HOUSING FOR A COMPRESSOR OF A GAS TURBINE, COMPRESSOR, AND METHOD FOR PRODUCING A HOUSING SEGMENT OF A COMPRESSOR HOUSING
Canada Patent
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Abstract
The present invention relates to a housing for a compressor of a gas turbine, particularly an aircraft gas turbine, having an outer housing (12) having at least one air inlet opening (14) and an inner housing (18) formed of at least two housing segments (16), wherein the housing segments (16) comprise at least one injection nozzle (20) for injecting air drawn in via the air inlet openings (14) into a flow channel (22) in the region of blade tips (26) of blades (24) of a rotor (28) of the compressor. The housing segment (16) thereby comprises at least one air guide channel (30), wherein the air guide channel (3) is designed such that air is directly guided by means of at least one air inlet element (32) disposed in the air inlet opening (14) of the outer housing (12) to the at least one injection nozzle (20). The invention further relates to a compressor of a gas turbine and a method for producing a housing segment (16) of a compressor housing (10).
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