WebJan 7, 2024 · The test vehicle selected for these assessments was a full annular combustor rig, which employs a modern lean-burn combustor technology (TAPS - Twin Annular Premixing Swirler). This combustor technology achieves lower emissions at high overall engine pressure ratios . GE Aviation 3 WebA twin annular premixing swirler (TAPS) combustor model of low emissions was developed in this study. And computational studies on combustion process in the combustor model were carried out. Standard k-ε Turbulence Model, PDF non-premixed combustion model, Zeldovich thermal NOx formation model and DPM two-phase model were employed. The …
Investigation on Reaction Flow Field of Low Emission TAPS …
WebMar 15, 2015 · The Twin Annular Premixing Swirler (TAPS) combustor [13], [16] was co-developed by the General Electric Aircraft Engines (GEAE) and NASA sponsorship. The … WebSep 1, 2009 · Abstract. The influences of different combustor configuration and spray mode on two phase spray combustion flows and combustion performances of twin annular … qianwh8094 top
Experimental study of flow dynamics and fuel spray …
WebSep 2, 2007 · Some typical aero-engine combustors, such as Twin Annular Premixing Swirler (TAPS) of General Electric (GE) [5], Lean Burn of Rolls-Royce (R-R) [6], low emission combustor of Japan Aerospace ... WebJun 15, 2024 · One of the most successful designs of such is the twin annular premixing swirler (TAPS) combustor by the General Electric Company in its GEnx engine [8]. Conventionally, the designs for the low-emission combustor and the HTR combustor are independently developed due to their different optimization targets. WebDec 1, 2024 · The Twin-Annular Premixing Swirler (TAPS) combustor, a 4th generation low-emissions technology, offers significant NOx reduction over state-of-the-art Low Emissions Combustor (LEC) technology for both low- and cruise- altitude operation. the last 40 years in the pollutant emissions of commercial aircraft. qiantang rivee tide waves