Íàöèîíàëüíûé
àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé
èíñòèòóò”
ISSN 1727-7337.
À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß.
– 2013. – ¹ 10(107). – 260 ñ.
ISSN
1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2013. – ¹ 10(107). –
260 ñ.
ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2013. – ¹ 10(107). – 260 ñ.
ÑÒÀÒÜè (articleS)
Àâòîðû |
Íàçâàíèå ñòàòüè
(article title) |
Ñòðàíèöû (pages) |
||
English |
Óêðà¿íñüêà
ìîâà |
Ðóññêèé
ÿçûê |
||
Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ |
||||
Êîìáàðîâ Â.Â., |
THE PROVIDING STABILITY
OF CONTOUR FEEDRATE IN CNC SYSTEM BY HIGH-SPEED EQUIPMENT ON EXAMPLE OF
CIRCULAR INTERPOLATION |
ÇÀÁÅÇÏÅ×ÅÍÍß ÑÒÀÁIËÜÍÎÑÒI ÊÎÍÒÓÐÍί
ÏÎÄÀ×I  ÑÈÑÒÅ̲ ×ÏÓ ÂÈÑÎÊÎØÂÈÄÊIÑÍÎÃÎ ÎÁËÀÄÍÀÍÍß ÍÀ ÏÐÈÊËÀIJ ÊÐÓÃÎÂί
IÍÒÅÐÏÎËßÖI¯ |
7–14 |
|
Íåâåøêèí Þ.À., |
OPTIMIZATION TECHNOLOGY MANUFACTURING DETAIL TYPE COUPLING HALF
USING A SOFTWARE PACKAGE DEFORM |
ÎÏÒÈ̲ÇÀÖ²ß ÒÅÕÍÎËÎò¯ ÂÈÃÎÒÎÂËÅÍÍß
ÄÅÒÀ˲ ÒÈÏÓ ÏÎËÓÌÓÔÒÀ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÏÐÎÃÐÀÌÍÎÃÎ ÏÀÊÅÒÓ DEFORM |
15–19 |
|
Óìàíñêèé À.Ï., |
THE STRUCTURE AND PROPERTIES INVESTIGATIONS OF COMPOSITE MATERIALS AND
COATINGS BASED ON NiAl-TiB2 SYSTEMS |
ÄÎÑË²ÄÆÅÍÍß ÑÒÐÓÊÒÓÐÈ ÒÀ ÂËÀÑÒÈÂÎÑÒÅÉ
ÊÎÌÏÎÇÈÖ²ÉÍÈÕ ÌÀÒÅвÀ˲ ÒÀ ÏÎÊÐÈÒÒ²Â Ç ÍÈÕ ÍÀ ÎÑÍβ ÑÈÑÒÅÌÈ NiAl-TiB2 |
20–24 |
|
Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ
àïïàðàòîâ |
||||
Íèêîëàåâ Â.Í., |
A
THERMAL-CONVECTION TRANSDUCER OF FLUID CONSUMPTION AND TEMPERATURE IN
PIPELINES OF AIRCRAFT ENGINE |
ÒÅÐÌÎÊÎÍÂÅÊÒÈÂÍÈÉ ÏÅÐÅÒÂÎÐÞÂÀ× ÂÈÒÐÀÒÈ
² ÒÅÌÏÅÐÀÒÓÐÈ Ð²ÄÈÍÈ Â ÒÐÓÁÎÏÐÎÂÎÄÀÕ ÄÂÈÃÓÍÀ ˲ÒÀËÜÍÎÃÎ ÀÏÀÐÀÒÀ |
25–29 |
|
Èãóìåíöåâ Å.À., |
ELECTROMAGNETIC COMPONENTS OF THE CHARGED GYROSCOPE rotational
frequency |
Åëåêòðîìàãí³òí³
ñêëàäîâ³ ÷àñòîòè îáåðòàííÿ çàðÿäæåíîãî ã³ðîñêîïó |
ÝËÅÊÒÐÎÌÀÃÍÈÒÍÛÅ
ÑÎÑÒÀÂËßÞÙÈÅ ×ÀÑÒÎÒÛ ÂÐÀÙÅÍÈß ÇÀÐ߯ÅÍÍÎÃÎ ÃÈÐÎÑÊÎÏÀ |
30–36 |
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
||||
Êèðè÷êîâ Ì.À., |
DEVELOPING A
SMALL-SIZE FAMILY OF GAS TURBINE ENGINE BASED
ON SINGLE CORE |
ÑÒÂÎÐÅÍÍß Ñ²ÌÅÉÑÒÂÀ ÌÀËÎÐÎÇ̲ÐÍÈÕ
ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ ÍÀ ÁÀDz ªÄÈÍÎÃÎ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ |
ÑÎÇÄÀÍÈÅ
ÑÅÌÅÉÑÒÂÀ ÌÀËÎÐÀÇÌÅÐÍÛÕ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÍÀ ÁÀÇÅ ÅÄÈÍÎÃÎ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ |
37–41 |
Ëîÿí À.Â., |
INVESTIGATION
OF THERMAL FLUXES DISTRIBUTION IN THE CONSTRUCTION OF HEATERLESS HOLLOW
CATHODE FOR ELECTRIC PROPULSION IN OPERATING CURRENT RANGE UP TO |
ÄÎÑË²ÄÆÅÍÍß ÐÎÇÏÎIJËÓ ÒÅÏËÎÂÈÕ ÏÎÒÎʲÂ
Ó ÊÎÍÑÒÐÓÊÖ²¯ ÁÅÇÍÀÊÀËÜÍÎÃÎ ÏÎËÎÃÎ ÊÀÒÎÄÓ ÅÐÄ ÏÐÈ
ÐÎÁÎ×ÈÕ ÑÒÐÓÌÀÕ ÄÎ 50 À |
42–46 |
|
Âèíîãðàäîâ À.Ñ., |
CREATING OF
METHOD FOR SUPPORT SEAL AIRCRAFT ENGINE DESIGN WITH THE PARAMETERS OF OIL
SYSTEM |
ÐÎÇÐÎÁÊÀ ÌÅÒÎÄÈÊÈ ÏÐÎÅÊÒÓÂÀÍÍß
ÓÙ²ËÜÍÅÍÍß ÎÏÎÐÈ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓÍ²Â Ç ÓÐÀÕÓÂÀÍÍßÌ ÏÀÐÀÌÅÒв ÌÀÑËßÍί
ÑÈÑÒÅÌÈ |
47–50 |
|
Íîâèêîâ Ä.Ê., |
MODELLING OF THE SQUEEZED FILM DAMPER IN A FLUENT |
Ìîäåëþâàííÿ
ã³äðîäèíàì³÷íîãî äåìïôåðà â ïàêåò³ Fluent |
51–54 |
|
Âîðîáüåâ Þ.Ñ., |
Analysis of vibrations of gas turbine
compressor blading |
Àíàë³ç êîëèâàíü ëîïàòêîâîãî àïàðàòó êîìïðåñîðà ÃÒÄ |
55–59 |
|
Íàçàðåíêî Þ.Á. |
AVOIDANCE OF RESONANCE WITH
ROTOR'S CRITICAL REVOLUTION FREQUENCY IN CASE OF ELLIPTIC TRAJECTORY OF
BEARING SHAFT AXIS REVOLUTION ON SUPPORT BEARING |
ÓÑÓÍÅÍÍß ÐÅÇÎÍÀÍÑÓ ÍÀ
ÊÐÈÒÈ×ÍIÉ ×ÀÑÒÎÒI ÎÁÅÐÒÀÍÍß ÐÎÒÎÐI ÏÐÈ EËIÏÒÈ×ÍIÉ ÒÐÀªÊÒÎÐI¯ ÎÁÅÐÒÀÍÍß ÂIÑI
ÂÀËÓ ÍÀ ÎÏÎÐI |
60–65 |
|
Ôåäîð÷åíêî Ä.Ã., |
THE USE OF HOLOGRAPHIC INTERFEROMETRY FOR ROTATING
OBJECT VIBRATIONS STUDY |
ÇÀÑÒÎÑÓÂÀÍÍß ÃÎËÎÃÐÀÔ²×Íί
²ÍÒÅÐÔÅÐÎÌÅÒв¯ ÄËß ÄÎÑË²ÄÆÅÍÍß ÊÎËÈÂÀÍÜ ÎÁ’ªÊÒ²Â, ÙÎ ÎÁÅÐÒÀÞÒÜÑß |
ÏÐÈÌÅÍÅÍÈÅ
ÃÎËÎÃÐÀÔÈ×ÅÑÊÎÉ ÈÍÒÅÐÔÅÐÎÌÅÒÐÈÈ ÄËß ÈÑÑËÅÄÎÂÀÍÈß ÊÎËÅÁÀÍÈÉ ÂÐÀÙÀÞÙÈÕÑß
ÎÁÚÅÊÒÎÂ |
66–71 |
Êóëèêîâ Ã.Ã., |
CALCULATION OF SMALL PARAMETERS IN PROPELLERS CONTROL SYSTEM MODEL OF
TURBOFAN ENGINES |
ÓÐÀÕÓÂÀÍÍß ÌÀËÈÕ ÏÀÐÀÌÅÒв ÌÎÄÅ˲
ÑÈÑÒÅÌÈ ÓÏÐÀÂ˲ÍÍß ÃÂÈÍÒÎÂÅÍÒÈËßÒÎÐÀ ÒÃÂÄ |
Ó×ÅÒ ÌÀËÛÕ
ÏÀÐÀÌÅÒÐÎÂ ÌÎÄÅËÈ ÑÈÑÒÅÌÛ ÓÏÐÀÂËÅÍÈß ÂÈÍÒÎÂÅÍÒÈËßÒÎÐÀ ÒÂÂÄ |
72–81 |
Åïèôàíîâ Ñ.Â., |
SYNTHESIS AND ANALYSIS OF AN ADVANCED GAS TURBINE ENGINE CONTROL |
ÑÈÍÒÅÇ ² ÀÍÀË²Ç ÏÅÐÑÏÅÊÒÈÂÍί ÑÀÓ ÃÒÄ |
82–86 |
|
Ïàí³í Â.Â., |
ALGORITHMIC
MAINTENANCE OF A SYSTEM OF IDENTIFICATION PRESURGE (OF SURGE) PHENOMENA IN
COMPRESSORS AVIATION GTE |
ÀËÃÎÐÈÒÌÈ×ÅÑÊÎÅ ÎÁÅÑÏÅ×ÅÍÈÅ ÔÓÍÊÖÈÎÍÈÐÎÂÀÍÈß ÑÈÑÒÅÌÛ ÈÄÅÍÒÈÔÈÊÀÖÈÈ
ÏÐÅÄÏÎÌÏÀÆÍÛÕ (ÏÎÌÏÀÆÍÛÕ) ßÂËÅÍÈÉ Â ÊÎÌÏÐÅÑÑÎÐÀÕ ÀÂÈÀÖÈÎÍÍÛÕ ÃÒÄ |
87–91 |
|
Bradac M., |
MODEL BASED DESIGN APPLIED FOR DEVELOPMENT OF FUEL METERING
PUMP CONTROL ALGORITHM |
ÇÀÑÒÎÑÓÂÀÍÍß ÌÎÄÅËÜÍÎ-ÎвªÍÒÎÂÀÍÎÃÎ
ÏÐÎÅÊÒÓÂÀÍÍß ÄËß ÐÎÇÐÎÁÊÈ ÀËÃÎÐÈÒÌÓ ÓÏÐÀÂ˲ÍÍß ÍÀÑÎÑÎÌ-ÄÎÇÀÒÎÐÎÌ |
ÏÐÈÌÅÍÅÍÈÅ ÌÎÄÅËÜÍÎ-ÎÐÈÅÍÒÈÐÎÂÀÍÍÎÃÎ
ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÄËß ÐÀÇÐÀÁÎÒÊÈ ÀËÃÎÐÈÒÌÀ ÓÏÐÀÂËÅÍÈß ÍÀÑÎÑÎÌ-ÄÎÇÀÒÎÐÎÌ |
92–96 |
Ïàâëþê Å.Â., |
APPLICATION OF THE STEPPER DRIVE IN THE FUEL
METERING SYSTEMS DEVELOPED BY SE “KhADB” |
ÇÀÑÒÎÑÓÂÀÍÍß ÊÐÎÊÎÂÎÃÎ ÅËÅÊÒÐÎÏÐÈÂÎÄÓ Ó ÑÈÑÒÅÌÀÕ
ÄÎÇÓÂÀÍÍß ÏÀËÈÂÀ ÐÎÇÐÎÁÊÈ ÄÏ «ÕÀÊÁ» |
ÏÐÈÌÅÍÅÍÈÅ
ØÀÃÎÂÎÃÎ ÝËÅÊÒÐÎÏÐÈÂÎÄÀ Â ÑÈÑÒÅÌÀÕ ÄÎÇÈÐÎÂÀÍÈß ÒÎÏËÈÂÀ ÐÀÇÐÀÁÎÒÊÈ ÃÏ «ÕÀÊÁ» |
97–100 |
Ìåíÿéëîâ Å.Ñ., |
METHOD FOR DETERMINING THE LAW ON TILTGuide Vanes of multistage axial COMPRESSORS
UNDER UNCERTAINTY OF INPUT DATA |
ÌÅÒÎÄ
ÂÈÇÍÀ×ÅÍÍß ÇÀÊÎÍÓ ÐÅÃÓËÞÂÀÍÍß ÏÎÂÎÐÎÒÍÈÌÈ ÍÀÏÐÀÂËßÞ×ÈÌÈ ÀÏÀÐÀÒÀÌÈ
ÁÀÃÀÒÎÑÒÓϲÍ×ÀÑÒÎÃÎ ÎÑÜÎÂÎÃÎ ÊÎÌÏÐÅÑÎÐÀ  ÓÌÎÂÀÕ
ÍÅÂÈÇÍÀ×ÅÍÎÑÒ² ÂÕ²ÄÍÈÕ ÄÀÍÈÕ |
101–106 |
|
Òàðàñåíêî À.È., |
DETAILS OF
DIGITAL CONTROL FOR POWER PLANT GTE ON STARTING AND OPERATING MODES |
îñîáëèâîñò³
öèôðîâîãî ðåãóëþâàííÿ ÃÒÄ äëÿ åëåêòðîñòàíö³¿ íà ïóñêîâÈõ òà ðîáî÷èõ ðåæèìàõ |
ÎÑÎÁÅÍÍÎÑÒÈ
ÖÈÔÐÎÂÎÃÎ ÐÅÃÓËÈÐÎÂÀÍÈß ÃÒÄ ÄËß ÝËÅÊÒÐÎÑÒÀÍÖÈÈ ÍÀ ÏÓÑÊÎÂÛÕ È ÐÀÁÎ×ÈÕ ÐÅÆÈÌÀÕ |
107–111 |
Kasianov V.A., |
ÎÏÒÈÌÀËÜÍÎ
ÊÅÐÎÂÀͲ ÑÓÁ’ªÊÒÈÂÍÎ ÏÅÐÅÂÀÆÍ² ÐÅÆÈÌÈ ÅÊÑÏËÓÀÒÀÖ²¯ ÃÎÐÈÇÎÍÒÀËÜÍÎÃÎ ÏÎËÜÎÒÓ
˲ÒÀÊÀ ÌÀÊÑÈÌÀËÜÍί ÒÐÈÂÀËÎÑÒ² |
ÎÏÒÈÌÀËÜÍÎ ÓÏÐÀÂËßÅÌÛÅ ÑÓÁÚÅÊÒÈÂÍÎ
ÏÐÅÄÏÎ×ÈÒÀÅÌÛÅ ÐÅÆÈÌÛ ÝÊÑÏËÓÀÒÀÖÈÈ ÃÎÐÈÇÎÍÒÀËÜÍÎÃÎ ÏÎËÅÒÀ ÑÀÌÎËÅÒÀ ÌÀÊÑÈÌÀËÜÍÎÉ
ÏÐÎÄÎËÆÈÒÅËÜÍÎÑÒÈ |
112–117 |
|
Ìèðãîðîä Â.Ô., |
ACCURACY EVALUATION OF GTE PIECE
WISE-LINEAR DYNAMIC MODELS |
ÎÖ²ÍÊÀ
ÒÎ×ÍÎÑÒ² ÊÓÑÊÎÂÎ-˲ͲÉÍÈÕ ÄÈÍÀ̲×ÍÈÕ ÌÎÄÅËÅÉ ÃÒÄ |
118–121 |
|
Õîðÿê Í.Â., |
PARAMETRIC IDENTIFICATION OF A MATHEMATICAL MODEL OF THE LOW-FREQUENCY DYNAMICS PUMPS OF LIQUID ROCKET
ENGINES |
ÏÀÐÀÌÅÒÐÈ×íà ²ÄÅÍÒÈÔ²ÊÀÖ²ß ìàòåìàòè÷Íί ìîäåë²
ÍÈÇÜÊÎ×ÀÑÒÎÒÍί äèíàì²êè øíåêî²ÄÖÅÍÒÐÎÂÈÕ íàñîñ²Â вÄÈÍÍÈÕ ÐÀÊÅÒÍÈÕ ÄÂÈÃÓͲ |
122–127 |
|
Åïèôàíîâ Ñ.Â., |
OVERVIEW OF
METHODS FOR SYNTHESIZING MATHEMATICAL MODELS OF GAS TURBINE ENGINES AT
SUB-IDLE MODES |
Àíàë³ç ÌÅÒÎÄÈÊ ÑÈÍÒÅÇÓ ÌÀÒÅÌÀÒÈ×ÍÈÕ
ÌÎÄÅËÅÉ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ ÍÀ ÅÒÀϲ ÇÀÏÓÑÊÓ |
ÀÍÀËÈÇ ÌÅÒÎÄÈÊ
ÑÈÍÒÅÇÀ ÌÀÒÅÌÀÒÈ×ÅÑÊÈÕ ÌÎÄÅËÅÉ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÍÀ ÝÒÀÏÅ ÇÀÏÓÑÊÀ |
128–135 |
Áàõìåò ß.Ã. |
BuilDING FLOW CHaracteristic of flow controller LJE |
ÏÎÁÓÄÎÂÀ
âèòðàòíî¿ õàðàêòåðèñòèêè ðåãóëÿòîð³â âèòðàò ÆÐÄ |
136–140 |
|
Àíòîíîâ À.Î., |
MODERN METHODS
OF DIAGNOSIS AND CONTROL OF GAS TURBINE AIRCRAFT ENGINES |
ÑÓ×ÀÑͲ ÌÅÒÎÄÈ ÊÎÍÒÐÎËÞ ÒÀ
IJÀÃÍÎÑÒÓÂÀÍÍß ÃÀÇÎÒÓÐÁ²ÍÍÈÕ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲ |
ÑÎÂÐÅÌÅÍÍÛÅ
ÌÅÒÎÄÛ ÊÎÍÒÐÎËß È ÄÈÀÃÍÎÑÒÈÊÈ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ |
141–145 |
Åïèôàíîâ Ñ.Â., |
ON-GROUND AUTOMATED
DIAGNOSIS COMPLEX FOR TURBOFAN |
ÍÀÇÅÌÍÈÉ ÀÂÒÎÌÀÒÈÇÎÂÀÍÈÉ ÊÎÌÏËÅÊÑ
IJÀÃÍÎÑÒÈÊÈ ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÎÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÓÍÀ |
ÍÀÇÅÌÍÛÉ
ÀÂÒÎÌÀÒÈÇÈÐÎÂÀÍÍÛÉ ÊÎÌÏËÅÊÑ ÄÈÀÃÍÎÑÒÈÊÈ ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÓÕÊÎÍÒÓÐÍÎÃÎ
ÄÂÈÃÀÒÅËß |
146–153 |
Ìàðöåíþê Å.Â., |
CHOOSING OPTIMAL MODEL OF TEMPERATURE AT COMPRESSOR DISCHARGE
SIMULATING FOR MONITORING LIFETIME EXHAUSTION OF MAIN PARTS OF THREE-SPOOL
TFE |
ÂÈÁ²Ð ÌÎÄÅ˲ ÄËß ÂÈÇÍÀ×ÅÍÍß
ÒÅÌÏÅÐÀÒÓÐÈ ÇÀ ÊÎÌÏÐÅÑÎÐÎÌ ÏÐÈ ÌÎͲÒÎÐÈÍDz ÂÈ×ÅÐÏÀÍÍß ÐÅÑÓÐÑÓ ÎÑÍÎÂÍÈÕ
ÄÅÒÀËÅÉ ÒÐÜÎÕÂÀËÜÍÎÃÎ ÒÐÄÄ |
154–160 |
|
Âàðáàíåö Ð.À., |
ÂËÈßÍÈÅ
ÑÈÑÒÅÌÛ VIT ÍÀ ÕÀÐÀÊÒÅÐ ÐÀÁÎ×ÅÃÎ ÏÐÎÖÅÑÑÀ ÌÀËÎÎÁÎÐÎÒÍÛÕ ÄÈÇÅËÅÉ MAN-B&W ÑÅÐÈÈ MC |
ÂÏËÈÂ ÑÈÑÒÅÌÛ
VIT ÍÀ ÕÀÐÀÊÒÅÐ ÐÎÁÎ×ÎÃÎ ÏÐÎÖÅÑÓ ÌÀËÎÎÁÅÐÒÎÂÈÕ ÄÈÇÅ˲ MAN-B&W ÑÅв¯ MC |
ÂËÈßÍÈÅ ÑÈÑÒÅÌÛ
VIT ÍÀ ÕÀÐÀÊÒÅÐ ÐÀÁÎ×ÅÃÎ ÏÐÎÖÅÑÑÀ ÌÀËÎÎÁÎÐÎÒÍÛÕ ÄÈÇÅËÅÉ MAN B&W ÑÅÐÈÈ MC |
161–165 |
Çàðåìáà Ý.Â., |
RESEARCH OF
VIBRATION CHARACTERISTICS OF ENGINE D-436TP FAN ON BE-200ES AMPHIBIAN IN
ICING CONDITIONS |
ÄÎÑË²ÄÆÅÍÍß Â²ÁÐÀÖ²ÉÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ
ÂÅÍÒÈËßÒÎÐÀ ÄÂÈÃÓÍÀ Ä-436òï ÍÀ ˲ÒÀÊÓ-ÀÌÔ²Á²¯ ÁÅ-200×Ñ Ï³ä ÷àñ ÎÁÌÅÐÇÀÍÍß |
166–170 |
|
Áóðàó Í.È., |
DEVELOPMENT
AND INVESTIGATION OF THE DIGITAL TRACKING FILTERS FOR THE VIBRATION CONTROL SYSTEM OF AVIATION ENGINE
AT TE NON-STEADY-STATE MODES |
ÐÎÇÐÎÁÊÀ ÒÀ ÄÎÑË²ÄÆÅÍÍß
ÖÈÔÐÎÂÈÕ Ñ˲ÄÊÓÞ×ÈÕ Ô²ËÜÒв ÄËß ÑÈÑÒÅÌÈ ÊÎÍÒÐÎËÞ Â²ÁÐÀÖ²¯ À²ÀÖ²ÉÍÎÃÎ
ÄÂÈÃÓÍÀ ÍÀ ÍÅÑÒÀÖ²ÎÍÀÐÍÈÕ
ÐÅÆÈÌÀÕ |
171–176 |
|
Þð Ò.Â., |
MODEL FOR EVALUATION OF GAS-TURBINE ENGINE ELEMENTS TECHNICAL STATE BY VIBRATION PARAMETERS BASED ON WAVELET-TRANSFOR |
ÌÎÄÅËÜ ÎÖÅÍÊÈ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÑÎÑÒÎßÍÈß
ÓÇËÎÂ ÃÒÄ ÏÎ ÏÀÐÀÌÅÒÐÀÌ ÂÈÁÐÀÖÈÈ Ñ ÏÐÈÌÅÍÅÍÈÅÌ
ÂÅÉÂËÅÒ-ÏÐÅÎÁÐÀÇÎÂÀÍÈß |
177–182 |
|
Øóëüæåíêî Í.Ã., |
APPLICATION OF METHODS AND MEANS OF VIBRATION DIAGNOSTICS FOR THE
ESTIMATION OF RELIABILITY OF WORK OF TURBINE SETS |
ÇÀÑÒÎÑÓÂÀÍÍß ÌÅÒÎIJ ² ÇÀÑÎÁ²Â ²ÁÐÎIJÀÃÍÎÑÒÈÊÈ
ÄËß ÎÖ²ÍÊÈ ÍÀIJÉÍÎÑÒ² ÐÎÁÎÒÈ ÒÓÐÁÎÀÃÐÅÃÀҲ |
ÏÐÈÌÅÍÅÍÈÅ
ÌÅÒÎÄÎÂ È ÑÐÅÄÑÒÂ ÂÈÁÐÎÄÈÀÃÍÎÑÒÈÊÈ ÄËß ÎÖÅÍÊÈ ÍÀÄÅÆÍÎÑÒÈ ÐÀÁÎÒÛ
ÒÓÐÁÎÀÃÐÅÃÀÒÎÂ |
183–188 |
Ðåçíèê Ñ.Á., |
SETTLEMENT AND EXPERIMENTAL EVALUATION different types of labyrinth
seals |
ÐÎÇÐÀÕÓÍÊÎÂÎ-ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÀ
ÎÖ²ÍÊÀ ÅÔÅÊÒÈÂÍÎÑÒ² вÇÍÈÕ ÒÈϲ ËÀÁ²ÐÈÍÒÎÂÈÕ ÓÙ²ËÜÍÅÍÜ |
ÐÀÑרÒÍÎ-ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÀß
ÎÖÅÍÊÀ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÐÀÇËÈ×ÍÛÕ ÒÈÏΠËÀÁÈÐÈÍÒÍÛÕ ÓÏËÎÒÍÅÍÈÉ |
189–193 |
Èíôîðìàöèîííûå òåõíîëîãèè |
||||
Äàíîâ À.Ñ. |
INFORMATION ENERGY
APPROACH TO PROJECTION PROBLEM |
²ÍÔÎÐÌÀÖ²ÉÍÎ-ÅÍÅÐÃÅÒÈ×ÍÈÉ Ï²ÄÕ²Ä ÄÎ ÏÐÎÁËÅÌÈ ÏÐÎÅÊÒÓÂÀÍÍß |
ÈÍÔÎÐÌÀÖÈÎÍÍÎ-ÝÍÅÐÃÅÒÈ×ÅÑÊÈÉ
ÏÎÄÕÎÄ Ê ÏÐÎÁËÅÌÅ ÏÐÎÅÊÒÈÐÎÂÀÍÈß |
194–198 |
Ëåùåíêî Þ.Ï. |
INTELLECTUAL CONTROL SYSTEM BY MEASURING ROBOT |
ÈÍÒÅËËÅÊÒÓÀËÜÍàÿ
ÑÈÑÒÅÌà ÓÏÐÀÂËÅÍÈß ÈÇÌÅÐÈÒÅËÜÍÛÌ ÐÎÁÎÒÎÌ |
199–202 |
|
Òàìàðãàç³í Î.À., |
CORRELATION FUNCTIONS OF THE NUMBER OF APPLICATIONS FOR ELIMINATION OF
DAMAGES OF POWER PLANTS IN THE OPERATIONAL MAINTENANCE |
ÊÎÐÐÅËßÖÈÎÍÍÛÅ ÔÓÍÊÖÈÈ ÊÎËÈ×ÅÑÒÂÀ
ÇÀßÂÎÊ ÍÀ ÓÑÒÐÀÍÅÍÈÅ ÏÎÂÐÅÆÄÅÍÈÉ ÑÈËÎÂÛÕ ÓÑÒÀÍÎÂÎÊ Â ÏÐÎÖÅÑÑÅ ÎÏÅÐÀÒÈÂÍÎÃÎ
ÒÅÕÍÈ×ÅÑÊÎÃÎ ÎÁÑËÓÆÈÂÀÍÈß |
203–207 |
|
ßêóøåíêî Î.Ñ., |
THE AUTOMATED MONITORING OF RELIABILITY IN AIRLINE |
ÀÂÒÎÌÀÒÈÇÈÐÎÂÀÍÍÛÉ ÌÎÍÈÒÎÐÈÍÃ
ÍÀÄÅÆÍÎÑÒÈ ÍÀ ÓÐÎÂÍÅ ÀÂÈÀÊÎÌÏÀÍÈÈ |
208–213 |
|
Ðåâà Î.Ì., |
FUZZY
MODEL OF AIR TRAFFIC CONTROLLERS ATTITUDE TO THE RISK OF POTENTIAL CONFLICTS
SITUATION APPEARANCE |
ÍÅײÒÊÀ ÌÎÄÅËÜ
ÑÒÀÂËÅÍÍß À²ÀÄÈÑÏÅÒ×ÅÐÀ ÄÎ ÐÈÇÈÊÓ ÍÀÑÒÀÍÍß ÏÎÒÅÍÖ²ÉÍÎ-ÊÎÍÔ˲ÊÒÍί ÑÈÒÓÀÖ²¯ |
ÍÅ×ÅÒÊÀß ÌÎÄÅËÜ ÎÒÍÎØÅÍÈß
ÀÂÈÀÄÈÑÏÅÒ×ÅÐÀ Ê ÐÈÑÊÓ ÍÀÑÒÓÏËÅÍÈß ÏÎÒÅÍÖÈÀËÜÍÎ ÊÎÍÔËÈÊÒÍÎÉ ÑÈÒÓÀÖÈÈ |
214–221 |
Õîìÿê Î.Â. |
ASSESSMENT OF LOSS IN RADIO PROPAGATION MODEL FOR POINT-TO-POINT FOR
REFLECTION FROM LOCAL ITEMS |
ÎÖÅÍÊÀ ÏÎÒÅÐÜ ÐÀÄÈÎÑÈÃÍÀËÀ ÏÐÈ ÐÀÑÏÐÎÑÒÐÀÍÅÍÈÈ Â ÌÎÄÅËÈ POINT-TO-POINT ÇÀ Ñ×ÅÒ ÎÒÐÀÆÅÍÈß
ÎÒ ÌÅÑÒÍÛÕ ÏÐÅÄÌÅÒÎÂ |
222–225 |
|
Áóòåíêî Þ.È. |
METHOD MACHINE
PROCESSING LANGUAGE UNITS IN THE CLASS «LANGUAGE SOFTWARE STANDARDS» |
ÌÅÒÎÄÈÊÀ ÌÀØÈÍÍί ÎÁÐÎÁÊÈ Ë²ÍòÑÒÈ×ÍÈÕ
ÎÄÈÍÈÖÜ ÊËÀÑÓ «ÌÎÂÀ ÑÒÀÍÄÀÐҲ ÏÐÎÃÐÀÌÍÎÃÎ ÇÀÁÅÇÏÅ×ÅÍÍß» |
ÌÅÒÎÄÈÊÀ ÌÀØÈÍÍÎÉ
ÎÁÐÀÁÎÒÊÈ ËÈÍÃÂÈÑÒÈ×ÅÑÊÈÕ ÅÄÈÍÈÖ ÊËÀÑÑÀ «ßÇÛÊ ÑÒÀÍÄÀÐÒΠÏÐÎÃÐÀÌÌÍÎÃÎ
ÎÁÅÑÏÅ×ÅÍÈß» |
226–230 |
Øóëüã³í Â.À. |
INDISTINCT
ENTHROPY AS A MEASURE OF PILOTING PRECISION APPRAISAL DISTINCTION, MADE BY
PILOTS |
ÍÅײÒÊÀ ÅÍÒÐÎÏ²ß ßÊ
̲ÐÀ ÐÎÇϲÇÍÀÂÀÍÍß Ï²ËÎÒÀÌÈ ÎÖ²ÍÎÊ ÒÎ×ÍÎÑÒ² ϲËÎÒÓÂÀÍÍß |
ÍÅ×ÅÒÊÀß
ÝÍÒÐÎÏÈß ÊÀÊ ÌÅÐÀ ÐÀÑÏÎÇÍÀÂÀÍÈß ÏÈËÎÒÀÌÈ ÎÖÅÍÎÊ ÒÎ×ÍÎÑÒÈ ÏÈËÎÒÈÐÎÂÀÍÈß |
231–235 |
Êó÷óê Ã.À. |
MULTISERVICE NETWORK SECTION TRAFFIC IS
CONTROLLED |
ÓÏÐÀÂËÅÍÈÅ
ÒÐÀÔÈÊÎÌ ÇÂÅÍÀ ÌÓËÜÒÈÑÅÐÂÈÑÍÎÉ ÑÅÒÈ |
236–239 |
|
Ðåâà Â.Ñ., |
DEFINITION OF THE OFF-NOMINAL SITUATIONS AND METHODS OF THEIR
MANAGEMENT AT THE STAGES OF GROUND COMPLEX POWER-SUPPLY SYSTEMS OPERATION |
ÂÈÇÍÀ×ÅÍÍß ÍÅØÒÀÒÍÈÕ ÑÈÒÓÀÖ²É ÒÀ
ÌÅÒÎIJ ¯Õ ÓÑÓÍÅÍÍß ÍÀ ÅÒÀÏÀÕ ÅÊÑÏËÓÀÒÀÖ²¯ ÑÈÑÒÅÌ ÅËÅÊÒÐÎÏÎÑÒÀ×ÀÍÍß ÍÀÇÅÌÍÎÃÎ
ÊÎÌÏËÅÊÑÓ |
240–243 |
|
Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè
ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè |
||||
Âîëêîâ Ä.È., |
CALLS OF
THE MARKET. THE DEVELOPMENT STRATEGY OF THE AVIONICS ENTERPRISE |
ÂÈÊËÈÊÈ ÐÈÍÊÓ. ÑÒÐÀÒÅòß
ÐÎÇÂÈÒÊÓ Ï²ÄÏÐȪÌÑÒÂÀ-ÐÎÇÐÎÁÍÈÊÀ À²ÀÖ²ÉÍί
ÅËÅÊÒÐÎͲÊÈ |
ÂÛÇÎÂÛ ÐÛÍÊÀ.
ÑÒÐÀÒÅÃÈß ÐÀÇÂÈÒÈß ÏÐÅÄÏÐÈßÒÈß-ÐÀÇÐÀÁÎÒ×ÈÊÀ ÀÂÈÀÖÈÎÍÍÎÉ ÝËÅÊÒÐÎÍÈÊÈ |
244–248 |
Äàâèäåíêî Â.Î. |
INFORMATION
TECHNOLOGY OF SUPPORT OF DECISION-MAKING ON POPULATION EVACUATION FROM THE
ZONE OF EMERGENCY SITUATIONS OF ANTHROPOGENIC CHARACTER |
²ÍÔÎÐÌÀÖ²ÉÍÀ
ÒÅÕÍÎËÎÃ²ß Ï²ÄÒÐÈÌÊÈ ÏÐÈÉÍßÒÒß Ð²ØÅÍÜ Ç ÅÂÀÊÓÀÖ²¯ ÍÀÑÅËÅÍÍß ²Ç ÇÎÍÈ
íàäçâè÷àéíèõ ñèòóàö³é òåõíîãåííîãî õàðàêòåðó |
249–253 |
|
Ïîòàïîâà Ì.Â. |
INFORMATION
TECHNOLOGY OF SCHEDULING IN CASE OF PORTFOLIO MANAGEMENT OF ORDERS OF THE IT
COMPANY IN THE CONDITIONS OF UNCERTAINTY |
²ÍÔÎÐÌÀÖ²ÉÍÀ ÒÅÕÍÎËÎÃ²ß ÊÀËÅÍÄÀÐÍÎÃÎ
ÏËÀÍÓÂÀÍÍß ÏÐÈ ÓÏÐÀÂ˲ÍͲ ÏÎÐÒÔÅËÅÌ ÇÀÌÎÂËÅÍÜ IT-ÊÎÌÏÀͲ¯  ÓÌÎÂÀÕ
ÍÅÂÈÇÍÀ×ÅÍÎÑÒ² |
254–258 |
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 íàóêîìåòðè÷åñêèå áàçû äàííûõ: íàó÷íîé ýëåêòðîííîé
áèáëèîòåêè eLIBRARY.RU (Ðîññèéñêàÿ Ôåäåðàöèÿ); Index Copernicus (Ïîëüøà);
Google Scholar.