Ultra-Lean Combustion at High Inlet Temperatures

Author:

Anderson D. N.1

Affiliation:

1. NASA Lewis Research Center, Cleveland, OH

Abstract

Combustion at inlet-air temperatures of 1100 to 1250 K was studied for application to advanced automotive gas turbine engines. Combustion was initiated by the hot environment, and therefore no external ignition source was used. Combustion was stabilized without a flameholder. The tests were performed in a 12-cm-diameter test section at a pressure of 2.5 × 105 Pa, with reference velocities of 32 to 60 m/s and at maximum combustion temperatures of 1350 to 1850 K. Number 2 diesel fuel was injected by means of a multiple-source fuel injector. Unburned hydrocarbons emissions were negligible for all test conditions. Nitrogen oxides emissions were less than 1.9 g NO2/kg fuel for combustion temperatures below 1680 K. Carbon monoxide emissions were less than 16 g CO/kg fuel for combustion temperatures greater than 1600 K, inlet-air temperatures higher than 1150 K, and residence times greater than 4.3 ms.

Publisher

American Society of Mechanical Engineers

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Spray Combustion Modeling in Lean Direct Injection Combustors, Part I: Single-Element LDI;Combustion Science and Technology;2014-12-23

2. Influence of the Primary Jets and Fuel Injection on the Aerodynamics of a Prototype Annular Gas Turbine Combustor Sector;Journal of Engineering for Gas Turbines and Power;2010-09-24

3. NOx model for lean combustion concept;Journal of Propulsion and Power;1995-01

4. Low NOx rich-lean combustion concept application;27th Joint Propulsion Conference;1991-06-24

5. Combustor Development for Automotive Gas Turbines;Journal of Energy;1983-09

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