fuel injection and combustion processes in small jet engines

More documents

Recommendations

Info

T E S T R E S U L T S 2. Droplet size. Comparison axial and radial swirlers 1.5bar 2.5bar 3bar 4bar 5bar 6bar 140 SMD, micron 120 100 80 60 Axial Radial 40 0 20 40 60 80 100 120 Air velocity, m/s DROPLET SIZE DEPENDS ONLY WEAKLY ON LIQUID PRESSURE DROP FOR AIR-BLAST ATOMIZER יום העיון החמישי במנוע סילון וטורבינות גז יום ה',‏ א'‏ בחשון תשס"ו,‏ 03/11/2005 SMD distribution along radius for the axial and radial swirlers Turbo and Jet Engine Laboratory Technion – Israel www. jet-engine-lab.technion.ac.il
SUCCESSFUL SPARK IGNITION AND COMBUSTION SHOW THAT SUCH ATOMIZERS CONFIGURATION CAN BE USED FOR SMALL JET ENGINES FURTHER STUDY OF THE COMBUSTOR FOR WIDENING OF THE OPERATING RANGE AND OF THE AIR-BLAST ATOMIZERS APPLICATIONS SHOULD BE CARRIED OUT 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 and 28: MODIFIED COMBUSTOR Modified fuel no
Page 29 and 30: Methane Combustion in small combust
Page 31 and 32: Conclusions: •Small combustor for
Page 33: T E S T R E S U L T S 3. Axial drop
Page 37 and 38: First combustor model does not work

fuel injection and combustion processes in small jet engines

Create successful ePaper yourself

Delete template?

Save as template?