Gas turbine and use of gas turbine comprising a compressor casing having an inlet opening for harmonizing the compressor casing
A technology for compressor casings and gas turbines, applied to parts of pumping devices for elastic fluids, machines/engines, mechanical equipment, etc., which can solve problems such as friction of rotor components
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[0018] The subject is a turbine 1 comprising at least one rotor assembly 10 and at least one compressor housing 11 . Turbine 1 is a gas turbine. Combustion exhaust gas is the working fluid of the gas turbine 1 for driving the rotor assembly 10 of the turbine 1 .
[0019] The compressor housing comprises at least one inner compressor housing chamber 1112 for arranging the rotor assembly and at least one outer compressor housing chamber 1113 for compressor discharge air extraction. The rotor assembly is located in the inner compressor housing cavity such that the rotor assembly and the compressor housing are arranged coaxially with each other. These elements comprise a common axis of rotation 12 .
[0020] The inner compressor housing chamber 1112 and the outer compressor housing chamber 1113 are separated from each other by a partition housing wall 1101 . The outer compressor casing chamber 1113 includes at least one bounding casing wall 110 . The boundary housing wall 110 ...
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