Examples of 'turbine section' in a sentence
Meaning of "turbine section"
turbine section - a part or component of a turbine, typically referring to a specific segment or area within the device
How to use "turbine section" in a sentence
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turbine section
Gas turbine engine with intercooling turbine section.
The turbine section typically employs a plurality of stationary vanes circumferentially arranged in rows.
The fan is also driven by the turbine section.
The turbine section typically employs a plurality of alternating rows of stationary vanes and rotating blades.
A liner for a turbine section.
The subsequent layers will show the detail conditions for each turbine section.
The hot compressed gas is then expanded in a turbine section to produce rotating shaft power.
The combustors may be annularly arranged between the compressor section and the turbine section.
A fire occurred in the turbine section of the Onagawa Nuclear Power Plant following the earthquake.
A cooling system for stationary vanes in the turbine section of a gas turbine.
The turbine section may comprise a free turbine connected to a power take-off shaft.
A turbine blade is the individual component which makes up the turbine section of a gas turbine.
The turbine section usually comprises a low-pressure turbine and a high-pressure turbine.
Like the compressor, the fan is powered by the turbine section of the engine.
The low-pressure turbine section C includes a first annular rotor.
See also
A turbine engine typically includes a compressor section, combustion section, and a turbine section.
Figure 1 schematically represents the turbine section through a plane containing its axis of rotation.
The flowpath extends sequentially through a compressor section, a combustion section and a turbine section.
The low-pressure turbine section C also comprises a second annular rotor.
Each feedwater preheater stage 34 has an inlet steam conduit originating from a steam turbine section.
The turbine section 18 may include one or more turbine stages.
BACKGROUND OF THE INVETION A conventional turbine engine has a compressor section, a combustor section and a turbine section.
An afterburner 9 can be provided between the turbine section 8 and the exhaust section 10.
In addition to the combustion section 6, the gas turbine comprises a compressor section 2 and a turbine section 3.
Each is powered by its own turbine section the high-pressure and low-pressure turbines, respectively.
An inlet in the base section houses an impeller to define a turbine section 24.
The turbine section 20 comprises a high pressure turbine, an intermediate pressure turbine and a low pressure turbine.
The expanded and cooled combustion gas leaves the turbine section 7 through an exhaust 23.
The turbine section was updated again in the " Evolution " upgrade.
The major components of the gas turbine are a compressor section 1, a combustion section 2, and a turbine section 3.
Turbine section 24 is disposed concentrically within bypass fan section 22.
FIG . 2 shows a braking device formed on the low-pressure turbine section of the gas turbine engine.
The turbine section 3 is comprised of an outer cylinder 10 that encloses an inner cylinder 11.
We have intruders in Turbine Section 3.
The turbine section 18 includes at least one rotor engaged on a turbine shaft 19.
The combustion gases 26 flow through a turbine 28 of a turbine section to produce work.
The turbine section 22 drives a shaft 28 which in turn drives the dynamic compressor section 12.
Accordingly, the exhaust flow from the internal combustion engine 12 is supplied to the turbine section 58.
The condensate from the steam turbine section 3 is returned to the economizer 20 of the boiler 18.
The first stream 85 flows radially outward into the hot gas 30 flowing through the turbine section 3.
Expansion of the combustion gas through turbine section 131 provides mechanical energy to drive compressor section 132.
The gas turbine 22 comprises a respective wall structure 13 surrounding the combustion chamber 19 and the turbine section 17.
FIG. 1 depicts the turbine section of a twin-spool turbine engine.
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