radial-outflow turbine type for 3 MW WHR organic Rankine cycle

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radial-outflow turbine type for 3 MW WHR organic Rankine cycle ( radial-outflow-turbine-type-3-mw-whr-organic-rankine-cycle )

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D.Maksiuta, L.Moroz, M.Burlaka, Y.Govorushenko / Energy Procedia 00 (2017) 000–000 7 For this purpose, axial high-pressure (HPT) and low-pressure (LPT) turbines were designed with the boundary conditions specified in Table 1. RIT for aforementioned boundary conditions were designed in paper [3]. In this article they are also presented and are turbines regarding to which performance comparison was carried out. Main characteristics of all aforementioned turbine types are collected in Tables 2, 3. It should be noted that in common practice, axial turbines for ORC are limited to 3 stages due to mechanical or compactness restrictions. The same conclusion can be drawn regarding ROT. Despite this it should be noted that aerodynamic efficiency changes unequally for axial turbines and ROT with the changing of number of stages. In Fig.6 are comparative charts of how number of stages affects a turbine’s total-to-static efficiency for axial turbine and ROT (both turbines were designed using HPT boundary conditions). 0.90 0.80 0.70 0.60 0.50 ROT axial 2 4 6 8 10 Number of stages Fig. 6. Dependence of the efficiency on the turbine stage number for axial turbine and ROT Obviously, the maximum efficiency for axial turbine’s and ROT are almost the same. However, in order to achieve maximum efficiency, the axial turbine should be performed with the high number of stages. The ROT efficiency slightly changes with decreasing of number of stages. For example, for considered ROT, efficiency of the seven-staged design is 2.8% lower than of the three-staged design, while for axial turbine this difference achieves 30%. Such efficiency benefit is a big advantage of ROT, especially when the maximum number of stages is limited. In present paper we do not consider any particular restrictions: mechanical or compactness limitations. Therefore, further analysis is performed using only one design criterion – turbine aerodynamic efficiency. Table 2. Performance data and crucial dimensions of the HPTs Parameter Internal t-s efficiency Power Shaft rotational speed Number of stages Max Mach number Min machine diameter Max machine diameter1 Axial length Machine volume2 Unit Axial – 0.9047 kW 269.5 rpm 18305 – 10 – 0.529 mm 62.48 mm 114.7 mm 86.1 dm3 (liter) 0.89 RIT 0.8518 211.4 40 000 1 1.142 45.2 106.1 37.7 0.333 ROT 0.8953 266.5 27 129 5 0.949 56.3 114 12.8 0.131 Table 2 shows that different HPT types have significant differences in efficiency. The highest efficiency (and power respectively) has the 10 staged axial turbine. Radial-outflow turbine efficiency is slightly lower because of the stage number limitation. Wherein, efficiency of both the axial and the radial-outflow turbines are superior far from RIT performance values. Due to reduced shaft rotational speed in ROT and axial turbine, maximum Mach number is also reduced, that is obviously beneficial to the flow in the flowpath. 1 without volute 2 approximate value calculated as multiplication of the circle area of maximal radial dimension to the axial length Efficiency (t-s)

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radial-outflow turbine type for 3 MW WHR organic Rankine cycle

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