Gas turbine including multiple can combustors
A gas turbine and combustor technology, applied in the field of interaction, can solve problems such as the separation plane sealing of the casing that cannot be guaranteed
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[0030] With reference to the accompanying drawings, the technical content and detailed description of the present invention are described below according to the preferred embodiments, and the preferred embodiments are not intended to limit the implementation scope of the present invention. Any equivalent changes and modifications made according to the appended claims are all covered by the claims of the present invention.
[0031] The present invention will now be described in detail with reference to the accompanying drawings.
[0032] refer to figure 1 , which is a schematic diagram of a gas turbine used in a power plant. according to figure 1 As an example, a gas turbine 1 includes a compressor 2 , a combustor 3 and a turbine 5 . As is known, the incoming air is compressed by compressor 2 and then enters the plenum defined by the casing of the gas turbine ( figure 1 not shown in ). Compressed air enters the burner stage from the plenum. In the burner stage, air is ...
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