小型ジェッ トエンジン付模型風洞試験法への取り組みについて
Contents
1. 2 1 2 1 2 3 2 4 2 5 400mm 300mm 7 300mm 10mX2 3m 3 500m3 min 300mmAq 440mm 9 3 7 KW We a ee 1Idle 30 000rpm 110 000rpm sweep 10 000rpm 4 0 3 0 m s sweep 30 0002. 3 TP S 80 6 2 IA 0 4 2 7 180mm 1 8 0 mm
3. 5 1 AdvancedMicro Turbines 01ympus 2 9 N 19 1975 1 3 4 S TT OL TR 790 1983 11 The aacuUrnernr ic Nrovided hv AXA 158 51 2 romper mn es am erm oopannon Re 1 300mm _ M 2 NRNNRWKee NSR 2 1 IM
4. SST STOL TP Sur bine Powered Simulator PS Ke Micro TurboJet Engine M M TP S
5. M TP 2 1 The CorinmenT ic mravwviaeaq hv AXA 148 51 CFD Computational Fluid Dynamics 1
6. 2 2 EI 0M SL 2 1 M M 2 1 1
7. LPG ECU L P G LPG M AMT OS MS DOS Windors98 2 TP S TTPS
8. TPS Bs 4 2 LM M Idle No TT 6 TS TPS The CorinmenT ic Nrovided hv AXA 64 65 157 4 1 4 2
9. 1 The Approach to the Wind Tunnel Test Method for a Aircraft Model Powered by Small Jet Engine An Engine Control System and Analysis of its Test KesultS Teruomi Nakaya Sigeo Baba Akira Koike Kennitirou Nagan Hideji Oinuma Katumi Takeda Sizuo Sekine NAL S S 2 TPS 1 S ST
10. 3 0 m s M TP S 2 TPS
11. Ga i pat 3 6 6 UF S 7520A150 1125M 190mm 80mm 50 8mm Skg Fx Fy 66kgf Fz 1 3 2 kegf Mx My 1200kgfrcm Mz 1200kgfcm 500 1 2000 0 2 0 2 QROM a RS232 RS422 16 8 8 6 The doci nernt ie Nrovided hv AXA 150 F x FyFz Mx MyMz ROM 6 4
12. The aacuUrnernr ic Nrovided hv AXA 64 65 155 2 _TPS TP S Normal 3 2 1 TPS STOL 3 4 105mm 60 000rpm 3 2 2 TP S 2 2 5 Fx Pi
13. ECU 2 M 2 5 F x X AA0 CA 2 1 3 M 1
14. 2 ed an 1 8Mpa LP 2 Jet A1 C27 S c M 2 _ Max 8 0 0 C 2 1 M
15. gt 2 The aacuUrnernr ic Nrovided hv AXA 156 51 3 2 3 2 M 3 2 4 4 1 M 110 000rpm 1 Max 1 1 6 0N 1 Max 1 PS M 1 6 0N 1
16. The aacuUrnernr ic Nrovided hv AXA 64 65 2 ANSU ASU ECU PG LPG Je t Ultimate Radio Control Syste m M M
17. ECU ECU ECU U1timate Radio Control System KOU S OU NAL CU E CU EGT ASU GT 4 0 RO M
18. 2 9 2 1 0 2 8 O The CornernT ic Nrovided hv AXA 154 51 3 3 1 M 3 1 1 M LPG Fx 3 1 3 1 2 Normal Normal 3 2 rpm
19. 2 1 2 2 1 M 20 CU ME M M Advanced Micro Turbines Olympus 2 3 M 2 Turbine Technolog ies SR 30 ECU Olympus
20. 6 2 1 2 2 2 1 Jet Al1 2 0 0 5 51 2 1 2 M 2 5 M 1 M M 2 5 ECU Electronic Con trol Unit ASU Automatic Start Unit
21. 4 72 9 7 LabVIEW Tr 1 SS Auto Start Unit LPG i i 2 5 M The aacuUrnernr ic Nrovided hv AXA 64 65 161 rim lt Max lsh N 30 000rpm 6 7 0 N 110 1 5 1000 sec 3 4 EcU ROM 2 6 M 1RUN TPS 30kg cm2
22. yLM sec g sec Fx N y P via P i Pa Ti P oj Pa Pj Pa Tj C 3 1 3 1 M 3 3 N Normal 0 30 40 50 60m s V 80 100 120 140 160m s V 0 m s 3 0m s 1 0 N 17 F x 0 F x gt 2 3 1 3 2
23. TP S LTPS M 1 TP S The aacuUrnernr ic Nrovided hv AXA 64 65 TP S STOL 3 2 TP S 2 8 M TP S TP S
24. no 2 0 MPa 50 AZ200 gt mn 2 7 TPS The aacuUrnernr ic nrovlrled hv AXA 162 51 5 SN 270 240 165 gt 18 a 3 5 N 1 lt 6190 NN 2 8 TPS The CorinmenT ic Nrovided hv AXA 64 65 163 6 M1 0 12 M6 O NN ei78 N pcPcp125 2 9 0 Thc aacuUrnernr ic Nrovided
25. Olympus Jet A Olympus 1 3 0 mm Diameter Length 2 7 0mm Turbine weight 2 4kg ThrustGmax rpm 170N 1 9 0 N ThrustGdle rpm 7 N The CorinmenT ic Nrovided hv AXA 64 65 149 Maximum rpm 110 000rpm 115 000rpm ldle rpm 30 000rpm Pressure ratioumax rpm 4 1 Mass flowGmax rpm 400g sec Normal EGT 6 Max EGT 3005 Limit EGT 8 00C Fuel consumer max rpm 4 0 0 gsec Fuel Jet A1 M E C U Electronic Control Unit ROM 40 ASU Automatic Start Unit
26. M M TP S TP S STOL STOL 3 2 2 1 TPS 2 7 2 6 MP Ye
27. gt a 1 le i eS P mE 8 De EE 1 I Es pe Es a J mm B TP Thic deci nent lc mraviaeq hv AXA 172 51 Ti Thic doAcLIMeNnt lc mraviaeq hv AXA 64 65 173 TP g Thic deci nent lc mraviaeq hv AXA
28. 2 2 2 1 2 X Y 1 2 1 1 5 X 1500mm Y 200mm 2 5 2 2 2 1 M ECU 3 0cm E CU
29. N E GT C Idle 7 N Max 1 6 ON EG TT 2 7 4 C 3 5 ECU 3 1 3 M M M V 0 30 40 50 60m s Sweep R 0 30 000rpmGdle 110 000rpm 10 000rpm kh3N 630mm 7 D Y 20mm 3 V m s gq Pa C Kpa P P R rp E GT C
30. The aaocuUrnernr ie Nrovided hv AXA 1 500mm TT S GION 64 65 159 700mm 1 500mm TAR ECU 2 2 92 A 855Smm 2 2 270mm 1 3 0mm 5 9 mm EGT i Diameter 1 3 0mm Length 270mm Turbine weight 2 4kg Thrust max rpm 170N Maximum rpm 110 000rpm _ 1dle rpm _30 000rpm 2 3 M Pressure ratio max rpm 4 1 3 Max EGT 750C _ The aacuUrnernr ic nmravwviaeaq hv AXA 160 51 2 4 M M Olympus _ i Mo Ym 1 ea U Ws lt i i
31. M _ 1RUN 4 0 2 60 6 1 RUN M L PG 2 Idle Max TIdle Home Max 51 UMNU CK 25 2 TP S TP S
32. 160 40m s ine 9 140 50m s ne 40 60m s 0m s 120 80m s 100m s 100 120m s 140m s lt 160m s 000 3 M 0 4 3 4 TP S kg cm 16 18 20 The aacuUrnernr ic Nrovided hv AXA 64 65 167 20 18 0 3 2 16 5 14 7 5 10 gt gt 1 10 _ gt 14 16 E 9 2 0 pS 2 3 95 LM 7 i 10 000 6 0 50 AFxkg kg F x gt gt gt
33. 153 7 5mm 35mm 77 7 5 mm 30mm X Y 2 OAM Z 1 2 1 3 0 kg em 4 2 7 STOL TP S 1 1 0 0mm 5 0 mm ee ee 50 mmX 5m ee 5 Da ea a a 80
34. Max 1 1 6 0N 1 Max 1 M 5 0 1 3 TPS 2 4 M Entropy TPS 4 4 1 M M AMT Olympus ECU ASU
35. 0 3 5 7 5 10 12 14 16 kg cm W 0 18 kg 3 5 kg F x kgg Fx 3 2 3 TPS TP SS P S M V 0 30 40 50 60m s Sweep R 0 30 000rpmGdle 110 000rpm 10 000rpm 5 2 X 540mm 6 D
36. EE oe A 2 N ee 50 000 60 000 70 000 a lt T PS The aacuUrnernr ic Nrovided hv AXA SN 168 51 0 0 1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 0 9 1 4 1 Max 1 Max 1 Thc aacuUrnernr ic Nrovided hv AXA 64 65 169 PT 2 2 Thic deci nent lc mraviaeq hv AXA 170 L224 _ 7U4y7 9 51 3 i 1 Thic aaocurnenr lc mraviaeq hv AXA 64 65 171 2 5 TPS
37. Y 20mm 3 V m s q Pa C Kpa P P R rpm kg cm 0y MM sec g sec Fx N 7 P i Pa Pi Pa Ti P j Pa Pj Pa Tj 3 2 3 1 T P S 3 6 Grpm N V 0 30 40 50 60m s CV 80 100 120 140m s V 0m s 3 0m s 2 3 N WV 1 Fx 0 Fg
38. hv AXA 51 SH 164 lt SL DD SS SN LN _O 140 HY _ A i 3 2 2 10 The COorinmenT ic nrnviner hv 1 AXA _ 64 65 165 F x V y 0 1508x 0 0008 kg 15 20 3 1 Fx Thrust N Throttle EGT C 200 a 800 Thrust N 180 Fe le OU VO Ne Bed Bd i i a Cs i EEE Throttle 96 160 Pa EGTOCC len A 750 120 700 100 80 _ 650 60 40 600 20 0 rm 550 0 20 000 40 000 _ 60 000 _80 000 100 000 120 000 pm 3 2 M The CornernT ic mrawiaeaq hv AXA 166 x 10 rpm 51 N 2 0m s 30m s
39. rpm 110 000rpm The CorinmenT ic Nrovided hv AXA 151 _152 4 0 m s 90 000rpm 1 0 m s 1 4 0 m s 2 4 2 1 4 M
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