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

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2014. – ¹ 8 (115). – 191 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2014. – ¹ 8 (115). – 191 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2014. – ¹ 8 (115). – 191 ñ.

 

Ìàòåðèàëû, ñîäåðæàùèåñÿ â æóðíàëå, îïóáëèêîâàíû
ïî ðåøåíèþ XIX 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.,
Ïàíàñåíêî Â. À.,
Áàëóøîê Ê. Á.,
Áèðóê Ì. Ê.

UNIFICATION OF OPERATING PROGRAMS OF PROCESSING DETAILS TURBINE ENGINE ON FIVE-COORDINATE MACHINE CNC

ÓͲԲÊÀÖ²ß ÊÅÐÓÞ×ÈÕ ÏÐÎÃÐÀÌ ÎÁÐÎÁÊÈ ÄÅÒÀËÅÉ ÃÒÄ ÍÀ Ï’ßÒÈÊÎÎÐÄÈÍÀÒÍÈÕ ÂÅÐÑÒÀÒÀÕ Ç ×ÏÊ

ÓÍÈÔÈÊÀÖÈß ÓÏÐÀÂËßÞÙÈÕ ÏÐÎÃÐÀÌÌ ÎÁÐÀÁÎÒÊÈ ÄÅÒÀËÅÉ ÃÒÄ ÍÀ ÏßÒÈÊÎÎÐÄÈÍÀÒÍÛÕ ÑÒÀÍÊÀÕ Ñ ×ÏÓ

6–11
(6)

Êàëèíè÷åíêî Í. Þ.,
Ìàðêîâè÷ Ñ. Å.

THE THERMAL MODEL OF ESTIMATION THERMAL FIELDS BELOW NEAR-SURFACES OF PARTS WHICH MACHINED BY PLANETARY GRINDING TECHNOLOGY

ÒÅÏËÎÔ²ÇÈ×ÍÀ ÌÎÄÅËÜ ÐÎÇÐÀÕÓÍÊÓ ÒÅÌÏÅÐÀÒÓÐÍÈÕ ÏÎË²Â Ó ÏÐÈÏÎÂÅÐÕÍÅÂÈÕ ØÀÐÀÕ ÄÅÒÀËÅÉ ÎÁÐÎÁËÞÂÀÍÈÕ ÇÀ ÒÅÕÍÎËÎòªÞ ÏËÀÍÅÒÀÐÍÎÃÎ ØË²ÔÓÂÀÍÍß

ÒÅÏËÎÔÈÇÈ×ÅÑÊÀß ÌÎÄÅËÜ ÐÀÑרÒÀ ÒÅÌÏÅÐÀÒÓÐÍÛÕ ÏÎËÅÉ Â ÏÐÈÏÎÂÅÐÕÍÎÑÒÍÛÕ ÑËÎßÕ ÄÅÒÀËÅÉ ÎÁÐÀÁÀÒÛÂÀÅÌÛÕ ÏÎ ÒÅÕÍÎËÎÃÈÈ ÏËÀÍÅÒÀÐÍÎÃÎ ØËÈÔÎÂÀÍÈß

12–17
(6)

Ñîðîêèí Â. Ô.,
Êîìáàðîâ Â. Â.,
Òåðíþê È. À.

STABILIZATION OF CONTOUR FEEDRATE FOR THE SPLINE INTERPOLATOR CNC SYSTEM BY HIGH PROCESSING SPEED CRITERION

ÑÒÀÁ²Ë²ÇÀÖ²ß ÊÎÍÒÓÐÍί ØÂÈÄÊÎÑÒ²  ÑÏËÀÉÍÎÂÎÌÓ ²ÍÒÅÐÏÎËßÒÎв ÑÈÑÒÅÌÈ ×ÏÓ ÇÀ ÊÐÈÒÅвªÌ ÂÈÑÎÊί ØÂÈÄÊÎIJ¯

ÑÒÀÁÈËÈÇÀÖÈß ÊÎÍÒÓÐÍÎÉ ÑÊÎÐÎÑÒÈ Â ÑÏËÀÉÍÎÂÎÌ ÈÍÒÅÐÏÎËßÒÎÐÅ ÑÈÑÒÅÌÛ ×ÏÓ ÏÎ ÊÐÈÒÅÐÈÞ ÂÛÑÎÊÎÃÎ ÁÛÑÒÐÎÄÅÉÑÒÂÈß

18–24
(7)

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

PROPERTIES INCREASEMENT OF WELDING JOINTS OF ROTOR PARTS MADE OF TITANIUM ALLOYS

ϲÄÂÈÙÅÍÍß ÂËÀÑÒÈÂÎÑÒÅÉ ÇÂÀÐÍÈÕ Ç¢ªÄÍÀÍÜ ÐÎÒÎÐÍÈÕ ÄÅÒÀËÅÉ ²Ç ÒÈÒÀÍÎÂÈÕ ÑÏËÀ²Â

ÏÎÂÛØÅÍÈÅ ÑÂÎÉÑÒÂ ÑÂÀÐÍÛÕ ÑÎÅÄÈÍÅÍÈÉ ÐÎÒÎÐÍÛÕ ÄÅÒÀËÅÉ ÈÇ ÒÈÒÀÍÎÂÛÕ ÑÏËÀÂÎÂ

25–29
(5)

Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Ëîñü À. Â.

CRITERIA OF EFFECTIVE APPLICATION OF ANTIFRICTIONAL COATINGS IN MOVABLE ULTIMATE AND SKEW LOADED AIRCRAFT UNITS

ÊÐÈÒÅв¯ ÅÔÅÊÒÈÂÍÎÑÒ² ÇÀÑÒÎÑÓÂÀÍÍß ÀÍÒÈÔвÊÖIÉÍÈÕ ÏÎÊÐÈÒҲ  ÐÓÕÎÌÈÕ ÃÐÀÍÈ×ÍÎ ÒÀ ÊÎÑÎÑÈÌÅÒÐÈ×ÍΠÍÀÂÀÍÒÀÆÅÍÈÕ ÂÓÇËÀÕ Ë²ÒÀÊÎÂÈÕ ÀÃÐÅÃÀÒ²Â

ÊÐÈÒÅÐÈÈ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÏÐÈÌÅÍÅÍÈß ÀÍÒÈÔÐÈÊÖÈÎÍÍÛÕ ÏÎÊÐÛÒÈÉ Â ÏÎÄÂÈÆÍÛÕ ÏÐÅÄÅËÜÍÎ È ÊÎÑÎÑÈÌÌÅÒÐÈ×ÍÎ ÍÀÃÐÓÆÅÍÍÛÕ ÓÇËÀÕ ÑÀÌÎËÅÒÍÛÕ ÀÃÐÅÃÀÒÎÂ

30–36
(7)

Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ

Êîòîâ À. Â.,
Øàðîâñêèé Ì. À.,
Øåëêîâñêèé Ì. Þ.

AERODYNAMIC IMPROVEMENT OF RADIAL VANED DIFFUSER OF COMPRESSOR CENTRIFUGAL STAGE

ÀÅÐÎÄÈÍÀ̲×ÍÅ ÂÄÎÑÊÎÍÀËÅÍÍß ÐÀIJÀËÜÍÎÃÎ ËÎÏÀÒÊÎÂÎÃÎ ÄÈÔÓÇÎÐÀ ²ÄÖÅÍÒÐÎÂÎÃÎ ÑÒÓÏÅÍß ÊÎÌÏÐÅÑÎÐÀ

ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÎÅ ÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈÅ ÐÀÄÈÀËÜÍÎÃÎ ËÎÏÀÒÎ×ÍÎÃÎ ÄÈÔÔÓÇÎÐÀ ÖÅÍÒÐÎÁÅÆÍÎÉ ÑÒÓÏÅÍÈ ÊÎÌÏÐÅÑÑÎÐÀ

37–43
(7)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Ïîïóãà À. È.,
Êîëÿäà Â. Â.,
Åëàíñêèé À. Â.

SHAPING A REASONABLE APPEARANCE OF ENGINE - ENGINE NACELLE - AIRCRAFT PYLON SYSTEM BY USING COMPUTATIONAL MODELING

ÔÎÐÌÓÂÀÍÍß ÐÀÖ²ÎÍÀËÜÍÎÃÎ ÎÁ˲ÊÓ ÑÈÑÒÅÌÈ ÄÂÈÃÓÍ - ÌÎÒÎÃÎÍÄÎËÀ - ˲ÒÀÊÎÂÈÉ Ï²ËÎÍ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ×ÈÑÅËÜÍÎÃÎ ÌÎÄÅËÞÂÀÍÍß

ÔÎÐÌÈÐÎÂÀÍÈÅ ÐÀÖÈÎÍÀËÜÍÎÃÎ ÎÁËÈÊÀ ÑÈÑÒÅÌÛ ÄÂÈÃÀÒÅËÜ - ÌÎÒÎÃÎÍÄÎËÀ - ÑÀÌÎËÅÒÍÛÉ ÏÈËÎÍ Ñ ÈÑÏÎËÜÇÎÂÀÍÈÅÌ ×ÈÑËÅÍÍÎÃÎ ÌÎÄÅËÈÐÎÂÀÍÈß

44–49
(6)

Êîðîáêî Â. Â.,
Ìîñêîâêî Î. Î.

FEATURES START THERMOACOUSTIC ENGINE UNDER CONDITIONS USING LOW-TEMPERATURE THERMAL ENERGY SOURCE

ÎÑÎÁËÈÂÎÑÒ² ÏÐÎÖÅÑѲ ÇÀÏÓÑÊÓ ÒÅÐÌÎÀÊÓÑÒÈ×ÍÈÕ ÄÂÈÃÓͲ ÇÀ ÓÌΠÂÈÊÎÐÈÑÒÀÍÍß ÍÈÇÜÊÎÒÅÌÏÅÐÀÒÓÐÍÈÕ ÄÆÅÐÅË ÒÅÏËÎÂί ÅÍÅÐò¯

ÎÑÎÁÅÍÍÎÑÒÈ ÇÀÏÓÑÊÀ ÒÅÐÌÎÀÊÓÑÒÈ×ÅÑÊÈÕ ÄÂÈÃÀÒÅËÅÉ Â ÓÑËÎÂÈßÕ ÈÑÏÎËÜÇÎÂÀÍÈß ÍÈÇÊÎÒÅÌÏÅÐÀÒÓÐÍÛÕ ÈÑÒÎ×ÍÈÊΠÒÅÏËÎÂÎÉ ÝÍÅÐÃÈÈ

50–54
(5)

Ìàìåäîâ Á. Ø.

ÒÍÅ SINGLE THEORY OF CONTINUOS FLOW PROPULSION. NEW DESTINATION AND WORK PRINCIPAL OF "ZERO" TURBO-JET COMPRESSORE LOW PRESSURE STEP

ªÄÈÍÀ ÒÅÎÐ²ß ÐÓØ²¯Â. ÍÎÂÅ ÏÐÈÇÍÀ×ÅÍÍß ÒÀ ÏÐÈÍÖÈÏ ÐÎÁÎÒÈ "ÍÓËÜÎÂί" ÑÒÓÏÅͲ ÊÎÌÏÐÅÑÎÐÀ ÍÈÇÜÊÎÃÎ ÒÈÑÊÓ ÒÓÐÁÎÐÅÀÊÒÈÂÍÈÕ ÄÂÈÃÓͲÂ

ÅÄÈÍÀß ÒÅÎÐÈß ÄÂÈÆÈÒÅËÅÉ. ÍÎÂÎÅ ÍÀÇÍÀ×ÅÍÈÅ È ÏÐÈÍÖÈÏ ÐÀÁÎÒÛ "ÍÓËÅÂÎÉ" ÑÒÓÏÅÍÈ ÊÎÌÏÐÅÑÑÎÐÀ ÍÈÇÊÎÃÎ ÄÀÂËÅÍÈß

55–60
(6)

Ãîðÿ÷êèí Å. Ñ.,
Ïîïîâ Ã. Ì.,
Ìàòâååâ Â. Í.

WORKFLOW MODELING OF THREE STAGE LOW PRESSURE COMPRESSOR OF GAS TURBINE ENGINE

ÌÎÄÅËÞÂÀÍÍß ÐÎÁÎ×ÎÃÎ ÏÐÎÖÅÑÓ ÒÐÜÎÕÑÒÓÏÅÍÅÂÎÃÎ ÊÎÌÏÐÅÑÎÐÀ ÍÈÇÜÊÎÃÎ ÒÈÑÊÓ ÃÀÇÎÒÓÐÁ²ÍÍÎÃÎ ÄÂÈÃÓÍÀ

ÌÎÄÅËÈÐÎÂÀÍÈÅ ÐÀÁÎ×ÅÃÎ ÏÐÎÖÅÑÑÀ ÒÐÅÕÑÒÓÏÅÍ×ÀÒÎÃÎ ÊÎÌÏÐÅÑÑÎÐÀ ÍÈÇÊÎÃÎ ÄÀÂËÅÍÈß ÃÀÇÎÒÓÐÁÈÍÍÎÃÎ ÄÂÈÃÀÒÅËß

61–65
(5)

Ãðèãîðüåâ Â. À.,
Êàëàáóõîâ Ä. Ñ.,
Ðàäüêî Â. Ì.

METHODS OF GENERALIZATION AND REPRESENTATION CHARACHTERISTICS OF AVIATION GAS TURBINES

ÌÅÒÎÄÈ ÓÇÀÃÀËÜÍÅÍÍß ÒÀ ÏÎÄÀÍÍß ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÒÓÐÁ²Í À²ÀÖ²ÉÍÈÕ ÃÒÄ

ÌÅÒÎÄÛ ÎÁÎÁÙÅÍÈß È ÏÐÅÄÑÒÀÂËÅÍÈÅ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÒÓÐÁÈÍ ÀÂÈÀÖÈÎÍÍÛÕ ÃÒÄ

66–72
(7)

Àáäóëèí Ì. Ç.,
Ñåðûé À. À.,
Æó÷åíêî À. Ì.

PRINCIPLES OF WORKING PROCEDURE ORGANIZATION OF COMBUSTION CHAMBERS

ÏÐÈÍÖÈÏÈ ÎÐÃÀͲÇÀÖ²¯ ÐÎÁÎ×ÎÃÎ ÏÐÎÖÅÑÓ ÊÀÌÅÐ ÇÃÎÐßÍÍß

ÏÐÈÍÖÈÏÛ ÎÐÃÀÍÈÇÀÖÈÈ ÐÀÁÎ×ÅÃÎ ÏÐÎÖÅÑÑÀ ÊÀÌÅÐ ÑÃÎÐÀÍÈß

73–78
()

Êðàâ÷åíêî È. Ô.,
Æóðàâëåâ Â. Í.,
Áîðçîâ Ñ. À.,
Ïàï÷¸íêîâ À. Â.

MATHEMATICAL MODELS OF ENERGETIC EFFECTIVENESS FOR COMBUSTION CHAMBER UNIT OF GAS TURBINE ENGINE

ÌÀÒÅÌÀÒÈ×Ͳ ÌÎÄÅ˲ ÏÀÐÀÌÅÒв ÅÍÅÐÃÅÒÈ×Íί ÅÔÅÊÒÈÂÍÎÑÒ² ÐÎÁÎÒÈ ÊÀÌÅÐÈ ÇÃÎÐßÍÍß ÃÒÄ

ÌÀÒÅÌÀÒÈ×ÅÑÊÈÅ ÌÎÄÅËÈ ÏÀÐÀÌÅÒÐΠÝÍÅÐÃÅÒÈ×ÅÑÊÎÉ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÐÀÁÎÒÛ ÊÀÌÅÐÛ ÑÃÎÐÀÍÈß ÃÒÄ

79–83
(5)

Ñåðáèí Ñ. È.,
Ìîñòèïàíåíêî À. Á.,
Êîçëîâñêèé À. Â.,
Âèëêóë Â. Â.

SUPPRESSING METHODS OF THE PULSATION BURNING IN GASEOUS FUELS GAS TURBINE COMBASTION CHAMBER

ÌÅÒÎÄÈ ÇÍÈÆÅÍÍß ²ÍÒÅÍÑÈÂÍÎÑÒ² ÏÓËÜÑÀÖ²ÉÍÎÃÎ ÃÎвÍÍß Â ÊÀÌÅв ÇÃÎÐßÍÍß ÃÒÄ, ÙÎ ÏÐÀÖÞª ÍÀ ÃÀÇÎÏÎIJÁÍÎÌÓ ÏÀËȲ

ÌÅÒÎÄÛ ÑÍÈÆÅÍÈß ÈÍÒÅÍÑÈÂÍÎÑÒÈ ÏÓËÜÑÀÖÈÎÍÍÎÃÎ ÃÎÐÅÍÈß Â ÊÀÌÅÐÅ ÑÃÎÐÀÍÈß ÃÒÄ, ÐÀÁÎÒÀÞÙÅÉ ÍÀ ÃÀÇÎÎÁÐÀÇÍÎÌ ÒÎÏËÈÂÅ

84–88
(5)

Äîëìàòîâ Ä. À.,
Õàäæèâàíä Ì.

SINGLE HYDROCARBON DROP COMBUSTION IN THE PRESENCE OF STATIONARY ARC

ÌÀÒÅÌÀÒÈ×ÍÅ ÌÎÄÅËÞÂÀÍÍß ÃÎвÍÍß ÃÅÒÅÐÎÃÅÍÍί ÑÓ̲ز ÏÐÈ ÄÎÄÀÒÊÎÂ²É ÑÒÈÌÓËßÖ²¯

ÌÀÒÅÌÀÒÈ×ÅÑÊÎÅ ÌÎÄÅËÈÐÎÂÀÍÈÅ ÃÎÐÅÍÈß ÃÅÒÅÐÎÃÅÍÍÎÉ ÑÌÅÑÈ ÏÐÈ ÄÎÏÎËÍÈÒÅËÜÍÎÉ ÑÒÈÌÓËßÖÈÈ

89–93
(5)

Õàëàòîâ À. À.,
Ïàí÷åíêî Í. À.,
Áîðèñîâ È. È.,
Äàøåâñêèé Þ. ß.

UNEVENNESS OF DOUBLE JET FILM COOLING

ÍÅвÂÍÎ̲ÐͲÑÒÜ ÄÂÎÑÒÐÓÌÅÍÅÂÎÃÎ Ï˲ÂÊÎÂÎÃÎ ÎÕÎËÎÄÆÅÍÍß

ÍÅÐÀÂÍÎÌÅÐÍÎÑÒÜ ÄÂÓÕÑÒÐÓÉÍÎÃÎ ÏËÅÍÎ×ÍÎÃÎ ÎÕËÀÆÄÅÍÈß

94–99
(6)

Íàçèí Â. È.

STAND, PILOT PLANT AND METHOD OF EXPERIMENTAL RESEARCHES OF HYDROSTATODYNAMIC BEARINGS OF THE DOUBLED TYPE

ÑÒÅÍÄ, ÄÎÑ˲ÄÍÀ ÓÑÒÀÍÎÂÊÀ ² ÌÅÒÎÄÈÊÀ ÄÎÑ˲ÄÍÈÕ ÄÎÑË²ÄÆÅÍÜ Ã²ÄÐÎÑÒÀÒÎÄÈÍÀ̲×ÍÈÕ Ï²ÄØÈÏÍÈʲ ÇÄÂΪÍÎÃÎ ÒÈÏÓ

ÑÒÅÍÄ, ÎÏÛÒÍÀß ÓÑÒÀÍÎÂÊÀ È ÌÅÒÎÄÈÊÀ ÎÏÛÒÍÛÕ ÈÑÑËÅÄÎÂÀÍÈÉ ÃÈÄÐÎÑÒÀÒÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÏÎÄØÈÏÍÈÊΠÑÄÂÎÅÍÍÎÃÎ ÒÈÏÀ

100–103
(4)

Íàçàðåíêî Þ. Á.,
Ðîäþê Ñ. À.

PARAMETRIC RESONANCE LOW PRESSURE TURBINE ROTOR WITH THE APPEARANCE OF A GAP ON THE LANDING GIRDLE SOCK AND SHAFT LPT

ÏÀÐÀÌÅÒÐÈ×ÍÈÉ ÐÅÇÎÍÀÍÑ ÐÎÒÎÐÓ ÒÓÐÁIÍÈ ÍÈÇÜÊÎÃÎ ÒÈÑÊÓ Ó ÂÈÏÀÄÊÓ ÊÎËÈ ª ÇÀÇÎÐ ÏÎÑÀÄÊÎÂÈÕ ÏÎßÑÊI ÍÎÑÊÀ ÍÀ ÂÀËI ÒÍÒ

ÏÀÐÀÌÅÒÐÈ×ÅÑÊÈÉ ÐÅÇÎÍÀÍÑ ÐÎÒÎÐÀ ÒÓÐÁÈÍÛ ÍÈÇÊÎÃÎ ÄÀÂËÅÍÈß ÏÐÈ ÐÀÇÇÀÇÎÐÈÂÀÍÈÈ ÏÎÑÀÄÎ×ÍÛÕ ÏÎßÑÊΠÍÎÑÊÀ ÍÀ ÂÀË ÒÍÄ

104–107
(4)

Ïàíàðèí Â. Å.,
Çàõàðîâ Ñ. Ì.,
Øìàòêî Î. À.,
Êèñåëü Â. Ì.,
Òåðåíòüåâ À. Å.

PLASMA COATING OF THE EUTEKTIC ALLOY QUASITHREEFOLD SYSTEM FE-TIB2-CRB2

ÏËÀÇÌÎÂÅ ÏÎÊÐÈÒÒß Ç ÅÂÒÅÊÒÈ×ÍÎÃÎ ÑÏËÀÂÓ ÊÂÀDzÏÎÒвÉÍί ÑÈÑÒÅÌÈ FE-TIÂ2-CRÂ2

ÏËÀÇÌÅÍÍÎÅ ÏÎÊÐÛÒÈÅ ÈÇ ÝÂÒÅÊÒÈ×ÅÑÊÎÃÎ ÑÏËÀÂÀ ÊÂÀÇÈÒÐÎÉÍÎÉ ÑÈÑÒÅÌÛ FE-TIB2-CRB2

108–112
(5)

Ñàëî Ì. Ï.,
Èâàíèöêèé Ã. Ì.,
Íàëåòà À. Ã.,
Ñè÷åâîé À. Â.

FUEL PERFORMANCE IMPROVEMENT METHOD OF LPS STAGES

ÌÅÒÎÄ Ï²ÄÂÈÙÅÍÍß ÅÊÑÏËÓÀÒÀÖ²ÉÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÏÀËÈÂÀ ÄËß ÏÐÄ ÊÎÑ̲×ÍÈÕ ÑÒÓÏÅͲÂ

ÌÅÒÎÄ ÏÎÂÛØÅÍÈß ÝÊÑÏËÓÀÒÀÖÈÎÍÍÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÒÎÏËÈÂÀ ÄËß ÆÐÄ ÊÎÑÌÈ×ÅÑÊÈÕ ÑÒÓÏÅÍÅÉ

113–119
(7)

Ëàçóòêèí Ã. Â.,
Áîÿðîâ Ê. Â.

DEVELOPMENT OF ALGORITHM DESIGN UNLOADING AND SHOCKPROOF DEVICES METAL RUBBER DAMPERS

ÐÎÇÐÎÁÊÀ ÀËÃÎÐÈÒÌÓ ÏÐÎÅÊÒÓÂÀÍÍß ÐÎÇÂÀÍÒÀÆÓÂÀËÜÍÈÕ ² ÏÐÎÒÈÓÄÀÐÍÈÕ ÏÐÈÑÒÐί ÄËß ÌÅÒÀËÎÃÓÌÎÂÈÕ Â²ÁÐβÇÎËßÒÎвÂ

ÐÀÇÐÀÁÎÒÊÀ ÀËÃÎÐÈÒÌÀ ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÐÀÇÃÐÓÇÎ×ÍÛÕ È ÏÐÎÒÈÂÎÓÄÀÐÍÛÕ ÓÑÒÐÎÉÑÒ ÄËß ÌÅÒÀËËÎÐÅÇÈÍÎÂÛÕ ÂÈÁÐÎÈÇÎËßÒÎÐÎÂ

120–125
(6)

Åðìàêîâ À. È.,
Óðëàïêèí À. Â.

RESEARCH OF INFLUENCE OF VIBRATION CONNECTEDNESS OF BLADES TO EIGENMODE OF MISTUNED BLADE DISK

ÀÍÀË²Ç ÂÏËÈÂÓ ÂÅËÈ×ÈÍÈ ÇÂ'ßÇÀÍÎÑÒ² ÊÎËÈÂÀÍÜ ËÎÏÀÒÎÊ ÍÀ ÐÎÇËÀÄ ÂËÀÑÍÈÕ ÔÎÐÌ ÊÎËÈÂÀÍÜ ÐÎÁÎ×ÈÕ ÊÎËÅÑ, ßʲ ²ÄÕÈËßÞÒÜÑß Â²Ä ÑÒÐÎÃί ÑÈÌÅÒв¯

ÀÍÀËÈÇ ÂËÈßÍÈß ÂÅËÈ×ÈÍÛ ÑÂßÇÀÍÍÎÑÒÈ ÊÎËÅÁÀÍÈÉ ËÎÏÀÒÎÊ ÍÀ ÈÑÊÀÆÅÍÈÅ ÑÎÁÑÒÂÅÍÍÛÕ ÔÎÐÌ ÐÀÁÎ×ÈÕ ÊÎ˨Ñ, ÎÒÊËÎÍßÞÙÈÕÑß ÎÒ ÑÒÐÎÃÎÉ ÑÈÌÌÅÒÐÈÈ

126–130
(5)

Êàáàííèê Ñ. Í.,
Ñòåëüìàõ À. Ë.,
Çèíüêîâñêèé À. Ï.

ALGORITHM FOR IMPLEMENTING THE EXPRESS-EVALUATION METHOD TO PREDICT THE STABILITY OF COMPRESSOR BLADING AGAINST SUBSONIC FLUTTER

ÀËÃÎÐÈÒÌ ÐÅÀ˲ÇÀÖ²¯ ÌÅÒÎÄÓ ÅÊÑÏÐÅÑ-ÎÖ²ÍÊÈ ÏÐÎÃÍÎÇÓÂÀÍÍß ÑÒ²ÉÊÎÑÒ² ÄÎ ÄÎÇÂÓÊÎÂÎÃÎ ÐÅØ²ÒÊÎÂÎÃÎ ÔËÀÒÅÐÓ ËÎÏÀÒÊÎÂÈÕ Â²Íֲ ÊÎÌÏÐÅÑÎвÂ

ÀËÃÎÐÈÒÌ ÐÅÀËÈÇÀÖÈÈ ÌÅÒÎÄÀ ÝÊÑÏÐÅÑÑ-ÎÖÅÍÊÈ ÏÐÎÃÍÎÇÈÐÎÂÀÍÈß ÓÑÒÎÉ×ÈÂÎÑÒÈ Ê ÄÎÇÂÓÊÎÂÎÌÓ ÐÅØÅÒÎ×ÍÎÌÓ ÔËÀÒÒÅÐÓ ËÎÏÀÒÎ×ÍÛÕ ÂÅÍÖΠÊÎÌÏÐÅÑÑÎÐÎÂ

131–137
(7)

Äîâãàíü Ä. Â.,
Æóê È. Þ.

EFFECT OF RETAINING PRESSURE TO THE NATURAL FREQUENCIES OF GTE BLADES

ÂÏËÈ ÂÅËÈ×ÈÍÈ ÇÀÒÈÑÍÅÍÍß ÐÎÁÎ×ÈÕ ËÎÏÀÒÎÊ ÃÒÄ ÍÀ ×ÀÑÒÎÒÓ ¯Õ ÂËÀÑÍÈÕ ÊÎËÈÂÀÍÜ

ÂËÈßÍÈÅ ÂÅËÈ×ÈÍÛ ÇÀÆÀÒÈß ÐÀÁÎ×ÈÕ ËÎÏÀÒÎÊ ÃÒÄ ÍÀ ×ÀÑÒÎÒÓ ÈÕ ÑÎÁÑÒÂÅÍÍÛÕ ÊÎËÅÁÀÍÈÉ

138–141
(4)

Ãîðáåíêî À. Í.

INFLUENCE OF INERTIAL ANISOTROPY ON THE FORCED OSCILLATIONS OF UNBALANCED GYROSCOPIC ROTOR

ÂÏËÈ ²ÍÅÐÖ²ÉÍί ÀͲÇÎÒÐÎϲ¯ ÍÀ ÂÈÌÓØÅͲ ÊÎËÈÂÀÍÍß ÍÅÂвÂÍÎÂÀÆÅÍÎÃΠòÐÎÑÊÎϲ×ÍÎÃÎ ÐÎÒÎÐÀ

ÂËÈßÍÈÅ ÈÍÅÐÖÈÎÍÍÎÉ ÀÍÈÇÎÒÐÎÏÈÈ ÍÀ ÂÛÍÓÆÄÅÍÍÛÅ ÊÎËÅÁÀÍÈß ÍÅÓÐÀÂÍÎÂÅØÅÍÍÎÃÎ ÃÈÐÎÑÊÎÏÈ×ÅÑÊÎÃÎ ÐÎÒÎÐÀ

142–147
(6)

Øóëüæåíêî Í. Ã.,
Ãîíòàðîâñêèé Ï. Ï.,
Ïðîòàñîâà Ò. Â.

CALCULATION METHOD FOR TRANSIENT PROCESS IN 3D AXISYMMETRIC CONSTRUCTIONS UNDER IMPULSE LOADING

ÌÅÒÎÄÈÊÀ ÐÎÇÐÀÕÓÍÊÓ ÏÅÐÅÕ²ÄÍÈÕ ÏÐÎÖÅѲ  ÒÐÈÂÈ̲ÐÍÈÕ ÎÑÅÑÈÌÅÒÐÈ×ÍÈÕ ÊÎÍÑÒÐÓÊÖ²ßÕ ÏÐÈ ²ÌÏÓËÜÑÍÎÌÓ ÍÀÂÀÍÒÀÆÅÍͲ

ÌÅÒÎÄÈÊÀ ÐÀÑ×ÅÒÀ ÏÅÐÅÕÎÄÍÛÕ ÏÐÎÖÅÑÑΠ ÒÐÅÕÌÅÐÍÛÕ ÎÑÅÑÈÌÌÅÒÐÈ×ÍÛÕ ÊÎÍÑÒÐÓÊÖÈßÕ ÏÐÈ ÈÌÏÓËÜÑÍÎÌ ÍÀÃÐÓÆÅÍÈÈ

148–151
(4)

Âîðîáüåâ Þ. Ñ.,
Îâ÷àðîâà Í. Þ.,
Êóëàêîâ Ï. Í.,
Êóëèøîâ Ñ. Á.,
Ñêðèöêèé À. Í. 

FORCED VIBRATIONS OF COMPRESSOR STAGES OF GAS TURBINE ENGINE IN THE FLOW

ÂÈÌÓØÅͲ ÊÎËÈÂÀÍÍß ÑÒÓÏÅÍß ÊÎÌÏÐÅÑÎÐÀ ÃÒÄ Â ÏÎÒÎÖ²

ÂÛÍÓÆÄÅÍÍÛÅ ÊÎËÅÁÀÍÈß ÑÒÓÏÅÍÈ ÊÎÌÏÐÅÑÑÎÐÀ ÃÒÄ Â ÏÎÒÎÊÅ

152–155
(4)

Öàãëîâ À. È.,
Íåñòåðåíêî Ñ. Þ.,
Ëîÿí À. Â.

MECHANISMS OF PLASMA ACCELERATION IN HELIÑON PLASMA THRUSTER

ÌÅÕÀͲÇÌÈ ÏÐÈÑÊÎÐÅÍÍß ÏËÀÇÌÈ Ó ÃÅ˲ÊÎÍÍÎÌÓ ÅÐÄ

ÌÅÕÀÍÈÇÌÛ ÓÑÊÎÐÅÍÈß ÏËÀÇÌÛ Â ÃÅËÈÊÎÍÍÎÌ ÝÐÄ

156–159
(4)

Èíôîðìàöèîííûå òåõíîëîãèè

Èãóìåíöåâ Å. À.,
Ïðîêîïåíêî Å. À.

CHARGED GYROSCOPE MOVEMENT MODEL

ÌÎÄÅËÜ ÐÓÕÓ ÇÀÐßÄÆÅÍÎÃΠòÐÎÑÊÎÏÓ

ÌÎÄÅËÜ ÄÂÈÆÅÍÈß ÇÀÐ߯ÅÍÍÎÃÎ ÃÈÐÎÑÊÎÏÀ

160–164
(4)

Ëþá÷åíêî Â. Â.

SYSTEM DATA VISUALIZATION IN AUTOMATED CONTROL SYSTEMS

ÑÈÑÒÅÌÀ ²ÇÓÀ˲ÇÀÖ²¯ ÄÀÍÈÕ Â ÀÂÒÎÌÀÒÈÇÎÂÀÍ²É ÑÈÑÒÅ̲ ÓÏÐÀÂ˲ÍÍß

ÑÈÑÒÅÌÀ ÂÈÇÓÀËÈÇÀÖÈÈ ÄÀÍÍÛÕ Â ÀÂÒÎÌÀÒÈÇÈÐÎÂÀÍÍÛÕ ÑÈÑÒÅÌÀÕ ÓÏÐÀÂËÅÍÈß

165–168
(4)

Ìèðãîðîä Â. Ô.,
Ãâîçäåâà È. Ì.,
Áóðÿ÷åíêî À. Ã.

OPTIMAL CONTROL BY PIECE-LINEAR DYNAMIC SYSTEMS

ÎÏÒÈÌÀËÜÍÅ ÓÏÐÀÂ˲ÍÍß ÊÓÑÎ×ÍÎ-˲ͲÉÍÈÌÈ ÄÈÍÀ̲×ÍÈÌÈ ÑÈÑÒÅÌÀÌÈ

ÎÏÒÈÌÀËÜÍÎÅ ÓÏÐÀÂËÅÍÈÅ ÊÓÑÎ×ÍÎ-ËÈÍÅÉÍÛÌÈ ÄÈÍÀÌÈ×ÅÑÊÈÌÈ ÑÈÑÒÅÌÀÌÈ

169–173
(5)

Òðåòüÿê Â. Â.

POSSIBILITIES AND REALIZATION OF OBJECTIVE APPROACH FOR DECISION OF INVENTION TASKS WITH THE USE OF MODEL RECEPTIONS OF REMOVAL OF CONTRADICTIONS

ÐÎÇÐÎÁÊÀ Ó×ÁÎÂÎÃÎ ÏÐÎÃÐÀÌÍÎÃÎ ÊÎÌÏËÅÊÑÓ ÄËß ÂÈвØÅÍÍß ÂÈÍÀÕ²ÄÍÈÖÜÊÈÕ ÇÀÂÄÀÍÜ ÌÅÒÎÄÎÌ ÁÅÇÏÐÎÒÎÒÈÏÍÎÃÎ ÏÐÎÅÊÒÓÂÀÍÍß Â ÎÁËÀÑÒ² ²ÌÏÓËÜÑÍÈÕ ÒÅÕÍÎËÎòÉ

ÐÀÇÐÀÁÎÒÊÀ Ó×ÅÁÍÎÃÎ ÏÐÎÃÐÀÌÌÍÎÃÎ ÊÎÌÏËÅÊÑÀ ÄËß ÐÅØÅÍÈß ÈÇÎÁÐÅÒÀÒÅËÜÑÊÈÕ ÇÀÄÀ× ÌÅÒÎÄÎÌ ÁÅÑÏÐÎÒÎÒÈÏÍÎÃÎ ÏÐÎÅÊÒÈÐÎÂÀÍÈß Â ÎÁËÀÑÒÈ ÈÌÏÓËÜÑÍÛÕ ÒÅÕÍÎËÎÃÈÉ

174–178
(5)

Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè

Øîñòàê È. Â.,
Äàíîâà Ì. À.

APPROACH TO COMPLEX AUTOMATION NATIONAL FORESIGHT PROJECTS

ϲÄÕ²Ä ÄÎ ÊÎÌÏËÅÊÑÍί ÀÂÒÎÌÀÒÈÇÀÖ²¯ ÍÀÖ²ÎÍÀËÜÍÈÕ ÔÎÐÑÀÉÒ - ÏÐÎÅÊÒ²Â

ÏÎÄÕÎÄ Ê ÊÎÌÏËÅÊÑÍÎÉ ÀÂÒÎÌÀÒÈÇÀÖÈÈ ÍÀÖÈÎÍÀËÜÍÛÕ ÔÎÐÑÀÉÒ-ÏÐÎÅÊÒÎÂ

179–188
(10)

ÀËÔÀÂÈÒÍÛÉ ÓÊÀÇÀÒÅËÜ

189

ÈÍÔÎÐÌÀÖÈÎÍÍÎÅ ÑÎÎÁÙÅÍÈÅ

190

 

 

 

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 (ñì. ïîñòàíîâëåíèå ïðåçèäèóìà ÂÀÊ Óêðàèíû ¹1-05/4 îò 14.10.2009 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 (Ïîëüøà); Google Scholar.