The turbine section includes a low pressure turbine section and a high pressure turbine section.
A gas turbine engine has a turbine section and an air moving section upstream of the turbine section.
The turbine section (16) surrounds the combustion chamber (52) and the compressor section (12) surrounds the turbine section (16).
A disclosed gas turbine engine includes a compressor section, a combustor section, a first turbine section and a second turbine section.
A gas turbine engine comprising a combustion chamber (52), a turbine section (16) and a compressor section (12).
The turbine section includes a turbine housing (1) that surrounds a turbine wheel (15).
The turbine engine also includes a turbine section spaced from the compressor section along a centerline axis.
A gas turbine engine is provided that includes a compressor section, a combustor section, a diffuser case module, a turbine section, and a manifold.
The turbine section is in flow communication with the compressor section such that the compressed fluid flow is received by the turbine section.
A gas turbine engine includes a core engine that has a compressor section, a combustor section and a turbine section.
A gas turbine engine includes a fan section, a gear arrangement configured to drive the fan section, a compressor section and a turbine section.
The turbine section includes a first turbine driving the first compressor and a second turbine driving the second compressor.
A gas turbine engine includes an engine static structure housing that includes a compressor section and a turbine section.
A turbine engine includes at least a compressor section and a turbine section, each having at least a first and second portion.
A turbine section (204) is arranged in flow communication with the compressor section.
The turbine section (58) comprises a low-pressure turbine portion (56) coupled to and driving the fan section (46) and a high-pressure turbine portion (68) coupled to and driving the compressor section (65).
A turbine section is coupled to the compressor section via a rotating member such that portions of the rotating member are located within the compressor section and the turbine section, respectively.
A turbine engine includes a compressor section, a combustor in fluid communication with the compressor section, and a turbine section in fluid communication with the combustor section.
The turbine section is configured to drive compressor section and the gear arrangement.
The gas turbine produces hot compressed gas and then is expanded in a turbine section.
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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