀÍÍß ÇÎÍÄÎÂÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ Ó ÐÎÇÐßÄÍÎÌÓ ÊÀÍÀ˲ ÑÒÀÖ²ÎÍÀÐÍÎÃÎ ÏËÀÇÌÎÂÎÃÎ ÄÂÈÃÓÍÀ

ÈÇÌÅÐÅÍÈÅ ÇÎÍÄÎÂÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ Â ÐÀÇÐßÄÍÎÌ ÊÀÍÀËÅ ÑÒÀÖÈÎÍÀÐÍÎÃÎ ÏËÀÇÌÅÍÍÎÃÎ ÄÂÈÃÀÒÅËß

82–88
(7)

Òêà÷ Ì. Ð.,
Òàðàñåíêî À. À.
 

RESEARCH STAND BASED ON PARAMETERS OF TORSIONAL VIBRATIONS ON LOW SPEED DIESEL ENGINE FOR DETERMINATION OF SIZE EFFECT

ÑÒÅÍÄ ÄËß ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ ÌÀÑØÒÀÁÍÎÃÎ ÔÀÊÒÎÐÓ ÍÀ ÏÀÐÀÌÅÒÐÈ ÊÐÓÒÈËÜÍÈÕ ÊÎËÈÂÀÍÜ ÅÍÅÐÃÅÒÈ×ÍÈÕ ÓÑÒÀÍÎÂÎÊ Ç ÌÎÄ

ÑÒÅÍÄ ÄËß ÈÑÑËÅÄÎÂÀÍÈß ÂËÈßÍÈß ÌÀÑØÒÀÁÍÎÃÎ ÔÀÊÒÎÐÀ ÍÀ ÏÀÐÀÌÅÒÐÛ ÊÐÓÒÈËÜÍÛÕ ÊÎËÅÁÀÍÈÉ ÝÍÅÐÃÅÒÈ×ÅÑÊÈÕ ÓÑÒÀÍÎÂÎÊ Ñ ÌÎÄ

89–92
(4)

Åïèôàíîâ Ñ. Â.,
Ùåðáàíü Á. À.,
Áàãàóòäèíîâ Í. Ä.,
×åðêàñîâ Þ. Â.

TURBOFAN TECHNICAL CONDITION FORECAST

ÏÐÎÃÍÎÇÓÂÀÍÍß ÒÅÕͲ×ÍÎÃÎ ÑÒÀÍÓ ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÎÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÓÍÀ

ÏÐÎÃÍÎÇÈÐÎÂÀÍÈÅ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÑÎÑÒÎßÍÈß ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÓÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÀÒÅËß

93–101
(9)

Èíôîðìàöèîííûå òåõíîëîãèè

Ãâîçäåâà È. Ì.

THE DIRECTIONAL CHARACTERISTICS OPTIMIZATION OF ACOUSTIC SENSORS SYSTEMS

ÎÏÒÈ̲ÇÀÖ²ß ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÑÏÐßÌÎÂÀÍÎÑÒ² ÑÈÑÒÅÌ ÀÊÓÑÒÈ×ÍÈÕ ÄÀÒ×ÈʲÂ

ÎÏÒÈÌÈÇÀÖÈß ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÍÀÏÐÀÂËÅÍÍÎÑÒÈ ÑÈÑÒÅÌ ÀÊÓÑÒÈ×ÅÑÊÈÕ ÄÀÒ×ÈÊÎÂ

102–106
(5)

Ãîæèé Î. Ï.,
Ãîæèé Â. Î.

DISTRIBUTION OF ENERGY RESOURCES MODELING BASED ON COLOR PETRI NETS

ÌÎÄÅËÞÂÀÍÍß ÐÎÇÏÎIJËÓ ÅÍÅÐÃÅÒÈ×ÍÈÕ ÐÅÑÓÐѲ ÍÀ ÎÑÍβ ÊÎËÜÎÐÎÂÈÕ ÌÅÐÅÆ ÏÅÒв

ÌÎÄÅËÈÐÎÂÀÍÈÅ ÐÀÑÏÐÅÄÅËÅÍÈß ÅÍÅÐÃÅÒÈ×ÅÑÊÈÕ ÐÅÑÓÐÑΠÍÀ ÎÑÍÎÂÅ ÖÂÅÒÍÛÕ ÑÅÒÅÉ ÏÅÒÐÈ

107–111
(5)

Æóðàâë¸â Â. Í.

PHENOMENOLOGICAL MODEL OF PROCESS OF RADIATION OF ENERGY OF THE SOUND IN THE COURSE OF DETONATION COMBUSTION

ÔÅÍÎÌÅÍÎËÎò×ÍÀ ÌÎÄÅËÜ ÏÐÎÖÅÑÓ ÂÈÏÐÎ̲ÍÞÂÀÍÍß ÅÍÅÐò¯ ÇÂÓÊÓ Â ÏÐÎÖÅѲ ÃÎвÍÍß

ÔÅÍÎÌÅÍÎËÎÃÈ×ÅÑÊÀß ÌÎÄÅËÜ ÏÐÎÖÅÑÑÀ ÈÇËÓ×ÅÍÈß ÝÍÅÐÃÈÈ ÇÂÓÊÀ  ÏÐÎÖÅÑÑÅ ÃÎÐÅÍÈß

112–118
(7)

²ãíàòê³í Â. Ó.,
Òîìàøåâñüêèé Î. Â.

CORRECTION FOR CALIBRATION INTERVAL OF MEASURING EQUIPMENT AT THEIR CURRENT TECHNICAL STATES

ÊÎÐÅÊÒÓÂÀÍÍß ÒÐÈÂÀËÎÑÒ² ̲ÆÏβÐÎ×ÍÈÕ ²ÍÒÅÐÂÀ˲ ÇÀÑÎÁ²Â ÂÈ̲ÐÞÂÀËÜÍί ÒÅÕͲÊÈ ÇÀ ¯Õ ÏÎÒÎ×ÍÈÌ ÒÅÕͲ×ÍÈÌ ÑÒÀÍÎÌ

ÊÎÐÐÅÊÒÈÐÎÂÊÀ ÄËÈÒÅËÜÍÎÑÒÈ ÌÅÆÏÎÂÅÐÎ×ÍÛÕ ÈÍÒÅÐÂÀËΠÑÐÅÄÑÒ ÈÇÌÅÐÈÒÅËÜÍÎÉ ÒÅÕÍÈÊÈ ÏÎ ÈÕ ÒÅÊÓÙÅÌÓ ÒÅÕÍÈ×ÅÑÊÎÌÓ ÑÎÑÒÎßÍÈÞ

119–122
(4)

Ðåâà Î. Ì.,
Ìóõòàðîâ Ï. Ø.,
̳ðçîºâ Á. Ì.,
Ñóëòàíîâ Â. Ç.

INTEGRATIVE MODEL OF ASSESSMENT AIR TRAFFIC CONTROLLERS TO VIOLATION OF THE SPERATION IN THE AIRSPACE

ÌÎÄÅËÜ ²ÍÒÅÃÐÀÒÈÂÍί ÎÖ²ÍÊÈ ÑÒÀÂËÅÍÍß À²ÀÄÈÑÏÅÒ×Åв ÄÎ ÏÎÐÓØÅÍÍß ÍÎÐÌÈ ÅØÅËÎÍÓÂÀÍÍß ÏβÒÐßÍÎÃÎ ÏÐÎÑÒÎÐÓ

ÌÎÄÅËÜ ÈÍÒÅÃÐÀÒÈÂÍÎÉ ÎÖÅÍÊÈ ÎÒÍÎØÅÍÈß ÀÂÈÀÄÈÑÏÅÒ×ÅÐÎÂ Ê ÍÀÐÓØÅÍÈßÌ ÍÎÐÌÛ ÝØÅËÎÍÈÐÎÂÀÍÈß ÂÎÇÄÓØÍÎÃÎ ÏÐÎÑÒÐÀÍÑÒÂÀ

123–129
(7)

Ñåì÷èøèí Ñ. Ì.,
Êà÷óðà Â.À.

PORTABLE AUTOMATED PARAMETERS RECORDER– EXTENTION OF FUNCTIONAL CAPABILITIES

ÀÂÒÎÌÀÒÈÇÎÂÀÍÈÉ ÐŪÑÒÐÀÒÎÐ ÏÀÐÀÌÅÒв ÏÅÐÅÍÎÑÍÈÉ – ÐÎÇØÈÐÅÍÍß ÔÓÍÊÖ²ÎÍÀËÜÍÈÕ ÌÎÆËÈÂÎÑÒÅÉ

ÀÂÒÎÌÀÒÈÇÈÐÎÂÀÍÍÛÉ ÐÅÃÈÑÒÐÀÒÎÐ ÏÀÐÀÌÅÒÐÎÂ ÏÅÐÅÍÎÑÍÎÉ – ÐÀÑØÈÐÅÍÈÅ ÔÓÍÊÖÈÎÍÀËÜÍÛÕ ÂÎÇÌÎÆÍÎÑÒÅÉ

130–133
(4)

Òðåòüÿê Â. Â.

THE IMPLEMENTATION OF THE CLASSIFICATION PHASE IN THE SYSTEM SPRUT TO DEVELOP NEW PROCESSES OF PULSE TECHNOLOGIES

ÐÅÀ˲ÇÀÖ²ß ÊËÀÑÈÔ²ÊÀÖ²ÉÍÎÃÎ ÅÒÀÏÓ Â ÑÈÑÒÅ̲ ÑÏÐÓÒ ÄËß ÐÎÇÐÎÁÊÈ ÍÎÂÈÕ ÒÅÕÍÎËÎò×ÍÈÕ ÏÐÎÖÅѲ ²ÌÏÓËÜÑÍÈÕ ÒÅÕÍÎËÎòÉ

ÐÅÀËÈÇÀÖÈß ÊËÀÑÑÈÔÈÊÀÖÈÎÍÍÎÃÎ ÝÒÀÏÀ  ÑÈÑÒÅÌÅ ÑÏÐÓÒ ÄËß ÐÀÇÐÀÁÎÒÊÈ ÍÎÂÛÕ ÒÅÕÍÎËÎÃÈ×ÅÑÊÈÕ ÏÐÎÖÅÑÑΠÈÌÏÓËÜÑÍÛÕ ÒÅÕÍÎËÎÃÈÉ

134–137
(4)

Èâàùåíêî À. È.,
Öàëèìîâ Ã. Ô.,
Íåðóáàññêèé Â. Â.,
Ëîïóíîâà Í. Í.

AUTOMATION OF TECHNOLOGICAL PROCESS CHECKS ELECTRICAL HARNESSES GTE OF THE AIRCRAFT

ÀÂÒÎÌÀÒÈÇÀÖ²ß ÒÅÕÍÎËÎò×ÍÎÃÎ ÏÐÎÖÅÑÓ ÏÅÐŲÐÊÈ ÅËÅÊÒÐÈ×ÍÈÕ ÄÆÃÓҲ À²ÀÖ²ÉÍÈÕ ÃÒÄ

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ÀËÔÀÂÈÒÍÛÉ ÓÊÀÇÀÒÅËÜ

142

 

 

 

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).