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 |
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 |
Ñîðîêèí Â.Ô., |
COMPARISON OF KINEMATICAL PARAMETERS OF MOVEMENT AT
path MODELING of HIGH-SPEED CNC processing WITH cubic AND quintic SPLINES |
ÏÎвÂÍßÍÍß
ʲÍÅÌÀÒÈ×ÍÈÕ ÏÀÐÀÌÅÒв ÐÓÕÓ ÏÐÈ ÌÎÄÅËÞÂÀÍͲ ÒÐÀªÊÒÎв¯ ÂÈÑÎÊÎØÂÈÄʲÑÍί ×ÏÊ ÎÁÐÎÁÊÈ
ÑÏËÀÉÍÀÌÈ ÒÐÅÒÜÎÃÎ òà Ï'ßÒÎÃÎ ÑÒÓÏÅÍß |
11–17 |
|
Ïëàíêîâñêèé Ñ.È., |
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 |
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˲ |
25–30 |
|
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
||||
Êðàâ÷åíêî È.Ô., |
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 |
31–37 |
|
Ñåðãèåíêî Ð.Â., |
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 |
38–42 |
|
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 |
Ñîðîãèí Ô.Ã., |
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 |
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 ÒÐÀÅÊÒÎÐÍÎÃÎ
ϲÄÕÎÄÓ |
52–55 |
|
Åðøîâ Ñ.Â., |
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 |
Ãåðàñèìåíêî Â.Ï., |
COMPUTATIONAL AND EXPERIMENTAL STUDY OF COMPRESSOR VANES GASDYNAMIC
CHARACTERISTICS IN MULTISTAGE COMPRESSOR |
ÐÎÇÐÀÕÓÍÊÎÂÎ-ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ
ÄÎÑË²ÄÆÅÍÍß ÃÀÇÎÄÈÍÀ̲×ÍÈÕ
ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÊÎÌÏÐÅÑÎÐÍÈÕ ÐÅØ²ÒÎÊ Ó ÑÈÑÒÅ̲ ÁÀÃÀÒÎÑÒÓÏÅÍÅÂÎÃÎ ÊÎÌÏÐÅÑÎÐÀ |
61–66 |
|
Ðóñàíîâ À.Â., |
DESIGN METHOD OF HIGH-PERFORMANCE SETTINGS FOR TURBINE EXPANSION ENGINE |
ÌÅÒÎÄ
ÏÐÎÅÊÒÓÂÀÍÍß ÂÈÑÎÊÎÅÔÅÊÒÈÂÍÈÕ ÏÐÎÒÎ×ÍÈÕ ×ÀÑÒÈÍ ÒÓÐÁÎÄÅÒÀÍÄÅÐÍÈÕ ÀÃÐÅÃÀҲ |
ÌÅÒÎÄ
ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÂÛÑÎÊÎÝÔÔÅÊÒÈÂÍÛÕ ÏÐÎÒÎ×ÍÛÕ ×ÀÑÒÅÉ ÒÓÐÁÎÄÅÒÀÍÄÅÐÍÛÕ ÀÃÐÅÃÀÒΠ|
67–72 |
Äîëìàòîâ Ä.À., |
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 |
Êîñòþê Â.Å., |
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 |
79–85 |
|
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 |
86–89 |
|
Âèíîãðàäîâ À.Ñ., |
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 |
90–93 |
|
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 |
Ñàëîâ Í.Í., |
CALCULATION OF
NONSTATIONARY THERMAL CONDITION OF AIRCRAFT
ENGINE AXIAL COMPRESSORS ROTOR DISCS |
ÐÎÇÐÀÕÓÍÎÊ ÍÅÑÒÀÖ²ÎÍÀÐÍÎÃÎ ÒÅÏËÎÂÎÃÎ
ÑÒÀÍÓ ÄÈÑʲ ÐÎÒÎв ÎÑÜÎÂÈÕ ÊÎÌÏÐÅÑÎв À²ÀÄÂÈÃÓͲ |
ÐÀÑ×ÅÒ
ÍÅÑÒÀÖÈÎÍÀÐÍÎÃÎ ÒÅÏËÎÂÎÃÎ ÑÎÑÒÎßÍÈß ÄÈÑÊΠÐÎÒÎÐΠÎÑÅÂÛÕ ÊÎÌÏÐÅÑÑÎÐÎÂ
ÀÂÈÀÄÂÈÃÀÒÅËÅÉ |
101–103 |
Àë¸õèíà Ñ.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 ÝËÅÌÅÍÒÎÂ ÏÀÐÎÂÛÕ ÒÓÐÁÈÍ |
104–108 |
Èñàåâ Ê.Á., |
INFLUENCE OF
SOME FACTORS ON THE DETERMINATION OF THERMAL CONDUCTIVITY OF COATINGS |
ÂÏËÈ ÄÅßÊÈÕ
ÔÀÊÒÎв ÍÀ ÂÈÇÍÀ×ÅÍÍß ÒÅÏËÎÏÐβÄÍÎÑÒ² ÏÎÊÐÈÒҲ |
ÂËÈßÍÈÅ ÍÅÊÎÒÎÐÛÕ
ÔÀÊÒÎÐÎÂ ÍÀ ÎÏÐÅÄÅËÅÍÈÅ ÒÅÏËÎÏÐÎÂÎÄÍÎÑÒÈ ÏÎÊÐÛÒÈÉ |
109–113 |
Ãðóáîé À.Ï., |
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 |
114–118 |
|
Ãðèãîðüåâ Î.Í., |
Ultra high temperature ceramics For aerospace technics |
Óëüòðàâèñîêîòåìïåðàòóðíà
êåðàì³êà äëÿ À²ÀÖ²ÉÍÎ-ÊÎÑ̲×Íί òåõí³êè |
ÓËÜÒÐÀÂÛÑÎÊÎÒÅÌÏÅÐÀÒÓÐÍÀß
ÊÅÐÀÌÈÊÀ ÄËß ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÎÉ ÒÅÕÍÈÊÈ |
119–128 |
Ãîëóá Â.Ï., |
ON THE PROBLEM
OF THE FATIGUE LIFE-TIME CALCULATION OF PRISMATIC RODS UNDER ASYMMETRIC BENDING AND TORSION |
ÄÎ
ÇÀÄÀײ ÐÎÇÐÀÕÓÍÊÓ
ÄÎÂÃβ×ÍÎÑÒ² ÏÐÈÇÌÀÒÈ×ÍÈÕ ÑÒÅÐÆÍ²Â ÂÍÀÑ˲ÄÎÊ ÂÒÎÌÈ ÇÀ
ÓÌΠÀÑÈÌÅÒÐÈ×ÍÎÃÎ ÇÃÈÍÓ ÒÀ
ÑÊÐÓ×ÅÍÍß |
129–134 |
|
Ôåðíàòè Ï.Â., |
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 |
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 |
Íåæâåäèëîâ À.Þ. |
EVALUATION OF THE INFLUENCE
OF TEMPERATURE UP TO |
ÎÖÅÍÊÀ ÂËÈßÍÈß ÒÅÌÏÅÐÀÒÓÐÛ
ÄÎ 640 °Ñ ÍÀ
ÖÈÊËÈ×ÅÑÊÓÞ ÏÐÎ×ÍÎÑÒÜ |
145–148 |
|
Áèáëèê È.Â., |
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 |
Äîðîøåíêî Å.Þ., |
METHOD OF STUDY ON DISTRIBUTION OF
RESIDUAL MICROSURFACE
LAYER CLAD
ALUMINUM DESIGNS |
ÌÅÒÎÄÈÊÀ ÄÎÑË²ÄÆÅÍÍß ÐÎÇÏÎIJËÓ
ÇÀËÈØÊÎÂÈÕ Ì²ÊÐÎÄÅÔÎÐÌÀÖ²É ÍÀ ÏÎÂÅÐÕͲ ÏËÀÊÎÂÀÍÎÃÎ ØÀÐÓ ÀËÞ̲ͲªÂÈÕ ÇÐÀÇʲ |
154–159 |
|
Øóëüæåíêî Í.Ã., |
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 |
160–164 |
|
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 |
165–168 |
|
Ãóñåâ Þ.À., |
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 |
Ïðèäîðîæíûé Ð.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
вÇÍÎÃΠвÂÍß |
ÐÀÑ×ÅÒÍÎÅ
ÈÑÑËÅÄÎÂÀÍÈÅ ÂËÈßÍÈß ÏÀÐÀÌÅÒÐΠÏÅÐÔÎÐÀÖÈÎÍÍÛÕ ÎÒÂÅÐÑÒÈÉ ÎÕËÀÆÄÀÅÌÎÉ ÐÀÁÎ×ÅÉ
ËÎÏÀÒÊÈ ÒÓÐÁÈÍÛ ÂÛÑÎÊÎÃÎ ÄÀÂËÅÍÈß ÍÀ ÅÅ ÍÀÏÐ߯ÅÍÍÎÅ ÑÎÑÒÎßÍÈÅ È ÄÎËÃÎÂÅ×ÍÎÑÒÜ |
173–177 |
Ìåäâåäîâñêàÿ Ò.Ô., |
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 |
Ëàïîòêî Â.Ì., |
METHOD OF NUMERICAL ASSESSMENT OF TONAL NOISE IN SOURCE AT UNSTATIONARY INTERACTION
OF TURBOMACHINARY RIMS |
ÌÅÒÎÄ ×ÈÑÅËÜÍί ÎÖ²ÍÊÈ Ð²ÂÍß ÒÎÍÀËÜÍÎÃÎ ØÓÌÓ Ó ÄÆÅÐÅ˲ ÏÐÈ ÍÅÑÒÀÖ²ÎÍÀÐͲÉ
ÂÇÀªÌÎIJ¯ ²Íֲ ÒÓÐÁÎÌÀØÈÍ |
184–189 |
|
Êóäèí Ì.Ì., |
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 |
Âîðîáüåâ Þ.Ñ., |
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 |
Ìåëüíèê Â.Ì., |
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 |
Òêà÷ Ì.Ð., |
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¯ |
203–207 |
|
Áîíäàð÷óê Ï.Â., |
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 |
Öàãëîâ À.È., |
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 |
Èíôîðìàöèîííûå òåõíîëîãèè |
||||
Áàõòèÿðîâ Ä.Â., |
CONTROL OF
VARIATIONS IN KEY CHARACTERISTICS OF ASSEMBLY UNITS, PARTS AND PROCESSES |
ÓÏÐÀÂ˲ÍÍß Ç̲ÍÀÌÈ ÊËÞ×ÎÂÈÕ
ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÑÊËÀÄÀËÜÍÈÕ ÎÄÈÍÈÖÜ, ÄÅÒÀËÅÉ ² ÏÐÎÖÅѲ |
ÓÏÐÀÂËÅÍÈÅ
ÈÇÌÅÍÅÍÈßÌÈ ÊËÞ×ÅÂÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÑÁÎÐÎ×ÍÛÕ ÅÄÈÍÈÖ, ÄÅÒÀËÅÉ È ÏÐÎÖÅÑÑΠ|
219–222 |
Âîëêîâ Ä.È., |
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 |
Ïàí³í Â.Â., |
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 |
Åïèôàíîâ Ñ.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 |
Ìèðîãîðîä Â.Ô., |
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 ÐßÄΠÂ
ÇÀÄÀ×ÀÕ ÎÖÅÍÊÈ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÑÎÑÒÎßÍÈß |
241–245 |
Êóçíåöîâà Þ.À., |
THE
VISUALIZATION OF CONTROLLING ALGORITHM TRACK IN THE SYSTEMS OF AUTOMATION
TESTS OF AIRCRAFT ENGINES |
²ÇÓÀ˲ÇÀÖ²ß ÒÐÀÑÈ ÊÅÐÓÞ×ÎÃÎ ÀËÃÎÐÈÒÌÓ
 ÑÈÑÒÅÌÀÕ ÀÂÒÎÌÀÒÈÇÀÖ²¯
ÂÈÏÐÎÁÓÂÀÍÜ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲ |
ÂÈÇÓÀËÈÇÀÖÈß
ÒÐÀÑÑÛ ÓÏÐÀÂËßÞÙÅÃÎ ÀËÃÎÐÈÒÌÀ Â ÑÈÑÒÅÌÀÕ ÀÂÒÎÌÀÒÈÇÀÖÈÈ ÈÑÏÛÒÀÍÈÉ ÀÂÈÀÖÈÎÍÍÛÕ
ÄÂÈÃÀÒÅËÅÉ |
246–252 |
Íåâåøêèí Þ.À., |
MODELING OF
PULSE FORMING PROCESSES |
ÌÎÄÅËÞÂÀÍÍß ÏÐÎÖÅѲ ²ÌÏÓËÜÑÍÎÃÎ
ÎÁ’ªÌÍÎÃÎ ØÒÀÌÏÓÂÀÍÍß |
253–256 |
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).