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

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ  ² ÒÅÕÍÎËÎòß. – 2012. – ¹ 8(95). – 258 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2012. – ¹ 8(95). – 258 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2012. – ¹ 8(95). – 258 p.

 

ÑÒÀÒÜè (articleS)

 

Àâòîðû
(ÿçûê
îðèãèíàëà)

Íàçâàíèå ñòàòüè  (article title)

Ñòðàíèöû

(pages)

English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Íèæíèê Ñ.Í.

ON OPTIMAL USE OF CUTTING PROPERTIES GRAINS IN A PLANE GRINDING

ÄÎ ÏÈÒÀÍÍß ÎÏÒÈÌÀËÜÍÎÃÎ ÂÈÊÎÐÈÑÒÀÍÍß Ð²ÇÀËÜÍÈÕ ÂËÀÑÒÈÂÎÑÒÅÉ ÇÅÐÅÍ ïðè ïëîñêîìó øë³ôóâàíí³

Ê ÂÎÏÐÎÑÓ ÎÏÒÈÌÀËÜÍÎÃÎ ÈÑÏÎËÜÇÎÂÀÍÈß ÐÅÆÓÙÈÕ ÑÂÎÉÑÒÂ ÇÅÐÅÍ ÏÐÈ ÏËÎÑÊÎÌ ØËÈÔÎÂÀÍÈÈ

7–10
(4)

Ñîðîêèí Â.Ô.,
Êîìáàðîâ Â.Â.

COMPARISON OF KINEMATICAL PARAMETERS OF MOVEMENT AT path MODELING of HIGH-SPEED CNC processing WITH cubic AND quintic SPLINES

ÏÎвÂÍßÍÍß Ê²ÍÅÌÀÒÈ×ÍÈÕ ÏÀÐÀÌÅÒв ÐÓÕÓ ÏÐÈ ÌÎÄÅËÞÂÀÍͲ ÒÐÀªÊÒÎв¯ ÂÈÑÎÊÎØÂÈÄʲÑÍί ×ÏÊ ÎÁÐÎÁÊÈ ÑÏËÀÉÍÀÌÈ ÒÐÅÒÜÎÃÎ òà Ï'ßÒÎÃÎ ÑÒÓÏÅÍß

ÑÐÀÂÍÅÍÈÅ ÊÈÍÅÌÀÒÈ×ÅÑÊÈÕ ÏÀÐÀÌÅÒÐΠÄÂÈÆÅÍÈß ÏÐÈ ÌÎÄÅËÈÐÎÂÀÍÈÈ ÒÐÀÅÊÒÎÐÈÉ ÂÛÑÎÊÎÑÊÎÐÎÑÒÍÎÉ ×ÏÓ ÎÁÐÀÁÎÒÊÈ ÑÏËÀÉÍÀÌÈ ÒÐÅÒÜÅÉ È ÏßÒÎÉ ÑÒÅÏÅÍÅÉ

11–17
(7)

Ïëàíêîâñêèé Ñ.È.,
Øèïóëü Î.Â.,
Êîçëîâ Â.Ã.,
Áîðèñîâà Î.Ñ.

TASKS OF FINISHING FLUID TRACT COMPONENTS OF PERSPECTIVE HYDRAULIC SYSTEMS

ÇÀÄÀײ ԲͲØÍί ÎÁÐÎÁÊÈ ÄÅÒÀËÅÉ Ð²ÄÈÍÍÎÃÎ ÒÐÀÊÒÓ ÏÅÐÑÏÅÊÒÈÂÍÈÕ À²ÀÖ²ÉÍÈÕ Ã²ÄÐÀÂ˲×ÍÈÕ ÑÈÑÒÅÌ

ÇÀÄÀ×È ÔÈÍÈØÍÎÉ ÎÁÐÀÁÎÒÊÈ ÄÅÒÀËÅÉ ÆÈÄÊÎÑÒÍÎÃÎ ÒÐÀÊÒÀ ÏÅÐÑÏÅÊÒÈÂÍÛÕ ÀÂÈÀÖÈÎÍÍÛÕ ÃÈÄÐÀÂËÈ×ÅÑÊÈÕ ÑÈÑÒÅÌ

18–24
(7)

Ãîðáà÷¸â À.À.

EFFICIENCY OF PLANETARY DEEP GRINDING FLAT AND FLAT SHAPED SURFACE OF AIRCRAFT ENGINE PARTS DIFFICULT TO CUT MATERIALS

ÅÔÅÊÒÈÂͲÑÒÜ ÂÈÊÎÐÈÑÒÀÍÍß ÏËÀÍÅÒÀÐÍÎÃÎ ÃËÈÁÈÍÍÎÃÎ ØË²ÔÓÂÀÍÍß ÏËÎÑÊÈÕ ² ÏËÎÑÊÎ ÔÀÑÎÍÍÈÕ ÏÎÂÅÐÕÎÍÜ ÄÅÒÀËÅÉ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓÍ²Â Ç ÂÀÆÊÎÎÁÐÎÁËÞÂÀÍÈÕ ÌÀÒÅвÀ˲Â

ÝÔÔÅÊÒÈÂÍÎÑÒÜ ÏÐÈÌÅÍÅÍÈß ÏËÀÍÅÒÀÐÍÎÃÎ ÃËÓÁÈÍÍÎÃÎ ØËÈÔÎÂÀÍÈß ÏËÎÑÊÈÕ È ÏËÎÑÊÎ ÔÀÑÎÍÍÛÕ ÏÎÂÅÐÕÍÎÑÒÅÉ ÄÅÒÀËÅÉ ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÈÇ ÒÐÓÄÍÎÎÁÐÀÁÀÒÛÂÀÅÌÛÕ ÌÀÒÅÐÈÀËÎÂ

25–30
(6)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Êðàâ÷åíêî È.Ô.,
ßêîâåíêî À.Â.

METHOD OF SOLUTION ENGINEERING TASK ON LIFE AVIATION ENGINE SMALL SCALE LOW BYPASS RATIO

ÌÅÒÎÄ ÐÎÇÂ'ßÇÀÍÍß ²ÍÆÅÍÅÐÍÎ-ÊÎÍÑÒÐÓÊÒÎÐÑÜÊÎÃÎ ÇÀÂÄÀÍÍß ÄÎÂÅÄÅÍÍß À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲ ÌÀËÎÃÎ ÑÒÓÏÅÍÞ ÄÂÎÊÎÍÒÓÐÍÎÑÒ²

ÌÅÒÎÄ ÐÅØÅÍÈß ÈÍÆÅÍÅÐÍÎ-ÊÎÍÑÒÐÓÊÒÎÐÑÊÎÉ ÇÀÄÀ×È ÄÎÂÎÄÊÈ ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÌÀËÎÉ ÑÒÅÏÅÍÈ ÄÂÓÕÊÎÍÒÓÐÍÎÑÒÈ

31–37
(7)

Ñåðãèåíêî Ð.Â.,
Áèëåêà Á.Ä.,
Êàáêîâ Â.ß.

WAYS TO IMPROVE THE EFFICIENCY OF THE WORKING CYCLE OF HEAT UTILIZED POWER PLANTS WITH LOW-BOILING WORKING MEDIUM

ØËßÕÈ Ï²ÄÂÈÙÅÍÍß ÅÔÅÊÒÈÂÍÎÑÒ² ÐÎÁÎ×ÎÃÎ ÖÈÊËÓ ÅÍÅÐÃÅÒÈ×ÍÈÕ ÒÅÏËÎÓÒÈ˲ÇÓÞ×ÈÕ ÓÑÒÀÍÎÂÎÊ Ç ÍÈÇÜÊÎÊÈÏËß×ÈÌÈ ÐÎÁÎ×ÈÌÈ Ò²ËÀÌÈ

ÏÓÒÈ ÏÎÂÛØÅÍÈß ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÐÀÁÎ×ÅÃÎ ÖÈÊËÀ ÝÍÅÐÃÅÒÈ×ÅÑÊÈÕ ÒÅÏËÎÓÒÈËÈÇÈÐÓÞÙÈÕ ÓÑÒÀÍÎÂÎÊ Ñ ÍÈÇÊÎÊÈÏßÙÈÌÈ ÐÀÁÎ×ÈÌÈ ÒÅËÀÌÈ

38–42
(5)

Òàðàñåíêî Ì.À., Òàðàñåíêî À.È.

partial regimeS of gas-turbine engine with different schemes with intermediate heat exchanger and HRO

÷àñòêîâ³ ðåæèìè ãòä ð³çíèõ ñõåì ñ ïðîì³æíèì òåïëîîáì³ííèêîì ³ ÒÓÊ

×ÀÑÒÈ×ÍÛÅ ÐÅÆÈÌÛ ÃÒÄ ÐÀÇÍÛÕ ÑÕÅÌ Ñ ÏÐÎÌÅÆÓÒÎ×ÍÛÌ ÒÅÏËÎÎÁÌÅÍÍÈÊÎÌ È ÒÓÊ

43–46
(4)

Ñîðîãèí Ô.Ã.,
Áàñîâ Þ.Ô.,
Øàõîâ Þ.Â.,
Ïåòóõîâ È.È.,
Ìèíÿ÷èõèí À.Â.

EFFECTIVENESS ANALYSIS OF THE D-336-2 GTU WITH CYCLIC AIR RECUSATION FOR SPRAY COOLING SYSTEM

ÀÍÀË²Ç ÅÔÅÊÒÈÂÍÎÑÒ² ÃÒÏ Ä-336-2 Ç Â²ÄÁÎÐÎÌ ÏβÒÐß ÄËß ÐÎÇÏÈËÞÂÀËÜÍί ÑÈÑÒÅÌÈ ÎÕÎËÎÄÆÅÍÍß

ÀÍÀËÈÇ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÃÒÏ Ä-336-2 Ñ ÎÒÁÎÐÎÌ ÂÎÇÄÓÕÀ ÄËß ÐÀÑÏÛËÈÒÅËÜÍÎÉ ÑÈÑÒÅÌÛ ÎÕËÀÆÄÅÍÈß

47–51
(5)

Áóãàåíêî Î.Ì.

ÑALCULATION OF THE RANGE OF MULTIPHASE FLOW AND SIZE oF OIL SPILL COVERING by USING TRAJECTORY APPROACH 

ÐÎÇÐÀÕÓÍÎÊ  ÄÀËÅÊÎÁ²ÉÍÎÑÒ² ÁÀÃÀÒÎÔÀÇÎÂÎÃÎ ÏÎÒÎÊÓ ÒÀ ÐÎÇ̲ÐÓ ÏËßÌÈ ÏÎÊÐÈÒÒß ÍÀÔÒÎÇÀÁÐÓÄÍÅÍÈÕ Ä²ËßÍÎÊ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÒÐÀÅÊÒÎÐÍÎÃΠϲÄÕÎÄÓ

ÐÀÑ×ÅÒ ÄÀËÜÍÎÁÎÉÍÎÑÒÈ ÌÍÎÃÎÔÀÇÍÎÃÎ ÏÎÒÎÊÀ È ÐÀÇÌÅÐÀ ÏßÒÍÀ ÏÎÊÐÛÒÈß ÍÅÔÒÅÇÀÃÐßÇÍÅÍÍÛÕ Ó×ÀÑÒÊÎÂ Ñ ÈÑÏÎËÜÇÎÂÀÍÈÅÌ ÒÐÀÅÊÒÎÐÍÎÃÎ ÏÎÄÕÎÄÀ

52–55
(4)

Åðøîâ Ñ.Â.,
Êîçûðåö Ä.À.

DEVELOPMENT OF SOFTWARE SYSTEM FOR COMPUTATIONS OF 3D VISCOUS COMPRESSIBLE FLOW IN TURBOMACHINERY BLADE ROWS

âäîñêîíàëåííÿ ÌÅÒÎÄÓ ÐÎÇÐÀÕÓÍÊÓ ÒÅ×²É â’ÿçêîãî ãàçó Ó Êîìïðåñîðíèõ ðåø³òêàõ

ÓÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈÅ ÌÅÒÎÄÀ ÐÀÑ×ÅÒÀ ÒÅ×ÅÍÈÉ ÂßÇÊÎÃÎ ÃÀÇÀ  ÊÎÌÏÐÅÑÑÎÐÍÛÕ ÐÅØÅÒÊÀÕ

56–60
(5)

Ãåðàñèìåíêî Â.Ï.,
Øåëêîâñêèé Ì.Þ.

COMPUTATIONAL AND EXPERIMENTAL STUDY OF COMPRESSOR VANES GASDYNAMIC CHARACTERISTICS IN MULTISTAGE COMPRESSOR

ÐÎÇÐÀÕÓÍÊÎÂÎ-ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ ÄÎÑË²ÄÆÅÍÍß ÃÀÇÎÄÈÍÀ̲×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÊÎÌÏÐÅÑÎÐÍÈÕ ÐÅØ²ÒÎÊ Ó ÑÈÑÒÅ̲ ÁÀÃÀÒÎÑÒÓÏÅÍÅÂÎÃÎ ÊÎÌÏÐÅÑÎÐÀ

ÐÀÑ×ÅÒÍÎ-ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÅ ÈÑÑËÅÄÎÂÀÍÈÅ ÃÀÇÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÊÎÌÏÐÅÑÑÎÐÍÛÕ ÐÅØÅÒÎÊ Â ÑÈÑÒÅÌÅ ÌÍÎÃÎÑÒÓÏÅÍ×ÀÒÎÃÎ ÊÎÌÏÐÅÑÑÎÐÀ

61–66
(6)

Ðóñàíîâ À.Â.,
Ìîèñååâ Ñ.Â.,
Ñóõîðåáðûé Ï.Í.,
Êîñüÿíîâà À.È.,
Ðóñàíîâ Ð.À.

DESIGN METHOD OF HIGH-PERFORMANCE SETTINGS FOR TURBINE EXPANSION ENGINE

ÌÅÒÎÄ ÏÐÎÅÊÒÓÂÀÍÍß ÂÈÑÎÊÎÅÔÅÊÒÈÂÍÈÕ ÏÐÎÒÎ×ÍÈÕ ×ÀÑÒÈÍ ÒÓÐÁÎÄÅÒÀÍÄÅÐÍÈÕ ÀÃÐÅÃÀÒ²Â

ÌÅÒÎÄ ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÂÛÑÎÊÎÝÔÔÅÊÒÈÂÍÛÕ ÏÐÎÒÎ×ÍÛÕ ×ÀÑÒÅÉ ÒÓÐÁÎÄÅÒÀÍÄÅÐÍÛÕ ÀÃÐÅÃÀÒÎÂ

67–72
(6)

Äîëìàòîâ Ä.À.,
Êóêóðóäçà À.Â.,
Õàäæèâàíä Ì.

 

CHEMICAL KINETIC OF THE EXCITING PARTICLE REACTIONS IN THE DOMAIN WITH LOW IONIZATION

ղ̲×ÍÀ ʲÍÅÒÈÊÀ ÐÅÀÊÖ²É ÇÁÓÄÆÅÍÈÕ ×ÀÑÒÎÊ ÏÐÈ ÑËÀÁÊ²É ²ÎͲÇÀÖ²¯ ÑÅÐÅÄÎÂÈÙÀ

ÕÈÌÈ×ÅÑÊÀß ÊÈÍÅÒÈÊÀ ÐÅÀÊÖÈÉ ÂÎÇÁÓÆÄÅÍÍÛÕ ×ÀÑÒÈÖ ÏÐÈ ÑËÀÁÎÉ ÈÎÍÈÇÀÖÈÈ ÑÐÅÄÛ

73–78
(6)

Êîñòþê Â.Å.,
Êèðèëàø Å.È.,
Ñòàñþê À.Â.,
Øåèí Â.Â.,
Êàðçîâ Ä.Â.

COMPUTATION OF THE EXIT GAS TEMPERATURE FIELD OF THEFULL-SIZE gas turbine COMBUSTOR AND ITS ONE-BURNER SECTOR

ÐÎÇÐÀÕÓÍÎÊ ÏÎËß ÒÅÌÏÅÐÀÒÓÐÈ ÃÀÇÓ ÍÀ ÂÈÕÎIJ ÏÎÂÍÎÐÎÇ̲ÐÍί ÊÀÌÅÐÈ ÇÃÎÐßÍÍß ÃÒÄ ÒÀ ¯¯ ÎÄÍÎÏÀËÜÍÈÊÎÂÎÃÎ ÑÅÊÒÎÐÀ

ÐÀÑ×¨Ò ÏÎËß ÒÅÌÏÅÐÀÒÓÐÛ ÃÀÇÀ ÍÀ ÂÛÕÎÄÅ ÏÎËÍÎÐÀÇÌÅÐÍÎÉ ÊÀÌÅÐÛ ÑÃÎÐÀÍÈß ÃÒÄ È Å¨ ÎÄÍÎÃÎÐÅËÎ×ÍÎÃÎ ÑÅÊÒÎÐÀ

79–85
(7)

Ðóáëåâñêèé Þ.Â.

BRUSH SEALS  THE EFECTIVE REMEDY OF IMPROVEMENT OF PARAMETERS AVIATION GTE AND STATIONARY POWERHOUSES

Ù²ÒÊβ ÓÙ²ËÜÍÅÍÍß – ÅÔÅÊÒÈÂÍÈÉ  ÇÀѲÁ ÏÎË²ÏØÅÍÍß ÏÀÐÀÌÅÒв  À²ÀÖ²ÉÍÈÕ ÃÒÄ  ² ÑÒÀÖ²ÎÍÀÐÍÈÕ ÅÍÅÐÃÎÓÑÒÀÍÎÂÎÊ

ÙÅÒÎ×ÍÛÅ ÓÏËÎÒÍÅÍÈß – ÝÔÔÅÊÒÈÂÍÎÅ ÑÐÅÄÑÒÂÎ ÓËÓרÅÍÈß ÏÀÐÀÌÅÒÐΠÀÂÈÀÖÈÎÍÍÛÕ ÃÒÄ  È ÑÒÀÖÈÎÍÀÐÍÛÕ ÝÍÅÐÃÎÓÑÒÀÍÎÂÎÊ

86–89
(4)

Âèíîãðàäîâ À.Ñ.,
×àëêèí À.Ñ.,
Øàêèðîâ Ä.Ô.

A CALCULATION OF DYNAMIC DESCRIPTIONS OF frontal gas-dynamic retainer IS IN SUPPORT OF AVIATION ENGINE

ÐÎÇÐÀÕÓÍÎÊ ÄÈÍÀ̲×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÒÎÐÖÅÂÎÃÎ ÃÀÇÎÄÈÍÀ̲×ÍÎÃÎ ÓÙ²ËÜÍÅÍÍß Â ÎÏÎв À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ

ÐÀÑ×ÅÒ ÄÈÍÀÌÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÒÎÐÖÎÂÎÃÎ ÃÀÇÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÓÏËÎÒÍÅÍÈß Â ÎÏÎÐÅ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß

90–93
(4)

Íàçèí Â.È.

RADIAL HYDROSTATICAL BEARING OF ENHANCEABLE BEARING STRENGTH

ÐÀIJÀËÜÍÈÉ Ã²ÄÐÎÑÒÀÒÈ×ÍÈÉ Ï²ÄØÈÏÍÈÊ Ï²ÄÂÈÙÅÍί ÍÅÑÓ×ί ÇÄÀÒÍÎÑÒ²

ÐÀÄÈÀËÜÍÛÉ ÃÈÄÐÎÑÒÀÒÈ×ÅÑÊÈÉ ÏÎÄØÈÏÍÈÊ ÏÎÂÛØÅÍÍÎÉ ÍÅÑÓÙÅÉ ÑÏÎÑÎÁÍÎÑÒÈ

94–100
(7)

Ñàëîâ Í.Í.,
Õàð÷åíêî À.À.,
Áóáåíöîâ Â.Ì.,
Òêà÷ Å.Ñ.

CALCULATION OF NONSTATIONARY THERMAL CONDITION OF AIRCRAFT  ENGINE AXIAL COMPRESSORS ROTOR DISCS

ÐÎÇÐÀÕÓÍÎÊ ÍÅÑÒÀÖ²ÎÍÀÐÍÎÃÎ ÒÅÏËÎÂÎÃÎ ÑÒÀÍÓ ÄÈÑʲ ÐÎÒÎв ÎÑÜÎÂÈÕ ÊÎÌÏÐÅÑÎв À²ÀÄÂÈÃÓͲÂ

ÐÀÑ×ÅÒ ÍÅÑÒÀÖÈÎÍÀÐÍÎÃÎ ÒÅÏËÎÂÎÃÎ ÑÎÑÒÎßÍÈß ÄÈÑÊΠÐÎÒÎÐΠÎÑÅÂÛÕ ÊÎÌÏÐÅÑÑÎÐΠÀÂÈÀÄÂÈÃÀÒÅËÅÉ

101–103
(3)

Àë¸õèíà Ñ.Â.,
Ãîëîùàïîâ Â.Í.,
Êîòóëüñêàÿ Î.Â.

THE HEAT TRANSFER ON SURFACES OF THE INLET AND OUTLET ELEMENTS OF STEAM TURBINE CASES

ÒÅÏËβÄÄÀ×À ÍÀ ÏÎÂÅÐÕÍßÕ ÂÕ²ÄÍÈÕ ÒÀ ÂÈÕ²ÄÍÈÕ ÊÎÐÏÓÑÍÈÕ ÅËÅÌÅÍҲ ÏÀÐÎÂÈÕ ÒÓÐÁ²Í

ÒÅÏËÎÎÒÄÀ×À ÍÀ ÏÎÂÅÐÕÍÎÑÒßÕ ÂÕÎÄÍÛÕ È ÂÛÕÎÄÍÛÕ ÊÎÐÏÓÑÍÛÕ ÝËÅÌÅÍÒΠÏÀÐÎÂÛÕ ÒÓÐÁÈÍ

104–108
(5)

Èñàåâ Ê.Á.,
Êðóêîâñêèé Ï.Ã.

INFLUENCE OF SOME FACTORS ON THE DETERMINATION OF THERMAL CONDUCTIVITY OF COATINGS

ÂÏËÈ ÄÅßÊÈÕ ÔÀÊÒÎв ÍÀ ÂÈÇÍÀ×ÅÍÍß ÒÅÏËÎÏÐβÄÍÎÑÒ² ÏÎÊÐÈÒÒ²Â

ÂËÈßÍÈÅ ÍÅÊÎÒÎÐÛÕ ÔÀÊÒÎÐΠÍÀ ÎÏÐÅÄÅËÅÍÈÅ ÒÅÏËÎÏÐÎÂÎÄÍÎÑÒÈ ÏÎÊÐÛÒÈÉ

109–113
(5)

Ãðóáîé À.Ï.,
Ãàêàë Ï.Ã.,
Òðåòüÿê À.Â.

DETERMINING OF THERMAL CONDITION OF THE OVERHANG STATOR WINDING BARS OF TURBOGENERATORS OF HIGH ANND AVERAGE POWER

ÂÈÇÍÀ×ÅÍÍß ÒÅÐÌÎÍÀÏÐÓÆÅÍÎÃÎ ÑÒÀÍÓ ËÎÁÎÂί ×ÀÑÒÈÍÈ ÑÒÐÈÆÍ²Â ÎÁÌÎÒÊÈ ÒÓÐÁÎÃÅÍÅÐÀÒÎв ÂÅËÈÊί ÒÀ ÑÅÐÅÄÍÜί ÏÎÒÓÆÍÎÑÒ²

ÎÏÐÅÄÅËÅÍÈÅ ÒÅÏËÎÂÎÃÎ ÑÎÑÒÎßÍÈß ËÎÁÎÂÛÕ ×ÀÑÒÅÉ ÑÒÅÐÆÍÅÉ ÎÁÌÎÒÊÈ ÒÓÐÁÎÃÅÍÅÐÀÒÎÐΠÁÎËÜØÎÉ È ÑÐÅÄÍÅÉ ÌÎÙÍÎÑÒÈ

114–118
(5)

Ãðèãîðüåâ Î.Í.,
Ôðîëîâ Ã.À.,
Åâäîêèìåíêî Þ.È.,
Êèñåëü Â.Ì.,

Ïàíàñþê À.Ä.,
Ìåëàõ Ë.Ì.,
Êîòåíêî Â.À.,
Êîðîòååâ À.Â.

Ultra high temperature ceramics For aerospace technics

Óëüòðàâèñîêîòåìïåðàòóðíà êåðàì³êà äëÿ À²ÀÖ²ÉÍÎ-ÊÎÑ̲×Íί òåõí³êè

ÓËÜÒÐÀÂÛÑÎÊÎÒÅÌÏÅÐÀÒÓÐÍÀß ÊÅÐÀÌÈÊÀ ÄËß ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÎÉ ÒÅÕÍÈÊÈ

119–128
(10)

Ãîëóá Â.Ï.,
Ïåëûõ Â.Í.,
Ïîãðåáíÿê À.Ä.

ON THE PROBLEM OF THE FATIGUE LIFE-TIME CALCULATION OF PRISMATIC RODS UNDER  ASYMMETRIC BENDING AND TORSION

ÄΠ ÇÀÄÀײ ÐÎÇÐÀÕÓÍÊÓ  ÄÎÂÃβ×ÍÎÑÒ²  ÏÐÈÇÌÀÒÈ×ÍÈÕ  ÑÒÅÐÆÍ²Â  ÂÍÀÑ˲ÄÎÊ ÂÒÎÌÈ  ÇÀ  ÓÌΠ ÀÑÈÌÅÒÐÈ×ÍÎÃÎ ÇÃÈÍÓ ÒÀ ÑÊÐÓ×ÅÍÍß

Ê ÇÀÄÀ×Å ÐÀÑ×ÅÒÀ ÓÑÒÀËÎÑÒÍÎÉ ÄÎËÃÎÂÅ×ÍÎÑÒÈ ÏÐÈÇÌÀÒÈ×ÅÑÊÈÕ ÑÒÅÐÆÍÅÉ ÏÐÈ ÀÑÈÌÌÅÒÐÈ×ÍÎÌ ÈÇÃÈÁÅ È ÊÐÓ×ÅÍÈÈ

129–134
(6)

Ôåðíàòè Ï.Â.,
Ïàâëþê ß.Â.,
Ðàãóëèíà Â.Ñ.

ABOUT ONE METHOD OF DETERMINATION OF PARAMETERS OF CREEP AND RELAXATION KERNELS

Ïðî îäèí ìåòîä âèçíà÷åííÿ ïàðàìåòð³â ÿäåð ïîâçó÷îñò³ òà ðåëàêñàö³¿

ÎÁ ÎÄÍÎÌ ÌÅÒÎÄÅ ÎÏÐÅÄÅËÅÍÈß ÏÀÐÀÌÅÒÐΠßÄÅÐ ÏÎËÇÓ×ÅÑÒÈ È ÐÅËÀÊÑÀÖÈÈ

135–140
(6)

Ñíåæíîé Ã.Â.

ROLE OF MAGNETIC AUSTENITE IN THE FORMATION OF CORROSION RESISTANCE OF austenitic chromium-nickel STEELS

Ðîëü ìàãí²òíîãî ñÒÀÍÓ àóñòåí²òÓ â ôîðìÓÂÀÍͲ êîðîç²ÉÍί ñò²éêîñò² àóñòåí²òíÈõ õðîìîí²êåëåâÈõ ÊÐÈÖÜ

ÐÎËÜ ÌÀÃÍÈÒÍÎÃÎ ÑÎÑÒÎßÍÈß ÀÓÑÒÅÍÈÒÀ  ÔÎÐÌÈÐÎÂÀÍÈÈ ÊÎÐÐÎÇÈÎÍÍÎÉ ÑÒÎÉÊÎÑÒÈ ÀÓÑÒÅÍÈÒÍÛÕ ÕÐÎÌÎÍÈÊÅËÅÂÛÕ ÑÒÀËÅÉ

141–144
(4)

Íåæâåäèëîâ À.Þ.

EVALUATION OF THE INFLUENCE OF TEMPERATURE UP TO 640 °C CYCLING STRENGTH

ÎÖ²ÍÊÀ ÂÏËÈÂÓ ÒÅÌÏÅÐÀÒÓÐÈ ÄÎ 640° Ñ ÍÀ ÖÈÊ˲×ÍÓ Ì²ÖͲÑÒÜ

ÎÖÅÍÊÀ ÂËÈßÍÈß ÒÅÌÏÅÐÀÒÓÐÛ ÄÎ 640 °Ñ ÍÀ ÖÈÊËÈ×ÅÑÊÓÞ ÏÐÎ×ÍÎÑÒÜ

145–148
(4)

Áèáëèê È.Â.,
Âàêóëåíêî Ê.Â.,
Êàçàê È.Á.

ESTIMATION OF STEEL 40X DAMAGE DEGREE IN THE CONDITIONS OF MULTICYCLIC FATIGUE

ÎÖ²ÍÊÀ ÑÒÓÏÅÍß ÏÎØÊÎÄÆÓÂÀÍÎÑÒ² ÑÒÀ˲ 40Õ Â ÓÌÎÂÀÕ ÁÀÃÀÒÎÖÈÊËÎÂί ÂÒÎÌÈ

ÎÖÅÍÊÀ ÑÒÅÏÅÍÈ ÏÎÂÐÅÆÄÅÍÍÎÑÒÈ ÑÒÀËÈ 40Õ  Â ÓÑËÎÂÈßÕ ÌÍÎÃÎÖÈÊËÎÂÎÉ ÓÑÒÀËÎÑÒÈ

149–153
(5)

Äîðîøåíêî Å.Þ.,
Èãíàòîâè÷ Ñ.Ð.,
Þöêåâè÷ Ñ.Ñ.

METHOD OF STUDY ON DISTRIBUTION OF RESIDUAL MICROSURFACE LAYER CLAD ALUMINUM DESIGNS

ÌÅÒÎÄÈÊÀ ÄÎÑË²ÄÆÅÍÍß ÐÎÇÏÎIJËÓ ÇÀËÈØÊÎÂÈÕ Ì²ÊÐÎÄÅÔÎÐÌÀÖ²É ÍÀ ÏÎÂÅÐÕͲ ÏËÀÊÎÂÀÍÎÃÎ ØÀÐÓ ÀËÞ̲ͲªÂÈÕ ÇÐÀÇʲÂ

ÌÅÒÎÄÈÊÀ ÈÑÑËÅÄÎÂÀÍÈß ÐÀÑÏÐÅÄÅËÅÍÈß ÎÑÒÀÒÎ×ÍÛÕ ÌÈÊÐÎÄÅÔÎÐÌÀÖÈÉ ÍÀ ÏÎÂÅÐÕÍÎÑÒÈ ÏËÀÊÈÐÎÂÀÍÍÎÃÎ ÑËÎß ÀËÞÌÈÍÈÅÂÛÕ ÎÁÐÀÇÖÎÂ

154–159
(6)

Øóëüæåíêî Í.Ã.,
Ãàðìàø Í.Ã.,
Ãîíòàðîâñêèé Â.Ï.

THE ESTIMATION OF PARTIAL LOAD MODES  EXPLOITATION OF TURBINES ON THE THERMOSTRESSED STATE OF THE HIGH-TEMPERATURE ROTOR

ÎÖ²ÍÊÀ ÙÀÄÍÈÕ ÐÅÆÈ̲ ÅÊÑÏËÓÀÒÀÖ²¯ ÒÓÐÁ²ÍÈ ÏÎ ÒÅÐÌÎÍÀÏÐÓÆÅÍÎÌÓ ÑÒÀÍÓ ÂÈÑÎÊÎÒÅÌÏÅÐÀÒÓÐÍÎÃÎ ÐÎÒÎÐÀ

ÎÖÅÍÊÀ ÙÀÄßÙÈÕ ÐÅÆÈÌΠÝÊÑÏËÓÀÒÀÖÈÈ ÒÓÐÁÈÍÛ ÏÎ ÒÅÐÌÎÍÀÏÐ߯ÅÍÍÎÌÓ ÑÎÑÒÎßÍÈÞ ÂÛÑÎÊÎÒÅÌÏÅÐÀÒÓÐÍÎÃÎ ÐÎÒÎÐÀ

160–164
(5)

Ïîâãîðîäíèé Â.Î.

The digit and analytical solution of invers problem for plate with element’s jf the turbine

ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÎ-ÒÅÎÐÅÒÈ×ÍÅ ÄÎÑË²ÄÆÅÍÍß ÒÅÐÌÎÏÐÓæíîãî ÑÒÀÍÓ ÅËÅÌÅÍҲ ÒÓÐÁ²Í ÂÈÕÎÄß×È Ç Ð²ØÅÍÍß ÇÂÎÐÎÒÍÈÕ ÇÀÄÀ× ÒÅÐÌÎÏÐÓæíîñò³

ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎ-ÒÅÎÐÅÒÈ×ÅÑÊÎÅ ÈÑÑËÅÄÎÂÀÍÈÅ ÒÅÐÌÎÓÏÐÓÃÎÃÎ ÑÎÑÒÎßÍÈß ÝËÅÌÅÍÒΠÒÓÐÁÈÍ ÈÑÕÎÄß ÈÇ ÐÅØÅÍÈß ÎÁÐÀÒÍÛÕ ÇÀÄÀ× ÒÅÐÌÎÓÏÐÓÃÎÑÒÈ

165–168
(4)

Ãóñåâ Þ.À.,
Êàìáèç Êàõðàè,
Ñèìáèðñêèé Ä.Ô.,
Òðèïîëüñêèé Ñ.Ñ.

FILM RESISTIVE-STRAIN SENSOR FOR VIBRATION TESTING OF GTE TURBINE BLADES

Ï˲ÂÊβ ÒÅÍÇÎÐÅÇÈÑÒÎÐÈ ÄËß Â²ÁÐÎÂÈÏÐÎÁÓÂÀÍÍß ËÎÏÀÒÎÊ ÒÓÐÁ²Í ÃÒÄ

ÏËÅÍÎ×ÍÛÉ ÒÅÍÇÎÐÅÇÈÑÒÎÐ ÄËß ÂÈÁÐÎÈÑÏÛÒÀÍÈÉ ËÎÏÀÒÎÊ ÒÓÐÁÈÍ ÃÒÄ

169–172
(4)

Ïðèäîðîæíûé Ð.Ï.,
Øåðåìåòüåâ À.Â.,
Çèíüêîâñêèé À.Ï.

computational research of influence of parameters of perforation holes of high-pressure turbine cooled blade on its stress state and durability

ÏÎвÂÍßËÜÍÈÉ ÀÍÀË²Ç ÍÀÏÐÓÆÅÍÎÃÎ ÑÒÀÍÓ ÎÕÎËÎÄÆÓÂÀÍÈÕ ÐÎÁÎ×ÈÕ ËÎÏÀÒÎÊ ÒÓÐÁ²ÍÈ ÇÀ ÄÎÏÎÌÎÃÎÞ ÐÎÇÐÀÕÓÍÊÎÂÈÕ ÌÎÄÅËÅÉ Ð²ÇÍÎÃΠвÂÍß

ÐÀÑ×ÅÒÍÎÅ ÈÑÑËÅÄÎÂÀÍÈÅ ÂËÈßÍÈß ÏÀÐÀÌÅÒÐΠÏÅÐÔÎÐÀÖÈÎÍÍÛÕ ÎÒÂÅÐÑÒÈÉ ÎÕËÀÆÄÀÅÌÎÉ ÐÀÁÎ×ÅÉ ËÎÏÀÒÊÈ ÒÓÐÁÈÍÛ ÂÛÑÎÊÎÃÎ ÄÀÂËÅÍÈß ÍÀ ÅÅ ÍÀÏÐ߯ÅÍÍÎÅ ÑÎÑÒÎßÍÈÅ È ÄÎËÃÎÂÅ×ÍÎÑÒÜ

173–177
(5)

Ìåäâåäîâñêàÿ Ò.Ô.,
Ðæåâñêàÿ È.Å.,
Ìåäâåäîâñêèé À.Â.,
Ãàí÷èí Å.Â.

ESTIMATION OF DURABILITY AND RESOURCE OF DRIVING WHEEL AND BEARING STRUCTURE OF PUMPING TURBINE OF KIEV HAES HYDRAULIC TURBINE

ÎÖ²ÍÊÀ ̲ÖÍÎÑÒ² É ÐÅÑÓÐÑÓ ÐÎÁÎ×ÎÃÎ ÊÎËÅÑÀ É ÍÅÑÓ×ί ÊÎÍÑÒÐÓÊÖ²¯ ÍÀÑÎÑÍί ÒÓÐÁ²ÍÈ ÊȯÂÑÜÊί ÃÀÅÑ

ÎÖÅÍÊÀ ÏÐÎ×ÍÎÑÒÈ È ÐÅÑÓÐÑÀ ÐÀÁÎ×ÅÃÎ ÊÎËÅÑÀ È ÍÅÑÓÙÅÉ ÊÎÍÑÒÐÓÊÖÈÈ ÍÀÑÎÑÍÎÉ ÒÓÐÁÈÍÛ ÊÈÅÂÑÊÎÉ ÃÀÝÑ

178–183
(6)

Ëàïîòêî Â.Ì.,
Êóõòèí Þ.Ï.,
Ñëûíüêî Ã.È.

METHOD OF NUMERICAL ASSESSMENT OF  TONAL NOISE IN SOURCE AT UNSTATIONARY INTERACTION OF TURBOMACHINARY  RIMS

ÌÅÒÎÄ ×ÈÑÅËÜÍί ÎÖ²ÍÊÈ Ð²ÂÍß ÒÎÍÀËÜÍÎÃÎ ØÓÌÓ Ó ÄÆÅÐÅ˲ ÏÐÈ ÍÅÑÒÀÖ²ÎÍÀÐÍ²É ÂÇÀªÌÎIJ¯ ²Íֲ ÒÓÐÁÎÌÀØÈÍ

ÌÅÒÎÄ ×ÈÑËÅÍÍÎÉ ÎÖÅÍÊÈ ÓÐÎÂÍß ÒÎÍÀËÜÍÎÃÎ ØÓÌÀ  ÈÑÒÎ×ÍÈÊÅ ÏÐÈ ÍÅÑÒÀÖÈÎÍÀÐÍÎÌ ÂÇÀÈÌÎÄÅÉÑÒÂÈÈ ÂÅÍÖΠÒÓÐÁÎÌÀØÈÍ

184–189
(6)

Êóäèí Ì.Ì.,
Áåðåæíîé Â.Þ.

LASER TECHNIQUE OF FAN TIP CLEARANCE AND VIBRATIONS MEASUREMENT

ËÀÇÅÐÍÅ ÂÈ̲ÐÞÂÀÍÍß ÐÀIJÀËÜÍÎÃÎ ÇÀÇÎÐÓ ÒÀ ²ÁÐÀÖ²É ËÎÏÀÒÎÊ ÂÅÍÒÈËßÒÎÐÀ

ËÀÇÅÐÍÎÅ ÈÇÌÅÐÅÍÈÅ ÐÀÄÈÀËÜÍÎÃÎ ÇÀÇÎÐÀ È ÂÈÁÐÀÖÈÉ ËÎÏÀÒÎÊ ÂÅÍÒÈËßÒÎÐÀ

190–193
(4)

Âîðîáüåâ Þ.Ñ.,
×óãàé Ì.À.,
Äüÿêîíåíêî Ê.Þ.,
Êóëèøîâ Ñ.Á.,
Ñêðèöêèé À.Í.

stress LOCALIZATION ANALYSIS on SINGLE-CRYSTAL BLADES VIBRATIONS

ÀÍÀË²Ç ËÎÊÀ˲ÇÀÖ²¯ ÍÀÏÐÓÆÅÍÜ ÏÐÈ ÊÎËÈÂÀÍÍßÕ ÌÎÍÎÊÐÈÑÒÀ˲×ÍÈÕ ËÎÏÀÒÎÊ

ÀÍÀËÈÇ ËÎÊÀËÈÇÀÖÈÈ ÍÀÏÐ߯ÅÍÈÉ ÏÐÈ ÊÎËÅÁÀÍÈßÕ ÌÎÍÎÊÐÈÑÒÀËËÈ×ÅÑÊÈÕ ËÎÏÀÒÎÊ

194–198
(5)

Ìåëüíèê Â.Ì.,
Êàðà÷óí Â.Â.

Diffraction of sound radiation on an impedance ache cover surfaces. The mixed regional problem

ÄÈÔÐÀÊÖ²ß ÇÂÓÊÎÂÎÃÎ ÂÈÏÐÎ̲ÍÞÂÀÍÍß ÍÀ ²ÌÏÅÄÀÍÑÍ²É ÏÎÂÅÐÕͲ ÎÁÎËÎÍÊÈ. Ç̲ØÀÍÀ ÊÐÀÉÎÂÀ ÇÀÄÀ×À

Äèôðàêöèÿ çâóêîâîãî èçëó÷åíèÿ íà èìïåäàíñ íîé ïîâåðõíîñòè îáîëî÷êè. Ñìåøàííàÿ êðàåâàÿ çàäà÷à

199–202
(4)

Òêà÷ Ì.Ð.,
Çîëîòîé Þ.Ã.,
Äîâãàíü Ä.Â.,
Æóê È.Þ.

DEFINITION THE DYNAMIC PARAMETERS OF GTE ELEMENTS IN REAL-TIME BY ELECTRONIC SPECKLE INTERFEROMETRY

ÂÈÇÍÀ×ÅÍÍß Â ÐÅÀËÜÍÎÌÓ ×ÀѲ ÔÎÐÌ ÂËÀÑÍÈÕ ÊÎËÈÂÀÍÜ ÅËÅÌÅÍҲ ÃÒÄ ÌÅÒÎÄÎÌ ÅËÅÊÒÐÎÍÍί ÑÏÅÊË-²ÍÒÅÐÔÅÐÎÌÅÒв¯

ÎÏÐÅÄÅËÅÍÈÅ ÔÎÐÌ ÑÎÁÑÒÂÅÍÍÛÕ ÊÎËÅÁÀÍÈÉ ÝËÅÌÅÍÒÎÂ ÃÒÄ Â ÐÅÀËÜÍÎÌ ÂÐÅÌÅÍÈ ÌÅÒÎÄÎÌ ÝËÅÊÒÐÎÍÍÎÉ ÑÏÅÊË-ÈÍÒÅÐÔÅÐÎÌÅÒÐÈÈ

203–207
(5)

Áîíäàð÷óê Ï.Â.,
Òèñàðåâ À.Þ.

METHOD OF CALCULATION THE RADIAL CLEARANCE BY THE GENERALIZED FLIGHT CYCLE ENGINE

ÌÅÒÎÄÈÊÀ ÐÎÇÐÀÕÓÍÊÓ ÐÀIJÀËÜÍÈÕ ÇÀÇÎв  ÏÎ ÓÇÀÃÀËÜÍÅÍÎÌÓ ÏÎËÜÎÒÍÎÌÓ ÖÈÊËÓ ÄÂÈÃÓÍÀ

ÌÅÒÎÄÈÊÀ ÐÀÑרÒÀ ÐÀÄÈÀËÜÍÛÕ ÇÀÇÎÐΠÏÎ ÎÁÎÁÙ¨ÍÍÎÌÓ ÏÎ˨ÒÍÎÌÓ ÖÈÊËÓ ÄÂÈÃÀÒÅËß

208–211
(4)

Öàãëîâ À.È.,
Ëîÿí À.Â.,
Êîøåëåâ Í.Í.,
Ðûáàëîâ Î.Ï.

TESTING RESULTS OF LOW POWER ELECTRODELESS PLASMA THRUSTER WITH RF IONIZATION OF WORKING MEDIUM

ÐÅÇÓËÜÒÀÒÈ ²ÑÏÈҲ ÁÅÇÅËÅÊÒÐÎÄÍÎÃÎ ÅËÅÊÒÐÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÈÃÓÍÀ ÌÀËί ÏÎÒÓÆÍÎÑÒ² Ç Â× ²ÎͲÇÀÖ²ªÞ ÐÒ

ÐÅÇÓËÜÒÀÒÛ ÈÑÏÛÒÀÍÈÉ ÁÅÇÝËÅÊÒÐÎÄÍÎÃÎ ÝËÅÊÒÐÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÈÃÀÒÅËß ÌÀËÎÉ ÌÎÙÍÎÑÒÈ Ñ Â× ÈÎÍÈÇÀÖÈÅÉ ÐÒ

212–218
(7)

Èíôîðìàöèîííûå òåõíîëîãèè

Áàõòèÿðîâ Ä.Â.,
Ñòåïàíåíêî Ñ.Ì.,
Õàð÷åíêî Â.Ã.

CONTROL OF VARIATIONS IN KEY CHARACTERISTICS OF ASSEMBLY UNITS, PARTS AND PROCESSES

ÓÏÐÀÂ˲ÍÍß Ç̲ÍÀÌÈ ÊËÞ×ÎÂÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÑÊËÀÄÀËÜÍÈÕ ÎÄÈÍÈÖÜ, ÄÅÒÀËÅÉ ² ÏÐÎÖÅѲÂ

ÓÏÐÀÂËÅÍÈÅ ÈÇÌÅÍÅÍÈßÌÈ ÊËÞ×ÅÂÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÑÁÎÐÎ×ÍÛÕ ÅÄÈÍÈÖ, ÄÅÒÀËÅÉ È ÏÐÎÖÅÑÑÎÂ

219–222
(4)

Âîëêîâ Ä.È.,
Ðàí÷åíêî Ã.Ñ.

SOME ASPECTS OF HELICOPTER TWIN-ENGINE CONTROL

ÄÅßʲ ÀÑÏÅÊÒÈ ÓÏÐÀÂ˲ÍÍß ÄÂÎÄÂÈÃÓÍÎÂÎÞ ÑÈËÎÂÎÞ ÓÑÒÀÍÎÂÊÎÞ  ÃÅ˲ÊÎÏÒÅÐÓ

ÍÅÊÎÒÎÐÛÅ ÀÑÏÅÊÒÛ ÓÏÐÀÂËÅÍÈß ÄÂÓÕÄÂÈÃÀÒÅËÜÍÎÉ ÑÈËÎÂÎÉ ÓÑÒÀÍÎÂÊÎÉ ÂÅÐÒÎ˨ÒÀ

223–226
(4)

Ïàí³í Â.Â.,
ªí÷åâ Ñ.Â.,
Òàêó Ñ.Î.

IDENTIFICATION OF AIRCRAFT GTE and its components based on neural networks

²ÄÅÍÒÈÔ²ÊÀÖ²ß À²ÀÖ²ÉÍÎÃÎ ÃÒÄ ² ÉÎÃÎ ÅËÅÌÅÍҲ ÍÀ ÎÑÍβ ÍÅÉÐÎÍÍÈÕ ÌÅÐÅÆ

ÈÄÅÍÒÈÔÈÊÀÖÈß ÀÂÈÀÖÈÎÍÍÎÃÎ ÃÒÄ È ÅÃÎ ÝËÅÌÅÍÒÎÂ ÍÀ ÎÑÍÎÂÅ ÍÅÉÐÎÍÍÛÕ ÑÅÒÅÉ

227–231
(5)

Åïèôàíîâ Ñ.Â.,
Ùåðáàíü Á.À.,
×åðêàñîâ Þ.Â.

EFFECTIVE TREND CRITERIA SELECTION FOR APPLICATION IN PARAMETRIC DIAGNOSTIC ALGORITHM

ÂÈÁ²Ð ÅÔÅÊÒÈÂÍÈÕ ÊÐÈÒÅв¯Â ÒÐÅÍÄÓ ÄËß ÇÀÑÒÎÑÓÂÀÍÍß Â ÀËÃÎÐÈÒ̲ ÏÀÐÀÌÅÒÐÈ×Íί IJÀÃÍÎÑÒÈÊÈ

ÂÛÁÎÐ ÝÔÔÅÊÒÈÂÍÛÕ ÊÐÈÒÅÐÈÅ ÒÐÅÍÄÀ ÄËß ÏÐÈÌÅÍÅÍÈß Â ÀËÃÎÐÈÒÌÀÕ ÏÀÐÀÌÅÒÐÈ×ÅÑÊÎÉ ÄÈÀÃÍÎÑÒÈÊÈ

232–240
(9)

Ìèðîãîðîä Â.Ô.,
Ãâîçäåâà È.Ì.

MULTIDIMENSIONAL TREND ANALYSIS OF TEMPORARY SERIES IN THE TASKS OF EVALUATION OF TECHNICAL CONDSTION

ÁÀÃÀÒÎÂÈ̲ÐÍÈÉ ÒÐÅÍÄÎÂÈÉ ÀÍÀË²Ç ×ÀÑÎÂÈÕ ÐßIJ  ÇÀÄÀ×ÀÕ ÎÖ²ÍÊÈ ÒÅÕͲ×ÍÎÃÎ ÑÒÀÍÓ

ÌÍÎÃÎÌÅÐÍÛÉ ÒÐÅÍÄÎÂÛÉ ÀÍÀËÈÇ ÂÐÅÌÅÍÍÛÕ  ÐßÄΠ ÇÀÄÀ×ÀÕ ÎÖÅÍÊÈ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÑÎÑÒÎßÍÈß

241–245
(5)

Êóçíåöîâà Þ.À.,
Òóðêèí È.Á.

THE VISUALIZATION OF CONTROLLING ALGORITHM TRACK IN THE SYSTEMS OF AUTOMATION TESTS OF AIRCRAFT ENGINES

²ÇÓÀ˲ÇÀÖ²ß ÒÐÀÑÈ ÊÅÐÓÞ×ÎÃÎ ÀËÃÎÐÈÒÌÓ Â ÑÈÑÒÅÌÀÕ ÀÂÒÎÌÀÒÈÇÀÖ²¯ ÂÈÏÐÎÁÓÂÀÍÜ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲÂ

ÂÈÇÓÀËÈÇÀÖÈß ÒÐÀÑÑÛ ÓÏÐÀÂËßÞÙÅÃÎ ÀËÃÎÐÈÒÌÀ Â ÑÈÑÒÅÌÀÕ ÀÂÒÎÌÀÒÈÇÀÖÈÈ ÈÑÏÛÒÀÍÈÉ ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ

246–252
(7)

Íåâåøêèí Þ.À.,
Îíîï÷åíêî À.Â.,
Òðåòüÿê Â.Â.

MODELING OF PULSE FORMING PROCESSES

ÌÎÄÅËÞÂÀÍÍß ÏÐÎÖÅѲ ²ÌÏÓËÜÑÍÎÃÎ ÎÁ’ªÌÍÎÃÎ ØÒÀÌÏÓÂÀÍÍß

ÌÎÄÅËÈÐÎÂÀÍÈÅ ÏÐÎÖÅÑÑÎÂ ÈÌÏÓËÜÑÍÎÉ ÎÁÚÅÌÍÎÉ ØÒÀÌÏÎÂÊÈ

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Óâàæàåìûå ÷èòàòåëè!

Íàó÷íî-òåõíè÷åñêèé æóðíàë “ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß
 âêëþ÷åí â ïåðå÷åíü íàó÷íûõ èçäàíèé, â êîòîðûõ ìîãóò ïóáëèêîâàòüñÿ îñíîâíûå ðåçóëüòàòû äèññåðòàöèîííûõ ðàáîò (ñì. ïîñòàíîâëåíèå ïðåçèäèóìà ÂÀÊ Óêðàèíû ¹1-05/4 îò 14.10.2009ã)

 

Ðåôåðàòèâíàÿ èíôîðìàöèÿ ñîõðàíÿåòñÿ:

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

– 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).