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

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2014. – ¹ 9 (116). – 188 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2014. – ¹ 9 (116). – 188 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2014. – ¹ 9 (116). – 188 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

Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Øóëüæåíêî Í. Ã.,
Çàéöåâ Á. Ô.,
Àñàåíîê À. Â.

Numerical simulation of dynamic response of structure under impulse impact

×ÈÑÅËÜÍÅ ÌÎÄÅËÞÂÀÍÍß ÄÈÍÀ̲×Íί ÐÅÀÊÖ²¯ ÊÎÍÑÒÐÓÊÖ²É ÍÀ ²ÌÏÓËÜÑÍÈÉ ÂÏËÈÂ

×ÈÑËÅÍÍÎÅ ÌÎÄÅËÈÐÎÂÀÍÈÅ ÄÈÍÀÌÈ×ÅÑÊÎÉ ÐÅÀÊÖÈÈ ÊÎÍÑÒÐÓÊÖÈÉ ÍÀ ÈÌÏÓËÜÑÍÎÅ ÂÎÇÄÅÉÑÒÂÈÅ

6–11
(6)

Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ

Òåðåøèí À. Ì.,
×åâàãèí À. Ô.

RESEARCHES AIR INLETS OF HIGH-SPEED RAMJET

ÄÎÑË²ÄÆÅÍÍß ÏβÒÐÎÇÀÁ²ÐÍÈÕ ÏÐÈÑÒÐί ÂÈÑÎÊÎØÂÈÄʲÑÍÈÕ ÏÏÐÄ

ÈÑÑËÅÄÎÂÀÍÈß ÂÎÇÄÓÕÎÇÀÁÎÐÍÛÕ ÓÑÒÐÎÉÑÒÂ ÂÛÑÎÊÎÑÊÎÐÎÑÒÍÛÕ ÏÂÐÄ

12–16
(5)

Ãðåöêîâ À. È.,
Ãðèãîðüåâ Â. À.,
Çàãðåáåëüíûé À. Î.,
Ðàäüêî Â. Ì.

AERODYNAMIC CHARACTERISTICS ESTIMATION OF HELICOPTER IN THE PROBLEM OF SELECTION PARAMETER VALUES OF WORK GAS TURBINE ENGINE WITH A FREE TURBINE

ÄÎ ÎÖ²ÍÊÈ ÀÅÐÎÄÈÍÀÌI×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÂÅÐÒÎËÜÎÒÀ  ÇÀÄÀײ ÂÈÁÎÐÓ ÇÍÀ×ÅÍÜ ÏÀÐÀÌÅÒв ÐÎÁÎ×ÎÃÎ ÏÐÎÖÅÑÓ ÃÒÄ ÂÒ

Ê ÎÖÅÍÊÅ ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÂÅÐÒÎËÅÒÀ  ÇÀÄÀ×Å ÂÛÁÎÐÀ ÇÍÀ×ÅÍÈÉ ÏÀÐÀÌÅÒÐΠÐÀÁÎ×ÅÃÎ ÏÐÎÖÅÑÑÀ ÃÒÄ ÑÒ

17–20
(4)

Êóõòèí Þ. Ï.,
Ëàïîòêî Â. Ì.,
Åëàíñêèé À. Â.

CONJUGATED NUMERICAL MODELING OF INTERNAL AND EXTERNAL AERODYNAMICS OF ENGINE-AIRFRAME SYSTEM

CÏÐ߯ÅÍÅ ÷èñÅËÜÍÅ ìîäåëþâàííÿ ÂÍÓÒвØÍÜο ² ÇÎÂͲØÍÜί àåðîäèíàì³êè ÑÈÑÒÅÌÈ ÄÂÈÃÓÍ - ÊÎÐÏÓÑ Ë²ÒÀËÜÍÎÃÎ ÀÏÀÐÀÒÓ

CÎÏÐ߯ÅÍÍÎÅ ×ÈÑËÅÍÍÎÅ ÌÎÄÅËÈÐÎÂÀÍÈÅ ÂÍÓÒÐÅÍÍÅÉ È ÂÍÅØÍÅÉ ÀÝÐÎÄÈÍÀÌÈÊÈ ÑÈÑÒÅÌÛ ÄÂÈÃÀÒÅËÜ – ÊÎÐÏÓÑ ËÅÒÀÒÅËÜÍÎÃÎ ÀÏÏÀÐÀÒÀ

21–26
(6)

Øåëêîâñêèé Ì. Þ.

AERODYNAMIC IMPROVEMENT OF AXIAL TEN-STAGE COMPRESSOR OF STATIONARY GTE

ÀÅÐÎÄÈÍÀ̲×ÍÅ ÂÄÎÑÊÎÍÀËÅÍÍß ÎÑÜÎÂÎÃÎ ÄÅÑßÒÈÑÒÓϲÍ×ÀÒÎÃÎ ÊÎÌÏÐÅÑÎÐÀ ÑÒÀÖ²ÎÍÀÐÍÎÃÎ ÃÒÄ

ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÎÅ ÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈÅ ÎÑÅÂÎÃÎ ÄÅÑßÒÈÑÒÓÏÅÍ×ÀÒÎÃÎ ÊÎÌÏÐÅÑÑÎÐÀ ÑÒÀÖÈÎÍÀÐÍÎÃÎ ÃÒÄ

27–32
(6)

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

THE INTERACTION OF POOR FLAMES WITH DIFFERENT TEMPERATURES

ÂÇÀªÌÎÄ²ß Á²ÄÍÈÕ ÃÅÒÅÐÎÃÅÍÍÈÕ ÏÎËÓÌ’¯Â Ç Ð²ÇÍÎÞ ÒÅÌÏÅÐÀÒÓÐÎÞ

ÂÇÀÈÌÎÄÅÉÑÒÂÈÅ ÁÅÄÍÛÕ ÃÅÒÅÐÎÃÅÍÍÛÕ ÏËÀÌÅÍ Ñ ÐÀÇËÈ×ÍÎÉ ÒÅÌÏÅÐÀÒÓÐÎÉ

33–38
(6)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

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

EFFICIENCY OF HEAT RECOVERY BY METAL-HYDRIDE INSTALLATION OF CONTINUOUS OPERATION

ÅÔÅÊÒÈÂͲÑÒÜ ÓÒÈ˲ÇÀÖ²¯ ÒÅÏËÀ ÌÅÒÀËÎòÄÐÈÄÍί ÓÑÒÀÍÎÂÊÈ ÁÅÇÏÅÐÅÐÂÍί IJ¯

ÝÔÔÅÊÒÈÂÍÎÑÒÜ ÓÒÈËÈÇÀÖÈÈ ÍÈÇÊÎÏÎÒÅÍÖÈÀËÜÍÎÃÎ ÒÅÏËÀ ÌÅÒÀËËÎÃÈÄÐÈÄÍÛÌÈ ÓÑÒÀÍÎÂÊÀÌÈ ÍÅÏÐÅÐÛÂÍÎÃÎ ÄÅÉÑÒÂÈß

39–44
(6)

Áåëîóñîâ Å. Â.

WASTE SEPARATION FUEL USING ENERGY BALANCE SHIP POWER PLANTS

ÂÈÊÎÐÈÑÒÀÍÍß Â²ÄÕÎIJ ÑÅÏÀÐÀÖ²¯ ÏÀËÈÂÀ  ÏÀËÈÂÍÎÌÓ ÁÀËÀÍѲ ÑÓÄÍÎÂί ÅÍÅÐÃÅÒÈ×Íί ÓÑÒÀÍÎÂÊÈ

ÈÑÏÎËÜÇÎÂÀÍÈÅ ÎÒÕÎÄΠÑÅÏÀÐÀÖÈÈ ÒÎÏËÈÂÀ  ÒÎÏËÈÂÍÎÌ ÁÀËÀÍÑÅ ÑÓÄÎÂÎÉ ÝÍÅÐÃÅÒÈ×ÅÑÊÎÉ ÓÑÒÀÍÎÂÊÈ

45–49
(5)

Ëèñèöà À. Þ.,
Íåì÷åíêî Ä. À.,
Ïåòóõîâ È. È.,
Ñîðîãèí Ô. Ã.

ON EFFICIENCY OF INDIRECT EVAPORATIVE COOLING FOR GTU CYCLIC AIR

ÄÎ ÏÈÒÀÍÍß ªÔÅÊÒÈÂÍÎÑÒ² ÍÅÏÐßÌÎÃÎ ÂÈÏÀÐÍÎÃÎ ÎÕÎËÎÄÆÅÍÍß ÖÈÊËÎÂÎÃÎ ÏβÒÐß ÃÒÏ

Ê ÂÎÏÐÎÑÓ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÊÎÑÂÅÍÍÎ-ÈÑÏÀÐÈÒÅËÜÍÎÃÎ ÎÕËÀÆÄÅÍÈß ÖÈÊËÎÂÎÃÎ ÂÎÇÄÓÕÀ ÃÒÏ

50–55
(6)

Ìàìåäîâ Á. Ø.

ÒÍÅ SINGLE THEORY OF CONTINUOS FLOW PROPULSION. THE REASONS OF TURBO-JET UNSTEADY WORK GENERATION WHILE TAKE OFF IN CONDITIONS OF HOT CLIMATE

ªÄÈÍÀ ÒÅÎÐ²ß ÐÓØ²¯Â. ÏÐÈ×ÈÍÈ ÃÅÍÅÐÓÂÀÍÍß ÍÅÑÒ²ÉÊί ÐÎÁÎÒÈ ÒÓÐÁÎÐÅÀÊÒÈÂÍÈÕ ÄÂÈÃÓͲ ÏÐÈ ÇËÜÎÒ²  ÓÌÎÂÀÕ ÑÏÅÊÎÒÍÎÃÎ Ê˲ÌÀÒÓ

ÅÄÈÍÀß ÒÅÎÐÈß ÄÂÈÆÈÒÅËÅÉ. ÏÐÈ×ÈÍÛ ÃÅÍÅÐÈÐÎÂÀÍÈß ÍÅÓÑÒÎÉ×ÈÂÎÉ ÐÀÁÎÒÛ ÒÓÐÁÎÐÅÀÊÒÈÂÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÏÐÈ ÂÇËÅÒÅ Â ÓÑËÎÂÈßÕ ÆÀÐÊÎÃÎ ÊËÈÌÀÒÀ

56–62
(7)

Øêàáóðà Â. À.

RESULTS OF ANALYSIS OF TURBINE ZONE AND COMPRESSOR ZONE OF TURBO-COMPRESSOR WITH GENERAL IMPELLER FOR GAS TURBINE ENGINES

ÐÅÇÓËÜÒÀÒÈ ÄÎÑË²ÄÆÅÍÜ ÒÓÐÁ²ÍÍί ÒÀ ÊÎÌÏÐÅÑÎÐÍί ×ÀÑÒÈÍ ÒÓÐÁÎÊÎÌÏÐÅÑÎÐÀ ²Ç ÑϲËÜÍÈÌ ÐÎÁÎ×ÈÌ ÊÎËÅÑÎÌ ÄËß ÇÀÑÒÎÑÓÂÀÍÍß Ó ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓÍÀÕ

ÐÅÇÓËÜÒÀÒÛ ÈÑÑËÅÄÎÂÀÍÈÉ ÒÓÐÁÈÍÍÎÉ È ÊÎÌÏÐÅÑÑÎÐÍÎÉ ×ÀÑÒÅÉ ÒÓÐÁÎÊÎÌÏÐÅÑÑÎÐÀ Ñ ÎÁÙÈÌ ÐÀÁÎ×ÈÌ ÊÎËÅÑÎÌ ÄËß ÏÐÈÌÅÍÅÍÈß Â ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËßÕ

63–67
(5)

Êóëèêîâ Ã. Ã.,
Ïîãîðåëîâ Ã. È.,
Áàäàìøèí Á. È.,
Àáäóëíàãèìîâ À. È.

METHOD OF CONSTRUCTING OF NEURAL NETWORK MODEL OF TWO-SHAFT GAS TURBINE ENGINE UNDER CONDITIONS OF STRUCTURAL ADEQUACY

ÌÅÒÎÄÈÊÀ ÏÎÁÓÄÎÂÈ ÍÅÉÐÎÌÅÐÅÆÅÂί ÌÎÄÅ˲ ÄÂÎÕÂÀËÜÍÎÃÎ ÃÒÄ ²Ç ÂÈÊÎÍÀÍÍßÌ ÓÌΠÑÒÐÓÊÒÓÐÍί ÀÄÅÊÂÀÒÍÎÑÒ²

ÌÅÒÎÄÈÊÀ ÏÎÑÒÐÎÅÍÈß ÍÅÉÐÎÑÅÒÅÂÎÉ ÌÎÄÅËÈ ÄÂÓÕÂÀËÜÍÎÃÎ ÃÒÄ Ñ ÑÎÁËÞÄÅÍÈÅÌ ÓÑËÎÂÈÉ ÑÒÐÓÊÒÓÐÍÎÉ ÀÄÅÊÂÀÒÍÎÑÒÈ

68–73
(6)

Òàðàñåíêî Ì. À.,
Òàðàñåíêî À. È.

COMPARATIVE ANALYSIS OF PARTIAL MODES FOR SINGLE-SHAFT AND MULTI-SHAFT TURBINE ENGINE WITH CHANGING AMBIENT TEMPERATURE

ÏÎвÂÍßËÜÍÈÉ ÀÍÀË²Ç ×ÀÑÒÊÎÂÈÕ ÐÅÆÈ̲ ÎÄÍÎÂÀËÜÍÎÃÎ ÒÀ ÌÍÎÃÎÂÀËÜÍÈÕ ÃÒÄ ÏÐÈ Ç̲Ͳ ÒÅÌÏÅÐÀÒÓÐÈ ÍÀÂÊÎËÈØÍÜÎÃÎ ÏβÒÐß

ÑÐÀÂÍÈÒÅËÜÍÛÉ ÀÍÀËÈÇ ×ÀÑÒÈ×ÍÛÕ ÐÅÆÈÌΠÎÄÍÎÂÀËÜÍÎÃÎ È ÌÍÎÃÎÂÀËÜÍÛÕ ÃÒÄ ÏÐÈ ÈÇÌÅÍÅÍÈÈ ÒÅÌÏÅÐÀÒÓÐÛ ÍÀÐÓÆÍÎÃÎ ÂÎÇÄÓÕÀ

74–79
(6)

Ìèðãîðîä Â. Ô.,
Äàíèëîâ Â. Â.

CALCULABLE REALIZATION OF MATHEMATICAL MODELS OF STATE SPACE IN FORM HAMMERSHTEIN

ÎÁ×ÈÑËÞÂÀËÜÍÀ ÐÅÀ˲ÇÀÖ²ß ÌÀÒÅÌÀÒÈ×ÍÈÕ ÌÎÄÅËÅÉ ÏÐÎÑÒÎÐÓ ÑÒÀÍ²Â Ó ÔÎÐ̲ ÃÀÌÌÅÐØÒÅÉÍÀ

ÂÛ×ÈÑËÈÒÅËÜÍÀß ÐÅÀËÈÇÀÖÈß ÌÀÒÅÌÀÒÈ×ÅÑÊÈÕ ÌÎÄÅËÅÉ ÏÐÎÑÒÐÀÍÑÒÂÀ ÑÎÑÒÎßÍÈÉ Â ÔÎÐÌÅ ÃÀÌÌÅÐØÒÅÉÍÀ

80–85
(6)

Ïàí³í Â. Â.,
ªí÷åâ Ñ. Â.,
Òàêó Ñ. Î.

FORMING OF NEURON-NETWORK MODEL OF HYDRAULIC-MECHANICAL AUTOMATIC CONTROL AVIATION ENGINES SYSTEM

ÔÎÐÌÓÂÀÍÍß ÍÅÉÐÎÌÅÐÅÆÅÂί ÌÎÄÅ˲ òÄÐÎÌÅÕÀͲ×Íί ÑÈÑÒÅÌÈ ÀÂÒÎÌÀÒÈ×ÍÎÃÎ ÊÅÐÓÂÀÍÍß À²ÀÖ²ÉÍÈÌÈ ÄÂÈÃÓÍÀÌÈ

ÔÎÐÌÈÐÎÂÀÍÈÅ ÍÅÉÐÎÑÅÒÅÂÎÉ ÌÎÄÅËÈ ÃÈÄÐÎÌÅÕÀÍÈ×ÅÑÊÎÉ ÑÈÑÒÅÌÛ ÀÂÒÎÌÀÒÈ×ÅÑÊÎÃÎ ÓÏÐÀÂËÅÍÈß ÀÂÈÀÖÈÎÍÍÛÌÈ ÄÂÈÃÀÒÅËßÌÈ

86–90
(5)

Êîíîíûõèí Å. À.

OPTIMIZATION OF TURBOSHAFT CONTROL ALGORITHMS FOR ACCELERATIONS

ÎÏÒÈ̲ÇÀÖ²ß ÏÐÎÃÐÀÌÈ ÊÅÐÓÂÀÍÍß ÒÂÀÄ ÍÀ ÅÒÀϲ ÏÐȪÌÈÑÒÎÑÒ²

ÎÏÒÈÌÈÇÀÖÈß ÏÐÎÃÐÀÌÌÛ ÓÏÐÀÂËÅÍÈß ÒÂÀÄ ÍÀ ÝÒÀÏÅ ÏÐÈÅÌÈÑÒÎÑÒÈ

91–94
(4)

Êîðîáêî Â. Â.,
Êîðîáêî Î. Â.,
Êîíäðàòåíêî Ã. Â.

CONTROL THERMOACOUSTIC THERMAL MACHINE TYPE "ENGINE - HEAT PUMPS" BASED ON FUZZY LOGIC

ÑÈÑÒÅÌÀ ÊÅÐÓÂÀÍÍß ÒÅÐÌÎÀÊÓÑÒÈ×ÍÎÞ ÒÅÏËÎÂÎÞ ÌÀØÈÍÎÞ ÒÈÏÓ «ÄÂÈÃÓÍ-ÒÅÏËÎÂÈÉ ÍÀÑÎÑ» ÍÀ ÁÀDz ÍÅײÒÊί ËÎÃÈʲ

ÑÈÑÒÅÌÀ ÓÏÐÀÂËÅÍÈß ÒÅÐÌÎÀÊÓÑÒÈ×ÅÑÊÎÉ ÒÅÏËÎÂÎÉ ÌÀØÈÍÎÉ ÒÈÏÀ «ÄÂÈÃÀÒÅËÜ - ÒÅÏËÎÂÎÉ ÍÀÑÎÑ» ÍÀ ÁÀÇÅ ÍÅ×ÅÒÊÎÉ ËÎÃÈÊÈ

95–102
(8)

Íàçèí Â. È.

ABOUT APPLICABILITY OF METHOD N'YUTONA-RAFSONA FOR DETERMINATION OF PRESSURES IN CHAMBERS OF HYDROSTATODYNAMIC BEARING OF THE DOUBLED TYPE

ÏÐÎ ÇÀÑÒÎÑÎÂͲÑÒÜ ÌÅÒÎÄÓ ÍÜÞÒÎÍÀ-ÐÀÔÑÎÍÀ ÄËß ÂÈÇÍÀ×ÅÍÍß ÒÈÑÊÓ Â ÊÀÌÅÐÀÕ Ã²ÄÐÎÑÒÀÒÎIJÍÀ̲×ÍÎÃÎ Ï²ÄØÈÏÍÈÊÀ ÇÄÂΪÍÎÃÎ ÒÈÏÓ

Î ÏÐÈÌÅÍÈÌÎÑÒÈ ÌÅÒÎÄÀ ÍÜÞÒÎÍÀ-ÐÀÔÑÎÍÀ ÄËß ÎÏÐÅÄÅËÅÍÈß ÄÀÂËÅÍÈÉ Â ÊÀÌÅÐÀÕ ÃÈÄÐÎÑÒÀÒÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÏÎÄØÈÏÍÈÊÀ ÑÄÂÎÅÍÍÎÃÎ ÒÈÏÀ

103–107
(5)

Õàóñòîâà À. Í.

CALIBRATION OF FIBER-OPTIC SPECTROMETER FOR OPTICAL EMISSION SPECTROSCOPY METHOD OF ELECTRIC PROPULSION

ÊÀ˲ÁÐÓÂÀÍÍß ÂÎËÎÊÎÍÍÎ-ÎÏÒÈ×ÍÎÃÎ ÑÏÅÊÒÐÎÌÅÒÐÀ ÄËß ÏÐÎÂÅÄÅÍÍß ÎÏÒÈ×Íί Å̲ѲÉÍί ÑÏÅÊÒÐÎÑÊÎϲ¯ ÅËÅÊÒÐÎÐÀÊÅÒÍÈÕ ÄÂÈÃÓͲÂ

ÊÀËÈÁÐÎÂÊÀ ÂÎËÎÊÎÍÍÎ-ÎÏÒÈ×ÅÑÊÎÃÎ ÑÏÅÊÒÐÎÌÅÒÐÀ ÄËß ÏÐÎÂÅÄÅÍÈß ÎÏÒÈ×ÅÑÊÎÉ ÝÌÈÑÑÈÎÍÍÎÉ ÑÏÅÊÒÐÎÑÊÎÏÈÈ ÝËÅÊÒÐÎÐÀÊÅÒÍÛÕ ÄÂÈÃÀÒÅËÅÉ

108–112
(5)

Èíôîðìàöèîííûå òåõíîëîãèè

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

TURBOFAN TECHNICAL CONDITION CONTROL BY ON-GROUND AUTOMATIC PARAMETRIC DIAGNOSIS COMPLEX

ÊÎÍÒÐÎËÜ ÒÅÕͲ×ÍÎÃÎ ÑÒÀÍÓ ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÎÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÓÍÀ ÍÀÇÅÌÍÈÌ ÀÂÒÎÌÀÒÈÇÎÂÀÍÈÌ ÊÎÌÏËÅÊÑÎÌ ÏÀÐÀÌÅÒÐÈ×Íί IJÀÃÍÎÑÒÈÊÈ

ÊÎÍÒÐÎËÜ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÑÎÑÒÎßÍÈß ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÓÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÀÒÅËß ÍÀÇÅÌÍÛÌ ÀÂÒÎÌÀÒÈÇÈÐÎÂÀÍÍÛÌ ÊÎÌÏËÅÊÑÎÌ ÏÀÐÀÌÅÒÐÈ×ÅÑÊÎÉ ÄÈÀÃÍÎÑÒÈÊÈ

113–120
(8)

Ñòðåëåö Â. Å.,
Óãðþìîâ Ì. Ë.,
Òðîôèìîâà È. À.,
Âàìáîëü Ñ. À.

TURBINE ENGINE TECHNICAL STATE DIAGNOSIS PROBLEMS SOLVING METHODOLOGY UNDER UNCERTAINTY INPUTS

ÌÅÒÎÄÎËÎÃ²ß ÐÎÇÂ’ßÇÀÍÍß ÇÀÄÀ× Ä²ÀÃÍÎÑÒÓÂÀÍÍß ÒÅÕͲ×ÍÎÃÎ ÑÒÀÍÓ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ  ÓÌÎÂÀÕ ÍÅÂÈÇÍÀ×ÅÍÎÑÒ² ÂÕ²ÄÍÈÕ ÄÀÍÈÕ

ÌÅÒÎÄÎËÎÃÈß ÐÅØÅÍÈß ÇÀÄÀ× ÄÈÀÃÍÎÑÒÈÐÎÂÀÍÈß ÒÅÕÍÈ×ÅÑÊÎÃÎ ÑÎÑÒÎßÍÈß ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ Â ÓÑËÎÂÈßÕ ÍÅÎÏÐÅÄÅËÅÍÍÎÑÒÈ ÂÕÎÄÍÛÕ ÄÀÍÍÛÕ

121–127
(7)

Àáäóëëàåâ Ï. Ø.,
Ìèðçîåâ À. Äæ.

APPLICATION OF THE DEMPSTER-SHAFER THEORY ON FUSION OF THE AVIATION GAS TURBINE ENGINES’ HEALTH INFORMATION

ÎÑÎÁËÈÂÎÑÒ² ÇÀÑÒÎÑÓÂÀÍÍß ÒÅÎв¯ ÄÅÌÏÑÒÅÐÀ-ØÅÔÅÐÀ ÄËß ÑÈÍÒÅÇÓ ²ÍÔÎÐÌÀÖ²¯ ÏÐÎ ÒÅÕͲ×ÍÈÉ ÑÒÀÍ ÃÒÄ

ÎÑÎÁÅÍÍÎÑÒÈ ÏÐÈÌÅÍÅÍÈß ÒÅÎÐÈÈ ÄÅÌÏÑÒÅÐÀ-ØÅÔÅÐÀ ÏÐÈ ÑÈÍÒÅÇÅ ÈÍÔÎÐÌÀÖÈÈ Î ÒÅÕÍÈ×ÅÑÊÎÌ ÑÎÑÒÎßÍÈÈ ÃÒÄ

128–132
(5)

Ãîëüöîâ À. Ñ.,
Ñàâ÷èö À. Â.,
Çóåâà Î. Â.

DIAGNOSTICS OF TECHNICAL CONDITION OF THE MAIN SPOOL AND SERVOMOTOR OPENING OF WICKED GATE HYDROUNIT

IJÀÃÍÎÑÒÓÂÀÍÍß ÒÅÕͲ×ÍÎÃÎ ÑÒÀÍÓ ÃÎËÎÂÍÎÃÎ ÇÎËÎÒÍÈÊÀ ² ÑÅÐÂÎÌÎÒÎÐÀ ÑÈÑÒÅÌÈ ÓÏÐÀÂ˲ÍÍß Â²ÄÊÐÈÒÒßÌ ÍÀÏÐÀÂËßÞ×ÎÃÎ ÀÏÀÐÀÒÓ Ã²ÄÐÎÒÓÐÁ²ÍÈ

ÄÈÀÃÍÎÑÒÈÐÎÂÀÍÈÅ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÑÎÑÒÎßÍÈß ÃËÀÂÍÎÃÎ ÇÎËÎÒÍÈÊÀ È ÑÅÐÂÎÌÎÒÎÐÀ ÑÈÑÒÅÌÛ ÓÏÐÀÂËÅÍÈß ÎÒÊÐÛÒÈÅÌ ÍÀÏÐÀÂËßÞÙÅÃÎ ÀÏÏÀÐÀÒÀ ÃÈÄÐÎÒÓÐÁÈÍÛ

133–138
(6)

Ïàï÷¸íêîâ À. Â.,
Áîðçîâ Ñ. À.

ADEQUACY ANALYSIS OF TRADITIONAL METHODS LIFETIME DIAGNOSTIC OF GAS TURBINE ENGINE PARTS

ÀÍÀË²Ç ÀÄÅÊÂÀÒÍÎÑÒ² ÒÐÀÄÈÖ²ÉÍÈÕ ÌÅÒÎIJ IJÀÃÍÎÑÒÓÂÀÍÍß ÐÅÑÓÐÑÓ ÄÅÒÀËÅÉ ÃÒÄ

ÀÍÀËÈÇ ÀÄÅÊÂÀÒÍÎÑÒÈ ÒÐÀÄÈÖÈÎÍÍÛÕ ÌÅÒÎÄÎÂ ÄÈÀÃÍÎÑÒÈÐÎÂÀÍÈß ÐÅÑÓÐÑÀ ÄÅÒÀËÅÉ ÃÒÄ

139–142
(4)

Ìóõòàðîâ Ï. Ø.

BASIC DOMINANTS IN MAKING DECISION BY AIR TRAFFIC CONTROLLER DURING ESTIMATING OF UTILITY-SAFETY OF NORM OF ECHELONING OF AIR SPACE

ÎÑÍÎÂͲ ÄÎ̲ÍÀÍÒÈ Â ÏÐÈÉÍßÒÒ² вØÅÍÜ À²ÀÄÈÑÏÅÒ×ÅÐÎÌ ÏÐÈ ÎÖ²ÍÖ² ÊÎÐÈÑÍÎÑÒ²-ÁÅÇÏÅÊÈ ÍÎÐÌÈ ÅØÅËÎÍÓÂÀÍÍß ÏβÒÐßÍÎÃÎ ÏÐÎÑÒÎÐÓ

ÎÑÍÎÂÍÛÅ ÄÎÌÈÍÀÍÒÛ Â ÏÐÈÍßÒÈÈ ÐÅØÅÍÈÉ ÀÂÈÀÄÈÑÏÅÒ×ÅÐÎÌ ÏÐÈ ÎÖÅÍÊÅ ÏÎËÅÇÍÎÑÒÈ-ÁÅÇÎÏÀÑÍÎÑÒÈ ÍÎÐÌÛ ÝØÅËÎÍÈÐÎÂÀÍÈß ÂÎÇÄÓØÍÎÃÎ ÏÐÎÑÒÐÀÍÑÒÂÀ

143–150
(8)

Ðåâà Î. Ì.,
Áîðñóê Ñ. Ï.,
Øóëüã³í Â. À.

FINDING OF BOARDER RISK LEVELS DURING AIR SPACE FLIGHT LEVELS NORMS VIOLATION

ÂÈÇÍÀ×ÅÍÍß ÃÐÀÍÈ×ÍÈÕ Ð²ÂͲ ÐÈÇÈÊÓ Ï²Ä ×ÀÑ ÏÎÐÓØÅÍÍß ÍÎÐÌÈ ÅØÅËÎÍÓÂÀÍÍß ÏβÒÐßÍÎÃÎ ÏÐÎÑÒÎÐÓ

ÎÏÐÅÄÅËÅÍÈÅ ÃÐÀÍÈ×ÍÛÕ ÓÐÎÂÍÅÉ ÐÈÑÊÀ ÂÎ ÂÐÅÌß ÍÀÐÖÓØÅÍÈß ÍÎÐÌÛ ÝØÅËÎÍÈÐÎÂÍÈß ÂÎÇÄÓØÍÎÃÎ ÏÐÎÑÒÐÀÍÑÒÂÀ

151–156
(6)

Óñòèìåíêî È. Ì.

INFORMATION CYBERNETIC MODEL OF ORGANIZATIONAL AIR NAVIGATION STRUCTURES

²ÍÔÎÐÌÀÖ²ÉÍÎ-ʲÁÅÐÍEÒÈ×ÍÀ ÌÎÄÅËÜ ÎÐÃÀͲÇÀÖ²ÉÍÈÕ ÀÅÐÎÍÀ²ÃÀÖ²ÉÍÈÕ ÑÒÐÓÊÒÓÐ

ÈÍÔÎÐÌÀÖÈÎÍÍÎ-ÊÈÁÅÐÍÅÒÈ×ÅÑÊÀß ÌÎÄÅËÜ ÎÐÃÀÍÈÇÀÖÈÎÍÍÛÕ ÀÝÐÎÍÀÂÈÃÀÖÈÎÍÍÛÕ ÑÒÐÓÊÒÓÐ

157–167
(11)

Ãðóçäî È. Â.,
Ðîññîõà Ñ. Â.,
Øîñòàê È. Â.

APPLICATION PARALLEL COMPUTING TO THE PROBLEM OF AUTHORSHIP ESTABLISHMENT OF TEXTS

ÇÀÑÒÎÑÓÂÀÍÍß ÏÀÐÀËÅËÜÍÈÕ ÎÁ×ÈÑËÅÍÜ ÄÎ ÂÈвØÅÍÍß ÇÀÂÄÀÍÍß ÂÑÒÀÍÎÂËÅÍÍß ÀÂÒÎÐÑÒÂÀ ÒÅÊÑÒ²Â

ÏÐÈÌÅÍÅÍÈÅ ÏÀÐÀËËÅËÜÍÛÕ ÂÛ×ÈÑËÅÍÈÉ Ê ÐÅØÅÍÈÞ ÇÀÄÀ×È ÓÑÒÀÍÎÂËÅÍÈß ÀÂÒÎÐÑÒÂÀ ÒÅÊÑÒÎÂ

168–176
(9)

Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè

Äìèòð³ºâ Ñ. Î.,
Áóðëàêîâ Â. ².,
Ïîïîâ Î. Â.,
Ïîïîâ Ä. Â.

THE PROCEDURES FORMALIZE AND IDENTIFY THE OPTIMAL MAINTENANCE PROGRAM AIRCRAFT AND AIRCRAFT ENGINES

ÔÎÐÌÀ˲ÇÀÖ²ß ÏÐÎÖÅÄÓÐ ÒÀ ÂÈÇÍÀ×ÅÍÍß ÎÏÒÈÌÀËÜÍÈÕ ÏÐÎÃÐÀÌ ÒÅÕͲ×ÍÎÃÎ ÎÁÑËÓÃÎÂÓÂÀÍÍß ÏβÒÐßÍÈÕ ÑÓÄÅÍ ÒÀ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲÂ

ÔÎÐÌÀËÈÇÀÖÈß ÏÐÎÖÅÄÓÐ È ÎÏÐÅÄÅËÅÍÈÅ ÎÏÒÈÌÀËÜÍÛÕ ÏÐÎÃÐÀÌÌ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÎÁÑËÓÆÈÂÀÍÈß ÂÎÇÄÓØÍÛÕ ÑÓÄÎÂ È ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ

177–181
(5)

ßêóøåíêî Î. C.,
Âëàñåíêî Ï. Î.

USING OF IMPROVED MAINTANANCE QUALITY RATE FOR CHOOSING THE MOST OPTIMAL MANTANANCE COMPANIES

ÂÈÊÎÐÈÑÒÀÍÍß ÓÄÎÑÊÎÍÀËÅÍÎÃÎ ÏÎÊÀÇÍÈÊÀ ÒÅÕͲ×ÍÎÃÎ ÎÁÑËÓÃÎÂÓÂÀÍÍß ÄËß ÎÁÃÐÓÍÒÎÂÀÍÎÃÎ ÂÈÁÎÐÓ ÎÏÒÈÌÀËÜÍÈÕ ÐÅÌÎÍÒÍÈÕ Ï²ÄÏÐȪÌÑÒÂ

ÈÑÏÎËÜÇÎÂÀÍÈÅ ÓÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÍÎÃÎ ÏÎÊÀÇÀÒÅËß ÒÅÕÍÈ×ÅÑÊÎÃÎ ÎÁÑËÓÆÈÂÀÍÈß ÄËß ÎÁÎÑÍÎÂÀÍÎÃÎ ÂÛÁÎÐÀ ÎÏÒÈÌÀËÜÍÛÕ ÐÅÌÎÍÒÍÛÕ ÏÐÅÄÏÐÈßÒÈÉ

182–186
(5)

ÀËÔÀÂÈÒÍÛÉ ÓÊÀÇÀÒÅËÜ

187

 

 

 

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.