DGLR-Publikationsdatenbank - Detailansicht
Titel:
Compact High Performance Heat Exchangers for ICR Aircraft Gas Turbines
Autor(en):
G. Pellischek
Zusammenfassung:
On the basis of the shrouded propfan engine, the principles of the intercooled / recuperated (ICR) gas turbine cycle are described. Design considerations for the intercooler that led to the selection of two plate-fin matrices and to the proposal of a possible matrix arrangement are given. After introducing the design objectives, a comparison of circular turbe arrangements with a profile tube matrix shows slight advantages in favour of the former layout as far as the matrix net weight and the gas-side frontal area are concerned, whereas the profile tube matrix is clearly superior regarding installation. Physical aspects influencing the matrix selection for the intercooler are presented.
Veranstaltung:
Eurpean Propulsion Forum, 1990, Köln
Medientyp:
Conference Paper
Sprache:
englisch
Format:
21,0 x 29,7 cm, 5 Seiten
Veröffentlicht:
DGLR-Bericht, 1990, 1990-01, Eurpean Propulsion Forum: Future Civil Engines and the Protection of the Atmosphere - Proceedings; S.175-179; 1990; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn
Preis:
NA
ISBN:
ISSN:
Kommentar:
Klassifikation:
Stichworte zum Inhalt:
Verfügbarkeit:
Bestellbar
Veröffentlicht:
1990
Dieses Dokument ist Teil einer übergeordneten Publikation:
Eurpean Propulsion Forum: Future Civil Engines and the Protection of the Atmosphere - Proceedings