2019
DOI: 10.1016/j.energy.2019.05.135
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A micro-turbine-generator-construction-kit (MTG-c-kit) for small-scale waste heat recovery ORC-Plants

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Cited by 28 publications
(19 citation statements)
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“…The values are taken to reflect similar actual systems of absorption chillers [70]. The expander efficiency is taken as a state of the art from micro turboexpander experimental investigations [94,95]. The controlled variables are the temperatures of the heat source fluid T hs (mass flow fixed for all cases) and of ambient air T amb , which provide cooling water from the dry cooler after rejecting heat.…”
Section: Calculation Methods and Boundary Conditionsmentioning
confidence: 99%
“…The values are taken to reflect similar actual systems of absorption chillers [70]. The expander efficiency is taken as a state of the art from micro turboexpander experimental investigations [94,95]. The controlled variables are the temperatures of the heat source fluid T hs (mass flow fixed for all cases) and of ambient air T amb , which provide cooling water from the dry cooler after rejecting heat.…”
Section: Calculation Methods and Boundary Conditionsmentioning
confidence: 99%
“…Compared with single-stage radial-outflow turbine, single-stage axial-flow turbine may have higher efficiency with a smaller size [35]. Two micro single stage impulse axial turbines with output power of 15 kW and 12 kW were designed and the total-to-static efficiency of 65.0% and 73.4% were obtained, respectively [36]. The maximum isentropic efficiency of the small-scall cantilever turbines also could reach 76.8% [37].…”
Section: Introductionmentioning
confidence: 99%
“…In the current project, the authors have investigated analytically and by an in-house 1D turbine design tool (1DTDT) [18] various un-common turbine architectures like multi-stage radial-outflow turbines [17], quasi-impulse cantilever turbines [19] and radial inflow Curtisturbines for the given expansion task (400 °C/17.5 bar, 0.2 bar, about 80 g/s steam). Few uncommon turbine architectures have been promising from an aerodynamic point of view.…”
Section: Introductionmentioning
confidence: 99%