Design and performance of an atmospheric pressure HF chemical laser

Author(s):  
D. Chuchem ◽  
Yehoshua Y. Kalisky ◽  
M. Amit ◽  
Israel Smilanski
Author(s):  
Kenneth A. Cornell ◽  
Amanda White ◽  
Adam Croteau ◽  
Jessica Carlson ◽  
Zeke Kennedy ◽  
...  

1996 ◽  
Author(s):  
Yehoshua Y. Kalisky ◽  
Karol Waichman ◽  
S. Kamin ◽  
D. Chuchem

2021 ◽  
Author(s):  
Stefan D. Cich ◽  
J. Jeffrey Moore ◽  
Meera Day Towler ◽  
Jason Mortzheim

Abstract Recent testing has been completed on a 1 MWe supercritical carbon dioxide (sCO2) closed loop recuperated cycle under funding from the US Department of Energy (DOE) Sunshot initiative and industry partners. Some of the goals of this funding included the development of a 1 MWe loop, a 10 MWe turbine, and performance and mechanical testing. One of the key challenges that presented itself was the filling, start-up, and shut down of the entire system. Understanding the loop transient performance is important when having to bring a turbine online, transitioning from peak to partial loading, and also managing routine and emergency shut downs. Due to large changes in density near the critical point for CO2 and its tendency to form dry ice when expanded to atmospheric pressure, managing loop filling and venting is critical in ensuring that components are not damaged. With successful testing up to 715°C and 234 bar, this paper will provide updated data to, “Loop Filling and Start Up with a Closed Loop sCO2 Brayton Cycle [1].” While the previous paper focused on early trips and start up challenges, this paper will focus on the specific challenges at maximum operating conditions, and how the loop was managed when getting up to these high temperatures and pressures and how the loop behaved during a high temperature trip when compared to a controlled shut down from maximum operating conditions.


1997 ◽  
Vol 137 (1-3) ◽  
pp. 59-63 ◽  
Author(s):  
Y Kalisky ◽  
K Waichman ◽  
S Kamin ◽  
D Chuchem

Author(s):  
Thien Pham ◽  
Viet Bui ◽  
Thi Phan ◽  
Ha Than

In this work, preparation and performance of catalysts as using a simple method and highly efficient heterogeneous nanocatalyst is described. The main advantages of the reaction are high yields for the oxidation of CO at low temperature. The catalysts based-on oxides of copper and manganese supported on alumina monoliths were prepared by the different methods: plasma corona discharge and wet impregnation. Structure and physical properties of catalysts were characterized by FT-IR, XRD, TEM, EDX and TG/DTA. The results showed that the using of plasma corona discharge at atmospheric pressure in the preparation process of catalyst gives a smaller particle size, uniform dispersion when compared with the catalysts prepared by the wet impregnation methods. The catalytic activities of these catalysts were investigated for complete oxidation of carbon monoxide (3000 ppm) to carbon dioxide in the air at the atmospheric pressure. On a single oxide catalyst, 10CuO/monolith was better than 10MnO2/monolith in the same experimental condition. With multi-oxide catalysts, all catalyst samples are more active than a single-oxide catalyst in the same impregnated content. In particular, the catalyst is prepared by plasma corona discharge indicate the best oxidation capacity of carbon monoxide (CO).


Author(s):  
Stefan D. Cich ◽  
J. Jeffrey Moore ◽  
Meera Day Towler ◽  
Jason Mortzheim ◽  
Douglas Hofer

Abstract Recent testing has been performed on a 1 MWe sCO2 closed loop recuperated cycle under funding from the US DOE Sunshot initiative and industry partners. Some of the goals of this funding included the development of a 1 MWe loop, a 10 MWe turbine, and performance and mechanical testing. One of the key challenges that presented itself was the filling, start-up, and shut down of the entire system. Understanding the loop transient performance is important when having to bring a turbine online, transitioning from peak to partial loading, and also managing routine and emergency shut downs. Due to large changes in density near the critical point for CO2 and its tendency to form dry ice when expanded to atmospheric pressure, managing loop filling and venting is critical in ensuring that components do not get damaged. Specific challenges were centered on protecting the dry gas seals, maintaining proper mass in the loop, and also thermal transients during trips. This paper will take a detailed look at the challenges encountered during start up and shut downs, and also the solutions that were implemented to successful transition between different phases of the testing.


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