GE To Demo Fuel-Cell/Gas-Turbine Hybrid For Propulsion Electrification | Aviation Week Network
Overview of Low Emission Combustion Research at NASA Glenn
A Triple-Flame, n+3 Generation Mixer
A Triple-Flame, n+3 Generation Mixer
The quantitative characterization of the ignition process for a lean staged injector: Influence of the air split between pilot swirlers - Jinhu Yang, Cunxi Liu, Fuqiang Liu, Yong Mu, Gang Xu, 2020
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition : Development of the GE Aviation
LEAP – Lowering emissions - YouTube
TAPS II Public Final
CLEEN Phase II GE TAPS
Experimental and numerical studies of a lean-burn internally-staged combustor - ScienceDirect
N+2 Advanced Low NOx Combustor Technology Final Report
DLR - Institute of Combustion Technology - Fuel placement in gas turbine combustion chambers
N+2 Advanced Low NOx Combustor Technology Final Report
Aerospace | Free Full-Text | Large Eddy Simulation of the Influences of the Pilot-Stage Structure on the Flow Characteristics in a Centrally Staged High-Temperature-Rise Combustor
Bjorn's Corner: Turbofan engine challenges, Part 5 - Leeham News and Analysis
Comparison of NO x emissions between the lean TAPS and a RQL combustor... | Download Scientific Diagram
GEnx - 1B2B TAPS II Fuel Nozzle Removal - GE Aviation Maintenance Minute - YouTube
Twin Annular Premixing Swirler (TAPS) - The Technology Transfer ...
Low Emissions Propulsion Engine Combustor Technology Evolution Past, Present and Future
TAPS II Public Final
Low Emissions Propulsion Engine Combustor Technology Evolution Past, Present and Future
TAPS II Public Final
TAPS II Public Final
TAPS II Public Final
