We have studied and developed a compact nanosecond laser system dedicated to the ignition of aeronautic combustion engines. This system is based on a nanosecond microchip laser delivering 6 μJ nanosecond pulses, which are amplified in two successive stages. The first stage is based on an Ytterbium doped fiber amplifier (YDFA) working in a quasi-continuous-wave (QCW) regime. Pumped at 1 kHz repetition rate, it delivers TEM00 and linearly polarized nanosecond pulses centered at 1064 nm with energies up to 350 μJ. These results are in very good agreement with the model we specially designed for a pulsed QCW pump regime. The second amplification stage is based on a compact Nd:YAG double-pass amplifier pumped by a 400 W peak power QCW diode centered at λ = 808 nm and coupled to a 800 μm core multimode fiber. At 10 Hz repetition rate, this system amplifies the pulse delivered by the YDFA up to 11 mJ while preserving its beam profile, polarization ratio, and pulse duration. Finally, we demonstrate that this compact nanosecond system can ignite an experimental combustion chamber.
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21 December 2016
Research Article|
December 19 2016
Compact nanosecond laser system for the ignition of aeronautic combustion engines
G. Amiard-Hudebine;
G. Amiard-Hudebine
Université de Bordeaux
, CNRS UMR 5798, Laboratoire Ondes et Matière d'Aquitaine, 351 Cours de la Libération, 33405 Talence Cedex, France
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G. Tison;
G. Tison
Université de Bordeaux
, CNRS UMR 5798, Laboratoire Ondes et Matière d'Aquitaine, 351 Cours de la Libération, 33405 Talence Cedex, France
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a)
Author to whom correspondence should be addressed. Electronic mail: eric.freysz@u-bordeaux.fr
J. Appl. Phys. 120, 233102 (2016)
Article history
Received:
September 09 2016
Accepted:
November 27 2016
Citation
G. Amiard-Hudebine, G. Tison, E. Freysz; Compact nanosecond laser system for the ignition of aeronautic combustion engines. J. Appl. Phys. 21 December 2016; 120 (23): 233102. https://doi.org/10.1063/1.4971964
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