| 摘要 |
<p>A late lean fuel injection nozzle (44) for a gas turbine includes a first outer air supply tube (46) having a relatively large inner diameter and an outlet (48) at a distal end thereof. The first outer air supply tube is adapted to supply air to a combustion chamber, and at least one fuel injection tube (50) having a relatively smaller diameter enters a distal end portion of the first outer air supply tube (46) and extends within the first outer air supply tube (46) substantially to the outlet (48).</p> |
