The jet engine (4) is of a type which generates an internal core flow (20) and an external fan flow (17) .
The fan flow path may extend from the fan inlet to the rear exhaust outlet of the bypass flow path.
A secondary flowpath extends from the secondary inlet to the outlet.
The secondary flow (2i) is determined.
A nacelle provides a first flow duct for the thrust fan blades and a secondary flow duct carries flow from the integral secondary flow blades.
A secondary flow is supplied to a mixing chamber of the jet pump, the secondary flow comprising a slurry of water and tailings, the slurry comprising more solids by mass than the primary flow.
In operation, the primary flow of engine exhaust is discharged from the high aspect ratio nozzles (30a, 30b) and entrains a secondary flow of ambient air through the longitudinal inlet (56) of the secondary flow shroud (26).
The multiplexed data stream includes substreams, where the substreams includes a descriptor substream, at least one media substream, and a compositing-instruction substream.
The second indication is related to the secondary stream.
Each sub-stream contains non-contiguous data.
Finally, scheduled data is allocated to the secondary stream in an amount not to exceed the determined secondary stream TBS.
In one implementation, the base layer stream of the SVC encoded stream is used as the secondary stream for the secondary display and the corresponding enhancement layer stream is used as the corresponding regular stream.
The first substream and the second substream are then recombined into a single working stream.
A secondary transmit power and a secondary transport block size for a secondary stream may also be determined.
A secondary transmit power and a secondary transport block size for a secondary stream may also be determined.
The liquid multi-component working stream is heated by a first external heat source stream at a first heat exchanger and is subsequently divided into a first substream and a second substream.
The recombined working stream is heated by the second external heat source stream at a fourth heat exchanger.
The stream to be transmitted resulting from the insertion of the secondary stream in the main stream is a symbol stream of a modified digital modulation.
A secondary sensor is positioned in a leakage flux path outside the first sensor or may be positioned in a secondary flux path.
The invention is intended for the suspension of a ducted-fan turbine engine with an elongate bypass duct.
The primary stream includes a primary data channel and a primary control channel and the secondary stream includes a secondary data channel and a secondary control channel.
The module comprises a hot flow channel through which the hot gas flow generated by the engine can flow and a bypass flow channel (14) through which the bypass air generated by the engine can flow.
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Traduction Translation Traducción Übersetzung Tradução Traduzione Traducere Vertaling Tłumaczenie Mετάφραση Oversættelse Översättning Käännös Aistriúchán Traduzzjoni Prevajanje Vertimas Tõlge Preklad Fordítás Tulkojumi Превод Překlad Prijevod 翻訳 번역 翻译 Перевод