| タイトル | Fuel premixing module for gas turbine engine combustor |
| 本文（外部サイト） | http://hdl.handle.net/2060/20080005032 |
| 著者（英） | Razdan, Mohan K.; Chin, Jushan; Marshall, Andre W.; Rizk, Nader K. |
| 著者所属（英） | Rolls-Royce Allison |
| 発行日 | 2005-11-29 |
| 言語 | eng |
| 内容記述 | A fuel-air premixing module is designed to reduce emissions from a gas turbine engine. In one form, the premixing module includes a central pilot premixer module with a main premixer module positioned thereround. Each of the portions of the fuel-air premixing module include an axial inflow swirler with a plurality of fixed swirler vanes. Fuel is injected into the main premixer module between the swirler vanes of the axial inflow swirler and at an acute angle relative to the centerline of the premixing module. |
| NASA分類 | Mechanical Engineering |
| 権利 | No Copyright |
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