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Titel:
Design and Certification of the Rolls-Royce BR725 Engine
Autor(en):
A. McIntosh, F. Koepf, U. Minkus, O. Rothfuss, S. Burggraf, P. Wehle
Zusammenfassung:
The BR725 is the newest and most advanced member of the BR700 engine family and has been selected to power the Gulfstream G650™ executive jet. Based upon the highly successful BR700 engine core, the BR725 is a two shaft, high by-pass ratio turbofan which has been designed for long life on wing, low fuel burn and excellent performance. By introducing a range of advanced design features from recent Rolls-Royce development programs as well as from the global Rolls-Royce Research and Technology program a low risk, right first time approach was achieved. Integrated by Rolls-Royce Deutschland, the BR725 has been developed by a truly global project team working across Rolls-Royce and suppliers sites and facilities. This paper describes the highlights of the BR725 engine design and development program which achieved all major targets and milestones, the most significant being the initial engine certification on 23. June 2009, only 42 months after program launch.
Veranstaltung:
Deutscher Luft- und Raumfahrtkongress 2010
Medientyp:
Conference Paper
Sprache:
englisch
Format:
21,0 x 29,7 cm, 10 Seiten
Veröffentlicht:
Deutscher Luft- und Raumfahrtkongress Tagungsband - Manuskripte, 2010, 2010, ; S.607-616; 2010; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn
Preis:
NA
ISBN:
ISSN:
Kommentar:
Klassifikation:
Stichworte zum Inhalt:
Verfügbarkeit:
Bestellbar
Veröffentlicht:
2010
Dieses Dokument ist Teil einer übergeordneten Publikation:
Deutscher Luft- und Raumfahrtkongress Tagungsband - Manuskripte, 2010