Gas turbine

A gas turbine and turbine shaft technology, applied in mechanical equipment, engine functions, engine components, etc., can solve problems such as gas turbine efficiency limitations, and achieve the effect of small pressure loss and simple discharge
CN1380487AInactive Publication Date: 2002-11-20SIEMENS AG

Patent Information

Authority / Receiving Office
CN Β· China
Patent Type
Applications(China)
Current Assignee / Owner
SIEMENS AG
Publication Date
2002-11-20
Estimated Expiration
Not applicable Β· inactive patent

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Abstract

In a turbine (1) with several working blades assembled on the turbine shaft (8) assembled into a working blade group and several guide blades (14) connected to the turbine casing assembled into a guide blade group, in order to Particularly high efficiency is achieved in the case of a simple and reliable cooling of the turbine blades (12), (14). According to the invention, at least some of the guide vanes (14) have a coolant inlet (48) at their free end facing the turbine shaft (8).
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Description

technical field

[0001] The invention relates to a gas turbine, which has a plurality of working blades arranged on a turbine shaft which are respectively assembled into a working blade group and several guide blades which are respectively assembled into a guide blade group and connected with a turbine casing. Background technique

[0002] Gas turbines are used in many fields to drive electrical generators or working machines. Here, the energy contained in the fuel is used to generate the rotation of the turbine shaft. For this purpose, fuel is burned in a combustion chamber into which is also fed air compressed by a compressor. The high-temperature and high-pressure working medium formed by fuel combustion in the combustion chamber passes through a turbine unit connected behind the combustion chamber, where it expands to perform work.

[0003] In order to generate the rotary motion of the turbine shaft, a number of working blades, usually assembled i...

Claims

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