Gas turbine, guide blade ring of a gas turbine and method for producing the same

Gas turbine, guide blade ring of a gas turbine and method for producing the same

A gas turbine (10) with a compressor (11) formed as axial compressor, wherein the compressor (11) comprises stator side guide blades (30, 30a) and rotor side moving blades (29), with a burner (13) comprising at least one combustion chamber (21); with a turbine (12); with a diffuser (22) arranged see...

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Hauptverfasser: Jaman EL MASALME, Stefan CLAUSS, Andreas KLEINFELDT, Michael BLASWICH, Emil ASCHENBRUCK
Format: Patent
Sprache:swe
Schlagworte:
BLASTING
HEATING
LIGHTING
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT PUMPS
POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS
PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
WEAPONS
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creator Jaman EL MASALME
Stefan CLAUSS
Andreas KLEINFELDT
Michael BLASWICH
Emil ASCHENBRUCK
description A gas turbine (10) with a compressor (11) formed as axial compressor, wherein the compressor (11) comprises stator side guide blades (30, 30a) and rotor side moving blades (29), with a burner (13) comprising at least one combustion chamber (21); with a turbine (12); with a diffuser (22) arranged seen in flow direction of the compressed air downstream of the compressor (12), which has an inside wall (26) and an outside wall (27); with an intermediate housing (28) following the outside wall (27). An outlet side guide blade ring (32) of stator side, outlet side guide blades (30a) of the compressor (11) comprises an inner shroud (33) and comprises an outer shroud (34), wherein on the outer shroud (34) of the guide blade ring (32) first fastening devices (35) are formed via which the guide blade ring (32) is directly attached to the intermediate housing (28), and wherein on the inner shroud (33) of the guide blade ring (32) second fastening devices (36) are formed, via which the inside wall (25) of the diffuser (22) is directly attached to the guide blade ring (32). Fig. 2
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An outlet side guide blade ring (32) of stator side, outlet side guide blades (30a) of the compressor (11) comprises an inner shroud (33) and comprises an outer shroud (34), wherein on the outer shroud (34) of the guide blade ring (32) first fastening devices (35) are formed via which the guide blade ring (32) is directly attached to the intermediate housing (28), and wherein on the inner shroud (33) of the guide blade ring (32) second fastening devices (36) are formed, via which the inside wall (25) of the diffuser (22) is directly attached to the guide blade ring (32). 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An outlet side guide blade ring (32) of stator side, outlet side guide blades (30a) of the compressor (11) comprises an inner shroud (33) and comprises an outer shroud (34), wherein on the outer shroud (34) of the guide blade ring (32) first fastening devices (35) are formed via which the guide blade ring (32) is directly attached to the intermediate housing (28), and wherein on the inner shroud (33) of the guide blade ring (32) second fastening devices (36) are formed, via which the inside wall (25) of the diffuser (22) is directly attached to the guide blade ring (32). Fig. 2</abstract><oa>free_for_read</oa></addata></record>
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subjects BLASTING
HEATING
LIGHTING
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT PUMPS
POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS
PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
WEAPONS
title Gas turbine, guide blade ring of a gas turbine and method for producing the same
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