| 摘要 |
<p>The present invention contemplates a gas turbine engine compressor (22) including a plurality of effervescent atomizers (43) to inject a mixture of water and methanol into the compressor inlet (33). A plurality of droplets, preferably less than ten microns in size, travels through the inlet duct to the compressor. In one embodiment the plurality of effervescent atomizers (43) are located around the circumference of the inlet duct (32) and upstream of the compressor inlet (33) and the injection occurs into a gas having a substantially ambient pressure.</p> |
