Advancing Pressure Gain Combustion in Terrestrial Turbine Systems Email Page
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Performer:  Purdue University Location:  West Lafayette, Indiana
Project Duration:  10/01/2015 – 03/29/2019 Award Number:  FE0025343
Technology Area:  Advanced Turbines Total Award Value:  $999,594
Key Technology:  Pressure Gain Combustion DOE Share:  $797,181
Performer Share:  $202,413

Rotating detonation engine test fire.
Rotating detonation engine test fire.

Project Description

The rotating detonation engine (RDE) or continuous detonation wave engine is acknowledged by many to be among the most promising pressure gain combustion technology approaches. While initially demonstrated in the 1960s, the highly transient operation, particularly relative to the injection system, has made it difficult to optimize performance. However, recent advances in high-speed data acquisition (including optical and laser-based measurements), combined with vastly improved computational tools, provide an environment suitable to rapidly advance the technology. The project team at Purdue University – along with industry consultant input from United Technologies Research Center (UTRC) – will conduct detailed measurements in both an operating RDE and a simplified system that will quantify key physics important for the design and optimization of RDEs, specifically, in the areas of fuel/air mixing, unsteady injector operation, and turbine integration characterization. The technical approach includes experimental studies (using an optically-accessible injection dynamics facility and a subscale combustor facility) as well as computational fluid dynamics (CFD) modeling analyses. The project team will ultimately work to develop a method to quantify net pressure gain in an operating RDE.

Project Benefits

The Purdue/UTRC team’s primary objectives for this work include assessment of dynamic injection and mixing performance; assessment of engine operability via interrogation of the spatio-temporal character of combustor inlet and exit flow conditions; assessment of engine emissions; and an overall assessment of the pressure gain potential of the device. Advances in these areas could lead to a whole new class of continuous detonation-based engines for future power generation applications.

Presentations, Papers, and Publications

Contact Information

Federal Project Manager Mark C. Freeman:
Technology Manager Richard Dennis:
Principal Investigator Stephen D. Heister: