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

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ  ² ÒÅÕÍÎËÎòß. – 2012. – ¹ 6(93). – 124 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2012. – ¹ 6(93). – 124 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2012. – ¹ 6(93). – 124 ñ.

 

ÑÒÀÒÜè (articleS)

 

Àâòîðû
(ÿçûê
îðèãèíàëà)

Íàçâàíèå ñòàòüè  (article title)

Ñòðàíèöû

(pages)

English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Ãàéäà÷óê Â.Å. ,
Êîâàëåíêî Â.À.

LEVELS OF STRUCTURAL DEFECTS THAT ARISE DURING MANUFACTURING PRODUCTS MADE OF POLYMERIC COMPOSITE MATERIALS

вÂͲ ÄÅÔÅÊҲ ÑÒÐÓÊÒÓÐÈ Ó ÂÈÐÎÁÀÕ ²Ç ÏÎ˲ÌÅÐÍÈÕ ÊÎÌÏÎÇÈÖ²ÉÍÈÕ ÌÀÒÅвÀ˲Â, ÙÎ ÂÈÍÈÊÀÞÒÜ Â ÏÐÎÖÅѲ ¯Õ ÂÈÐÎÁÍÈÖÒÂÀ

ÓÐÎÂÍÈ ÄÅÔÅÊÒÎÂ ÑÒÐÓÊÒÓÐÛ Â ÈÇÄÅËÈßÕ ÈÇ ÏÎËÈÌÅÐÍÛÕ ÊÎÌÏÎÇÈÖÈÎÍÍÛÕ ÌÀÒÅÐÈÀËÎÂ, ÂÎÇÍÈÊÀÞÙÈÕ Â ÏÐÎÖÅÑÑÅ ÈÕ ÏÐÎÈÇÂÎÄÑÒÂÀ

5–12
(8)

×åñíîêîâ Î.Â.,
×îðíà Â.².,
Íàáîê³í Î.Ì.

DETERMINATION OF GEOMETRY OF AREA OF DEFORMATION AT ROTARY EXTRACTION OF THECAL DETAILS WITHOUT INTENTIONAL THINNING

ÂÈÇÍÀ×ÅÍÍß ÃÅÎÌÅÒв¯ ÎÑÅÐÅÄÊÓ ÄÅÔÎÐÌÀÖ²¯ ÏÐÈ ÐÎÒÀÖ²ÉÍ²É ÂÈÒֲ߯ ÎÁÎËÎÍÊÎÂÈÕ ÄÅÒÀËÅÉ ÁÅÇ ÍÀÂÌÈÑÍÎÃÎ ÑÒÎÍØÓÂÀÍÍß

ÎÏÐÅÄÅËÅÍÈÅ ÃÅÎÌÅÒÐÈÈ ÎÁËÀÑÒÈ ÄÅÔÎÐÌÀÖÈÈ ÏÐÈ ÐÎÒÀÖÈÎÍÍÎÉ ÂÛÒ߯ÊÅ ÎÁÎËÎ×ÊÎÂÛÕ ÄÅÒÀËÅÉ ÁÅÇ ÏÐÅÄÍÀÌÅÐÅÍÍÎÃÎ ÓÒÎÍÅÍÈß

13–17
(5)

Äîëìàòîâ À.È.,
Êóðèí Ì.À.,
Íèæíèê Ñ.Í.,
Ïåòðåíêî À.Ï.

DEFINITION ACTIVE SURFACE AREA OF CUTTING ABRASIVE GRAIN

ÂÈÇÍÀ×ÅÍÍß ÏËÎÙ² ÀÊÒÈÂÍί ÏÎÂÅÐÕͲ вÆÓ×ÎÃÎ ÀÁÐÀÇÈÂÍÎÃÎ ÇÅÐÍÀ

ÎÏÐÅÄÅËÅÍÈÅ ÏËÎÙÀÄÈ ÀÊÒÈÂÍÎÉ ÏÎÂÅÐÕÍÎÑÒÈ ÐÅÆÓÙÅÃÎ ÀÁÐÀÇÈÂÍÎÃÎ ÇÅÐÍÀ

18–21
(4)

Êðó÷èíà Â.Â.

INFLUENCE OF PHYSICAL PROCESSES OF TREATMENT TO LIQUID WASTE PRODUCTION

ÂÏËÈ ԲÇÈ×ÍÈÕ ÏÐÎÖÅѲ ÎÁÐÎÁÊÈ ÍÀ вÄÊÈ Â²ÄÕÎÄÈ ÂÈÐÎÁÍÈÖÒÂÀ

ÂËÈßÍÈÅ ÔÈÇÈ×ÅÑÊÈÕ ÏÐÎÖÅÑÑΠÎÁÐÀÁÎÒÊÈ ÍÀ ÆÈÄÊÈÅ ÎÒÕÎÄÛ ÏÐÎÈÇÂÎÄÑÒÂÀ

22–26
(5)

Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Ôèëèïêîâñêèé Ñ.Â. 

LONGITUDINAL VIBRATIONS OF FUEL AT ROCKET FUEL PIPELINE WITH NONLINEAR ELASTIC ELEMENT

ÏÎÇÄÎÂÆÍ² ÊÎËÈÂÀÍÍß ÏÀËÈÂÀ  ÒÐÓÁÎÏÐÎÂÎIJ ÐÀÊÅÒÈ Ç ÍÅ˲ͲÉÍÈÌ ÏÐÓÆÍÈÌ ÅËÅÌÅÍÒÎÌ

ÏÐÎÄÎËÜÍÛÅ ÊÎËÅÁÀÍÈß ÒÎÏËÈÂÀ Â ÒÐÓÁÎÏÐÎÂÎÄÅ ÐÀÊÅÒÛ Ñ ÍÅËÈÍÅÉÍÛÌ ÓÏÐÓÃÈÌ ÝËÅÌÅÍÒÎÌ

27–32
(6)

Èâàíîâ Ï.È.,
Êóÿíîâ À.Þ.

Analysis of deployment of a gliding parachute with a slider

ÀÍÀË²Ç ïðîöåñó íàïîâíåííÿ ÏËÀͲÐÓÞ×ÎÃÎ ïàðàøóòó ç³ ñëàéäåðîì

ÀÍÀËÈÇ ÏÐÎÖÅÑÑÀ ÍÀÏÎËÍÅÍÈß ÏËÀÍÈÐÓÞÙÅÃÎ ÏÀÐÀØÞÒÀ ÑÎ ÑËÀÉÄÅÐÎÌ

33–36
(4)

Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ

Ïðèõîäüêî À.À.,
Àëåêñååíêî Ñ.Â.

Ice Accretion: icing conditions AND CALCULATION PROCEDURES

ÎÁÌÅÐÇÀÍÍß ÀÅÐÎÄÈÍÀ̲×ÍÈÕ ÏÎÂÅÐÕÎÍÜ: ÓÌÎÂÈ ÂÈÍÈÊÀÍÍß ÒÀ ÌÅÒÎÄÈÊÈ ÐÎÇÐÀÕÓÍÊÓ

ÎÁËÅÄÅÍÅÍÈÅ ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÏÎÂÅÐÕÍÎÑÒÅÉ: ÓÑËÎÂÈß ÂÎÇÍÈÊÍÎÂÅÍÈß È ÌÅÒÎÄÈÊÈ ÐÀÑ×ÅÒÀ

37–47
(11)

Îâ÷àðîâ Ì.Ì.

METHOD OF CALCULATION OF NONLINEAR AERODYNAMIC CHARACTERISTICS OF AIRCRAFT AT ASYMMETRICAL FLOWING AROUND

ÌÅÒÎÄÈÊÀ ÐÎÇÐÀÕÓÍÊÓ ÍÅ˲ͲÉÍÈÕ ÀÅÐÎÄÈÍÀ̲×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ Ë²ÒÀËÜÍÎÃÎ ÀÏÀÐÀÒÓ ÏÐÈ ÍÅÑÈÌÅÒÐÈ×ÍÎÌÓ ÎÁÒ²ÊÀÍͲ

ÌÅÒÎÄÈÊÀ ÐÀÑ×ÅÒÀ ÍÅËÈÍÅÉÍÛÕ ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ËÅÒÀÒÅËÜÍÎÃÎ ÀÏÏÀÐÀÒÀ ÏÐÈ ÍÅÑÈÌÌÅÒÐÈ×ÍÎÌ ÎÁÒÅÊÀÍÈÈ

48–52
(5)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Loboda I.,
Rios Urban E.,
Sanchez Cruces E.

PROBABILISTIC NEURAL NETWORKS FOR GAS TURBINE FAULT RECOGNITION

²ÌβÐͲÑͲ ÍÅÉÐÎÍͲ ÌÅÐÅÆ² ÄËß ÐÎÇϲÇÍÀÂÀÍÍß ÄÅÔÅÊҲ ÃÒÄ

ÂÅÐÎßÒÍÎÑÒÍÛÅ ÍÅÉÐÎÍÍÛÅ ÑÅÒÈ ÄËß ÐÀÑÏÎÇÍÀÂÀÍÈß ÄÅÔÅÊÒÎÂ ÃÒÄ

53–58
(6)

Ðàä÷åíêî À.Í.,
Ðàä÷åíêî Í.È.,
Êîíîâàëîâ  À.Â.

COOLING OF INTAKE AIR AND CHARGED GAS-AIR MIXTURE OF RECIPROCATING GAS ENGINE FOR INTEGRATED ENERGY SYSTEM

ÎÕÎËÎÄÆÅÍÍß ÏβÒÐß ÍÀ ÂÕÎIJ ÒÀ ÍÀÄÄÓÂÍί ÃÀÇÎÏβÒÐßÍί ÑÓ̲ز ÃÀÇÎÏÎÐØÍÅÂÎÃÎ ÄÂÈÃÓÍÀ ÓÑÒÀÍÎÂÊÈ ÀÂÒÎÍÎÌÍÎÃÎ ÅÍÅÐÃÎÇÀÁÅÇÏÅ×ÅÍÍß

ÎÕËÀÆÄÅÍÈÅ ÂÎÇÄÓÕÀ ÍÀ ÂÕÎÄÅ È ÍÀÄÄÓÂÎ×ÍÎÉ ÃÀÇÎÂÎÇÄÓØÍÎÉ ÑÌÅÑÈ ÃÀÇÎÏÎÐØÍÅÂÎÃÎ ÄÂÈÃÀÒÅËß ÓÑÒÀÍÎÂÊÈ ÀÂÒÎÍÎÌÍÎÃÎ ÝÍÅÐÃÎÎÁÅÑÏÅ×ÅÍÈß

59–63
(5)

Àçàðíîâ À.Ë.,
Áåçðó÷êî Ê.Â.,
Äàâèäîâ À.Î.,
Ëàçíåíêî Â.È.,
Ôðîëîâ Â.Ï.,
Õàð÷åíêî À.À.,
Øèðèíñêèé Ñ.Â.

THE USE OF SEALED LEAD-ACID BATTERIES IN THE PROCESSING EQUIPMENT OF THE LAUNCHER OF THE LAUNCH VEHICLES IN ALCANTARA SPACEPORT

ÂÈÊÎÐÈÑÒÀÍÍß ÃÅÐÌÅÒÈ×ÍÈÕ ÑÂÈÍÖÅÂÎ-ÊÈÑËÎÒÍÈÕ ÀÊÓÌÓËßÒÎв  ÒÅÕÍÎËÎò×ÍÎÌÓ ÎÁËÀÄÍÀÍͲ ÑÒÀÐÒÎÂÈÕ ÊÎÌÏËÅÊѲ ÐÀÊÅÒÎÍÎѲ¯Â  ÓÌÎÂÀÕ

ÏÐÈÌÅÍÅÍÈÅ ÃÅÐÌÅÒÈ×ÍÛÕ ÑÂÈÍÖÎÂÎ-ÊÈÑËÎÒÍÛÕ ÀÊÊÓÌÓËßÒÎÐΠ ÒÅÕÍÎËÎÃÈ×ÅÑÊÎÌ ÎÁÎÐÓÄÎÂÀÍÈÈ ÑÒÀÐÒÎÂÛÕ ÊÎÌÏËÅÊÑΠÐÀÊÅÒÎÍÎÑÈÒÅËÅÉ Â ÓÑËÎÂÈßÕ ÊÎÑÌÎÄÐÎÌÀ ÀËÊÀÍÒÀÐÀ

64–68
(5)

Àíäðååâà Ò.Ï.,
Èâàíîâà Ë.Å.,
Ãóáàéäóëëèí È.Ò.

THE TECHNICAL OBJECTS POWER PLANTS FLAME CONTROL SYSTEM SKP

ÑÈÑÒÅÌÀ ÊÎÍÒÐÎËÞ ÏÎËÓÌ'ß ÑÊÏ ÄËß ÅÍÅÐÃÎÓÑÒÀÍÎÂÎÊ ÒÅÕͲ×ÍÈÕ ÎÁ'ªÊÒ²Â

ÑÈÑÒÅÌÀ ÊÎÍÒÐÎËß ÏËÀÌÅÍÈ ÑÊÏ ÄËß ÝÍÅÐÃÎÓÑÒÀÍÎÂÎÊ ÒÅÕÍÈ×ÅÑÊÈÕ ÎÁÚÅÊÒÎÂ

69–72
(4)

Êîíîâàëîâ Ä.Â.,
Äæóðèíñüêà À.Î.

THE  METHODOLOGICAL approach NEAR COOLING OF  scavenging AIR OF medium speed  ENGINE

ÌÅÒÎÄÎËÎò×ÍÈÉ Ï²ÄÕ²Ä ÄÎ ÎÕÎËÎÄÆÅÍÍß ÍÀÄÄÓÂÍÎÃÎ ÏβÒÐß ÑÅÐÅÄÍÜÎÎÁÅÐÒÎÂÎÃÎ ÄÂÈÃÓÍÀ

ÌÅÒÎÄÎËÎÃÈ×ÅÑÊÈÉ ÏÎÄÕÎÄ Ê ÎÕËÀÆÄÅÍÈÞ ÍÀÄÄÓÂÎ×ÍÎÃÎ ÂÎÇÄÓÕÀ ÑÐÅÄÍÅÎÁÎÐÎÒÍÎÃÎ ÄÂÈÃÀÒÅËß

73–78
(6)

Øåìåíòîâ À.Í.,
Ôèëèïïåíêî Ï.Ï.

CENTRIFUGAL PUMP DESIGN WITH USING OF MAIN PUMP EXPERIMENTAL DATA

ÏÐÎÅÊÒÓÂÀÍÍß Â²ÄÖÅÍÒÐÎÂÎÃÎ ÍÀÑÎÑÓ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÐÅÇÓËÜÒÀҲ ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÈÕ ÄÎÑË²ÄÆÅÍÜ ÁÀÇÎÂÎÃÎ ÍÀÑÎÑÓ

ÏÐÎÅÊÒÈÐÎÂÀÍÈÅ ÖÅÍÒÐÎÁÅÆÍÎÃÎ ÍÀÑÎÑÀ Ñ ÈÑÏÎËÜÇÎÂÀÍÈÅÌ ÐÅÇÓËÜÒÀÒÎÂ ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÛÕ ÈÑÑËÅÄÎÂÀÍÈÉ ÁÀÇÎÂÎÃÎ ÍÀÑÎÑÀ

79–84
(6)

Èíôîðìàöèîííûå òåõíîëîãèè

Íàóìåíêî À.Â.,
Ëóêèí Â.Â.

NEURAL NETWORK SAR-IMAGE EDGE DETECTION USING PRELIMINARY FILTERING

ÂÈßÂËÅÍÍß ÌÅÆ ÍÀ ÐÑÀ-ÇÎÁÐÀÆÅÍÍßÕ ÍÅÉÐÎÌÅÐÅÆÅÞ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÏÎÏÅÐÅÄÍÜί Ô²ËÜÒÐÀÖ²¯

ÎÁÍÀÐÓÆÅÍÈÅ ÃÐÀÍÈÖ ÍÀ ÐÑÀ ÈÇÎÁÐÀÆÅÍÈßÕ ÍÅÉÐÎÑÒÜÞ Ñ ÏÐÈÌÅÍÅÍÈÅÌ ÏÐÅÄÂÀÐÈÒÅËÜÍÎÉ ÔÈËÜÒÐÀÖÈÈ

85–94
(10)

²çáàø Þ.Ì.

SYNTHESIS OF SYSTEM OF DIAGNOSTICS OF THE MEASURING ROBOT

ÑÈÍÒÅÇ ÑÈÑÒÅÌÈ Ä²ÀÃÍÎÑÒÈÊÈ ÂÈ̲ÐÞÂÀËÜÍÎÃÎ ÐÎÁÎÒÀ

ÑÈÍÒÅÇ ÑÈÑÒÅÌÛ ÄÈÀÃÍÎÑÒÈÊÈ ÈÇÌÅÐÈÒÅËÜÍÎÃÎ ÐÎÁÎÒÀ

95–98
(4)

Çåìëÿ÷åíêî À.Í.,
Êîæåìÿêèí Ð.À.,
Àáðàìîâ Ñ.Ê.,
Ëóêèí Â.Â.,
×îáàíó Ì.Ê.

AUTOMATIC IMAGE COMPRESSION IN THE NEIGHBORHOOD OF OPTIMAL OPERATION POINT BASED ON MODEL OF HUMAN VISION SYSTEM FOR SIGNAL-DEPENDENT NOISE

ÀÂÒÎÌÀÒÈ×ÍÅ ÑÒÈÑÍÅÍÍß ÇÎÁÐÀÆÅÍÜ Â ÎÊÎËÈÖ² ÎÏÒÈÌÀËÜÍί ÐÎÁÎ×ί ÒÎ×ÊÈ Ç ÓÐÀÕÓÂÀÍÍßÌ Â²ÇÓÀËÜÍί ÌÎÄÅ˲ ÑÏÐÈÉÍßÒÒß ËÞÄÈÍÈ ÏÐÈ ÑÈÃÍÀËÜÍÎ-ÇÀËÅÆÍÈÕ ÇÀÂÀÄÀÕ

ÀÂÒÎÌÀÒÈ×ÅÑÊÎÅ ÑÆÀÒÈÅ ÈÇÎÁÐÀÆÅÍÈÉ Â ÎÊÐÅÑÒÍÎÑÒÈ ÎÏÒÈÌÀËÜÍÎÉ ÐÀÁÎ×ÅÉ ÒÎ×ÊÈ Ñ Ó×ÅÒÎÌ ÂÈÇÓÀËÜÍÎÉ ÌÎÄÅËÈ ÂÎÑÏÐÈßÒÈß ×ÅËÎÂÅÊÀ ÏÐÈ ÑÈÃÍÀËÜÍÎ-ÇÀÂÈÑÈÌÛÕ ÏÎÌÅÕÀÕ

99–108
(10)

Haein Ò.

TEMPERATURE ERRORS MODELING OF COORDINATE MEASURING MACHINES

ÌÎÄÅËÞÂÀÍÍß ÒÅÌÏÅÐÀÒÓÐÍÈÕ ÏÎÕÈÁÎÊ ÍÀ ÊÎÎÐÄÈÍÀÒÍÎ-ÂÈ̲ÐÞÂÀËÜÍÈÕ ÌÀØÈÍÀÕ

ÌÎÄÅËÈÐÎÂÀÍÈÅ ÒÅÌÏÅÐÀÒÓÐÍÛÕ ÏÎÃÐÅØÍÎÑÒÅÉ ÍÀ ÊÎÎÐÄÈÍÀÒÍÎ-ÈÇÌÅÐÈÒÅËÜÍÛÕ ÌÀØÈÍÀÕ

109–112
(4)

Ìàêàðîâ À.Ë.,
Ìîçãîâîé Ä.Ê.,
Êóëàáóõîâ À.Ì.,
Õîðîøèëîâ Â.Ñ.,
Îëüøåâñêèé À.Ë.,
Ïîïåëü Â.Ì.

efficiency INCREASING OF SATELLITE SURVEY OF extensive TERRITORY with complex configuration

ϲÄÂÈÙÅÍÍß ÎÏÅÐÀÒÈÂÍÎÑÒ² ÑÓÏÓÒÍÈÊÎÂί ÇÉÎÌÊÈ ÏÐÎÒ߯ÍÈÕ ÒÅÐÈÒÎÐ²É ÑÊËÀÄÍί ÊÎÍÔ²ÃÓÐÀÖ²¯

ÏÎÂÛØÅÍÈÅ ÎÏÅÐÀÒÈÂÍÎÑÒÈ ÑÏÓÒÍÈÊÎÂÎÉ ÑÚÅÌÊÈ ÏÐÎÒ߯ÅÍÍÛÕ ÒÅÐÐÈÒÎÐÈÉ ÑËÎÆÍÎÉ ÊÎÍÔÈÃÓÐÀÖÈÈ

113–122
(10)

 

 

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).