fuel injection and combustion processes in small jet engines

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Tests demonstrated stable combustion a) b) c) d) יום העיון החמישי במנוע סילון וטורבינות גז יום ה',‏ א'‏ בחשון תשס"ו,‏ 03/11/2005 Combustion regimes: a), b) – moderate eq. ratio c), d) – lean combustion limit (low equivalence ratio) Turbo and Jet Engine Laboratory Technion – Israel www. jet-engine-lab.technion.ac.il
Methane Combustion in small combustor for the micro Gas Turbine יום העיון החמישי במנוע סילון וטורבינות גז יום ה',‏ א'‏ בחשון תשס"ו,‏ 03/11/2005 Turbo and Jet Engine Laboratory Technion – Israel www. jet-engine-lab.technion.ac.il
Page 1 and 2: FUEL INJECTION AND COMBUSTION PROCE
Page 3 and 4: 1. Atomization systems for small co
Page 5 and 6: דוגמא למאיידי דלק ב
Page 7 and 8: Air swirl atomizer The same swirl a
Page 9 and 10: Principal atomizer dimensions: •d
Page 11 and 12: Tests range •The liquid (water) p
Page 13 and 14: 3 Droplet size: comparison with oth
Page 15 and 16: T E S T R E S U L T S Cone Angle; S
Page 17 and 18: EXAMPLE OF THE JUMP CHANGE OF THE O
Page 19 and 20: Principal results: Swirl atomizer
Page 21 and 22: • The jump-wise spray cone angle
Page 23 and 24: TEST OF MANIFOLD COMBUSTOR TEST SWI
Page 25 and 26: SMALL COMBUSTOR DEVELOPMENT FOR MIC
Page 27: MODIFIED COMBUSTOR Modified fuel no
Page 31 and 32: Conclusions: •Small combustor for
Page 33 and 34: T E S T R E S U L T S 3. Axial drop
Page 35 and 36: SUCCESSFUL SPARK IGNITION AND COMBU
Page 37 and 38: First combustor model does not work

fuel injection and combustion processes in small jet engines

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