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

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2015. – ¹ 9 (126). – 171 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2015. – ¹ 9 (126). – 171 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2015. – ¹ 9 (126). – 171 ñ.

 

 

Ìàòåðèàëû, ñîäåðæàùèåñÿ â æóðíàëå, îïóáëèêîâàíû
ïî ðåøåíèþ XX ìåæäóíàðîäíîãî êîíãðåññà äâèãàòåëåñòðîèòåëåé

 

ÑÒÀÒÜè (articleS)

 

Àâòîðû
(ÿçûê
îðèãèíàëà)

Íàçâàíèå ñòàòüè (article title)

Ñòðàíèöû

(pages)

English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Êîáçàðü Þ. Ì.

TO ASSESS THE DURABILITY TO FATIGUE SMOOTH CYLINDRICAL RODS UNDER UNIAXIAL SYMMETRIC STRETCHCOMPRESSION

ÄÎ ÎÖ²ÍÊÈ ÄÎÂÃβ×ÍÎÑÒ² ÏÐÈ ÂÒÎ̲ ÃËÀÄÊÈÕ ÖÈ˲ÍÄÐÈ×ÍÈÕ ÑÒÅÐÆÍ²Â ÏÐÈ ÎÄÍβÑÍÎÌÓ ÑÈÌÅÒÐÈ×ÍÎÌÓ ÐÎÇÒßÃÓ-ÑÒÈÑÊÓ

Ê ÎÖÅÍÊÅ ÓÑÒÀËÎÑÒÍÎÉ ÄÎËÃÎÂÅ×ÍÎÑÒÈ ÃËÀÄÊÈÕ ÖÈËÈÍÄÐÈ×ÅÑÊÈÕ ÑÒÅÐÆÍÅÉ ÏÐÈ ÎÄÍÎÎÑÍÎÌ ÑÈÌÌÅÒÐÈ×ÍÎÌ ÐÀÑÒ߯ÅÍÈÈ-ÑÆÀÒÈÈ

6–14
(9)

Ïîâãîðîäíèé Â. Î.

MODERN AREAS OF APPENDIX OF REVERSE TASKS OF MECHANICS AND THERMOMECHANICS

ÑÓ×ÀÑͲ ÃÀËÓDz ÂÈÊÎÐÈÑÒÀÍÍß ÎÁÅÐÍÅÍÈÕ ÇÀÄÀ× ÌÅÕÀͲÊÈ ÒÀ ÒÅÐÌÎÌÅÕÀͲÊÈ

ÑÎÂÐÅÌÅÍÍÛÅ ÎÁËÀÑÒÈ ÏÐÈËÎÆÅÍÈß ÎÁÐÀÒÍÛÕ ÇÀÄÀ× ÌÅÕÀÍÈÊÈ È ÒÅÐÌÎÌÅÕÀÍÈÊÈ

15–19
(5)

Ïîïóãà À. È.

MAIN DIRECTIONS OF REDUCTION OF AIRCRAFT NOISE

ÎÑÍÎÂͲ ÍÀÏÐßÌÊÈ ÇÌÅÍØÅÍÍß ØÓÌÓ ÏβÒÐßÍÈÕ ÑÓÄÅÍ

ÎÑÍÎÂÍÛÅ ÍÀÏÐÀÂËÅÍÈß ÓÌÅÍÜØÅÍÈß ØÓÌÀ ÂÎÇÄÓØÍÛÕ ÑÓÄÎÂ

20–25
(6)

Õîðÿê Í. Â.,
Íèêîëàåâ À. Ä.,
Äîëãîïîëîâ Ñ. È.

THEORETICAL EFFICIENCY ESTIMATION OF DYNAMIC DAMPER OF POGO VIBRATIONS OF LIQUID ROCKET LAUNCH VECHICLE

ÒÅÎÐÅÒÈ×ÍÀ ÎÖ²ÍÊÀ ÅÔÅÊÒÈÂÍÎÑÒ² ÄÈÍÀ̲×ÍÎÃÎ ÃÀÑÈÒÅËß ÏÎÇÄÎÂÆÍ²Õ ÊÎËÈÂÀÍÜ Ð²ÄÈÍÍÈÕ ÐÀÊÅÒ-ÍÎѲ¯Â

ÒÅÎÐÅÒÈ×ÅÑÊÀß ÎÖÅÍÊÀ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÃÀÑÈÒÅËß ÏÐÎÄÎËÜÍÛÕ ÊÎËÅÁÀÍÈÉ ÆÈÄÊÎÑÒÍÎÉ ÐÀÊÅÒÛ-ÍÎÑÈÒÅËß

26–32
(7)

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Ãàéäóê Ñ. Â.,
Òèõîìèðîâà Ò. Â.

APPLICATION OF ANALITIC METHODS TO CALCULATE OF CHEMICAL COMPOSITION γ-, γ'- PHASES AND PARAMETRIES PHASE STABILITIES CASTING NI-BASED SUPERALLOYS

ÇÀÑÒÎÑÓÂÀÍÍß ÀÍÀ˲ÒÈ×ÍÈÕ ÌÅÒÎIJ ÄËß ÐÎÇÐÀÕÓÍÊÓ Õ²Ì²×ÍÎÃÎ ÑÊËÀÄÓ γ-, γ'- ÔÀÇ ÒÀ ÏÀÐÀÌÅÒв ÔÀÇÎÂί ÑÒÀÁ²ËÜÍÎÑÒ² ËÈÂÀÐÍÈÕ ÆÀÐÎ̲ÖÍÈÕ Í²ÊÅËÅÂÈÕ ÑÏËÀ²Â

ÏÐÈÌÅÍÅÍÈÅ ÀÍÀËÈÒÈ×ÅÑÊÈÕ ÌÅÒÎÄΠÄËß ÐÀÑ×ÅÒÀ ÕÈÌÈ×ÅÑÊÎÃÎ ÑÎÑÒÀÂÀ γ-, γ'- ÔÀÇ È ÏÀÐÀÌÅÒÐΠÔÀÇÎÂÎÉ ÑÒÀÁÈËÜÍÎÑÒÈ ËÈÒÅÉÍÛÕ ÆÀÐÎÏÐÎ×ÍÛÕ ÍÈÊÅËÅÂÛÕ ÑÏËÀÂÎÂ

33–37
(5)

Ôðîëîâ Ã. À.,
Áîðîâèê Ä. Â.,
Êîëîòèëî À. Ä.,
Ëàìåêî À. Ë.,
Îëèãîâ Å. Â.,
Ïàíû÷ À. Â.,
Ïîòàïîâ À. Ì.,
Òèõèé Â. Ã.,
Ãóñàðîâà È. À.

IDENTIFICATION OF THERMOPHYSICAL PROPERTIES OF HONEYCOMB STRUCTURE SAMPLES WITHIN TEMPERATURE RANGING BETWEEN -60 AND + 250 °C AND UNDER PRESSURE BETWEEN 105 TO 10-1 PA

ÂÈÇÍÀ×ÅÍÍß ÒÅÏËÎÔ²ÇÈ×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÇÐÀÇʲ ÑÒ²ËÜÍÈÊÎÂÈÕ ÊÎÍÑÒÐÓÊÖ²É Â Ä²ÀÏÀÇÎͲ ÒÅÌÏÅÐÀÒÓÐ -60 ... + 250 ° Ñ ² ÒÈÑÊÓ Â²Ä 105 ÄÎ 10-1 ÏÀ

ÎÏÐÅÄÅËÅÍÈÅ ÒÅÏËÎÔÈÇÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÎÁÐÀÇÖΠÑÎÒÎÂÛÕ ÊÎÍÑÒÐÓÊÖÈÉ Â ÄÈÀÏÀÇÎÍÀÕ ÒÅÌÏÅÐÀÒÓÐ -60...+250 °Ñ È ÄÀÂËÅÍÈÉ ÎÒ 105 ÄÎ 10-1 ÏÀ

38–43
(6)

Ñîðîêèí Â. Ô.,
Êîìáàðîâà Å. Â.,
Ñîòíèêîâ Â. Ä.

CREATING SMOOTH LAW CHANGES JERK IN THE INTERVAL OF ACCELERATION/DECELERATION IN HIGH-SPEED MACHINING ON CNC EQUIPMENT

ÔÎÐÌÓÂÀÍÍß ÃËÀÄÊÎÃÎ ÇÀÊÎÍÓ Ç̲ÍÈ ÐÈÂÊÀ ÍÀ IJËÜÍÈÖßÕ ÐÎÇÃÎÍÓ- ÃÀËÜÌÓÂÀÍÍß ÏÐÈ ÂÈÑÎÊÎØÂÈÄʲÑÍ²É ÎÁÐÎÁÖ² ÍÀ ÎÁËÀÄÍÀÍͲ Ç ×ÏÓ

ÔÎÐÌÈÐÎÂÀÍÈÅ ÃËÀÄÊÎÃÎ ÇÀÊÎÍÀ ÈÇÌÅÍÅÍÈß ÐÛÂÊÀ ÍÀ Ó×ÀÑÒÊÀÕ ÐÀÇÃÎÍÀ-ÒÎÐÌÎÆÅÍÈß ÏÐÈ ÂÛÑÎÊÎÑÊÎÐÎÑÒÍÎÉ ÎÁÐÀÁÎÒÊÅ ÍÀ ÎÁÎÐÓÄÎÂÀÍÈÈ Ñ ×ÏÓ

44–50
(7)

Ïëàíêîâñêèé Ñ. È.,
Øèïóëü Î. Â.

MATHEMATICAL MODEL OF EDGE FINISHING WITH THERMAL-PULSE TREATMENT

ÌÀÒÅÌÀÒÈ×ÍÀ ÌÎÄÅËÜ ÎÏÎÐßÄÆÅÍÍß ÊÐÀÉÎÊ ÏÐÈ ÒÅÐÌβÌÏÓËÜÑÍ²É ÎÁÐÎÁÖ²

ÌÀÒÅÌÀÒÈ×ÅÑÊÀß ÌÎÄÅËÜ ÎÒÄÅËÊÈ ÊÐÎÌÎÊ ÏÐÈ ÒÅÐÌÎÈÌÏÓËÜÑÍÎÉ ÎÁÐÀÁÎÒÊÅ

51–55
(5)

Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ

Òåðåøèí À. Ì.

ESTIMATION OF MAIN VEHICLE PERFORMANCE CHARACTERISTICS (THRUST, LIFT-TO-DRAG RATIO, RANGE) BY USING RESULTS OF RAMJET BRANCH TESTING

ÎÖ²ÍÊÀ ÎÑÍÎÂÍÈÕ ËÜÎÒÍÎ-ÒÅÕͲ×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ (ÒßÃÀ, ßʲÑÒÜ, ÄÀËÜͲÑÒÜ) ˲ÒÀËÜÍÎÃÎ ÀÏÀÐÀÒÓ ÇÀ ÐÅÇÓËÜÒÀÒÀÌÈ ÂÎÃÍÅÂÈÕ ÑÒÅÍÄÎÂÈÕ ÂÈÏÐÎÁÓÂÀÍÜ ÏÐßÌÎÒÎ×ÍÈÕ ÏβÒÐßÍÎ-ÐÅÀÊÒÈÂÍÈÕ ÄÂÈÃÓͲÂ

ÎÖÅÍÊÀ ÎÑÍÎÂÍÛÕ Ë¨ÒÍÎ-ÒÅÕÍÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ (ÒßÃÀ, ÊÀ×ÅÑÒÂÎ, ÄÀËÜÍÎÑÒÜ) ËÅÒÀÒÅËÜÍÎÃÎ ÀÏÏÀÐÀÒÀ ÏÎ ÐÅÇÓËÜÒÀÒÀÌ ÎÃÍÅÂÛÕ ÑÒÅÍÄÎÂÛÕ ÈÑÏÛÒÀÍÈÉ ÏÐßÌÎÒÎ×ÍÎÃÎ ÂÎÇÄÓØÍÎ-ÐÅÀÊÒÈÂÍÎÃÎ ÄÂÈÃÀÒÅËß

56–59
(4)

Êóëèê À. Ñ.,
Ïàñè÷íèê Ñ. Í.

FRACTIONAL ORDER TRANSFER FUNCTION USAGE FOR SYNTHESIS OF THE AUTOMATIC POSITIONING SYSTEM OF OPERATING MODE OF VORTICAL POWER SEPARATOR

ÂÈÊÎÐÈÑÒÀÍÍß ÏÅÐÅÄÀÒÎ×ÍÈÕ ÔÓÍÊÖ²É ÄÐÎÁÎÂÎÃÎ ÏÎÐßÄÊÓ ÄËß ÂÈвØÅÍÍß ÇÀÄÀײ ÑÈÍÒÅÇÓ ÑÈÑÒÅÌÈ ÏÎÇÈÖ²ÞÂÀÍÍß ÐÅÆÈ̲ ÂÈÕÐÎÂÎÃÎ ÅÍÅÐÃÎÐÎÇIJËÞÂÀ×À

ÈÑÏÎËÜÇÎÂÀÍÈÅ ÏÅÐÅÄÀÒÎ×ÍÛÕ ÔÓÍÊÖÈÉ ÄÐÎÁÍÎÃÎ ÏÎÐßÄÊÀ ÄËß ÐÅØÅÍÈß ÇÀÄÀ×È ÑÈÍÒÅÇÀ ÑÈÑÒÅÌÛ ÏÎÇÈÖÈÎÍÈÐÎÂÀÍÈß ÐÅÆÈÌΠÂÈÕÐÅÂÎÃÎ ÝÍÅÐÃÎÐÀÇÄÅËÈÒÅËß

60–66
(7)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Æàðèêîâ Â. Í.

AERODERIVATIVE GAS TURBINES. SCOPE OF APPLICATION. STANDARDS

À²ÀÖ²ÉͲ ÊÎÍÂÅÐÒÎÂÀͲ ÃÀÇβ ÒÓÐÁ²ÍÈ. ÑÔÅÐÀ ÇÀÑÒÎÑÓÂÀÍÍß. ÑÒÀÍÄÀÐÒÈ

ÀÂÈÀÖÈÎÍÍÛÅ ÊÎÍÂÅÐÒÈÐÎÂÀÍÍÛÅ ÃÀÇÎÂÛÅ ÒÓÐÁÈÍÛ. ÑÔÅÐÀ ÏÐÈÌÅÍÅÍÈß. ÑÒÀÍÄÀÐÒÛ

67–74
(8)

Ðóñàíîâ À. Â.,
Êîñüÿíîâà À. È.,
Êîñüÿíîâ Ä. Þ.
 

RESEARCH OF STREAM FLOW STRUCTURE IN REGULATIVE COMPARTMENT OF THE HPC OF STEAM TURBINE Ê-325-23,5 WITH PARTIAL 0,4

ÄÎÑË²ÄÆÅÍÍß ÑÒÐÓÊÒÓÐÈ ÏÎÒÎÊÓ Â ÐÅÃÓËÞÞ×ÎÌÓ Â²ÄѲÊÓ ÖÂÒ ÏÀÐÎÂί ÒÓÐÁ²ÍÈ Ê-325-23,5 ÍÀ ÐÅÆÈ̲ ÏÀÐÖ²ÀËÜÍÎÑÒ² 0,4

ÈÑÑËÅÄÎÂÀÍÈÅ ÑÒÐÓÊÒÓÐÛ ÏÎÒÎÊÀ Â ÐÅÃÓËÈÐÓÞÙÅÌ ÎÒÑÅÊÅ ÖÂÄ ÏÀÐÎÂÎÉ ÒÓÐÁÈÍÛ Ê-325-23,5 ÍÀ ÐÅÆÈÌÅ ÏÀÐÖÈÀËÜÍÎÑÒÈ 0,4

75–80
(6)

Ñàâ÷åíêî Ê. Â.,
Êðóãëèé ß. Ä.,
Çèíüêîâñêèé À. Ï.,
Òîêàðü È. Ã.

INFLUENCE OF THE TYPE OF SHROUDS ON THE STATIC STRESS STATE OF BLADE RINGS

ÂÏËÈ ÒÈÏÓ ÁÀÍÄÀÆÍÈÕ ÏÎËÈÖÜ ÍÀ ÑÒÀÒÈ×ÍÈÉ ÍÀÏÐÓÆÅÍÈÉ ÑÒÀÍ ËÎÏÀÒÊÎÂÈÕ Â²ÍÖ²Â

ÂËÈßÍÈÅ ÒÈÏÀ ÁÀÍÄÀÆÍÛÕ ÏÎËÎÊ ÍÀ ÑÒÀÒÈ×ÅÑÊÎÅ ÍÀÏÐ߯ÅÍÍÎÅ ÑÎÑÒÎßÍÈÅ ËÎÏÀÒÎ×ÍÛÕ ÂÅÍÖÎÂ

81–84
(4)

Íàçèí Â. È.

COMPARISON OF DYNAMIC DESCRIPTIONS OF THE DOUBLED AND SINGLE HYDROSTATODINAMIC BEARINGS

ÏÎвÂÍßÍÍß ÄÈÍÀ̲×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÇÄÂΪÍÈÕ ² ÎÄÈÍÀÐÍÈÕ Ã²ÄÐÎÑÒÀÒÎÄÈÍÀ̲×ÍÈÕ Ï²ÄØÈÏÍÈʲÂ

ÑÐÀÂÍÅÍÈÅ ÄÈÍÀÌÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÑÄÂÎÅÍÍÛÕ È ÎÄÈÍÀÐÍÛÕ ÃÈÄÐÎÑÒÀÒÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÏÎÄØÈÏÍÈÊÎÂ

85–88
(4)

Ñèðåíêî Ô. Ô.,
Åïèôàíîâ Ñ. Â.,
Æåìàíþê Ï. Ä.,
Íå÷óíàåâ Ñ. À.

SYNTHESIS TECHNIC OF A TORQUE MEASURING ALGORITHM FOR A TORQUE MEASURING UNIT, WHICH IMPLEMENTS THE PHASE METERING PRINCIPLE, IN CONDITIONS OF LIMITED INFORMATION ABOUT THE PROPERTIES OF UNIT

ÑÈÍÒÅÇ ÀËÃÎÐÈÒÌÓ ÂÈÇÍÀ×ÅÍÍß ÂÅËÈ×ÈÍÈ ÊÐÓÒÈËÜÍÎÃÎ ÌÎÌÅÍÒÓ ÔÀÇÎÌÅÒÐÈ×ÍÈÌ ÌÅÒÎÄÎÌ Â ÓÌÎÂÀÕ ÎÁÌÅÆÅÍί ²ÍÔÎÐÌÀÖ²¯ ÏÐÎ ÂËÀÑÒÈÂÎÑÒ² ÂÈ̲ÐÞÂÀ×À

ÑÈÍÒÅÇ ÀËÃÎÐÈÒÌÀ ÎÏÐÅÄÅËÅÍÈß ÂÅËÈ×ÈÍÛ ÊÐÓÒßÙÅÃÎ ÌÎÌÅÍÒÀ ÔÀÇÎÌÅÒÐÈ×ÅÑÊÈÌ ÌÅÒÎÄÎÌ Â ÓÑËÎÂÈßÕ ÎÃÐÀÍÈ×ÅÍÍÎÉ ÈÍÔÎÐÌÀÖÈÈ Î ÑÂÎÉÑÒÂÀÕ ÈÇÌÅÐÈÒÅËß

89–97
(9)

Sumtsov A.,
Szurman K.

MODEL BASED DESIGN APPROACH APPLIED ON THE DEVELOPMENT OF THE ENGINE MONITORING MODULE

ÇÀÑÒÎÑÓÂÀÍÍß ÌÎÄÅËÜÍÎ-ÎвªÍÒÎÂÀÍÎÃÎ ÏÐÎÅÊÒÓÂÀÍÍß ÄËß ÐÎÇÐÎÁÊÈ ÁËÎÊÀ ÊÅÐÓÂÀÍÍß ÄÂÈÃÓÍÀ ˲ÒÀÊÀ

ÏÐÈÌÅÍÅÍÈÅ ÌÎÄÅËÜÍÎ-ÎÐÈÅÍÒÈÐÎÂÀÍÍÎÃÎ ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÄËß ÐÀÇÐÀÁÎÒÊÈ ÁËÎÊÀ ÓÏÐÀÂËÅÍÈß ÑÀÌÎ˨ÒÍÎÃÎ ÄÂÈÃÀÒÅËß

98–102
(5)

Ëîÿí À. Â.

POSSIBILITY INVESTIGATION OF HALL EFFECT THRUSTER DIRECT ELECTRIC POWER SUPPLYING (WITHOUT INTERMEDIATE CONVERTERS) FROM SOLAR BATTERY

ÄÎÑË²ÄÆÅÍÍß ÌÎÆËÈÂÎÑÒ² ÁÅÇÏÎÑÅÐÅÄÍÜÎÃÎ ÅËÅÊÒÐÎÆÈÂËÅÍÍß (ÁÅÇ ÏÐÎ̲ÆÍÈÕ ÏÅÐÅÒÂÎÐÞÂÀײÂ) ÄÂÈÃÓÍÀ ÕÎË˲ÂÑÜÊÎÃÎ ÒÈÏÓ Â²Ä ÂÈÑÎÊÎÂÎËÜÒÍί ÁÀÒÀÐů ÔÎÒÎÅËÅÊÒÐÈ×Íί

ÈÑÑËÅÄÎÂÀÍÈÅ ÂÎÇÌÎÆÍÎÑÒÈ ÍÅÏÎÑÐÅÄÑÒÂÅÍÍÎÃÎ ÝËÅÊÒÐÎÏÈÒÀÍÈß (ÁÅÇ ÏÐÎÌÅÆÓÒÎ×ÍÛÕ ÏÐÅÎÁÐÀÇÎÂÀÒÅËÅÉ) ÄÂÈÃÀÒÅËß ÕÎËËÎÂÑÊÎÃÎ ÒÈÏÀ ÎÒ ÂÛÑÎÊÎÂÎËÜÒÍÎÉ ÁÀÒÀÐÅÈ ÔÎÒÎÝËÅÊÒÐÈ×ÅÑÊÎÉ

103–107
(5)

Íåðóáàññêèé Â. Â.

USING MAHALANOBIS-TAGUCHI SYSTEM IN TASKS RELATED TO THE TURBINE ENGINE FAULT RECOGNITION

ÂÈÊÎÐÈÑÒÀÍÍß ÑÈÑÒÅÌÈ ÌÀÕÀËÀÍÎÁ²ÑÀ-ÒÀÃÓÒ² Ó ÇÀÄÀ×ÀÕ ÐÎÇϲÇÍÀÂÀÍÍß ÍÅÑÏÐÀÂÍÎÑÒÅÉ ÃÒÄ

ÈÑÏÎËÜÇÎÂÀÍÈÅ ÑÈÑÒÅÌÛ ÌÀÕÀËÀÍÎÁÈÑÀ-ÒÀÃÓÒÈ Â ÇÀÄÀ×ÀÕ ÐÀÑÏÎÇÍÀÂÀÍÈß ÍÅÈÑÏÐÀÂÍÎÑÒÅÉ ÃÒÄ

108–112
(5)

Õàóñòîâà À. Í.

DEVELOPMENT OF HIGH RESOLUTION SPECTRAL COMPLEX FOR THE STATIONARY PLASMA THRUSTER SPECTRUM RESEARCH

ÐÎÇÐÎÁÊÀ ÑÏÅÊÒÐÀËÜÍÎÃÎ ÊÎÌÏËÅÊÑÓ ÂÈÑÎÊÎÃÎ ÐÎÇIJËÅÍÍß ÄËß ÄÎÑË²ÄÆÅÍÍß ÑÏÅÊÒÐÓ ÑÒÀÖ²ÎÍÀÐÍÎÃÎ ÏËÀÇÌÎÂÎÃÎ ÄÂÈÃÓÍÀ

ÐÀÇÐÀÁÎÒÊÀ ÑÏÅÊÒÐÀËÜÍÎÃÎ ÊÎÌÏËÅÊÑÀ ÂÛÑÎÊÎÃÎ ÐÀÇÐÅØÅÍÈß ÄËß ÈÑÑËÅÄÎÂÀÍÈß ÑÏÅÊÒÐÀ ÑÒÀÖÈÎÍÀÐÍÎÃÎ ÏËÀÇÌÅÍÍÎÃÎ ÄÂÈÃÀÒÅËß

113–118
(6)

ßêóøåíêî Î. Ñ.,
Êîðîëüîâ Ï. Â.,
̳ëüöîâ Â. ª.,
Áîðèñþê Ã. Þ.,
×óìàê Î. ².

THE MODELLING OF ACCUMULATION OF AVIATION ENGINE’S DAMAGES AT DIFFERENT LAWS OF CONTROL BY ITS OPERATION DURING TAKE-OFF

ÌÎÄÅËÞÂÀÍÍß ÏÐÎÖÅѲ ÍÀÊÎÏÈ×ÅÍÍß ÏÎØÊÎÄÆÅÍÜ ÍÀ ÇËÜÎÒ² ÏÐÈ ÂÈÊÎÐÈÑÒÀÍͲ вÇÍÈÕ ÇÀÊÎͲ ÓÏÐÀÂ˲ÍÍß ÃÒÄ

ÌÎÄÅËÈÐÎÂÀÍÈÅ ÏÐÎÖÅÑÑΠÍÀÊÎÏËÅÍÈß ÏÎÂÐÅÆÄÅÍÍÎÑÒÅÉ ÍÀ ÂÇËÅÒÅ ÏÐÈ ÈÑÏÎËÜÇÎÂÀÍÈÈ ÐÀÇËÈ×ÍÛÕ ÇÀÊÎÍΠÓÏÐÀÂËÅÍÈß ÃÒÄ

119–122
(4)

Òêà÷ Ì. Ð.,
Òèìîøåâñêèé Á. Ã.,
Äîöåíêî Ñ. Ì.,
Ãàëûíêèí Þ. Í.

PERFORMANCE OF THE WORKING FLUID FOR METAL HYDRIDE UTILIZATION CONTINUOUS PLANT

ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÐÎÁÎ×ÎÃÎ Ò²ËÀ ÌÅÒÀËÎòÄÐÈÄÍί ÓÒÈ˲ÇÀÖ²ÉÍί ÓÑÒÀÍÎÂÊÈ ÁÅÇÏÅÐÅÐÂÍί IJ¯

ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÐÀÁÎ×ÅÃÎ ÒÅËÀ ÌÅÒÀËËÎÃÈÄÐÈÄÍÎÉ ÓÒÈËÈÇÀÖÈÎÍÍÎÉ ÓÑÒÀÍÎÂÊÈ ÍÅÏÐÅÐÛÂÍÎÃÎ ÄÅÉÑÒÂÈß

123–128
(6)

Áîðçîâ Ñ. À. 

SPECTRAL-CORRELATION METHOD ESTIMATION OF EFFECTIVE WORK THE COMBUSTION CHAMBER OF GAS TURBINE ENGINE

ÑÏÅÊÒÐÀËÜÍÎ-ÊÎÐÅËßÖ²ÉÍÈÉ ÌÅÒÎÄ ÎÖ²ÍÊÈ ÅÔÅÊÒÈÂÍÎÑÒ² ÐÎÁÎÒÈ ÂÓÇËÀ ÊÀÌÅÐÈ ÇÃÎÐßÍÍß ÃÀÇÎÒÓÐÁ²ÍÍÎÃÎ ÄÂÈÃÓÍÀ

ÑÏÅÊÒÐÀËÜÍÎ-ÊÎÐÐÅËßÖÈÎÍÍÛÉ ÌÅÒÎÄ ÎÖÅÍÊÈ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÐÀÁÎÒÛ ÓÇËÀ ÊÀÌÅÐÛ ÑÃÎÐÀÍÈß ÃÀÇÎÒÓÐÁÈÍÍÎÃÎ ÄÂÈÃÀÒÅËß

129–135
(7)

ªí÷åâ Ñ. Â.,
Òîâêà÷ Ñ. Ñ.

PROGNOSTIC VIBRATION STATE OF KNOTS AVIATION ENGINES GAS-TURBINES AFTER PARAMETERS OF WAVELET-DECOMPOSITION

ÏÐÎÃÍÎÇÓÂÀÍÍß Â²ÁÐÎÑÒÀÍÓ ÂÓÇ˲ À²ÀÖ²ÉÍÈÕ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ ÇÀ ÏÀÐÀÌÅÒÐÀÌÈ ÂÅÉÂËÅÒ-ÐÎÇÊËÀÄÓ

ÏÐÎÃÍÎÇÈÐÎÂÀÍÈÅ ÂÈÁÐÎÑÎÑÒÎßÍÈß ÓÇËΠÀÂÈÀÖÈÎÍÍÛÕ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÏÎ ÏÀÐÀÌÅÒÐÀÌ ÂÅÉÂËÅÒ-ÐÀÇËÎÆÅÍÈß

136–140
(5)

Òàðàñåíêî À. È.,
Òàðàñåíêî
 À. À.

PARTIAL MODES OF OPERATION OF THE COMPRESSORS ON A SINGLE-SHAFT TURBINE ENGINE OR TURBINE ENGINE WITH A FREE POWER TURBINE WORKING WITH VARYING TEMPERATURES OF OUTSIDE AIR

ÐÎÁÎÒÀ ÊÎÌÏÐÅÑÎÐÀ ÍÀ ×ÀÑÒÊÎÂÈÕ ÐÅÆÈÌÀÕ ÎÄÍÎÂÀËÜÍÎÃÎ ÃÒÄ ÒÀ ÃÒÄ Ç Â²ËÜÍÎÞ ÑÈËÎÂÎÞ ÒÓÐÁ²ÍÎÞ ÏÐÈ Ç̲Ͳ ÒÅÌÏÅÐÀÒÓÐÈ ÇÎÂͲØÍÜÎÃÎ ÏβÒÐß

ÐÀÁÎÒÀ ÊÎÌÏÐÅÑÑÎÐÀ ÍÀ ×ÀÑÒÈ×ÍÛÕ ÐÅÆÈÌÀÕ ÎÄÍÎÂÀËÜÍÎÃÎ ÃÒÄ È ÃÒÄ ÑÎ ÑÂÎÁÎÄÍÎÉ ÑÈËÎÂÎÉ ÒÓÐÁÈÍÎÉ ÏÐÈ ÈÇÌÅÍÅÍÈÈ ÒÅÌÏÅÐÀÒÓÐÛ ÍÀÐÓÆÍÎÃÎ ÂÎÇÄÓÕÀ

141–144
(4)

Èíôîðìàöèîííûå òåõíîëîãèè

Áàáåíêî Þ. Â.

THE METHOD OF VALUATION OF MODIFICATIONS SHORT-HAUL PASSENGER AIRCRAFT

ÌÅÒÎÄÈÊÀ ÂÀÐÒ²ÑÍί ÎÖ²ÍÊÈ ÌÎÄÈÔ²ÊÀÖ²É ÁËÈÇÜÊÎÌÀòÑÒÐÀËÜÍÈÕ ÏÀÑÀÆÈÐÑÜÊÈÕ Ë²ÒÀʲÂ

ÌÅÒÎÄÈÊÀ ÑÒÎÈÌÎÑÒÍÎÉ ÎÖÅÍÊÈ ÌÎÄÈÔÈÊÀÖÈÉ ÁËÈÆÍÅÌÀÃÈÑÒÐÀËÜÍÛÕ ÏÀÑÑÀÆÈÐÑÊÈÕ ÑÀÌÎËÅÒÎÂ

145–148
(4)

Ëîãèíîâ Â. Â.

SOFTWARE FOR FORMING OF OPERATIONAL PERFORMANCE OF ENGINE AIRCRAFT POWER PLANT

ÏÐÎÃÐÀÌÍÈÉ ÊÎÌÏËÅÊÑ ÏÎ ÔÎÐÌÓÂÀÍÍÞ ÅÊÑÏËÓÀÒÀÖ²ÉÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÄÂÈÃÓÍÀ ÑÈËÎÂί ÓÑÒÀÍÎÂÊÈ Ë²ÒÀÊÀ

ÏÐÎÃÐÀÌÌÍÛÉ ÊÎÌÏËÅÊÑ ÏÎ ÔÎÐÌÈÐÎÂÀÍÈÞ ÝÊÑÏËÓÀÒÀÖÈÎÍÍÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÄÂÈÃÀÒÅËß ÑÈËÎÂÎÉ ÓÑÒÀÍÎÂÊÈ ÑÀÌÎËÅÒÀ

149–152
(4)

Ðåâà Î. Ì.,
Áîðñóê Ñ. Ï.

PILOT ANALYSIS OF AIR TRAFFIC CONTROLLERS DESIRABILITY LEVELS ON THE SPECTER OF THE HORIZONTAL AIR SPACE FLIGHT SEPARATION NORMS

ϲËÎÒÍÈÉ ÀÍÀË²Ç Ð²ÂͲ ÄÎÌÀÃÀÍÜ À²ÀÄÈÑÏÅÒ×Åв ÍÀ ÑÏÅÊÒв ÃÎÐÈÇÎÍÒÀËÜÍÈÕ ÍÎÐÌ ÅØÅËÎÍÓÂÀÍÍß ÏβÒÐßÍÎÃÎ ÏÐÎÑÒÎÐÓ

ÏÈËÎÒÍÛÉ ÀÍÀËÈÇ ÓÐÎÂÍÅÉ ÏÐÈÒßÇÀÍÈÉ ÀÂÈÀÄÈÑÏÅÒ×ÅÐΠÍÀ ÑÏÅÊÒÐÅ ÃÎÐÈÇÎÍÒÀËÜÍÈÕ ÍÎÐÌ ÝØÅËÎÍÈÐÎÂÀÍÈß ÂÎÇÄÓØÍÎÃÎ ÏÐÎÑÒÐÀÍÑÒÂÀ

153–160
 (8)

Òðåòüÿê Â. Â.,
Îíîï÷åíêî À. Â.,
Ôåäîðîâà À. Ñ.,
Ñòàäíèê Ñ. À.

THE POSSIBILITY OF INTERACTIVE SOFTWARE SYSTEMS FOR THE DESIGN PULSE PROCESSES TO MANUFACTURE COMPLEX PARTS BY ADDRESSING AND SYNTHESIS

ÌÎÆËÈÂÎÑÒ² ²ÍÒÅÐÀÊÒÈÂÍÎÃÎ ÏÐÎÃÐÀÌÍÎÃÎ ÊÎÌÏËÅÊÑÓ ÄËß ÏÐÎÅÊÒÓÂÀÍÍß ÒÅÕÍÎËÎò×ÍÈÕ ÏÐÎÖÅѲ ²ÌÏÓËÜÑÍί ÎÁÐÎÁÊÈ ÏÐÈ ÂÈÃÎÒÎÂËÅÍͲ ÑÊËÀÄÍÈÕ ÄÅÒÀËÅÉ ÌÅÒÎÄÎÌ ÀÄÐÅÑÀÖ²¯ ÒÀ ÑÈÍÒÅÇÓ

ÂÎÇÌÎÆÍÎÑÒÈ ÈÍÒÅÐÀÊÒÈÂÍÎÃÎ ÏÐÎÃÐÀÌÌÍÎÃÎ ÊÎÌÏËÅÊÑÀ ÄËß ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÒÅÕÍÎËÎÃÈ×ÅÑÊÈÕ ÏÐÎÖÅÑÑΠÈÌÏÓËÜÑÍÎÉ ÎÁÐÀÁÎÒÊÈ ÏÐÈ ÈÇÃÎÒÎÂËÅÍÈÈ ÑËÎÆÍÛÕ ÄÅÒÀËÅÉ ÌÅÒÎÄÎÌ ÀÄÐÅÑÀÖÈÈ È ÑÈÍÒÅÇÀ

161–165
(5)

Ôåäîðîâè÷ Î. Å.,
Ëåùåíêî Þ. À.

THE RATIONAL ALLOCATION OF FUNDS TO IMPROVE THE QUALITY OF PRODUCTS TO DEVELOP THE ENTERPRISE

ÐÀÖ²ÎÍÀËÜÍÈÉ ÐÎÇÏÎÄ²Ë ÊÎØÒ²Â ÄËß ÏÎÊÐÀÙÅÍÍß ßÊÎÑÒ² ÏÐÎÄÓÊÖ²¯ ϲÄÏÐȪÌÑÒÂÀ, ÙÎ ÐÎÇÂÈÂÀªÒÜÑß

ÐÀÖÈÎÍÀËÜÍÎÅ ÐÀÑÏÐÅÄÅËÅÍÈÅ ÑÐÅÄÑÒ ÄËß ÓËÓרÅÍÈß ÊÀ×ÅÑÒÂÀ ÂÛÏÓÑÊÀÅÌÎÉ ÏÐÎÄÓÊÖÈÈ ÐÀÇÂÈÂÀÞÙÅÃÎÑß ÏÐÅÄÏÐÈßÒÈß

166–169
(4)

ÀËÔÀÂÈÒÍÛÉ ÓÊÀÇÀÒÅËÜ

170

 

 

 

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 (ïðèêàç ÌÎÍ Óêðàèíû ¹1279 îò 6.11.2014 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 áèáëèîìåòðè÷åñêèå è íàóêîìåòðè÷åñêèå áàçû äàííûõ: íàó÷íîé ýëåêòðîííîé áèáëèîòåêè eLIBRARY.RU (Ðîññèéñêàÿ Ôåäåðàöèÿ); Index Copernicus (ICV 2013: 4,83) (Ïîëüøà); Google Scholar (áèáëèîìåòðè÷åñêèå ïîêàçàòåëè – quot.=2094 / h = 10 / i10 = 15).