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

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ  ² ÒÅÕÍÎËÎòß. – 2012. – ¹ 4(91). – 122 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2012. – ¹ 4(91). – 122 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2012. – ¹ 4(91). – 122 p.

 

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Àâòîðû
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îðèãèíàëà)

Íàçâàíèå ñòàòüè  (article title)

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English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Êîâàëåíêî Â.À.

 

RESEARCHING OF DEFECTS RESULTING IN PRODUCTION AGGREGATES OF ROCKET AND SPACE TECHNOLOGY MADE OF POLYMERIC COMPOSITE MATERIALS. REPORT 2. TOLERANCES FOR MATERIAL DISCONTINUITY AND THE LOCAL PRODUCT STRAINS

ÄÎÑË²ÄÆÅÍÍß ÒÅÕÍÎËÎò×ÍÈÕ ÄÅÔÅÊÒ²Â, ÙÎ ÂÈÍÈÊÀÞÒÜ Ó ÂÈÐÎÁÍÈÖÒ² ÀÃÐÅÃÀҲ ÐÀÊÅÒÍÎ-ÊÎÑ̲×Íί ÒÅÕͲÊÈ Ç ÏÎ˲ÌÅÐÍÈÕ ÊÎÌÏÎÇÈÖ²ÉÍÈÕ ÌÀÒÅвÀ˲Â. ÏβÄÎÌËÅÍÍß 2. ÄÎÏÓÑÊÈ ÍÀ ÏÎÐÓØÅÍÍß ÑÓÖ²ËÜÍÎÑÒ² ÌÀÒÅвÀËÓ ÒÀ ËÎÊÀËÜͲ ÏÎÂÎÄÊÈ ÂÈÐÎÁÓ

ÈÑÑËÅÄÎÂÀÍÈÅ ÒÅÕÍÎËÎÃÈ×ÅÑÊÈÕ ÄÅÔÅÊÒÎÂ, ÂÎÇÍÈÊÀÞÙÈÕ Â ÏÐÎÈÇÂÎÄÑÒÂÅ ÀÃÐÅÃÀÒΠÐÀÊÅÒÍÎ-ÊÎÑÌÈ×ÅÑÊÎÉ ÒÅÕÍÈÊÈ ÈÇ ÏÎËÈÌÅÐÍÛÕ ÊÎÌÏÎÇÈÖÈÎÍÍÛÕ ÌÀÒÅÐÈÀËÎÂ. ÑÎÎÁÙÅÍÈÅ 2. ÄÎÏÓÑÊÈ ÍÀ ÍÀÐÓØÅÍÈß ÑÏËÎØÍÎÑÒÈ ÌÀÒÅÐÈÀËÀ È ËÎÊÀËÜÍÛÅ ÏÎÂÎÄÊÈ ÈÇÄÅËÈß

5–15
(11)

Øåðñòþê Ä.Ã.,
Øåðñòþê Ã.Ã.,
Ôîê³í À.À.,
Ñîøí³êîâ ª.À.,
Êóëèê Î.Â.

SETTLEMENT AND ANALYTICAL DETERMINATION PROCESS PARAMETERS OF THE THERMOMECHANICAL CALIBRATION OF LARGE SHELLS WITH INTERNAL FUNCTIONAL ELEMENTS

ÐÎÇÐÀÕÓÍÊÎÂÎ-ÀÍÀ˲ÒÈ×ÍÅ ÂÈÇÍÀ×ÅÍÍß ÏÀÐÀÌÅÒв ÏÐÎÖÅÑÓ ÒÅÐÌÎÌÅÕÀͲ×ÍÎÃÎ ÊÀ˲ÁÐÓÂÀÍÍß ÂÅËÈÊÎÃÀÁÀÐÈÒÍÈÕ ÎÁÈ×ÀÉÎÊ Ç ÂÍÓÒвØÍ²ÌÈ ÔÓÍÊÖ²ÎÍÀËÜÍÈÌÈ ÅËÅÌÅÍÒÀÌÈ

ÐÀÑ×ÅÒÍÎ-ÀÍÀËÈÒÈ×ÅÑÊÎÅ ÎÏÐÅÄÅËÅÍÈÅ ÏÀÐÀÌÅÒÐΠÏÐÎÖÅÑÑÀ ÒÅÐÌÎÌÅÕÀÍÈ×ÅÑÊÎÃÎ ÊÀËÈÁÐÎÂÀÍÈß ÊÐÓÏÍÎÃÀÁÀÐÈÒÍÛÕ ÎÁÅ×ÀÅÊ Ñ ÂÍÓÒÐÅÍÍÈÌÈ ÔÓÍÊÖÈÎÍÀËÜÍÛÌÈ ÝËÅÌÅÍÒÀÌÈ

16–22
(7)

Ñåðãååâ À.À.,
Øåïåëü Â.Ò.

EXPERIMENTAL STUDY OF DAMAGING OF COMPOSITE ACOUSTIC PANELS OF AVIATION GAS-TURBINE ENGINES

ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ ÄÎÑË²ÄÆÅÍÍß ÓØÊÎÄÆÓªÌÎÑÒ² ÊÎÌÏÎÇÈÒÍÈÕ ÀÊÓÑÒÈ×ÍÈÕ ÏÀÍÅËÅÉ À²ÀÖ²ÉÎÍÎÃÎ ÃÒÄ

ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÅ ÈÑÑËÅÄÎÂÀÍÈÅ ÏÎÂÐÅÆÄÀÅÌÎÑÒÈ ÊÎÌÏÎÇÈÒÍÛÕ ÀÊÓÑÒÈ×ÅÑÊÈÕ ÏÀÍÅËÅÉ ÀÂÈÀÖÈÎÍÍÎÃÎ ÃÒÄ

23–26
(4)

Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Êàëèíè÷åíêî Ä.Ñ.,
Àêñ¸íåíêî À.Â.,
Êàøàíîâ À.Ý.,
Ïîëóÿí Í.Â.,
Òàðàñîâ Â.Å.

THE METHODOLOGICAL APPROACH TO DESIGNING OF SPSCE TRANSPORTATION SYSTEM

ÌÅÒÎÄÎËÎò×ÍÈÉ Ï²ÄÕ²Ä ÄÎ ÏÐÎÅÊÒÓÂÀÍÍß ÒÐÀÍÑÏÎÐÒÍÎ-ÊÎÑ̲×Íί ÑÈÑÒÅÌÈ

ÌÅÒÎÄÈ×ÅÑÊÈÉ ÏÎÄÕÎÄ Ê ÏÐÎÅÊÒÈÐÎÂÀÍÈÞ ÒÐÀÍÑÏÎÐÒÍÎ-ÊÎÑÌÈ×ÅÑÊÎÉ ÑÈÑÒÅÌÛ

27–32
(6)

Êîâàëåâ Â.À.

THE VELOCITY DISTRIBUTION FEATURES IN AXISYMMETRIC FLOWS WITH BAFFLES

ÎÑÎÁËÈÂÎÑÒ² ÐÎÇÏÎIJËÓ ØÂÈÄÊÎÑÒÅÉ Ó Â²ÑÅÑÈÌÅÒÐÈ×ÍÈÕ ÒÅײßÕ Ç ÏÅÐÅÃÎÐÎÄÊÀÌÈ

ÎÑÎÁÅÍÍÎÑÒÈ ÐÀÑÏÐÅÄÅËÅÍÈß ÑÊÎÐÎÑÒÅÉ Â ÎÑÅÑÈÌÌÅÒÐÈ×ÍÛÕ ÒÅ×ÅÍÈßÕ Ñ ÏÅÐÅÃÎÐÎÄÊÀÌÈ

33–37
(5)

Ìèíòþê Â.Á.

RESEARCH OF GEOMETRICALLY AND PHYSICALLY NONLINEAR GENERALIZED PLANE STRESS

ÄÎÑË²ÄÆÅÍÍß ÃÅÎÌÅÒÐÈ×ÍÎ ÒÀ Ô²ÇÈ×ÍÎ ÍÅ˲ͲÉÍÎÃÎ ÓÇÀÃÀËÜÍÅÍÎÃÎ ÏËÎÑÊÎÃÎ ÍÀÏÐÓÆÅÍÎÃÎ ÑÒÀÍÓ

ÈÑÑËÅÄÎÂÀÍÈÅ ÃÅÎÌÅÒÐÈ×ÅÑÊÈ È ÔÈÇÈ×ÅÑÊÈ ÍÅËÈÍÅÉÍÎÃÎ ÎÁÎÁÙÅÍÍÎÃÎ ÏËÎÑÊÎÃÎ ÍÀÏÐ߯ÅÍÍÎÃÎ ÑÎÑÒÎßÍÈß

38–44
(7)

Æóíü Ã.Ã.

REVEALING AND ELIMINATION DEFECTS IN CRYOVESSELS

ÂÈßÂËÅÍÍß ÒÀ ÓÑÓÍÅÍÍß ÄÅÔÅÊÒ²Â Ó ÊвÎÏÎÑÓÄÀÕ

ÂÛßÂËÅÍÈÅ È ÓÑÒÐÀÍÅÍÈÅ ÄÅÔÅÊÒΠ ÊÐÈÎÑÎÑÓÄÀÕ

45–49
(5)

Íåæâåä³ëîâ À.Þ.

CALCULATION OF THE STRESS-DEFORMATION OF COMPRESSOR BLADES AIRCRAFT GAS TURBINE ENGINE THE FINITE-ELEMENT ANALYSIS

ÐÎÇÐÀÕÓÍÎÊ ÍÀÏÐÓÆÅÍÎ-ÄÅÔÎÐÌÎÂÀÍÎÃÎ ÑÒÀÍÓ ËÎÏÀÒÊÈ ÊÎÌÏÐÅÑÎÐÀ À²ÀÖ²ÉÍÎÃÎ ÃÀÇÎÒÓÐÁ²ÍÍÎÃÎ ÄÂÈÃÓÍÀ Dz Ç̲ÖÍÅÍÈÌ ÏÎÂÅÐÕÍÅÂÈÌ ØÀÐÎÌ ÌÅÒÎÄÎÌ Ê²ÍÖÅÂÎ-ÅËÅÌÅÍÒÍÎÃÎ ÀÍÀ˲ÇÓ

ÐÀÑ×ÅÒ ÍÀÏÐ߯ÅÍÍÎ-ÄÅÔÎÐÌÈÐÎÂÀÍÎÃÎ ÑÎÑÒÎßÍÈß ËÎÏÀÒÊÈ ÊÎÌÏÐÅÑÑÎÐÀ ÀÂÈÀÖÈÎÍÍÎÃÎ ÃÀÇÎÒÓÐÁÈÍÍÎÃÎ ÄÂÈÃÀÒÅËß ÌÅÒÎÄÎÌ ÊÎÍÅ×ÍÎ-ÝËÅÌÅÍÒÍÎÃÎ ÀÍÀËÈÇÀ

50–54
(5)

Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ

Ôèðñîâ Ñ.Í.

ANALYTICAL METHOD FOR THE DETERMINATION OF THE PARAMETERS OF ORIENTATION OF SPACECRAFT

ÀÍÀ˲ÒÈ×ÍÈÉ ÌÅÒÎÄ ÂÈÇÍÀ×ÅÍÍß ÏÀÐÀÌÅÒв ÓÏÐÀÂ˲ÍÍß ÑÈÑÒÅÌÈ ÎвªÍÒÀÖ²¯ ÊÎÑ̲×ÍÎÃÎ ÀÏÀÐÀÒÓ

ÀÍÀËÈÒÈ×ÅÑÊÈÉ ÌÅÒÎÄ ÎÏÐÅÄÅËÅÍÈß ÏÀÐÀÌÅÒÐΠÓÏÐÀÂËÅÍÈß ÑÈÑÒÅÌÛ ÎÐÈÅÍÒÀÖÈÈ ÊÎÑÌÈ×ÅÑÊÎÃÎ ÀÏÏÀÐÀÒÀ

55–59
(5)

Kulik A.S.,
Martinez-Bastida J.P.

AN IMPROVED FAULT-TOLERANT ALGORITHM FOR A GYROSCOPIC SENSORS UNIT

Óäîñêîíàëåíèé àëãîðèòì â³äìîâîñò³éêîñò³ äëÿ áëîêó ã³ðîñêîï³÷íèõ äàò÷èê³â

Óñîâåðøåíñòîâàííûé àëãîðèòì îòêàçîóñòîé÷èâîñòè äëÿ  áëîêà ãèðîñêîïè÷åñêèõ äàò÷èêîâ

60–66
(
7)

Ãîðä³í Î.Ã.,
Ãóáà ª.À.

MEASURING UNIT OF STRAPDOWN INERTIAL NAVIGATION SYSTEM

ÂÈ̲ÐÞÂÀËÜÍÈÉ ÁËÎÊ ÁÅÇÊÀÐÄÀÍÍί ²ÍÅÐÖ²ÀËÜÍί ÍÀ²ÃÀÖ²ÉÍί ÑÈÑÒÅÌÈ

ÈÇÌÅÐÈÒÅËÜÍÛÉ ÁËÎÊ ÁÅÇÊÀÐÄÀÍÍÎÉ ÈÍÅÐÖÈÀËÜÍÎÉ ÍÀÂÈÃÀÖÈÎÍÍÎÉ ÑÈÑÒÅÌÛ

67–73
(7)

Åð¸ìåíêî Ñ.Ì.,
Êàñüÿíåíêî À.Á.,
Êóëåøîâ Â.È.

RESULTS OF RESEARCHES OF AERODYNAMIC CHARACTERISTICS OF NON-PLANAR WINGS

ÐÅÇÓËÜÒÀÒÈ ÄÎÑË²ÄÆÅÍÜ ÀÅÐÎÄÈÍÀ̲×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÍÅÏËÎÑÊÈÕ ÊÐÈË

ÐÅÇÓËÜÒÀÒÛ ÈÑÑËÅÄÎÂÀÍÈÉ ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÍÅÏËÎÑÊÈÕ ÊÐÛËÜÅÂ

74–78
(5)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Ñêîá Þ.À.

HEAT TRANSFER NUMERICAL MODELING IN COMPLEX SHAPED SOLIDS IN THERMAL CAMERAS

×ÈÑÅËÜÍÅ ÐÎÇÂ’ßÇÀÍÍß ÑÏÐ߯ÅÍί ÇÀÄÀײ ÒÅÏËÎÎÁ̲ÍÓ Â ÊÀÌÅÐÀÕ ÒÅÐÌÎÎÁÐÎÁÊÈ

×ÈÑËÅÍÍÎÅ ÐÅØÅÍÈÅ ÑÎÏÐ߯ÅÍÍÎÉ ÇÀÄÀ×È ÒÅÏËÎÎÁÌÅÍÀ  ÊÀÌÅÐÀÕ ÒÅÐÌÎÎÁÐÀÁÎÒÊÈ

79–83
(5)

Áëîõèí Â.È.,
Ìåðêóøèí Â.Ê.,
Âåëèêàíîâà Í.Ï.,
Èâàíîâ Ï.Â.

OPTIMIZING THE DESIGN PARAMETERS OF THE BUMER TO ADJUST THE CHARACTERISTICS OF THE TEMPERATURE FIELD WITHOUT DISMANTLING AND REMOVAL OF THE COMBUSTION CHAMBER BUMERS

ÎÏÒÈ̲ÇÀÖ²ß ÊÎÍÑÒÐÓÊÖ²¯ ïàëüíèêà ÄËß ÐÅÃÓËÞÂÀÍÍß ÏÀÐÀÌÅÒв ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÒÅÌÏÅÐÀÒÓÐÍÎÃÎ ÏÎËß ÁÅÇ ÐÎÇÁÈÐÀÍÍß ÊÀÌÅÐÈ ÇÃÎÐßÍÍß ² ÇͲÌÀÍÍß ÏÀËÜÍÈʲÂ

ÎÏÒÈÌÈÇÀÖÈß ÊÎÍÑÒÐÓÊÖÈÈ ÃÎÐÅËÊÈ ÄËß ÐÅÃÓËÈÐÎÂÊÈ ÏÀÐÀÌÅÒÐΠÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÒÅÌÏÅÐÀÒÓÐÍÎÃÎ ÏÎËß ÁÅÇ ÐÀÇÁÎÐÊÈ ÊÀÌÅÐÛ ÑÃÎÐÀÍÈß È ÑÚ¨ÌÀ ÃÎÐÅËÎÊ

84–87
(4)

Ñóááîòà À.Ì.,
Ðåçíèêîâà Î.Â.,
Àíäðóùåíêî Ò.Í.

FEATURES OF MOTOR-REACTION WHEELS on small spacecraft

ÎÑÎÁËÈÂÎÑÒ² ÇÀÑÒÎÑÓÂÀÍÍß ÄÂÈÃÓͲÂ-ìàõîâèê³â íà ìàëèõ êîñì³÷íèõ àïàðàòàõ

ÎÑÎÁÅÍÍÎÑÒÈ ÏÐÈÌÅÍÅÍÈß ÄÂÈÃÀÒÅËÅÉ-ÌÀÕÎÂÈÊΠÍÀ ÌÀËÛÕ ÊÎÑÌÈ×ÅÑÊÈÕ ÀÏÏÀÐÀÒÀÕ

88–92
(5)

Loyan A.V.,
Nesterenco S.U.,
Roshanpour S.

NON-EMISSION ELECTRON SOURCE WITH HIGH FREQUENCY IONIZATION

ÁÅÇÅ̲ѲÉÍÅ ÄÆÅÐÅËÎ ÅËÅÊÒÐÎÍ²Â Ç ÂÈÑÎÊÎ×ÀÑÒÎÒÍÎÞ ²ÎͲÇÀÖ²ªÞ

ÁÅÇÝÌÈÑÑÈÎÍÍÛÉ ÈÑÒÎ×ÍÈÊ ÝËÅÊÒÐÎÍÎÂ Ñ ÂÛÑÎÊÎ×ÀÑÒÎÒÍÎÉ ÈÎÍÈÇÀÖÈÅÉ

93–101
(9)

Ïàðîâàé Å.Ô.,
Ãîðäååâ Â.Á.,
Ôàëàëååâ Ñ.Â.

Calculation of the aviation engine's hydrodynamic bearing

ÐÎÇÐÀÕÓÍÎÊ Ã³äðîäèíàì³÷íîãî ï³äøèïíèêà ÎÏÎÐÈ À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ

ÐÀÑ×ÅÒ ÃÈÄÐÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÏÎÄØÈÏÍÈÊÀ ÎÏÎÐÛ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß

102–105
(4)

Èíôîðìàöèîííûå òåõíîëîãèè

Ðåâà Î.Ì.,
Êàìèøèí Â.Â.,
Íàñ³ðîâ Ø.Ø.

KEMENY’S MEDIAN AS GROUP SYSTEM OF PREFERENCES OF AIR TRAFFIC CONTROLLERS ON GREAT NUMBER OF CHARACTERISTIC ERRORS

ÌÅIJÀÍÀ ÊÅÌÅͲ ßÊ ÃÐÓÏÎÂÀ ÑÈÑÒÅÌÀ ÏÅÐÅÂÀà À²ÀÄÈÑÏÅÒ×Åв ÍÀ ÌÍÎÆÈͲ ÕÀÐÀÊÒÅÐÍÈÕ ÏÎÌÈËÎÊ

ÌÅÄÈÀÍÀ ÊÅÌÅÍÈ ÊÀÊ ÃÐÓÏÏÎÂÀß ÑÈÑÒÅÌÀ ÏÐÅÄÏÎ×ÒÅÍÈÉ ÀÂÈÀÄÈÑÏÅÒ×ÅÐΠÍÀ ÌÍÎÆÅÑÒÂÅ ÕÀÐÀÊÒÅÐÍÛÕ ÎØÈÁÎÊ

106–115
(10)

Êîëîìåíöåâ À.È.,
Õîõëîâ À.Í.

Software for building regression relationships parameters of complex technical systems

ÏÐÎÃÐÀÌÍÅ ÇÀÁÅÇÏÅ×ÅÍÍß ÄËß ÏÎÁÓÄÎÂÈ ðåãðåñ³éíî¿ çàëåæíîñò³ ÏÀÐÀÌÅÒв ÑÊËÀÄÍÈÕ ÒÅÕͲ×ÍÈÕ ÑÈÑÒÅÌ

ÏÐÎÃÐÀÌÌÍÎÅ ÎÁÅÑÏÅ×ÅÍÈÅ ÄËß ÏÎÑÒÐÎÅÍÈß ÐÅÃÐÅÑÑÈÎÍÍÛÕ ÇÀÂÈÑÈÌÎÑÒÅÉ ÏÀÐÀÌÅÒÐΠÑËÎÆÍÛÕ ÒÅÕÍÈ×ÅÑÊÈÕ ÑÈÑÒÅÌ

116–120
(5)

 

 

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).