Supercritical CO2 Cycle Development at Pratt and Whitney Rocketdyne

Author(s):  
Gregory A. Johnson ◽  
Michael W. McDowell ◽  
George M. O’Connor ◽  
Chandrashekhar G. Sonwane ◽  
Ganesan Subbaraman

Pratt & Whitney Rocketdyne’s extensive experience in both the rocket engine and energy industries, provides an effective underpinning for work in supercritical CO2 power cycle development. Our current thrusts are supercritical CO2 power conversion for a LMR, a solar power system using molten salt energy storage, and a zero emission coal power system. Key observations from our nuclear power application work is that large, highly-effective heat exchangers will need to be developed, system architecture is driven by start-up operations, etc. along with steady-state full-power operations, and the large volumetric flow rates associated with this cycle coupled with the desire to keep pressure losses low will lead to parallel runs of large diameter pipe. Our solar power work is focused on developing a system architecture that can take advantage of the full thermal storage temperature spectrum while maintaining the high-efficiency and low-cost potential of this cycle. And in the fossil-fuel arena, the efficiency improvements derived from supercritical CO2 are particularly interesting as a way to make up the losses that are caused by CO2 sequestration.

2018 ◽  
Vol 90 (8) ◽  
pp. 1295-1304 ◽  
Author(s):  
Susan Liscouet-Hanke ◽  
Arash Shafiei ◽  
Luiz Lopes ◽  
Sheldon Williamson

Purpose This paper aims to analyze the viability of a solar power system as a supplemental power source for commercial and business aircraft. Design/methodology/approach First, a model is established to estimate the potential available power from suitable aircraft surfaces for various meteorological conditions, ground and flight mission characteristics. A proposed aircraft system architecture and an associated parametric conceptual sizing model are presented. This supplemental solar power system sizing model is integrated into an aircraft multidisciplinary design optimization environment to evaluate the aircraft-level impact on mission fuel burn. A parametric study for a business jet aircraft is performed to analyze various solar cell types and power densities for converters. Trade-off studies are performed between efficiency and weight. Findings Considering today’s efficiency and power-to-weight ratio of the system components, overall fuel burn reduction can be achieved. Therefore, the technology development work can start now to target short to mid-term applications. In addition, promising system integration scenarios are identified, such as the use of solar power for autonomous operation of the air conditioning system on ground, which yield potential further benefit. In conclusion, a supplemental solar power system seems a promising candidate for more efficient aircraft operation. Originality/value The presented novel supplemental solar power system architecture concept and its foreseen aircraft integration show potential benefits for near term applications. The results show that the break even for this technology is already reached and therefore build the foundation to further investigate the technology integration challenges. Clear directions for future research and development are outlined enabling the advancement of the technology readiness level.


2009 ◽  
Vol 631-632 ◽  
pp. 9-14
Author(s):  
Yoshikazu Shinohara ◽  
Katsuto Kisara ◽  
Hiroaki Suzuki

Laser medium for solar-pumped solid laser of 10MW-1GW power is a key to realize Laser Space Solar Power System (L-SSPS). Since it is an ultrahigh power system operated in space, the laser medium must satisfy the conditions such as high efficiency, high power per weight or volume, excellent durability and maintainability, thermal equilibrium operation, and excellent long-range propagation of oscillated laser. YAG (Y3Al5O12) ceramics doped doubly with Nd and Cr is considered to be a suitable laser medium for L-SSPS at present. There are the following important points for L-SSPS application: 1) Optimization of the doping amount, 2) Process, 3) Temperature control. Feasibility of YAG ceramics is discussed from a view point of material science and proposed a YAG ceramics structure with graded distribution of dopants.


2022 ◽  
pp. 0958305X2110738
Author(s):  
Paolo Iodice ◽  
Amedeo Amoresano ◽  
Giuseppe Langella ◽  
Francesco Saverio Marra

In the current context of increasing public awareness of the externalities of fossil fuel-based energy consumption, improvement in new technologies for energy-saving systems has become a crucial target to reduce both global warming and air pollution. Being motivated by such a critical matter, this study presents an innovative solar thermal plant based on volumetric expanders as work-producing devices coupled with Scheffler solar receivers as a thermal source. Nowadays, Scheffler receivers are well performing owing to high efficiency of the focal receiver which reduce heat losses. Simultaneously, screw expanders are volumetric machines which are able to convert thermal to mechanical power with acceptable efficiency also by expanding vapor-liquid blends at low operating pressures. The numerical model presented in this study evaluates the energetic benefits of the proposed solar power system for various operating situations. Parametric optimization of this solar power plant is then performed in a broad range of operating conditions: the optimum evaporation temperatures, together with the corresponding maximum global efficiencies, were so defined under various solar radiation intensities. The numerical results attained in this research prove that solar electricity generation systems based on screw expanders coupled with the Scheffler receivers are a promising technology.


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