Housing means a casing around the impeller which guides the gas stream towards, through and from the impeller
The stage includes a rotatable impeller (124) that has an impeller hub with a centrally disposed eye and a plurality of impeller vanes.
The impellers include a first impeller (104) and a second impeller (102).
This supercharger (42) is provided with a centrifugal impeller (50) and an impeller casing (52) that covers the impeller (50).
The air impeller (3) is a vortex air impeller.
A turbine nozzle segment, a turbine nozzle, a turbine, and a gas turbine engine.
The turbine is equipped with a high-pressure turbine, a medium-pressure turbine, and a low-pressure turbine.
A turbine section includes a high pressure turbine, an intermediate turbine and a fan drive turbine.
The turbine section includes a fan drive turbine and a second turbine.
The turbine includes at least one turbine stage having turbine blades.
A boss structure of an impeller of a blower in which the impeller has an increased strength and an impeller of a blower having the same.
supercharging by means of exhaust turbo-blowers
The blower unit is connected to the heating unit and has an outlet port, a blower fan for blowing heated air, and a drive motor for rotating the blower fan.
Advantageously, the turbine machine (1) is a pneumatic turbine.
A mid-turbine frame is incorporated into a turbine section of a gas turbine engine intermediate a high pressure turbine and a low pressure turbine.
[…] % (Low Pressure Turbine less Nozzle Guide Vanes
The turbine is fitted with multiple turbine vanes.
The turbine includes a turbine rotor and a plurality of vanes connected to the turbine rotor.
The turbine comprises a staged helical blade turbine,
The turbine wheel (16) includes a turbine hub (24) and a plurality of turbine blades (26) extending radially from the turbine hub (24).
A mid-turbine frame is incorporated into a turbine section of a gas turbine engine intermediate a high pressure turbine and a low pressure turbine.
A gas turbine engine comprises a first turbine module, a second turbine module, and a frame interconnecting the first turbine module with the second turbine module.
The invention relates to a turbine (6), especially a gas turbine.
A turbine wheel (16) is disposed in the turbine shroud (12) and includes a plurality of turbine blades (26).
The turbine (610) has a turbine body (640, 650, 650a, 650b) around a turbine shaft (630), the turbine body (640, 650, 650a, 650b) having a turbine stabiliser (650, 650a, 650b).
The invention relates to a low-pressure turbine of a gas turbine.
A gas turbine engine turbine disk assembly includes a turbine disk, turbine blades, and pin seals.
The inter-stage channel transports the first turbine exhaust gas from the first turbine to the second turbine.
A turbine engine includes a turbine section with a low pressure turbine and a turbine case disposed about an axis.
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,
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