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 |
Íàçâàíèå ñòàòüè
(article title) |
Ñòðàíèöû
|
||
English |
Óêðà¿íñüêà
ìîâà |
Ðóññêèé
ÿçûê |
||
Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ |
||||
Áîðèñåâè÷ Â.Ê., |
RESEARCH
POSSIBILITY OF OBTAINING OF NEW MATERIAL WITH PULSED ULTRAHIGH PRESSURE |
ÄÎÑË²ÄÆÅÍÍß ÌÎÆËÈÂÎÑÒ² ÎÒÐÈÌÀÍÍß ÍÎÂÈÕ ÌÀÒÅвÀ˲Â
ÇÀ ÄÎÏÎÌÎÃÎÞ ²ÌÏÓËÜÑÍÈÕ ÍÀÄÂÈÑÎÊÈÕ ÒÈÑʲ |
ÈÑÑËÅÄÎÂÀÍÈÅ
ÂÎÇÌÎÆÍÎÑÒÈ ÏÎËÓ×ÅÍÈß ÍÎÂÛÕ ÌÀÒÅÐÈÀËΠÏÐÈ ÏÎÌÎÙÈ ÈÌÏÓËÜÑÍÛÕ ÑÂÅÐÕÂÛÑÎÊÈÕ
ÄÀÂËÅÍÈÉ |
7–10 |
Õóäÿêîâ Ñ.Â., |
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 |
Áîëñóíîâñêèé Ñ.À., |
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 |
16–19 |
|
Ãîëäóí Â.Þ., |
UPGRADING
CAST-IRON OF COMPRESSION PISTON-RINGS OF TRANSPORT ENGINES |
ϲÄÂÈÙÅÍÍß ßÊÎÑÒ²
×ÀÂÓÍÓ ÊÎÌÏÐÅѲÉÍÈÕ ÏÎÐØÍÅÂÈÕ Ê²ËÅÖÜ ÒÐÀÍÑÏÎÐÒÍÈÕ ÄÂÈÃÓͲ |
ÏÎÂÛØÅÍÈÅ ÊÀ×ÅÑÒÂÀ
×ÓÃÓÍÀ ÊÎÌÏÐÅÑÑÈÎÍÍÛÕ ÏÎÐØÍÅÂÛÕ ÊÎËÅÖ ÒÐÀÍÑÏÎÐÒÍÛÕ ÄÂÈÃÀÒÅËÅÉ |
20–23 |
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ
àïïàðàòîâ |
||||
Ñìèðíîâ Ä.Ñ., |
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 |
Âîðîáüåâ Þ.Ñ., |
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 |
Âèíîãðàäîâ À.Ñ., |
PECULIARITIES
OF RETAINER DESIGN AS A PART OF AIR-ENGINE
SYSTEMS |
ÎÑÎÁËÈÂÎÑÒ² ÏÐÎÅÊÒÓÂÀÍÍß ÓÙ²ËÜÍÅÍÜ Ó
ÑÊËÀIJ ÑÈÑÒÅÌ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲ |
ÎÑÎÁÅÍÍÎÑÒÈ
ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÓÏËÎÒÍÅÍÈÉ Â ÑÎÑÒÀÂÅ ÑÈÑÒÅÌ ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ |
33–38 |
Ëåïåøêèí À.Ð., |
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 |
39–43 |
|
Äîðîôååâ Â.Ë., |
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 |
Óìàíñêèé À.Ï., |
INFLUENCE OF
TiB2 ADDITIVES
ON STRUCNURE AND PROPERTIES OF NiCrSiB-BASED PLASMA SPRAY COATINGS |
ÂÏËÈÂ ÄÎÁÀÂÎÊ TiB2 ÍÀ
ÑÒÐÓÊÒÓÐÓ ÒÀ ÂËÀÑÒÈÂÎÑÒ²ÏËÀÇÌÎÂÈÕ ÏÎÊÐÈÒҲ ÍÀ ÎÑÍβ NiCrSiB |
ÂËÈßÍÈÅ ÄÎÁÀÂÎÊ TiB2 ÍÀ ÑÒÐÓÊÒÓÐÓ È ÑÂÎÉÑÒÂÀ ÏËÀÇÌÅÍÍÛÕ
ÏÎÊÐÛÒÈÉ ÍÀ ÎÑÍÎÂÅ NiCrSiB |
50–54 |
Ðûæêîâ Ñ.Ñ., |
TRIGENERATION
PLANT FOR INTEGRATED ENERGY SUPPLY |
ÒÐÈÃÅÍÅÐÀÖ²ÉÍÀ
ÓÑÒÀÍÎÂÊÀ ÀÂÒÎÍÎÌÍÎÃÎ ÅÍÅÐÃÎÇÀÁÅÇÏÅ×ÅÍÍß |
55–60 |
|
Ðàä÷åíêî Ð.Í., |
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 |
Ðàä÷åíêî À.Í., |
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 |
68–71 |
|
Àë¸õèí Ñ.À., |
COMPLEX GAS-DYNAMIC
IMPROVEMENT OF TWO-STROKE TURBO-PISTON TRANSPORT DIESEL ENGINES |
ÊÎÌÏËÅÊÑÍÅ ÃÀÇÎÄÈÍÀ̲×ÍÅ
ÓÄÎÑÊÎÍÀËÞÂÀÍÍß ÄÂÎÒÀÊÒÍÈÕ ÒÓÐÁÎÏÎÐØÍÅÂÈÕ ÒÐÀÍÑÏÎÐÒÍÈÕ ÄÈÇÅ˲ |
ÊÎÌÏËÅÊÑÍÎÅ
ÃÀÇÎÄÈÍÀÌÈ×ÅÑÊÎÅ ÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈÅ ÄÂÓÕÒÀÊÒÍÛÕ ÒÓÐÁÎÏÎÐØÍÅÂÛÕ ÒÐÀÍÑÏÎÐÒÍÛÕ
ÄÈÇÅËÅÉ |
72–76 |
Ìóðçàãàëèåâ À.Æ., |
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 |
Ñàôîíîâ Â.À., |
ABOUT SOME FEATURES OF WORK OF
thermosonicAND thermoreversible ENGINES |
ÏÐÎ ÄÅßʲ ÎÑÎÁËÈÂÎÑÒ²
ÐÎÁÎÒÈ ÒÅÐÌÎÀÊÓÑÒÈ×ÍÈÕ ÒÀ ÒÅÐÌÎÎÁÎÐÎÒÍÈÕ ÄÂÈÃÓͲ |
Î ÍÅÊÎÒÎÐÛÕ
ÎÑÎÁÅÍÍÎÑÒßÕ ÐÀÁÎÒÛ ÒÅÐÌÎÀÊÓÑÒÈ×ÅÑÊÈÕ È ÒÅÐÌÎÎÁÐÀÒÈÌÛÕ ÄÂÈÃÀÒÅËÅÉ |
82–85 |
Ìîðîçîâà Â.Ñ., |
ANALYSIS OF INFLUENCE
OF THE MAGNETIC STREAM ON ECOLOGICAL INDICATORS OF ENGINE |
ÀÍÀË²Ç ÂÏËÈÂÓ ÌÀÃͲÒÍÎÃÎ ÏÎÒÎÊÓ |
ÀÍÀËÈÇ ÂËÈßÍÈß
ÌÀÃÍÈÒÍÎÃÎ ÏÎÒÎÊÀ ÍÀ ÝÊÎËÎÃÈ×ÅÑÊÈÅ ÏÎÊÀÇÀÒÅËÈ ÄÂÑ |
86–91 |
Ìîøåíöåâ Þ.Ë., |
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 ÒÅÏËÎÂÎDz |
92–97 |
|
Âàðáàíåö Ð.À., |
Vibroacoustic CONTROL OF MARINE turbocharged diesel REVOLUTION |
²áðîàêóñòè÷íèé
êîíòðîëü ÷àñòîòíèõ õàðàêòåðèñòèê |
ÂÈÁÐÎÀÊÓÑÒÈ×ÅÑÊÈÉ
ÊÎÍÒÐÎËÜ ×ÀÑÒÎÒÍÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÑÓÄÎÂÎÃÎ ÄÈÇÅËß Ñ ÒÓÐÁÎÍÀÄÄÓÂÎÌ |
98–105 |
Áûëèíêèíà Î.Í., |
PECULIARITIES
OF VIBRATION DIAGNOSTICS SIGNES
MANIFESTATION FOR AFTERBURNING TURBOFAN BEARINGS WHILE OPERATING IN HIGH MANEUVERABLE AIRPLANE |
ÎÑÎÁËÈÂÎÑÒ² ÏÐÎßÂËÅÍÍß Â²ÁÐÀÖ²ÉÍÈÕ Ä²ÀÃÍÎÑÒÈ×ÍÈÕ ÏÐÈÇÍÀʲ ÑÒÀÍÓ
Ï²ÄØÈÏÍÈʲ ÒÐÄÄÔ Ï²Ä ×ÀÑ ÅÊÑÏËÓÀÒÀÖ²¯ ÍÀ ÌÀÍÅÂÐÎÂÎÌÓ Ë²ÒÀÊÓ |
106–112 |
|
Áîãóñëàåâ Â.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 |
Guyot M., |
|
̲ÊÐÎõîëëîâñüêèé ÄÂÈÃÓÍ ÄËß íàíîñóïóòíèê³â |
ÌÈÊÐÎõîëëîâñêèé äâèãàòåëÜ äëÿ íàíîñïóòíèêîâ |
118–122 |
Cenian A., |
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 |
Lino da Silva
M., |
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 |
Ãóáàéäóëëèí È.Ò., |
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 |
133–139 |
|
Ãîëîâ÷óê À.Ô., |
DEVELOPMENT of STRUCTURAL CHART ELECTRONIC-GUIDED fuel supply DIESEL
And gas-diesel engines |
ÐÎÇÐÎÁÊÀ ÊÎÍÑÒÐÓÊÒÈÂÍί
ÑÕÅÌÈ ÅËÅÊÒÐÎÍÍÎ-ÊÅÐÎÂÀÍί ÏÀËÈÂÎÏÎÄÀײ ÄÈÇÅ˲ ² ÃÀÇÎÄÈÇÅ˲ |
Ðàçðàáîòêà êîíñòðóêòèâíîé ñõåìû ýëåêòðîííî-óïðàâëÿåìîé ñèñòåìû
òîïëèâîïîäà÷è äèçåëåé è ãàçîäèçåëåé |
140–143 |
Èíôîðìàöèîííûå òåõíîëîãèè |
||||
Øåâ÷åíêî Ì.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 |
Ìèðãîðîä Â.Ô., |
SIMULATION OF
MEASURING CHANNELS WITH TRANSCENDENTAL TRANSFER FUNCTIONS |
ÌÎÄÅËÞÂÀÍÍß ÂÈ̲ÐÞÂÀËÜÍÈÕ ÊÀÍÀ˲ Ç
ÒÐÀÍÑÖÅÍÄÅÍÒÍÈÌÈ ÏÅÐÅÄÀÒÍÈÌÈ ÔÓÍÊÖ²ßÌÈ |
ÌÎÄÅËÈÐÎÂÀÍÈÅ
ÈÇÌÅÐÈÒÅËÜÍÛÕ ÊÀÍÀËÎÂ Ñ ÒÐÀÍÑÖÅÍÄÅÍÒÍÛÌÈ ÏÅÐÅÄÀÒÎ×ÍÛÌÈ ÔÓÍÊÖÈßÌÈ |
153–155 |
˳íí³ê ².²., |
COMPLEX MODEL OF MAINTENANCE SYSTEM SERVICE OF POWER INSTALLATIONS OF LAND AERONAUTICS |
ÊÎÌÏËÅÊÑÍÀß
ÌÎÄÅËÜ ÑÈÑÒÅÌÛ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÎÁÑËÓÆÈÂÀÍÈß ÝÍÅÐÃÅÒÈ×ÅÑÊÈÕ ÓÑÒÀÍÎÂÎÊ ÀÂÈÀÖÈÎÍÍÎÉ ÍÀÇÅÌÍÎÉ ÒÅÕÍÈÊÈ |
156–160 |
|
Ïîãîðåëîâ Ã.È., |
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¯ |
161–169 |
|
Ïàøàåâ À.Ì., |
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
IJÀÃÍÎÑÒÓÂÀÍÍß ÒÑ ÀÃÒÄ |
170–175 |
|
Ðåâà Î.Ì., |
ASSESSMENT OF
STRUCTURAL EFFICIENCY OF THE AIR
TRAFFIC DEPARTMENT (ON THE EXAMPLE OF THE KRASNOYARSK CENTER OF AIR
TRAFFIC SERVICE) |
ÎÖÅÍÊÀ ÑÒÐÓÊÒÓÐÍÎÉ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÑËÓÆÁÛ
ÄÂÈÆÅÍÈß (ÍÀ ÏÐÈÌÅÐÅ ÊÐÀÑÍÎßÐÑÊÎÃÎ ÖÅÍÒÐÀ ÎÁÑËÓÆÈÂÀÍÈß ÂÎÇÄÓØÍÎÃÎ ÄÂÈÆÅÍÈß) |
176–186 |
|
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 |
Ñòàøèíñüêèé Î.Ï. |
SYSTEM OF
INTELLECTUAL MANAGEMENT ROBOT-TECHNICAL DEVICE FOR DIAGNOSTICS OF PIPELINES
OF THE COMPRESSOR STATIONS |
ÑÈÑÒÅÌÀ ÈÍÒÅËËÅÊÒÓÀËÜÍÎÃÎ ÓÏÐÀÂËÅÍÈß
ÐÎÁÎÒÎÒÅÕÍÈ×ÅÑÊÈÌ ÓÑÒÐÎÉÑÒÂÎÌ ÄËß ÄÈÀÃÍÎÑÒÈÊÈ ÒÐÓÁÎÏÐÎÂÎÄΠÊÎÌÏÐÅÑÑÎÐÍÛÕ
ÑÒÀÍÖÈÉ |
192–195 |
|
Êâàñí³êîâ
Â.Ï., |
MATHEMATICAL
MODEL OF RADIO MOBILE ROBOT |
ÌÀÒÅÌÀÒÈ×ÅÑÊÀß ÌÎÄÅËÜ ÐÀÄÈÎÓÏÐÀÂËÅÍÈß
ÌÎÁÈËÜÍÛÌ ÐÎÁÎÒÎÌ |
196–200 |
|
Êâàñí³êîâ
Â.Ï., |
SYNTHESIS OF INFORMATION PROCESSING IN MEASURING ROBOT |
ÑÈÍÒÅÇ ÑÈÑÒÅÌÛ ÎÁÐÀÁÎÒÊÈ ÈÍÔÎÐÌÀÖÈÈ Â ÈÇÌÅÐÈÒÅËÜÍÛÕ ÐÎÁÎÒÀÕ |
201–204 |
|
Ëåùåíêî Þ.Ï. |
HOW IT WORKS COORDINATE MEASURING machines
and intelligent measurement ROBOTS |
ÏÐÈÍÖÈÏ ÐÎÁÎÒÈ
ÊÎÎÐÄÈÍÀÒÍÎ-ÂÈ̲ÐÞÂÀËÜÍÈÕ ÌÀØÈÍ ÒÀ ²ÍÒÅËÅÊÒÓÀËÜÍÈÕ ÂÈ̲ÐÞÂÀËÜÍÈÕ ÐÎÁÎҲ |
ÏÐÈÍÖÈÏ ÐÀÁÎÒÛ
ÊÎÎÐÄÈÍÀÒÍÎ-ÈÇÌÅÐÈÒÅËÜÍÛÕ ÌÀØÈÍ È ÈÍÒÅËËÅÊÒÓÀËÜÍÛÕ ÈÇÌÅÐÈÒÅËÜÍÛÕ ÐÎÁÎÒÎÂ |
205–208 |
Êâàñí³êîâ Â.Ï., |
THE CONTROL SYSTEM CONSTRUCTION OF AN AUTONOMOUS
MOBILE ROBOT BASED ON MULTILEVEL SYSTEM OF CONVERTING INFORMATION |
ÏÎÑÒÐÎÅÍÈÅ
ÑÈÑÒÅÌÛ ÓÏÐÀÂËÅÍÈß ÀÂÒÎÍÎÌÍÛÌ ÌÎÁÈËÜÍÛÌ ÐÎÁÎÒÎÌ ÍÀ ÎÑÍÎÂÅ ÌÍÎÃÎÓÐÎÂÍÅÂÎÉ
ÑÈÑÒÅÌÛ ÏÐÅÎÁÐÀÇÎÂÀÍÈß ÈÍÔÎÐÌÀÖÈÈ |
209–212 |
|
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 |
Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè
ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè |
||||
Ñâèñòóíîâ Â.À. |
Intelligent control systemS with multi-level information
transformation FOR AIRCRAFT ENTERPRISE |
ÈíòåëËåêòóàëüíÛÅ
ñèñòåìÛ ÓÏÐÀÂËÅÍÈß Ñ ÌÍÎÃÎÓÐÎÂÍÅÂÛÌ ÏÐÅÎÁÐÀÇÎÂÀÍÈÅÌ ÈíôîðìàöÈÈ íà àâÈàöÈÎÍÍÎÌ
ÏÐÅÄÏÐÈßÒÈÈ |
219–222 |
|
Àìèíå Õàäè |
CUSTOMER RELATIONSHIP MANAGEMENT
CRM |
ÑÈÑÒÅÌÀ
ÓÏÐÀÂ˲ÍÍß ÂÇÀªÌÈÍÀÌÈ Ç Ê˲ªÍÒÀÌÈ CRM |
223–228 |
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).