3D Printed Radial Impulse Cantilever Micro-Turboexpander for Preliminary Air Testing
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F21%3A00348640" target="_blank" >RIV/68407700:21220/21:00348640 - isvavai.cz</a>
Nalezeny alternativní kódy
RIV/68407700:21720/21:00348640
Výsledek na webu
<a href="https://doi.org/10.1063/5.0041433" target="_blank" >https://doi.org/10.1063/5.0041433</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1063/5.0041433" target="_blank" >10.1063/5.0041433</a>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
3D Printed Radial Impulse Cantilever Micro-Turboexpander for Preliminary Air Testing
Popis výsledku v původním jazyce
This work introduces a modular experimental micro turboexpander system designed to perform air turbine tests of a radial impulse cantilever turbine. The system has high modularity and is intended primarily to test flow-path components which are manufactured by 3D printing and rapid prototyping. System design from the fluid dynamic viewpoint is based on a previously described tool proven and validated during the design of micro turboexpanders in range of mainly dozens of kW. In order to achieve maximal simplicity, the system uses a converted aeromodelling motor as a permanent magnet generator and housing for bearings. Overall parameters are obtained from electrical performance and known generator’s characteristics. The mechanical design then takes into account request of simplicity, modularity and properties of materials in additive manufacturing, especially plastics. First experimental tests show a comparison between different manufacturing technologies and resulting flow components surface roughness and the impact of pressure ratio on the isentropic efficiency.
Název v anglickém jazyce
3D Printed Radial Impulse Cantilever Micro-Turboexpander for Preliminary Air Testing
Popis výsledku anglicky
This work introduces a modular experimental micro turboexpander system designed to perform air turbine tests of a radial impulse cantilever turbine. The system has high modularity and is intended primarily to test flow-path components which are manufactured by 3D printing and rapid prototyping. System design from the fluid dynamic viewpoint is based on a previously described tool proven and validated during the design of micro turboexpanders in range of mainly dozens of kW. In order to achieve maximal simplicity, the system uses a converted aeromodelling motor as a permanent magnet generator and housing for bearings. Overall parameters are obtained from electrical performance and known generator’s characteristics. The mechanical design then takes into account request of simplicity, modularity and properties of materials in additive manufacturing, especially plastics. First experimental tests show a comparison between different manufacturing technologies and resulting flow components surface roughness and the impact of pressure ratio on the isentropic efficiency.
Klasifikace
Druh
D - Stať ve sborníku
CEP obor
—
OECD FORD obor
20303 - Thermodynamics
Návaznosti výsledku
Projekt
<a href="/cs/project/8E18B012" target="_blank" >8E18B012: Cenově dostupné turboexpandéry pro aplikace v decentralizované energetice – možnosti výroby 3D tiskem z moderních plastů</a><br>
Návaznosti
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Ostatní
Rok uplatnění
2021
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název statě ve sborníku
19TH CONFERENCE ON POWER SYSTEM ENGINEERING
ISBN
978-0-7354-4067-8
ISSN
0094-243X
e-ISSN
1551-7616
Počet stran výsledku
10
Strana od-do
—
Název nakladatele
AIP Publishing LLC
Místo vydání
Melville (NY)
Místo konání akce
Plzeň
Datum konání akce
8. 9. 2020
Typ akce podle státní příslušnosti
WRD - Celosvětová akce
Kód UT WoS článku
000668075000006