Íàöèîíàëüíûé
àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé
èíñòèòóò”
ISSN
1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ²
ÒÅÕÍÎËÎòß. – 2013. – ¹ 9(106). – 286 ñ.
ISSN
1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2013. – ¹ 9(106). –
286 ñ.
ISSN 1727-7337. AEROSPACE TECHNIC AND
TECHNOLOGY. – 2013. – ¹ 9(106). – 286 ñ.
ÑÒÀÒÜè (articleS)
Àâòîðû |
Íàçâàíèå ñòàòüè
(article title) |
Ñòðàíèöû (pages) |
||
English |
Óêðà¿íñüêà
ìîâà |
Ðóññêèé
ÿçûê |
||
Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ |
||||
Ñîðîêèí Â.Ô., |
METHOD OF
DIRECT STABILIZATION OF CONTOUR FEEDRATE FOR THE SPLINE INTERPOLATOR CNC SYSTEM |
ÌÅÒÎÄ
ÏÐßÌί ÑÒÀÁ²Ë²ÇÀÖ²¯ ÊÎÍÒÓÐÍί ØÂÈÄÊÎÑÒ² ÄËß ÑÏËÀÉÍÎÂîÃÎ
²ÍÒÅÐÏÎËßÒÎÐà ÑÈÑÒÅÌè ×ÏÓ |
ÌÅÒÎÄ ÏÐßÌÎÉ ÑÒÀÁÈËÈÇÀÖÈÈ ÊÎÍÒÓÐÍÎÉ ÑÊÎÐÎÑÒÈ ÄËß
ÑÏËÀÉÍÎÂÎÃÎ ÈÍÒÅÐÏÎËßÒÎÐÀ ÑÈÑÒÅÌÛ ×ÏÓ |
7–13 |
Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ
àïïàðàòîâ |
||||
Çàäîíöåâ Â.À. |
HERO OF
SOCIALISTIC LABOR IVAN IVANOVYCH IVANOV (1918-1999) –
THE FIRST CHIEF DESIGNER OF ENGINE DESIGN OFFICE KB-4 OF OKB-586
/ YUZHNOYE DESIGN BUREAU |
ÃÅÐÎÉ ÑÎÖ²À˲ÑÒÈ×Íί ÏÐÀÖ² ²ÂÀÍ
²ÂÀÍÎÂÈ× ²ÂÀÍΠ(1918-1999) – ÏÅÐØÈÉ ÃÎËÎÂÍÈÉ
ÊÎÍÑÒÐÓÊÒÎÐ ÄÂÈÃÓÍÍÎÃÎ ÊÁ-4 ÎÊÁ-586/ ÊÁ «ÞÆÍΪ» |
14–24 |
|
Äåãòÿðåâ À.Â., |
ZENITH-3SL ILV
LAUNCH DYNAMICS ANALYSIS from sea launch
platform |
Ðåçóëüòàòè
àíàë²çó Äèíàì²êè ñòàðòó ÐÊÏ «ÇåíIò-3SL» ç ìîðñüêί
ñòàðòîâî¯ ïëàòôîðìÈ, ùî çíàõîäèòüñÿ íà ïëàâó |
25–31 |
|
Äðîíü Í.Ì., |
FORECASTING OF
CHARACTERISTICS OF THE SPECIALIZED SPACECRAFT FOR THE GATHERING SMALL SPACE DEBRIS |
ÏÐÎÃÍÎÇÓÂÀÍÍß ÕÀÐÀÊÒÅÐÈÑÒÈÊ
ÑÏÅÖ²À˲ÇÎÂÀÍÎÃÎ ÊÎÑ̲×ÍÎÃÎ ÀÏÀÐÀÒÀ ÄËß ÇÁÈÐÀÍÍß ÄвÁÍÎÃÎ ÊÎÑ̲×ÍÎÃÎ Ñ̲ÒÒß |
32–37 |
|
Êóøíèðåíêî C.È., |
POSSIBILITY
ANALYSIS OF USING DIFFERENT KINDS OF THE SPACECRAFT PROPULSION SYSTEMS FOR
STRUGGLE AGAINST POLLUTION OF OUTER SPACE |
ÀÍÀË²Ç ÌÎÆËÈÂÎÑÒ² ÂÈÊÎÐÈÑÒÀÍÍß Ð²ÇÍÈÕ
ÒÈϲ ÄÂÈÃÓÍÍÈÕ ÓÑÒÀÍÎÂÎÊ ÄËß ÁÎÐÎÒÜÁÈ ²Ç
ÇÀÑ̲×ÅÍÍßÌ ÊÎÑ̲×ÍÎÃÎ ÏÐÎÑÒÎÐÓ |
38–42 |
|
Íèêîëàåâ À.Ä., |
AN INTERACTION
OF CAVITATION SURGE OSCILLATIONS AND LONGITUDINAL
OSCILLATIONS OF A LAUNCHER STRUCTURE IN «ROCKET STRUCTURE – PROPULSION
SYSTEM» DYNAMIC SYSTEM |
ÂÇÀªÌÎÄ²ß ÊÀ²ÒÀÖ²ÉÍÈÕ ÊÎËÈÂÀÍÜ
Ó Ð²ÄÈÍÍ²É ÐÀÊÅÒÍ²É ÄÂÈÃÓÍÍ²É ÓÑÒÀÍÎÂÖ²
² ÏÎÇÄÎÂÆÍ²Õ ÊÎËÈÂÀÍÜ ÊÎÐÏÓÑÓ ÐÀÊÅÒÈ-ÍÎÑ²ß |
43–47 |
|
Êàðà÷óí Â.Â., |
INTERACTION OF CONVEX
SHELL WITH A STRONG SHOCK WAVE |
ÂÇÀªÌÎÄ²ß ÎÏÓÊËί ÎÁÎËÎÍÊÈ Ç ÏÎÒÓÆÍÎÞ
ÓÄÀÐÍÎÞ ÕÂÈËÅÞ |
48–52 |
|
Øóëüæåíêî Í.Ã., |
REACTION OF SHELL ELEMENTS OF SPACE VEHICLES ON THE IMPULSE ACTION |
ÐÅÀÊÖ²ß ÎÁÎËÎÍÊÎÂÈÕ ÅËÅÌÅÍҲ ÊÎÑ̲×ÍÈÕ
ÀÏÀÐÀҲ ÍÀ ²ÌÏÓËÜÑÍÅ ÇÁÓÄÆÅÍÍß |
ÐÅÀÊÖÈß ÎÁÎËÎ×Å×ÍÛÕ ÝËÅÌÅÍÒΠÊÎÑÌÈ×ÅÑÊÈÕ ÀÏÏÀÐÀÒΠÍÀ
ÈÌÏÓËÜÑÍÎÅ ÂÎÇÄÅÉÑÒÂÈÅ |
53–58 |
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
||||
Êîíîõ Â.È., |
CREATION OF HYDRAULIC POWER SYSTEM WITH A PNEUMATIC PISTON ACTUATOR FOR THRUST VECTOR CONTROL SYSTEMS |
ÑÒÂÎÐÅÍÍß ÄÆÅÐÅË Ã²ÄÐÀÂ˲×Íί ÏÎÒÓÆÍÎÑÒ² Ç ÏÎÐØÍÅÂÈÌ ÏÍÅÂÌÀÒÈ×ÍÈÌ
ÏÐÈÂÎÄÎÌ ÄËß ÑÈÑÒÅÌ ÊÅÐÓÂÀÍÍß ÂÅÊÒÎÐÎÌ ÒßÃÈ ÐÀÊÅÒÈ-ÍÎÑ²ß |
59–66 |
|
Êîâàëåíêî À.Í., |
METHODOLOGICAL
FEATURES OF PREPARATION AND TESTING THE OPERABILITY OF HIGH-ALTITUDE LRE WITH FREE GAS INJECTION BLOWDOWN
PROPULSION |
ÌÅÒÎÄÈ×Ͳ ÎÑÎÁËÈÂÎÑÒ² ϲÄÃÎÒÎÂÊÈ ÒÀ
ÏÐÎÂÅÄÅÍÍß ÂÈÏÐÎÁÓÂÀÍÜ Ç ÏÅÐŲÐÊÈ ÏÐÀÖÅÇÄÀÒÍÎÑÒ² ÂÈÑÎÒÍÈÕ ÐÐÄ Ç ÂÈÒÈÑÊÍÎÞ ÑÈÑÒÅÌÎÞ ÏÎÄÀײ
ÏÀËÈÂÀ ÇI ÂÄÓÂÎÌ Â²ËÜÍÎÃÎ ÃÀÇÓ |
67–71 |
|
Âîñêîáîéíèê Ä.Â., |
ANALYSIS OF THE
ENERGY ANALYSIS OF ENERGY PERFORMANCE FUEL MIXTURE «LIQUID OXYGEN AND ALCOHOL-AMMONIA SOLUTION» IN SELF-PRESSURISED FEED SYSTEM LPRE LOW TRUST |
ÀÍÀË²Ç ÅÍÅÐÃÅÒÈ×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ
ÏÀËÈÂÍί ÏÀÐÈ «Ð²ÄÊÈÉ ÊÈÑÅÍÜ ² ÑÏÈÐÒÎ-À̲À×ÍÈÉ
ÐÎÇ×ÈÍ»  ÑÀÌÎÂÈÒÈÑÊÍÈÕ ÑÈÑÒÅÌÀÕ ÏÎÑÒÀ×ÀÍÍß ÐÐÄÌÒ |
72–75 |
|
Êðèâñóí Ð.Þ., |
DESIGN IMPROVEMENT FOR SPECIAL EQUIPMENT OF SOLID ROCKET MOTOR TEST |
ÓÄÎÑÊÎÍÀËÅÍÍß ÊÎÍÑÒÐÓÊÖ²¯ ÑÏÅÖ²ÀËÜÍÎÃÎ
ÎÁËÀÄÍÀÍÍß ÄËß ÂÈÏÐÎÁÓÂÀÍÍß ÐÄÒÏ |
ÓÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈÅ ÊÎÍÑÒÐÓÊÖÈÈ ÑÏÅÖÈÀËÜÍÎÃÎ ÎÁÎÐÓÄÎÂÀÍÈß
ÄËß ÈÑÏÛÒÀÍÈÉ ÐÄÒÒ |
76–79 |
Ðûæêîâ Ñ.Ñ., |
APPROACHES OF ENCREASING EFFICIENCY OF TRIGENERATION
PLANTS FOR INTEGRATED ENERGY SUPPLY |
ÍÀÏÐßÌÈ
ϲÄÂÈÙÅÍÍß ÅÔÅÊÒÈÂÍÎÑÒ² ÒÐÈÃÅÍÅÐÀÖ²ÉÍÈÕ ÓÑÒÀÍÎÂÎÊ
ÀÂÒÎÍÎÌÍÎÃÎ ÅÍÅÐÃÎÇÀÁÅÇÏÅ×ÅÍÍß |
ÍÀÏÐÀÂËÅÍÈß ÏÎÂÛØÅÍÈß ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÒÐÈÃÅÍÅÐÀÖÈÎÍÍÛÕ
ÓÑÒÀÍÎÂÎÊ ÀÂÒÎÍÎÌÍÎÃÎ ÝÍÅÐÃÎÎÁÅÑÏÅ×ÅÍÈß |
80–85 |
Ðàä÷åíêî Í.È., |
THREE CONTOUR SCAVENGE AIR COOLING
SYSTEM OF MARINE LOW SPEED DIESEL
ENGINE |
ÒÐÈÊÎÍÒÓÐÍÀ ÑÈÑÒÅÌÀ ÎÕÎËÎÄÆÅÍÍß ÍÀÄÄÓÂÍÎÃÎ ÏβÒÐß ÑÓÄÍÎÂÎÃÎ ÌÀËÎÎÁÅÐÒÎÂÎÃÎ ÄÈÇÅËß |
86–91 |
|
Áîãóñëàåâ Â.À., |
Electrochemical control of low rate reactions into hexane-oxygen flame |
ÅËÅÊÒÐÎղ̲×ÍÅ ÊÅÐÓÂÀÍÍß ÏβËÜÍÈÌÈ
ÐÅÀÊÖ²ßÌÈ Ó ÃÅÊÑÀÍÎ-ÊÈÑÍÅÂÎÌÓ ÏÎËÓÌ’¯ |
ÝËÅÊÒÐÎÕÈÌÈ×ÅÑÊÎÅ ÓÏÐÀÂËÅÍÈÅ ÌÅÄËÅÍÍÛÌÈ ÐÅÀÊÖÈßÌÈ Â
ÃÅÊÑÀÍÎ-ÊÈÑËÎÐÎÄÍÎÌ ÏËÀÌÅÍÈ |
92–96 |
Ìèõàëêèí À.À. |
THE FAN BLADES
OF PERSPECTIVE TURBOJETS |
Ðîáî÷³ËÎÏÀÒʲ ÂÅÍÒÈËßÒÎÐÀ ÏÅÐÑÏÅÊÒÈÂÍÈÕ ÒÐÄÄ |
97–100 |
|
Ñàëüíèêîâ À.Â. |
GAS-TURBINE
ENGINE IMPELLER UNIT’S DESIGN-STRESS MULTICRITERION
OPTIMIZATION |
ÊÎÍÑÒÐÓÊÒÈÂÍÎ-̲ÖͲÑÍÀ ÁÀÃÀÒÎÊÐÈÒÅвÀËÜÍÀ ÎÏÒÈ̲ÇÀÖ²ß
ÂÓÇ˲ ÐÎÁÎ×ÈÕ ÊÎË²Ñ ÂÌÄ |
ÊÎÍÑÒÐÓÊÒÈÂÍÎ-ÏÐÎ×ÍÎÑÒÍÀß ÌÍÎÃÎÊÐÈÒÅÐÈÀËÜÍÀß ÎÏÒÈÌÈÇÀÖÈß
ÓÇËΠÐÀÁÎ×ÈÕ ÊÎËÅÑ ÃÒÄ |
101–109 |
Ïàðîâàé Å.Ô. |
GTE Free turbine with slide bearings |
²ËÜÍÀ
ÒÓÐÁ²ÍÀ ÃÒÄ íà ï³äøèïíèêàõ êîâçàííÿ |
110–114 |
|
Øàòîõèí Â.Ô., |
EFFECTS OF TURBOGENERATOR PROTECTION SYSTEM SPEED CAPABILITIES ON
THE DEVELOPMENT OF THE ROTOR ROLL OVER THE STATOR |
ÂÏËÈ ØÂÈÄÊÎIJ¯ ÑÈÑÒÅÌÈ ÇÀÕÈÑÒÓ ÒÓÐÁÎÀÃÐÅÃÀÒÀ ÍÀ ÐÎÇÂÈÒÎÊ ÎÁÊÀÒÓ ÐÎÒÎÐÀ ÏÎ ÑÒÀÒÎÐÓ |
ÂËÈßÍÈÅ ÁÛÑÒÐÎÄÅÉÑÒÂÈß ÑÈÑÒÅÌÛ ÇÀÙÈÒÛ ÒÓÐÁÎÀÃÐÅÃÀÒÀ ÍÀ
ÐÀÇÂÈÒÈÅ ÎÁÊÀÒÀ ÐÎÒÎÐÀ ÏÎ ÑÒÀÒÎÐÓ |
115–126 |
Íàçèí Â.È. |
MATHEMATICAL
MODEL DOUBLE ANGULAR CONTACT
HYDROSTATIC BEARINGS |
ÌÀÒÅÌÀÒÈ×ÍÀ ÌÎÄÅËÜ
ÇÄÂΪÍÎÃÎ ÐÀIJÀËÜÍÎ-óïîðíîÎÃÎ
òÄÐÎÑÒÀÒÈ×ÍÎÃÎ Ï²ÄØÈÏÍÈÊÀ |
ÌÀÒÅÌÀÒÈ×ÅÑÊÀß
ÌÎÄÅËÜ ÑÄÂÎÅÍÍÎÃÎ ÐÀÄÈÀËÜÍÎ-ÓÏÎÐÍÎÃÎ ÃÈÄÐÎÑÒÀÒÈ×ÅÑÊÎÃÎ ÏÎÄØÈÏÍÈÊÀ |
127–133 |
Àíàíüåâ Â.Ì., |
IMPROVING METHODS OF TURBOFAN GEARBOX DESIGN |
ÓÄÎÑÊÎÍÀËÅÍÍß ÌÅÒÎIJ ÏÐÎÅÊÒÓÂÀÍÍß
ÇÓÁ×ÀÑÒÈÕ ÏÅÐÅÄÀ× ÐÅÄÓÊÒÎв ÏÐÈÂÎÄÓ ÂÅÍÒÈËßÒÎÐÀ ÒÐÄÄ |
ÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈÅ ÌÅÒÎÄΠÏÐÎÅÊÒÈÐÎÂÀÍÈß ÇÓÁ×ÀÒÛÕ
ÏÅÐÅÄÀ× ÐÅÄÓÊÒÎÐΠÏÐÈÂÎÄÀ ÂÅÍÒÈËßÒÎÐÀ ÒÐÄÄ |
134–139 |
Êðàâ÷åíêî È.Ô., |
EVOLUTION METHOD MANAGEMENT TASK ON LIFE AVIATION ENGINE FOR CTF |
ÐÎÇÂÈÒÎÊ ÌÅÒÎÄÈÊÈ ÊÅÐÓÂÀÍÍß ÄÎÂÅÄÅÍÍß ÀÂIÀÖIÉÍÈÕ ÄÂÈÃÓÍIÂ ÄËß ÓÁË |
140–149 |
|
Âåëèêàíîâà Í.Ï., |
EFFECT OF ATMOSPHERIC CONDITIONS FOR USE DURABILITY OF THE TURBINE
DISK GAS TURBINE ENGINES |
ÂÏËÈ ÀÒÌÎÑÔÅÐÍÈÕ ÓÌΠÍÀ ÄÎÂÃÎÒÐÈÂÀ˲ÑÒÜ ÄÈÑʲ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ |
ÂËÈßÍÈÅ ÀÒÌÎÑÔÅÐÍÛÕ ÓÑËÎÂÈÉ ÝÊÑÏËÓÀÒÀÖÈÈ ÍÀ ÄÎËÃÎÂÅ×ÍÎÑÒÜ
ÄÈÑÊÎÂ ÒÓÐÁÈÍ ÀÂÈÀÖÈÎÍÍÛÕ ÃÒÄ |
150–154 |
Ñìûñëîâ À.Ì., |
VOLUMETRIC STRESSES OF THE COMPRESSOR’S BLADES OF GTE INVESTIGATION |
ÄÎÑË²ÄÆÅÍÍß ÇÀËÈØÊÎÂÈÕ
ÎÁ'ªÌÍÈÕ ÍÀÏÐÓÆÅÍÜ Â ËÎÏÀÒÊÀÕ ÊÎÌÏÐÅÑÎÐÀ ÃÒÄ |
ÈÑÑËÅÄÎÂÀÍÈÅ ÎÑÒÀÒÎ×ÍÛÕ ÎÁÚ¨ÌÍÛÕ ÍÀÏÐ߯ÅÍÈÉ Â ËÎÏÀÒÊÀÕ
ÊÎÌÏÐÅÑÑÎÐÀ ÃÒÄ |
155–158 |
Ãîëóá Â.Ï. |
THE METHOD OF
THE FATIGUE LIFE-TIME CALCULATION OF STRUCTURAL COMPONENTS UNDER BIAXIAL COMBINED LOADING |
ÌÅÒÎÄ ÐÎÇÐÀÕÓÍÊÓ ÄÎÂÃβ×ÍÎÑÒ²
ÅËÅÌÅÍҲ ÊÎÍÑÒÐÓÊÖ²É ÂÍÀÑ˲ÄÎÊ ÂÒÎÌÈ ÇÀ ÓÌΠÄÂβÑÍÎÃÎ ÊÎÌÁ²ÍÎÂÀÍÎÃÎ ÍÀÂÀÍÒÀÆÅÍÍß |
159–165 |
|
Ñèìáèðñêèé Ä.Ô., |
MODEL ANALYSES OF
HOLD IMPACT IN THE CYCLE ON THE MATERIAL RESISTANCE TO THE LOW-CYCLE FATIGUE
USING LAWS OF REPEATED-STATIC LOADING |
ÌÎÄÅËÜͲ ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ ÂÈÒÐÈÌÊÈ Â
ÖÈÊ˲ ÍÀ ÎϲРÌÀÒÅвÀËÓ ÌÀËÎÖÈÊËÎÂ²É ÂÒÎ̲ Ç
ÂÈÊÎÐÈÑÒÀÍÍßÌ ÇÀÊÎÍÎ̲ÐÍÎÑÒÅÉ ÏÎÂÒÎÐÍÎ-ÑÒÀÒÈ×ÍÎÃÎ ÍÀÂÀÍÒÀÆÅÍÍß |
166–172 |
|
Åïèôàíîâ Ñ.Â., |
“RAIN” METHOD MODERNIZING FOR TURBINE ENGINE
BASIC COMPONENTS LIFE TIME MONITORING |
ÌÎÄÅÐͲÇÀÖ²ß ÌÅÒÎÄÓ «ÄÎÙÓ» ÄËß
ÌÎͲÒÎÐÈÍÃÓ ÂÈÐÎÁ²ÒÊÓ ÐÅÑÓÐÑÓ ÎÑÍÎÂÍÈÕ ÄÅÒÀËÅÉ ÃÒÄ |
ÌÎÄÅÐÍÈÇÀÖÈß ÌÅÒÎÄÀ «ÄÎÆÄß» ÄËß ÌÎÍÈÒÎÐÈÍÃÀ ÂÛÐÀÁÎÒÊÈ
ÐÅÑÓÐÑÀ ÎÑÍÎÂÍÛÕ ÄÅÒÀËÅÉ ÃÒÄ |
173–176 |
Ïûëåâ Â.À., |
PREDICTING THE RESOURCE STRENGTH
OF PISTON SMALL-ENGINE AIRCRAFT ENGINES |
ÏÐÎÃÍÎÇÓÂÀÍÍß ÐÅÑÓÐÑÍί ̲ÖÍÎÑÒ² ÏÎÐØÍß
ËÅÃÊÎÌÎÒÎÐÍÎÃÎ À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ |
ÏÐÎÃÍÎÇÈÐÎÂÀÍÈÅ
ÐÅÑÓÐÑÍÎÉ ÏÐÎ×ÍÎÑÒÈ ÏÎÐØÍß ËÅÃÊÎÌÎÒÎÐÍÎÃÎ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß |
177–182 |
Áèáëèê È.Â. |
RELIABILITY ASSESSMENT OF PERFORMANCE BASED ON PROBABILISTIC SUMMATION OF FATIGUE DAMAGES |
ÎÖ²ÍÊÀ
ÏÎÊÀÇÍÈʲ ÍÀIJÉÍÎÑÒ² ÍÀ ÎÑÍβ ²ÌβÐͲÑÍÎÃΠϲÄÑÓÌÎÂÓÂÀÍÍß ÂÒÎÌÍÈÕ
ÏÎØÊÎÄÆÅÍÜ |
ÎÖÅÍÊÀ ÏÎÊÀÇÀÒÅËÅÉ ÍÀÄÅÆÍÎÑÒÈ ÍÀ ÎÑÍÎÂÅ ÂÅÐÎßÒÍÎÑÒÍÎÃÎ
ÑÓÌÌÈÐÎÂÀÍÈß ÓÑÒÀËÎÑÒÍÛÕ ÏÎÂÐÅÆÄÅÍÈÉ |
183–187 |
Óìàíñêèé À.Ï., |
EFFECT OF TITANIUM DIBORIDE ADDITIVES ON THE
STRUCTURE AND PROPERTIES OF HVAF-COATINGS OF (Ni-Cr-Si-B) – TiB2
SYSTEM |
ÂÏËÈÂ ÄÈÑÏÅÐÑÍÈÕ
ÄÎ̲ØÎÊ ÄÈÁÎÐÈÄÓ ÒÈÒÀÍÓ ÍÀ ÑÒÐÓÊÒÓÐÓ ² ÂËÀÑÒÈÂÎÑÒ² HVAF - ÏÎÊÐÈÒҲ ÑÈÑÒÅÌÈ (Ni-Cr-Si-B) – TiB2 |
188–194 |
|
Ñíåæíîé Ã.Â. |
magnetometric EVALUATION OF CORROSION RESISTANCE austenitic chromium-nickel steels
with different phase composition |
Ìàãí³òîìåòðè÷íà
îö³íêà êîðîç³éíî¿ òðèâêîñò³ àóñòåí³òíèõ õðîìîí³êåëåâèõ ÑÒÀËÅÉ â çàëåæíîñò³
â³ä ôàçîâîãî ñêëàäó |
195–201 |
|
Âàêóëåíêî Ê.Â., |
CORROSION RESISTANCE OF STEEL 20X13 With
vacuum-plasma coatings |
Êîðîç³éíà
ñò³éê³ñòü ñòàë³ 20Õ13 ç âàêóóìíî-ïëàçìîâèìè ïîêðèòòÿìè |
ÊÎÐÐÎÇÈÎÍÍÀß ÑÒÎÉÊÎÑÒÜ ÑÒÀËÈ 20Õ13 Ñ
ÂÀÊÓÓÌÍÎ-ÏËÀÇÌÅÍÍÛÌÈ ÏÎÊÐÛÒÈßÌÈ |
202–207 |
Êàèðîâ À.Ñ., |
TURBINE ENGINES
BLADED DISKS SUBMITED AS NON-CYCLICAL SYSTEM
VIBRATION, STRESS AND DEFORMATION ANALYSIS |
ÊÎËÈÂÀÍÍß ÒÀ ÍÀÏÐÓÆÅÍÎ-ÄÅÔÎÐ̲ÂÍÈÉ
ÑÒÀÍ Â²Íֲ ÐÎÁÎ×ÈÕ ËÎÏÀÒÎÊ ÒÓÐÁÎÌÀØÈÍ ÏÐÈ ÏÎÐÓØÅÍͲ ÖÈÊ˲×Íί ÑÈÌÌÅÒв¯ |
208–215 |
|
Íàçàðåíêî Þ.Á., |
NEW APPROACH OF
FLOATING INTERSHAFT BEARING
SLIPPING ELIMINATION |
ÍÎÂÈÉ ÏIÄÕIÄ
ÄÎ ÂÈÐIØÅÍÍß ÏÐÎÁËÅÌÈ ÓÑÓÍÅÍÍß ÏÐÎÊÎÂÇÓÂÀÍÍß ÌÀËÎÍÀÂÀÍÒÀÆÅÍÈÕ ÌIÆÂÀËÜÍÛÕ ÏIÄØÈÏÍÈÊIÂ |
ÍÎÂÛÉ ÏÎÄÕÎÄ Ê ÐÅØÅÍÈÞ ÏÐÎÁËÅÌÛ ÓÑÒÐÀÍÅÍÈß
ÏÐÎÑÊÀËÜÇÛÂÀÍÈß ÑËÀÁÎÍÀÃÐÓÆÅÍÍÛÕ ÌÅÆÂÀËÜÍÛÕ ÏÎÄØÈÏÍÈÊÎÂ |
216–219 |
Ìåäâåäîâñêàÿ Ò.Ô., |
STRENGTH
OF THE COVER AND POWER PIN GIDROAGREGAT |
̲ÖͲÑÒÜ ÊÐÈØÊÈ ² ÑÈËÎÂί ØÏÈËÜÊÈ
òÄÐÎÀÃÐÅÃÀÒÓ ÃÀÅÑ |
220–225 |
|
Ïàí³í Â.Â., |
FOG COMPRESSION
IN GAS TURBINE ENGINES |
ÐÅÀËÈÇÀÖÈß «ÂËÀÆÍÎÃÎ
ÑÆÀÒÈß» Â ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËßÕ |
226–230 |
|
Ãðèãîðüåâ Â.Â., |
CONCEPTUAL
SCHEMES OF AIRCRAFT ENGINES WITH HIGH FUEL EFFICIENCY |
Ïåðñïåêòèâí³
ñõåìè àâ³àö³éíèõ äâèãóí³â ç âèñîêîþ ïàëèâíîþ åôåêòèâí³ñòþ |
ÏÅÐÑÏÅÊÒÈÂÍÛÅ ÑÕÅÌÛ ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ Ñ ÂÛÑÎÊÎÉ
ÒÎÏËÈÂÍÎÉ ÝÔÔÅÊÒÈÂÍÎÑÒÜÞ |
231–236 |
Èíôîðìàöèîííûå òåõíîëîãèè |
||||
Äàíèëêèí Ñ.Þ., |
NON-CONTACT
DIAGNOSTIC OF THE TURBOMACHINERY
ROTOR BLADES RESONANT OSCILLATIONS |
ÁÅÇÊÎÍÒÀÊÒÍÀ
IJÀÃÍÎÑÒÈÊÀ ÐÅÇÎÍÀÍÑÍÈÕ ÊÎËÈÂÀÍÜ ÐÎÁÎ×ÈÕ ËÎÏÀÒÎÊ ÒÓÐÁÎÌÀØÈÍ |
ÁÅÑÊÎÍÒÀÊÒÍÀß ÄÈÀÃÍÎÑÒÈÊÀ ÐÅÇÎÍÀÍÑÍÛÕ ÊÎËÅÁÀÍÈÉ ÐÀÁÎ×ÈÕ ËÎÏÀÒÎÊ ÒÓÐÁÎÌÀØÈÍ |
237–241 |
Òêà÷ Ì.Ð., |
AUTOMATION OF
OSCILLATION FORMS DETERMINATION OF LOW POWER GTE ELEMENTS |
ÀÂÒÎÌÀÒÈÇÀÖ²ß ÂÈÇÍÀ×ÅÍÍß ÂËÀÑÍÈÕ ×ÀÑÒÎÒ
² ÔÎÐÌ ÊÎËÈÂÀÍÜ ÅËÅÌÅÍҲ ÒÓÐÁ²Í ÌÀËί ÏÎÒÓÆÍÎÑÒ² |
ÀÂÒÎÌÀÒÈÇÀÖÈß
ÎÏÐÅÄÅËÅÍÈß ÑÎÁÑÒÂÅÍÍÛÕ ×ÀÑÒÎÒ È ÔÎÐÌ ÊÎËÅÁÀÍÈÉ ÝËÅÌÅÍÒΠÒÓÐÁÈÍ ÌÀËÎÉ
ÌÎÙÍÎÑÒÈ |
242–248 |
Îãèåíêî Ñ.A. |
MICROWAVE RANGE RADIATION OF STATIONARY PLASMA THRUSTER AS RESULT OF
TRANSFORMATION OF WAVES IN DISCHARGE
INTERVAL PLASMA |
ÑÂ× ÂÈÏÐÎ̲ÍÞÂÀÍÍß
ÑÒÀÖ²ÎÍÀÐÍÎÃÎ ÏËÀÇÌÎÂÎÃÎ ÄÂÈÃÓÍÀ ßÊ ÍÀÑ˲ÄÎÊ ÒÐÀÍÑÔÎÐÌÀÖ²¯ ÕÂÈËÜ Ó ÏËÀÇ̲
ÐÎÇÐßÄÍÎÃÎ ÏÐÎ̲ÆÊÀ |
249–253 |
|
Ìàêñèìåíêî Ò.À., |
INVESTIGATIONS
OF INTEGRAL CHARACTERISTICS OF SMALL SPT WITH
DISCHARGE CHAMBER MADE OF BN COMPOSITIONS |
ÄÎÑË²ÄÆÅÍÍß ²ÍÒÅÃÐÀËÜÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ
ÌÀËÎÃÎ ÑÏÄ Ç ÐÎÇÐßÄÍÎÞ ÊÀÌÅÐÎÞ Ç ÁÎÐÎͲÒÐÈÄÍÈÕ ÊÎÌÏÎÇÈÖ²É |
ÈÑÑËÅÄÎÂÀÍÈÅ ÈÍÒÅÃÐÀËÜÍÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÌÀËÎÃÎ ÑÏÄ Ñ
ÐÀÇÐßÄÍÎÉ ÊÀÌÅÐÎÉ ÈÇ ÁÎÐÎÍÈÒÐÈÄÍÛÕ ÊÎÌÏÎÇÈÖÈÉ |
254–257 |
Öàãëîâ À.È., |
REDUCTION OF TEST SAMPLE SURFACE TEMPERATURE NONUNIFORMITY DURING
ELECTRIC PROPULSION CATHODE’S EMITTERS TESTING |
̲Ͳ̲ÇÀÖ²ß ÒÅÌÏÅÐÀÒÓÐÍί
ÍÅвÂÍÎ̲ÐÍÎÑÒ² ÏÎÂÅÐÕͲ ÄÎÑË²ÄÆÓÂÀÍÎÃÎ
ÇÐÀÇÊÀ ÏÐÈ ÂÈÏÐÎÁÓÂÀÍÍßÕ
Å̲ÒÅв ÊÀÒÎIJ ÅÐÄ |
258–261 |
|
Íåñòåðåíêî Ñ.Þ., |
PECULIARITIES OF ELECTRONS REFLECTION FROM POTENTIAL BARRIER AND THEIR
GAS DYNAMICS CHATACTERISTICS FLOWS ON THE BORDERS OF
ELECTRIC PROPULSION THTUSTERS PLASMA |
ÎÑÎÁËÈÂÎÑÒ² ²ÄÁÈÒÒß ÅËÅÊÒÐÎͲ ²Ä
ÏÎÒÅÍÖ²ÀËÜÍÎÃÎ ÁÀÐ'ªÐÓ ² ÏÎÒÎÊÈ ¯Õ ÃÀÇÎÄÈÍÀ̲×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÍÀ ÌÅÆÀÕ
ÏËÀÇÌÈ ÅËÅÊÒÐÎÐÀÊÅÒÍÈÕ ÄÂÈÃÓͲ |
262–265 |
|
Áåçðó÷êî Ê.Â., |
METHOD OF
ESTIMATION OF EFFICIENCY OF SPACEPORTS AND THEIR SYSTEMS DURING THE DESIGN
PHASE |
ÌÅÒÎÄÈÊÀ ÎÖ²ÍÊÈ ÅÔÅÊÒÈÂÍÎÑÒ²
ÊÎÑÌÎÄÐÎ̲ ÒÀ ¯Õ ÑÈÑÒÅÌ ÍÀ ÅÒÀϲ ÏÐÎÅÊÒÓÂÀÍÍß |
ÌÅÒÎÄÈÊÀ ÎÖÅÍÊÈ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÊÎÑÌÎÄÐÎÌÎÂ È ÈÕ ÑÈÑÒÅÌ ÍÀ
ÝÒÀÏÅ ÏÐÎÅÊÒÈÐÎÂÀÍÈß |
266–270 |
Äçåíçåðñêèé Â.À., |
IMPROVEMENT OF TECHNOLOGIES OF LEAD BATTERY GRID MANUFACTURING |
ÓÄÎÑÊÎÍÀËÅÍÍß ÒÅÕÍÎËÎÃ²É ÂÈÃÎÒÎÂËÅÍÍß ÑÒÐÓÌβÄÂÎIJÂ
ÄËß ÑÂÈÍÖÅÂÈÕ ÀÊÓÌÓËßÒÎв |
ÓÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈÅ ÒÅÕÍÎËÎÃÈÉ ÈÇÃÎÒÎÂËÅÍÈß ÒÎÊÎÎÒÂÎÄÎÂ
ÄËß ÑÂÈÍÖÎÂÛÕ ÀÊÊÓÌÓËßÒÎÐÎÂ |
271–275 |
Äàíîâ À.Ñ. |
VECTOR NATURE OF COMMON
FIELD OF INTERACTION |
ÂÅÊÒÎÐÍÀ ÏÐÈÐÎÄÀ ªÄÈÍÎÃÎ ÏÎËß ÂÇÀªÌÎIJ¯ |
276–279 |
|
Êó÷óê Ã.À. |
SYNTHESIS OF DATA DEPOSITORY CLOUD HYBRID
TOPOLOGY IN HETEROGENEOUS NETWORK |
ÑÈÍÒÅÇ ÒÎÏÎËÎò¯ òÁÐÈÄÍÎÃÎ ÕÌÀÐÍÎÃÎ ÑÕÎÂÈÙÀ ÄÀÍÈÕ Ó ÃÅÒÅÐÎÃÅÍÍÎÌÓ ÑÅÐÅÄÎÂÈÙ² |
ÑÈÍÒÅÇ ÒÎÏÎËÎÃÈÈ ÃÈÁÐÈÄÍÎÃÎ ÎÁËÀ×ÍÎÃÎ ÕÐÀÍÈËÈÙÀ ÄÀÍÍÛÕ Â ÃÅÒÅÐÎÃÅÍÍÎÉ ÑÐÅÄÅ |
280–284 |
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.