MODULE 15 — GAS TURBINE ENGINE
A plurality of gas turbine blades are attachable to a gas turbine disk, where each of the gas turbine blades includes a blade dovetail engageable in a correspondingly-shaped dovetail slot in the gas turbine disk.
The gas turbine engine system includes a gas turbine engine and an exhaust gas conditioning system.
A plurality of gas turbine blades are attachable to a gas turbine disk, where each of the gas turbine blades includes a blade dovetail engageable in a correspondingly-shaped dovetail slot in the gas turbine disk.
Furthermore, the invention discloses a gas turbine and methods for operating such a gas turbine.
A seal for a gas turbine engine and a gas turbine engine employing such a seal are disclosed.
A gas turbine engine, a fan section for a gas turbine engine, and a method for assembling a fan section of a gas turbine engine are disclosed.
A system includes an oxidant compressor and a gas turbine engine turbine, which includes a turbine combustor, a turbine, and an exhaust gas compressor.
A gas turbine engine is provided.
A gas turbine engine is provided.
A gas turbine engine is disclosed having a vane disposed in a flow path of a gas turbine engine component, for example a gas turbine engine compressor.
The exhaust gas conditioning system is coupled between a discharge outlet of the gas turbine engine and an inlet of the gas turbine engine.
A gas turbine engine is also disclosed.
The gas turbine engine propulsion system comprises a gas turbine engine that includes a fan flow path.
The gas turbine engine includes a fan.
The invention relates to a gas turbine (1), and to a method for operating said gas turbine.
supercharging by means of exhaust gas turbines
supercharging by means of exhaust turbo-blowers
open cycle of a gas turbine
simple cycle of a gas turbine
closed cycle of a gas turbine
rated speed of a gas turbine
The industrial turbine may be a gas turbine (1) or a steam turbine (11).
gas turbine locomotive with electric transmission
The GT operating power can be the rated power of the gas turbine.
The turbine stage (14) is equipped with a gas turbine to which hot gas from the burner can be supplied.
A gas turbine system is described, comprising a gas turbine (23), at least a first load (71) and a second load (72) powered by the gas turbine.
The gas turbine produces hot compressed gas and then is expanded in a turbine section.
intercooled cycle of a gas turbine
The exhaust gas turbine has two exhaust gas flows via which exhaust gas is fed to the turbine wheel.
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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