NASA NTRS · 20100027521
Two stage catalytic combustor
Abstract
A catalytic combustor (14) includes a first catalytic stage (30), a second catalytic stage (40), and an oxidation completion stage (49). The first catalytic stage receives an oxidizer (e.g., 20) and a fuel (26) and discharges a partially oxidized fuel/oxidizer mixture (36). The second catalytic stage receives the partially oxidized fuel/oxidizer mixture and further oxidizes the mixture. The second catalytic stage may include a passageway (47) for conducting a bypass portion (46) of the mixture past a catalyst (e.g., 41) disposed therein. The second catalytic stage may have an outlet temperature elevated sufficiently to complete oxidation of the mixture without using a separate ignition source. The oxidation completion stage is disposed downstream of the second catalytic stage and may recombine the bypass portion with a catalyst exposed portion (48) of the mixture and complete oxidation of the mixture. The second catalytic stage may also include a reticulated foam support (50), a honeycomb support, a tube support or a plate support.
Keep this discovery
Explore connections, maps & timelines
Alvin, Mary Anne, Bachovchin, Dennis, Smeltzer, Eugene E., Lippert, Thomas E., Bruck, Gerald J.. 2010-04-06. Two stage catalytic combustor. https://ntrs.nasa.gov/citations/20100027521
Cite the original work for its findings. Save a collection to share your selection of sources.