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Autor:
Hunt, H. J.
Publikováno v:
The Modern Language Review, 1953 Jul 01. 48(3), 348-349.
Externí odkaz:
https://www.jstor.org/stable/3718630
Autor:
Charles, Robert Alan
Publikováno v:
The Modern Language Journal, 1954 May 01. 38(5), 261-261.
Externí odkaz:
https://www.jstor.org/stable/320074
Autor:
Mathieu Picard, P. K. Dubois, Jean-Sébastien Plante, Dominik Thibault, Cederick Landry, Benoit Picard
Publikováno v:
Journal of Propulsion and Power. 38:221-228
Distributed aircraft propulsion has renewed the interest in power-dense, high-efficiency power packs. Ceramic turbomachinery could be a major enabler, although no successful design has been achieve...
Autor:
Jean-Benoît Picard
Marco, un publicitaire désabusé, vit selon la devise « pas de femme, pas d'enfants, pas de poisson rouge ». Cependant, cette philosophie se retourne contre lui et le pousse à entreprendre un voyage introspectif. Il se retrouve plongé dans les m
Publikováno v:
Aircraft Engineering and Aerospace Technology. 92:717-726
Purpose The limited energy density of batteries generates the need for high-performance power sources for emerging eVTOL applications with radical operational improvement potential over traditional aircraft. This paper aims to evaluate on-design and
Autor:
Jean-Sébastien Plante, Alexandre Landry-Blais, Antoine Gauvin-Verville, Benoit Picard, P. K. Dubois, Mathieu Picard
Publikováno v:
Volume 6: Ceramics and Ceramic Composites; Coal, Biomass, Hydrogen, and Alternative Fuels; Microturbines, Turbochargers, and Small Turbomachines.
Increasing turbine inlet temperature (TIT) of recuperated gas turbines would lead to simultaneously high efficiency and power density, making them prime candidates for low-emission aeronautics applications, such as hybrid-electric aircraft. The insid
Publikováno v:
Volume 6: Ceramics and Ceramic Composites; Coal, Biomass, Hydrogen, and Alternative Fuels; Microturbines, Turbochargers, and Small Turbomachines.
Recuperated, high-temperature microturbines (< 1 MW) could be a key enabler for hybrid powertrains of tomorrow’s small aircraft. To achieve competitive thermal efficiencies, turbine inlet temperature (TIT) must increase to 1550 K, well beyond conve
Autor:
Alexandre Landry-Blais, Benoit Picard, Dominik Thibault, J.-S. Plante, Mathieu Picard, P. K. Dubois
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 143
In order to reach 40% efficiency, sub-MW turbines must operate in a recuperated gas Brayton cycle at a turbine inlet temperature (TIT) above 1300°C. Current sub-MW turbines have material-related operating temperature limits. Still to this day, there