Explosion protection for a turbine and combustion engine
In an explosion protection for gas a turbine which includes a turbine wheel and a turbine housing surrounding the turbine wheel, wherein the explosion protection comprises a multi-layer structure of material of a high rupture strength, the explosion protection is in the form of an essentially closed pot including a bottom section and a sash extending fully around the bottom section for accommodating the turbine housing.
1. A gas turbine ( 100 ) including a turbine wheel ( 11 ) and a turbine housing ( 12 ) completely surrounding the turbine wheel ( 11 ) and having an axial exhaust gas outlet duct ( 12 a ), and an explosion protection ( 1 ) comprising a multi-layer (a, b, c) structure of a material of high rupture strength in the form of an essentially closed pot structure including a bottom section ( 2 ) with an opening ( 2 a ) accommodating the axial exhaust gas outlet duct ( 12 a ) in spaced relationship, and a sash ( 3 ) extending fully around the turbine housing ( 12 ) and being supported by a cover plate ( 4 ) which is arranged opposite the bottom section ( 2 ).
2. The explosion protection according to claim 1 , wherein the multi-layer structure is formed by a deformation of individual metal sheet parts into pot-like metal parts and the multi-layer structure is formed by assembly of such individual pot-like metal parts into the pot-like multi-layer structure.
3. The explosion protection according to claim 1 , wherein the multi-layer pot-like structure is obtained by a deformation of a multi-layer arrangement of individual metal sheets.
4. The explosion protection according to claim 1 , wherein the cover ( 4 ) is in the form of a backplate consisting of metal.
5. The explosion protection according to claim 1 , wherein the cover ( 4 ) includes a circumferential rim ( 6 ) via which it is mounted to the sash ( 3 ).
6. The explosion protection according to claim 5 , wherein the sash ( 3 ) is joined to the rim ( 6 ) of the cover ( 4 ) along the circumferential inside area of the rim ( 6 ) of the cover ( 4 ).
7. The gas turbine ( 100 ) according to claim 1 , wherein the cover plate ( 4 ) which is arranged opposite the bottom section ( 2 ) is mounted to a gas turbine wheel bearing housing ( 22 ).
8. The gas turbine ( 100 ) according to claim 7 , wherein the turbine wheel ( 11 ) is mounted on a shaft ( 21 ) supported on a bearing ( 20 ) arranged in the wheel bearing housing ( 22 ).