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

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ  ² ÒÅÕÍÎËÎòß. – 2012. – ¹ 10(97). – 230 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2012. – ¹ 10(97). – 230 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2012. – ¹ 10(97). – 230 p.

 

ÑÒÀÒÜè (articleS)

 

Àâòîðû
(ÿçûê
îðèãèíàëà)

Íàçâàíèå ñòàòüè  (article title)

Ñòðàíèöû
(
pages)

English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Áîðèñåâè÷ Â.Ê.,
Äîëìàòîâ À.È.,
Ñêîð÷åíêî È.Â.,
Ñàáàêàðü À.È.,
Òðåòüÿê Â.Â.

RESEARCH POSSIBILITY OF OBTAINING OF NEW MATERIAL WITH PULSED ULTRAHIGH PRESSURE

ÄÎÑË²ÄÆÅÍÍß ÌÎÆËÈÂÎÑÒ² ÎÒÐÈÌÀÍÍß ÍÎÂÈÕ ÌÀÒÅвÀ˲ ÇÀ ÄÎÏÎÌÎÃÎÞ ²ÌÏÓËÜÑÍÈÕ ÍÀÄÂÈÑÎÊÈÕ ÒÈÑʲÂ

ÈÑÑËÅÄÎÂÀÍÈÅ ÂÎÇÌÎÆÍÎÑÒÈ ÏÎËÓ×ÅÍÈß ÍÎÂÛÕ ÌÀÒÅÐÈÀËΠÏÐÈ ÏÎÌÎÙÈ ÈÌÏÓËÜÑÍÛÕ ÑÂÅÐÕÂÛÑÎÊÈÕ ÄÀÂËÅÍÈÉ

7–10
(4)

Õóäÿêîâ Ñ.Â.,
Òðåòüÿê Â.Â.,
Ñîòíèêîâ Â.Ä.

DEVELOPMENT  OF TECHNOLOGICAL PROCESSES OF MAKING  OF DETAILS  OF AVIATION ENGINES IN ENVIRONMENT ADEM

ÐÎÇÐÎÁÊÀ ÒÅÕÍÎËÎò×ÍÈÕ ÏÐÎÖÅѲ ÂÈÃÎÒÎÂËÅÍÍß  ÄÅÒÀËÅÉ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲ  ÑÅÐÅÄÎÂÈÙ² ÀÄÅÌ

ÐÀÇÐÀÁÎÒÊÀ ÒÅÕÍÎËÎÃÈ×ÅÑÊÈÕ ÏÐÎÖÅÑÑΠÈÇÃÎÒÎÂËÅÍÈß ÄÅÒÀËÅÉ ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ Â ÑÐÅÄÅ ÀÄÅÌ

11–15
(5)

Áîëñóíîâñêèé Ñ.À.,
Âåðìåëü Â.Ä.,
Ãóáàíîâ Ã.À.,
Ëåîíòüåâ À.Å.,
Ñêàçêèí Ð.Î.

Cutting Forces theoretical calculation and experimental measurement for high-Speed finish milling of a gas-turbine engine compressor blade

ÐÎçðàõóíêîâà îöiíêà òà åêñïåðèìåíòàëüíèé âèìið çóñèëü ðiçàííÿ äëÿ ÷iñòîâîÏ âèñîêîøâèäêiñíîÏ ôðåçåðíîÏ îáðîáêè êîìïðåñîðíîÏ ëîïàòêè ÃÒÄ

ÐÀÑרÒÍÀß ÎÖÅÍÊÀ È ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÅ ÈÇÌÅÐÅÍÈÅ ÓÑÈËÈÉ ÐÅÇÀÍÈß ÄËß ×ÈÑÒÎÂÎÉ ÂÛÑÎÊÎÑÊÎÐÎÑÒÍÎÉ ÔÐÅÇÅÐÍÎÉ ÎÁÐÀÁÎÒÊÈ ËÎÏÀÒÊÈ ÃÒÄ

16–19
(4)

Ãîëäóí Â.Þ.,
Êëèìåíêî Ë.Ï.,
Àíäðººâ Â.².,
Ïðèùåïîâ Î.Ô.

UPGRADING CAST-IRON OF COMPRESSION PISTON-RINGS OF TRANSPORT ENGINES

ϲÄÂÈÙÅÍÍß ßÊÎÑÒ² ×ÀÂÓÍÓ ÊÎÌÏÐÅѲÉÍÈÕ ÏÎÐØÍÅÂÈÕ Ê²ËÅÖÜ ÒÐÀÍÑÏÎÐÒÍÈÕ ÄÂÈÃÓͲÂ

ÏÎÂÛØÅÍÈÅ ÊÀ×ÅÑÒÂÀ ×ÓÃÓÍÀ ÊÎÌÏÐÅÑÑÈÎÍÍÛÕ ÏÎÐØÍÅÂÛÕ ÊÎËÅÖ ÒÐÀÍÑÏÎÐÒÍÛÕ ÄÂÈÃÀÒÅËÅÉ

20–23
(4)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Ñìèðíîâ Ä.Ñ.,
Êàùååâ À.Â.,
Øåïåëü Â.Ò.

FIRE TESTS OF FAN CASE IN THE PROCESS OF AVIATION GAS-TURBINE ENGINE DEVELOPMENT AND CERTIFICATION

ÂÎÃÍų ÂÈÏÐÎÁÓÂÀÍÍß ÊÎÐÏÓÑÀ ÂÅÍÒÈËßÒÎÐÀ  ÏÐÎÖÅѳ ÄÎÂÅÄÅÍÍß ÑÅÐÒÈÔ³ÊÀÖ³¿ À³ÀÖ³éÍÎÃÎ ÃÒÄ

ÎÃÍÅÂÛÅ ÈÑÏÛÒÀÍÈß ÊÎÐÏÓÑÀ ÂÅÍÒÈËßÒÎÐÀ Â ÏÐÎÖÅÑÑÅ ÄÎÂÎÄÊÈ È ÑÅÐÒÈÔÈÊÀÖÈÈ ÀÂÈÀÖÈÎÍÍÎÃÎ ÃÒÄ

24–28
(5)

Âîðîáüåâ Þ.Ñ.,
Îâ÷àðîâà Í.Þ.

LOCAL IMPACT action ON cylindrical STRUCTURE elements

ËÎÊÀËÜÍÅ óäàðíèé âïëèâ ÍÀ ÖÈ˲ÍÄÐÈ×Ͳ ÅËÅÌÅÍÒÈ ÊÎÍÑÒÐÓÊÖ²É

ËÎÊÀËÜÍÎÅ ÓÄÀÐÍÎÅ ÂÎÇÄÅÉÑÒÂÈÅ ÍÀ ÖÈËÈÍÄÐÈ×ÅÑÊÈÅ ÝËÅÌÅÍÒÛ ÊÎÍÑÒÐÓÊÖÈÉ

29–32
(4)

Âèíîãðàäîâ À.Ñ.,
Òèñàðåâ À.Þ.,
Áàäûêîâ Ð.Ð.

PECULIARITIES OF RETAINER DESIGN AS A PART OF  AIR-ENGINE SYSTEMS

ÎÑÎÁËÈÂÎÑÒ² ÏÐÎÅÊÒÓÂÀÍÍß ÓÙ²ËÜÍÅÍÜ Ó ÑÊËÀIJ ÑÈÑÒÅÌ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲÂ

ÎÑÎÁÅÍÍÎÑÒÈ ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÓÏËÎÒÍÅÍÈÉ Â ÑÎÑÒÀÂÅ ÑÈÑÒÅÌ ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ

33–38
(6)

Ëåïåøêèí À.Ð.,
Âàãàíîâ Ï.À.,
Áû÷êîâ Í.Ã.,
Áàëóåâ Á.À.

METHOD FOR CALCULATION OF SSS AND STRENGTH OF GTE BLADE IN VIEW OF TANGENT STRESSES AT THE CONTAINMENT CASING TESTS

ÌÅÒÎÄÈÊÀ ÐÎÇÐÀÕÓÍÊÓ íàïðóæåíî-äåôîðìîâàíîãî ñòàíó ² Ì²ÖÍÎÑÒ² ËÎÏÀÒÊÈ ÃÒÄ Ç ÓÐÀÕÓÂÀÍÍßÌ ÄÎÒÈ×Íί ÍÀÏÐÓÃÈ ÏÐÈ ÂÈÏÐÎÁÓÂÀÍÍßÕ ÊÎÐÏÓÑÓ ÍÀ ÍÅÏÐÎÁ²ÂÀªÌÎÑÒÜ

ÌÅÒÎÄÈÊÀ ÐÀÑ×ÅÒÀ ÍÀÏÐ߯ÅÍÍÎ-ÄÅÔÎÐÌÈÐÎÂÀÍÍÎÃÎ ÑÎÑÒÎßÍÈß È ÏÐÎ×ÍÎÑÒÈ ËÎÏÀÒÊÈ ÃÒÄ Ñ Ó×ÅÒÎÌ ÊÀÑÀÒÅËÜÍÛÕ ÍÀÏÐ߯ÅÍÈÉ ÏÐÈ ÈÑÏÛÒÀÍÈßÕ ÊÎÐÏÓÑÀ ÍÀ ÍÅÏÐÎÁÈÂÀÅÌÎÑÒÜ

39–43
(5)

Äîðîôååâ Â.Ë.,
Ãîëîâàíîâ Â.Â.,
Àíàíüåâ Â.Ì.

MATHEMATICAL MODEL OF THE AVIATION GEAR DESIGN

ÌÀÒÅÌÀÒÈ×ÍÀ ÌÎÄÅËÜ ÏÐÎÅÊÒÓÂÀÍÍß À²ÀÖ²ÉÍÈÕ ÇÓÁ×ÀÑÒÈÕ ÏÅÐÅÄÀ×

ÌÀÒÅÌÀÒÈ×ÅÑÊÀß ÌÎÄÅËÜ ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÀÂÈÀÖÈÎÍÍÛÕ ÇÓÁ×ÀÒÛÕ ÏÅÐÅÄÀ×

44–49
(6)

Óìàíñêèé À.Ï.,
Òåðåíòüåâ À.Å ,
Ñòîðîæåíêî Ì.Ñ.,
Áîíäàðåíêî À.À.

INFLUENCE OF TiB2 ADDITIVES ON STRUCNURE AND PROPERTIES OF NiCrSiB-BASED PLASMA SPRAY COATINGS

ÂÏËÈ ÄÎÁÀÂÎÊ TiB2 ÍÀ ÑÒÐÓÊÒÓÐÓ ÒÀ ÂËÀÑÒÈÂÎÑÒ²ÏËÀÇÌÎÂÈÕ ÏÎÊÐÈÒҲ ÍÀ ÎÑÍβ NiCrSiB 

ÂËÈßÍÈÅ ÄÎÁÀÂÎÊ TiB2 ÍÀ ÑÒÐÓÊÒÓÐÓ È ÑÂÎÉÑÒÂÀ ÏËÀÇÌÅÍÍÛÕ ÏÎÊÐÛÒÈÉ ÍÀ ÎÑÍÎÂÅ NiCrSiB

50–54
(5)

Ðûæêîâ Ñ.Ñ.,
Ðàä÷åíêî Í.È.,
Ôîðäóé Ñ.Ã.

TRIGENERATION PLANT FOR INTEGRATED ENERGY SUPPLY

ÒÐÈÃÅÍÅÐÀÖ²ÉÍÀ ÓÑÒÀÍÎÂÊÀ ÀÂÒÎÍÎÌÍÎÃÎ ÅÍÅÐÃÎÇÀÁÅÇÏÅ×ÅÍÍß

ÒÐÈÃÅÍÅÐÀÖÈÎÍÍÀß ÓÑÒÀÍÎÂÊÀ ÀÂÒÎÍÎÌÍÎÃÎ ÝÍÅÐÃÎÎÁÅÑÏÅ×ÅÍÈß

55–60
(6)

Ðàä÷åíêî Ð.Í.,
Ðàä÷åíêî Í.È.,
Áåñ Ò.,
Ñèðîòà À.À.

COOLING OF AIR AT THE INLET OF MAIN ENGINE OF TRANSPORT SHIP

ÎÕÎËÎÄÆÅÍÍß ÏβÒÐß ÍÀ ÂÕÎIJ ÃÎËÎÂÍÎÃÎ ÄÂÈÃÓÍÀ ÒÐÀÍÑÏÎÐÒÍÎÃÎ ÑÓÄÍÀ

ÎÕËÀÆÄÅÍÈÅ ÂÎÇÄÓÕÀ ÍÀ ÂÕÎÄÅ ÃËÀÂÍÎÃÎ ÄÂÈÃÀÒÅËß ÒÐÀÍÑÏÎÐÒÍÎÃÎ ÑÓÄÍÀ

61–67
(7)

Ðàä÷åíêî À.Í.,
Êîíîâàëîâ À.Â.

Cooling the intake air to the engine room for reciprocating gas engines in integrated energy system

ÎÕÎËÎÄÆÅÍÍß ÏÐÈÒÎ×ÍÎÃÎ ÏβÒÐß ÌÀØÈÍÍÎÃΠ²ÄIJËÅÍÍß ÃÀÇÎÏÎÐØÍÅÂÈÕ ÄÂÈÃÓͲ ÓÑÒÀÍÎÂÊÈ ÀÂÒÎÍÎÌÍÎÃÎ ÅÍÅÐÃÎÇÀÁÅÇÏÅ×ÅÍÍß

ÎÕËÀÆÄÅÍÈÅ ÏÐÈÒÎ×ÍÎÃÎ ÂÎÇÄÓÕÀ ÌÀØÈÍÍÎÃÎ ÎÒÄÅËÅÍÈß ÃÀÇÎÏÎÐØÍÅÂÛÕ ÄÂÈÃÀÒÅËÅÉ ÓÑÒÀÍÎÂÊÈ ÀÂÒÎÍÎÌÍÎÃÎ ÝÍÅÐÃÎÎÁÅÑÏÅ×ÅÍÈß

68–71
(4)

Àë¸õèí Ñ.À.,
Ãåðàñèìåíêî Â.Ï.,
Îâ÷àðîâ Å.Í.,
Îïàëåâ Â.À.

COMPLEX GAS-DYNAMIC IMPROVEMENT OF TWO-STROKE TURBO-PISTON TRANSPORT DIESEL ENGINES

ÊÎÌÏËÅÊÑÍÅ ÃÀÇÎÄÈÍÀ̲×ÍÅ ÓÄÎÑÊÎÍÀËÞÂÀÍÍß ÄÂÎÒÀÊÒÍÈÕ ÒÓÐÁÎÏÎÐØÍÅÂÈÕ ÒÐÀÍÑÏÎÐÒÍÈÕ ÄÈÇÅ˲Â

ÊÎÌÏËÅÊÑÍÎÅ ÃÀÇÎÄÈÍÀÌÈ×ÅÑÊÎÅ ÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈÅ ÄÂÓÕÒÀÊÒÍÛÕ ÒÓÐÁÎÏÎÐØÍÅÂÛÕ ÒÐÀÍÑÏÎÐÒÍÛÕ ÄÈÇÅËÅÉ

72–76
(5)

Ìóðçàãàëèåâ À.Æ.,
Íåêðàñîâ Â.Ã.,
Êóàíûøåâ Ì.Ê.,
Ìóõòàðîâ À.Ò.,
Êàóêàðîâ À.Ê.

EXPERIMENTAL  IVESTIGATION IN THE FIELD OF CREATION OF TWO-STROKE ENGINE

ÅÊÑÏÅÐÈÌÅÍÒÀËÜͲ ÄÎÑË²ÄÆÅÍÍß Â ÎÁËÀÑÒ² ÑÒÂÎÐÅÍÍß  ÄÂÎÒÀÊÒÍÎÃÎ ÄÂÈÃÓÍÀ

ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÛÅ ÈÑÑËÅÄÎÂÀÍÈß  Â ÎÁËÀÑÒÈ ÑÎÇÄÀÍÈß ÄÂÓÕÒÀÊÒÍÎÃÎ ÄÂÈÃÀÒÅËß

77–81
(5)

Ñàôîíîâ Â.À.,
Êóçíåöîâ Ï.Í.

ABOUT SOME FEATURES OF WORK OF thermosonicAND thermoreversible ENGINES

ÏÐÎ ÄÅßʲ ÎÑÎÁËÈÂÎÑÒ² ÐÎÁÎÒÈ ÒÅÐÌÎÀÊÓÑÒÈ×ÍÈÕ ÒÀ ÒÅÐÌÎÎÁÎÐÎÒÍÈÕ ÄÂÈÃÓͲÂ

Î ÍÅÊÎÒÎÐÛÕ ÎÑÎÁÅÍÍÎÑÒßÕ ÐÀÁÎÒÛ ÒÅÐÌÎÀÊÓÑÒÈ×ÅÑÊÈÕ È ÒÅÐÌÎÎÁÐÀÒÈÌÛÕ ÄÂÈÃÀÒÅËÅÉ

82–85
(4)

Ìîðîçîâà Â.Ñ.,
Ãóí Â.Ñ.,
Ïîëÿöêî Â.Ë.

ANALYSIS OF INFLUENCE OF THE MAGNETIC STREAM ON ECOLOGICAL INDICATORS OF ENGINE

ÀÍÀË²Ç ÂÏËÈÂÓ ÌÀÃͲÒÍÎÃÎ ÏÎÒÎÊÓ
ÍÀ ÅÊÎËÎò×Ͳ ÏÎÊÀÇÍÈÊÈ ÄÂÑ

ÀÍÀËÈÇ ÂËÈßÍÈß ÌÀÃÍÈÒÍÎÃÎ ÏÎÒÎÊÀ ÍÀ ÝÊÎËÎÃÈ×ÅÑÊÈÅ ÏÎÊÀÇÀÒÅËÈ ÄÂÑ

86–91
(6)

Ìîøåíöåâ Þ.Ë.,
Ãîãîðåíêî À.À.,
Ìèí÷åâ Ä.Ñ.,
Íàãîðíûé À.Â.,
Ìàêñèìîâ Þ.Ñ.

Options for cooling liquids and SUPERcharged air temperatures control for the alternative slow-flow cooling system of mainline locomotive diesel engines.

ÌÎÆËÈÂÎÑÒ² ÐÅÃÓËÞÂÀÍÍß ÒÅÌÏÅÐÀÒÓÐ ÒÅÏËÎÍÎѲ¯Â  ÀËÜÒÅÐÍÀÒÈÂÍ²É ÑÈÑÒÅ̲ ÎÕÎËÎÄÆÅÍÍß ÄÈÇÅËÜÍÈÕ ÄÂÈÃÓͲ ÌÀòÑÒÐÀËÜÍÈÕ ÒÅÏËÎÂÎDzÂ

ÂÎÇÌÎÆÍÎÑÒÈ ÐÅÃÓËÈÐÎÂÀÍÈß ÒÅÌÏÅÐÀÒÓÐ ÒÅÏËÎÍÎÑÈÒÅËÅÉ Â ÀËÜÒÅÐÍÀÒÈÂÍÎÉ ÑÈÑÒÅÌÅ ÎÕËÀÆÄÅÍÈß ÄÈÇÅËÜÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÌÀÃÈÑÒÐÀËÜÍÛÕ ÒÅÏËÎÂÎÇÎÂ

92–97
(6)

Âàðáàíåö Ð.À.,
Êó÷åðåíêî Þ.Í.,
Ãîëîâàíü À.È.

Vibroacoustic CONTROL OF MARINE turbocharged diesel REVOLUTION

²áðîàêóñòè÷íèé êîíòðîëü ÷àñòîòíèõ õàðàêòåðèñòèê
ñóäíîâîãî äèçåëÿ ç òóðáîíàääóâîì

ÂÈÁÐÎÀÊÓÑÒÈ×ÅÑÊÈÉ ÊÎÍÒÐÎËÜ ×ÀÑÒÎÒÍÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÑÓÄÎÂÎÃÎ ÄÈÇÅËß Ñ ÒÓÐÁÎÍÀÄÄÓÂÎÌ

98–105
(8)

Áûëèíêèíà Î.Í.,
Êîðîâèí Á.Á.,
Ñòàñåâè÷ À.À.

PECULIARITIES OF VIBRATION DIAGNOSTICS SIGNES MANIFESTATION FOR AFTERBURNING TURBOFAN BEARINGS WHILE OPERATING IN  HIGH MANEUVERABLE AIRPLANE

ÎÑÎÁËÈÂÎÑÒ² ÏÐÎßÂËÅÍÍß  ²ÁÐÀÖ²ÉÍÈÕ Ä²ÀÃÍÎÑÒÈ×ÍÈÕ ÏÐÈÇÍÀʲ ÑÒÀÍÓ Ï²ÄØÈÏÍÈʲ ÒÐÄÄÔ Ï²Ä ×ÀÑ ÅÊÑÏËÓÀÒÀÖ²¯ ÍÀ ÌÀÍÅÂÐÎÂÎÌÓ Ë²ÒÀÊÓ

ÎÑÎÁÅÍÍÎÑÒÈ ÏÐÎßÂËÅÍÈß ÂÈÁÐÀÖÈÎÍÍÛÕ ÄÈÀÃÍÎÑÒÈ×ÅÑÊÈÕ ÏÐÈÇÍÀÊΠÑÎÑÒÎßÍÈß ÏÎÄØÈÏÍÈÊΠÒÐÄÄÔ ÏÐÈ ÝÊÑÏËÓÀÒÀÖÈÈ ÍÀ ÌÀÍÅÂÐÅÍÍÎÌ ÑÀÌÎËÅÒÅ

106–112
(7)

Áîãóñëàåâ Â.À.,
Äîëìàòîâ Ä.À.

METHOD OF  THE DETAILED KINETIC SCHEME FORMATION FOR AIR GAS COMBUSTION

ÌÅÒÎÄ ÔÎÐÌÓÂÀÍÍß ÄÅÒÀ˲ÇÎÂÀÍί ʲÍÅÒÈ×Íί ÑÕÅÌÈ ÏβÒÐßÍÎÃÎ ÃÎвÍÍß ÊÅÐÎÑÈÍÓ

ÌÅÒÎÄ ÔÎÐÌÈÐÎÂÀÍÈß ÄÅÒÀËÈÇÈÐÎÂÀÍÍÎÉ ÊÈÍÅÒÈ×ÅÑÊÎÉ ÑÕÅÌÛ ÏÐÈ ÂÎÇÄÓØÍÎÌ ÃÎÐÅÍÈÈ ÊÅÐÎÑÈÍÀ

113–117
(5)

Guyot M.,
Denise S.,
Dudeck M.,
Claude P.,
Dusseau L.,
Saigne F.,
Bernard M.

 

 

MICRO HALL EFFECT THRUSTER FOR NANOSATELLITE PROPULSION

 

 

̲ÊÐÎõîëëîâñüêèé ÄÂÈÃÓÍ ÄËß íàíîñóïóòíèê³â

 

 

ÌÈÊÐÎõîëëîâñêèé äâèãàòåëÜ äëÿ íàíîñïóòíèêîâ

118–122
(5)

Cenian A.,
Chernukho A.,
Rachubiński H.,
Do A.,
Lino da Silva M.,
Dudeck M.

ENERGY DEPOSITION ON THE INNER SURFACES OF A HALL EFFECT THRUSTER FOR SATELLITE

ÅÍÅÐÃÅÒÈ×Íèé ÂÏËÈ ÍÀ ÂÍÓÒвØÍ² ÏÎÂÅÐÕͲ õîëëîâñüêîãî ÏÐÈÑÊÎÐÞÂÀ×À

Ýíåðãåòè÷åñêîå âîçäåéñòâèå íà âíóòðåííèå ïîâåðõíîñòè Õîëëîâñêîãî óñêîðèòåëÿ

123–127
(
5)

Lino da Silva M.,
Chikhaoui A.,
Smith A.

DEVELOPMENT OF A KINETIC SHOCK-TUBE FOR PLANETARY EXPLORATION

ÐÎÇÐÎÁÊÀ ê³íåòè÷íî¿ óäàðíî¿ òðóáè ÄËß ÄÎÑË²ÄÆÅÍÍß ÏËÀÍÅÒ

Ðàçðàáîòêà êèíåòè÷åñêîé óäàðíîé òðóáû äëÿ èññëåäîâàíèÿ ïëàíåò

128–132
(5)

Ãóáàéäóëëèí È.Ò.,
Àíäðååâà Ò.Ï.,
Ñêëàä÷èêîâ À.Ñ.

THE OPTICAL PYROMETRIC SYSTEM FOR MEASURING THE SURFACE TEMPERATURE OF THE TURBINE BLADES OF GAS TURBINE ENGINE GAS GENERATOR AND DIAGNOSTICS OF TECHNICAL CONDITION

ÎÏÒÈ×ÍÀ ϲÐÎÌÅÒв×íà ÑÈÑÒÅÌÀ ÄËß ÂÈ̲ÐÞÂÀÍÍß ÒÅÌÏÅÐÀÒÓÐÈ ÏÎÂÅÐÕͲ ËÎÏÀÒÎÊ ÒÓÐÁ²ÍÈ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ ÃÀÇÎÒÓÐÁ²ÍÍÎÃÎ ÄÂÈÃÓÍÀ ² IJÀÃÍÎÑÒÈÊÈ ÒÅÕͲ×ÍÎÃÎ ÑÒÀÍÓ

ÎÏÒÈ×ÅÑÊÀß ÏÈÐÎÌÅÒÐÈ×ÅÑÊÀß ÑÈÑÒÅÌÀ ÄËß ÈÇÌÅÐÅÍÈß ÒÅÌÏÅÐÀÒÓÐÛ ÏÎÂÅÐÕÍÎÑÒÈ ËÎÏÀÒÎÊ ÒÓÐÁÈÍÛ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ ÃÀÇÎÒÓÐÁÈÍÍÎÃÎ ÄÂÈÃÀÒÅËß È ÄÈÀÃÍÎÑÒÈÊÈ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÑÎÑÒÎßÍÈß

133–139
(7)

Ãîëîâ÷óê À.Ô.,
Ãàáð³ºëü Þ.².,
Ãîëîäíÿê Ð.².

DEVELOPMENT of STRUCTURAL CHART ELECTRONIC-GUIDED fuel supply DIESEL And gas-diesel engines

ÐÎÇÐÎÁÊÀ ÊÎÍÑÒÐÓÊÒÈÂÍί ÑÕÅÌÈ ÅËÅÊÒÐÎÍÍÎ-ÊÅÐÎÂÀÍί ÏÀËÈÂÎÏÎÄÀײ ÄÈÇÅ˲ ² ÃÀÇÎÄÈÇÅ˲Â

Ðàçðàáîòêà êîíñòðóêòèâíîé ñõåìû ýëåêòðîííî-óïðàâëÿåìîé ñèñòåìû òîïëèâîïîäà÷è äèçåëåé è ãàçîäèçåëåé

140–143
(4)

Èíôîðìàöèîííûå òåõíîëîãèè

Øåâ÷åíêî Ì.Â.,
Åïèôàíîâ Ñ.Â.

GTE THRUST ESTIMATION TAKING INTO ACCOUNT THE MEASURMENT SYSTEM FAULT AND TECHNICAL CONDITION CHANGING

ÎÖ²ÍÞÂÀÍÍß ÒßÃÈ Ç ÓÐÀÕÓÂÀÍÍßÌ ÏÎÃвØÍÎÑÒÅÉ ÂÈ̲ÐÞÂÀËÜÍί ÑÈÑÒÅÌÈ ² Ç̲ÍÈ ÒÅÕͲ×ÍÎÃÎ ÑÒÀÍÓ ÃÒÄ

ÎÖÅÍÈÂÀÍÈÅ ÒßÃÈ Ñ Ó×ÅÒÎÌ ÏÎÃÐÅØÍÎÑÒÅÉ ÈÇÌÅÐÈÒÅËÜÍÎÉ ÑÈÑÒÅÌÛ È ÈÇÌÅÍÅÍÈß ÒÅÕÍÈ×ÅÑÊÎÃÎ ÑÎÑÒÎßÍÈß ÃÒÄ

144–152
(9)

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

SIMULATION OF MEASURING CHANNELS WITH TRANSCENDENTAL TRANSFER FUNCTIONS

ÌÎÄÅËÞÂÀÍÍß ÂÈ̲ÐÞÂÀËÜÍÈÕ ÊÀÍÀË²Â Ç ÒÐÀÍÑÖÅÍÄÅÍÒÍÈÌÈ ÏÅÐÅÄÀÒÍÈÌÈ ÔÓÍÊÖ²ßÌÈ

ÌÎÄÅËÈÐÎÂÀÍÈÅ ÈÇÌÅÐÈÒÅËÜÍÛÕ ÊÀÍÀËÎÂ Ñ ÒÐÀÍÑÖÅÍÄÅÍÒÍÛÌÈ ÏÅÐÅÄÀÒÎ×ÍÛÌÈ  ÔÓÍÊÖÈßÌÈ

153–155
(3)

˳íí³ê ².².,
Áîãàéñüêà Ê.Â.,
Êðàìàðåíêî Ò.Þ.

COMPLEX MODEL OF MAINTENANCE SYSTEM SERVICE OF POWER  INSTALLATIONS OF LAND AERONAUTICS

ÊÎÌÏËÅÊÑÍÀ ÌÎÄÅËÜ ÑÈÑÒÅÌÈ ÒÅÕͲ×ÍÎÃÎ ÎÁÑËÓÃÎÂÓÂÀÍÍß ÅÍÅÐÃÅÒÈ×ÍÈÕ ÓÑÒÀÍÎÂÎÊ À²ÀÖ²ÉÍί ÍÀÇÅÌÍί ÒÅÕͲÊÈ

ÊÎÌÏËÅÊÑÍÀß ÌÎÄÅËÜ ÑÈÑÒÅÌÛ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÎÁÑËÓÆÈÂÀÍÈß ÝÍÅÐÃÅÒÈ×ÅÑÊÈÕ ÓÑÒÀÍÎÂÎÊ ÀÂÈÀÖÈÎÍÍÎÉ ÍÀÇÅÌÍÎÉ ÒÅÕÍÈÊÈ

156–160
(5)

Ïîãîðåëîâ Ã.È., 
Êóëèêîâ Ã.Ã.,
Ôàòèêîâ Â.Ñ.,
Áàãàåâà Þ.Î.

SYSTEM MODEL OF PROCESSES OF INFORMATIVE ACCOMPANIMENT OF LIFE CYCLE OF ACS GTE FOR THE STAGE OF INSTALLATION AND CHECK-OUT PHASE

ÑÈÑÒÅÌÍÀ ÌÎÄÅËÜ ÏÐÎÖÅѲ ²ÍÔÎÐÌÀÖ²ÉÍÎÃÎ ÑÓÏÐÎÂÎÄÓ ÆÈÒÒªÂÎÃÎ ÖÈÊËÓ ÑÀÓ ÃÒÄ ÄËß ÅÒÀÏÓ ÄÎÑ˲ÄÍί ÅÊÑÏËÓÀÒÀÖ²¯

ÑÈÑÒÅÌÍÀß ÌÎÄÅËÜ ÏÐÎÖÅÑÑÎÂ ÈÍÔÎÐÌÀÖÈÎÍÍÎÃÎ ÑÎÏÐÎÂÎÆÄÅÍÈß ÆÈÇÍÅÍÍÎÃÎ ÖÈÊËÀ ÑÀÓ ÃÒÄ ÄËß ÝÒÀÏÀ ÎÏÛÒÍÎÉ ÝÊÑÏËÓÀÒÀÖÈÈ

161–169
(9)

Ïàøàåâ À.Ì.,
Àáäóëëàåâ Ï.Ø.,
Ìèðçîåâ À.Äæ.,
Ìåëèêîâ Ý.Ò.

INTERGARTION SCHEME OF THE MATHEMATIC STATISTICS AND NEURAL NETWORKS METHODS FOR AVIATION GAS TURBINE ENGINE DIAGNOSTICS  

ÏÎÐßÄÎÊ ²ÍÒÅÃÐÓÂÀÍÍß ÌÅÒÎIJ ÌÀÒÅÌÀÒÈ×Íί ÑÒÀÒÈÑÒÈÊÈ ÒÀ ÍÅÉÐÎÍÍÈÕ ÌÅÐÅÆ Ó ÇÀÄÀ×ÀÕ Ä²ÀÃÍÎÑÒÓÂÀÍÍß ÒÑ ÀÃÒÄ

ÏÎÐßÄÎÊ ÈÍÒÅÃÐÀÖÈÈ ÌÅÒÎÄΠÌÀÒÅÌÀÒÈ×ÅÑÊÎÉ ÑÒÀÒÈÑÒÈÊÈ È ÍÅÉÐÎÍÍÛÕ ÑÅÒÅÉ Â ÇÀÄÀ×ÀÕ ÄÈÀÃÍÎÑÒÈÐÎÂÀÍÈß ÒÑ ÀÃÒÄ  

170–175
(6)

Ðåâà Î.Ì.,
Âäîâè÷åíêî Â.².,
Óñòèìåíêî ².Ì.

ASSESSMENT OF STRUCTURAL EFFICIENCY  OF THE AIR TRAFFIC DEPARTMENT (ON THE EXAMPLE OF THE KRASNOYARSK CENTER OF AIR TRAFFIC SERVICE)

ÎÖ²ÍÊÀ ÑÒÐÓÊÒÓÐÍί ÅÔÅÊÒÈÂÍÎÑÒ² ÑËÓÆÁÈ ÐÓÕÓ (ÍÀ ÏÐÈÊËÀIJ ÊÐÀÑÍÎßÐÑÜÊÎÃÎ ÖÅÍÒÐÀ ÎÁÑËÓÃÎÂÓÂÀÍÍß ÏβÒÐßÍÎÃÎ ÐÓÕÓ)

ÎÖÅÍÊÀ ÑÒÐÓÊÒÓÐÍÎÉ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÑËÓÆÁÛ ÄÂÈÆÅÍÈß (ÍÀ ÏÐÈÌÅÐÅ ÊÐÀÑÍÎßÐÑÊÎÃÎ ÖÅÍÒÐÀ ÎÁÑËÓÆÈÂÀÍÈß ÂÎÇÄÓØÍÎÃÎ ÄÂÈÆÅÍÈß)

176–186
(11)

Áîðñóê Ñ.Ï.

REGISTRATION OF OPERATORS “FLOATING” PROGRESS WITH HELP OF PERTAINMENT TABLES

ÐŪÑÒÐÀÖ²ß «ÏËÀÂÀÞ×ί» ÓÑϲØÍÎÑÒ² ÎÏÅÐÀÒÎв ÇÀ ÄÎÏÎÌÎÃÎÞ ÒÀÁËÈÖÜ ÍÀËÅÆÍÎÑÒ²

ÐÅÃÈÑÒÐÀÖÈß «ÏËÀÂÀÞÙÅÉ» ÓÑÏÅÂÀÅÌÎÑÒÈ ÎÏÅÐÀÒÎÐÎÂ ÏÐÈ ÏÎÌÎÙÈ ÒÀÁËÈÖ ÏÐÈÍÀÄËÅÆÍÎÑÒÈ

187–191
(5)

Ñòàøèíñüêèé Î.Ï.

SYSTEM OF INTELLECTUAL MANAGEMENT ROBOT-TECHNICAL DEVICE FOR DIAGNOSTICS OF PIPELINES OF THE COMPRESSOR STATIONS

ÑÈÑÒÅÌÀ ²ÍÒÅËÅÊÒÓÀËÜÍÎÃÎ ÓÏÐÀÂ˲ÍÍß ÐÎÁÎÒÎÒÅÕͲ×ÍÈÌ ÏÐÈÑÒÐÎªÌ ÄËß Ä²ÀÃÍÎÑÒÈÊÈ ÒÐÓÁÎÏÐÎÂÎIJ ÊÎÌÏÐÅÑÎÐÍÈÕ ÑÒÀÍÖ²É

ÑÈÑÒÅÌÀ ÈÍÒÅËËÅÊÒÓÀËÜÍÎÃÎ ÓÏÐÀÂËÅÍÈß ÐÎÁÎÒÎÒÅÕÍÈ×ÅÑÊÈÌ ÓÑÒÐÎÉÑÒÂÎÌ ÄËß ÄÈÀÃÍÎÑÒÈÊÈ ÒÐÓÁÎÏÐÎÂÎÄΠÊÎÌÏÐÅÑÑÎÐÍÛÕ ÑÒÀÍÖÈÉ

192–195
(4)

Êâàñí³êîâ Â.Ï.,
Êóëèø ª.Î.

MATHEMATICAL MODEL OF RADIO MOBILE ROBOT

ÌÀÒÅÌÀÒÈ×ÍÀ ÌÎÄÅËÜ ÐÀIJÎÊÅÐÓÂÀÍÍß ÌÎÁ²ËÜÍÈÌ ÐÎÁÎÒÎÌ

ÌÀÒÅÌÀÒÈ×ÅÑÊÀß ÌÎÄÅËÜ ÐÀÄÈÎÓÏÐÀÂËÅÍÈß ÌÎÁÈËÜÍÛÌ ÐÎÁÎÒÎÌ

196–200
(5)

Êâàñí³êîâ Â.Ï.,
Ôåäîðîâ Ä.Ì.

SYNTHESIS OF INFORMATION PROCESSING IN MEASURING ROBOT

ÑÈÍÒÅÇ ÑÈÑÒÅÌÈ ÎÁÐÎÁÊÈ ²ÍÔÎÐÌÀÖ²¯ Ó ÂÈ̲ÐÞÂÀËÜÍÈÕ ÐÎÁÎÒÀÕ

ÑÈÍÒÅÇ ÑÈÑÒÅÌÛ ÎÁÐÀÁÎÒÊÈ ÈÍÔÎÐÌÀÖÈÈ Â ÈÇÌÅÐÈÒÅËÜÍÛÕ ÐÎÁÎÒÀÕ

201–204
(4)

Ëåùåíêî Þ.Ï.

HOW IT WORKS COORDINATE MEASURING machines and intelligent measurement ROBOTS

ÏÐÈÍÖÈÏ ÐÎÁÎÒÈ ÊÎÎÐÄÈÍÀÒÍÎ-ÂÈ̲ÐÞÂÀËÜÍÈÕ ÌÀØÈÍ ÒÀ ²ÍÒÅËÅÊÒÓÀËÜÍÈÕ ÂÈ̲ÐÞÂÀËÜÍÈÕ ÐÎÁÎÒ²Â

ÏÐÈÍÖÈÏ ÐÀÁÎÒÛ ÊÎÎÐÄÈÍÀÒÍÎ-ÈÇÌÅÐÈÒÅËÜÍÛÕ ÌÀØÈÍ È ÈÍÒÅËËÅÊÒÓÀËÜÍÛÕ ÈÇÌÅÐÈÒÅËÜÍÛÕ ÐÎÁÎÒÎÂ

205–208
(4)

Êâàñí³êîâ Â.Ï.,
Íåì÷åíêî Â.Â.

THE CONTROL SYSTEM CONSTRUCTION OF AN AUTONOMOUS MOBILE ROBOT BASED ON MULTILEVEL SYSTEM OF CONVERTING INFORMATION

ÏÎÁÓÄÎÂÀ ÑÈÑÒÅÌÈ ÊÅÐÓÂÀÍÍß ÀÂÒÎÍÎÌÍÈÌ ÌÎÁ²ËÜÍÈÌ ÐÎÁÎÒÎÌ ÍÀ ÎÑÍβ ÁÀÃÀÒÎвÂÍÅÂί ÑÈÑÒÅÌÈ ÏÅÐÅÒÂÎÐÅÍÍß ²ÍÔÎÐÌÀÖ²¯

ÏÎÑÒÐÎÅÍÈÅ ÑÈÑÒÅÌÛ ÓÏÐÀÂËÅÍÈß ÀÂÒÎÍÎÌÍÛÌ ÌÎÁÈËÜÍÛÌ ÐÎÁÎÒÎÌ ÍÀ ÎÑÍÎÂÅ ÌÍÎÃÎÓÐÎÂÍÅÂÎÉ ÑÈÑÒÅÌÛ ÏÐÅÎÁÐÀÇÎÂÀÍÈß ÈÍÔÎÐÌÀÖÈÈ

209–212
(4)

Áîðêîâñüêèé Î.Â.

RECOGNITION OF MOVING OBJECTS WITH DIGITAL CAMERASIN THE SOFTWARE PRODUCT LABVIEW

²ÄÅÍÒÈÔ²ÊÀÖ²ß ÐÓÕÎÌÈÕ ÎÁ’ªÊҲ ÇÀ ÄÎÏÎÌÎÃÎÞ ÖÈÔÐÎÂί ÊÀÌÅÐÈ Â ÏÐÎÃÐÀÌÍÎÌÓ ÏÐÎÄÓÊÒ² LABVIEW

ðàñïîçíàâàíèå ïîäâèæíûõ îáúåêòîâ ñ ïîìîùüþ öèôðîâîé êàìåðû â ïðîãðàììíîì ïðîäóêòå LABVIEW

213–218
(6)

Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè

Ñâèñòóíîâ Â.À.

Intelligent control systemS with multi-level information transformation FOR AIRCRAFT ENTERPRISE

²ÍÒÅËÅÊÒÓÀËÜͲ ÑÈÑÒÅÌÈ ÊÅÐÓÂÀÍÍß Ç ÁÀÃÀÒÎвÂÍÅÂÈÌ ÏÅÐÅÒÂÎÐÅÍÍßÌ ²ÍÔÎÐÌÀÖ²¯ ÍÀ À²ÀÖ²ÉÍÎÌÓ Ï²ÄÏÐȪÌÑÒ²

ÈíòåëËåêòóàëüíÛÅ ñèñòåìÛ ÓÏÐÀÂËÅÍÈß Ñ ÌÍÎÃÎÓÐÎÂÍÅÂÛÌ ÏÐÅÎÁÐÀÇÎÂÀÍÈÅÌ ÈíôîðìàöÈÈ íà àâÈàöÈÎÍÍÎÌ ÏÐÅÄÏÐÈßÒÈÈ

219–222
(4)

Àìèíå Õàäè

CUSTOMER RELATIONSHIP MANAGEMENT CRM

ÑÈÑÒÅÌÀ ÓÏÐÀÂ˲ÍÍß ÂÇÀªÌÈÍÀÌÈ Ç Ê˲ªÍÒÀÌÈ CRM

ÑÈÑÒÅÌÀ ÓÏÐÀÂËÅÍÈß ÂÇÀÈÌÎÎÒÍÎØÅÍÈßÌÈ Ñ ÊËÈÅÍÒÀÌÈ CRM

223–228
(6)

 

 

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).