초록 ▼

The invention provides a gas turbine intake air filter unit, wherein flow resistance of intake air passing through a tertiary filter layer does not become unreasonably great despite the filter layers are increased from two stages to three stages, and a balance of collecting efficiency of the filter

The invention provides a gas turbine intake air filter unit, wherein flow resistance of intake air passing through a tertiary filter layer does not become unreasonably great despite the filter layers are increased from two stages to three stages, and a balance of collecting efficiency of the filter layers and the intake air flow resistance is optimized.A weather louver 10 , a primary filter layer 11 , a secondary filter layer 12 , and a tertiary filter layer 13 are sequentially disposed from an upstream side in the filter unit 1 installed at an upstream side end portion of an intake duct 2 communicating with a gas turbine 3 , at least a recess 13 e is formed toward a downstream side of the intake air flow A′ on an end face filter layer portion 13 a that is a constituent of the tertiary filter layer 13 and is disposed orthogonally to the intake air flow A′ inside the intake duct 2.

대표청구항 ▼

1. A gas turbine intake air filter unit, comprising:a primary filter layer, a secondary filter layer, and a tertiary filter layer placed at an upstream side end portion of an intake duct that leads intake air into an internal area of a gas turbine and sequentially aligned from an upstream side; wher

1. A gas turbine intake air filter unit, comprising:a primary filter layer, a secondary filter layer, and a tertiary filter layer placed at an upstream side end portion of an intake duct that leads intake air into an internal area of a gas turbine and sequentially aligned from an upstream side; whereinsaid primary, secondary and tertiary filter layers respectively include a plurality of unitary filters; andsaid plurality of unitary filters of said tertiary filter layer are aligned in such a manner that at least a recess is provided in a downstream direction of said intake air flow. 2. The gas turbine intake air filter unit as set forth in claim 1, whereina downstream side end portion of said recess is located at an upstream side of a wind velocity reference line serving as an index of whether or not a turbulent flow of intake air causes noise and/or vibration. 3. The gas turbine intake air filter unit as set forth in claim 2, whereinsaid recess is disposed so as to confront an upstream end opening of said intake duct. 4. The gas turbine intake air filter unit as set forth in claim 3, whereineach of said unitary filters of said primary filter layer and of said secondary filter layer is insert-fitted to a first fixing frame; andeach of said unitary filters of said tertiary filter layer is insert-fitted to a second fixing frame. 5. The gas turbine intake air filter unit as set forth in claim 3, further comprising:a weather louver for integrating and refracting intake air flow located at an upstream side of said primary filter layer. 6. The gas turbine intake air filter unit as set forth in claim 5, whereinsaid weather louver is formed so as to cover said upstream end opening of said intake duct in a bag shape. 7. The gas turbine intake air filter unit as set forth in claim 2, whereinsaid primary, secondary and tertiary filter layers are formed so as to cover said upstream end opening of said intake duct in a bag shape. 8. The gas turbine intake air filter unit as set forth in claim 2, whereineach of said unitary filters of said primary filter layer and of said secondary filter layer is insert-fitted to a first fixing frame; andeach of said unitary filters of said tertiary filter layer is insert-fitted to a second fixing frame. 9. The gas turbine intake air filter unit as set forth in claim 2, further comprising:a weather louver for integrating and refracting intake air flow located at an upstream side of said primary filter layer. 10. The gas turbine intake air filter unit as set forth in claim 9, whereinsaid weather louver is formed so as to cover said upstream end opening of said intake duct in a bag shape. 11. The gas turbine intake air filter unit as set forth in claim 1, whereinsaid recess is disposed so as to confront an upstream end opening of said intake duct. 12. The gas turbine intake air filter unit as set forth in claim 11, whereinsaid primary, secondary and tertiary filter layers are formed so as to cover said upstream end opening of said intake duct in a bag shape. 13. The gas turbine intake air filter unit as set forth in claim 11, whereineach of said unitary filters of said primary filter layer and of said secondary filter layer is insert-fitted to a first fixing frame; andeach of said unitary filters of said tertiary filter layer is insert-fitted to a second fixing frame. 14. The gas turbine intake air filter unit as set forth in claim 11, further comprising:a weather louver for integrating and refracting intake air flow located at an upstream side of said primary filter layer. 15. The gas turbine intake air filter unit as set forth in claim 14, whereinsaid weather louver is formed so as to cover said upstream end opening of said intake duct in a bag shape. 16. The gas turbine intake air filter unit as set forth in claim 1, whereinsaid primary, secondary and tertiary filter layers are formed so as to cover said upstream end opening of said intake duct in a bag shape. 17. The gas turbine intake air filter unit as set forth in claim 16, further comprising:a weather louver for integrating and refracting intake air flow located at an upstream side of said primary filter layer. 18. The gas turbine intake air filter unit as set forth in claim 1, whereineach of said unitary filters of said primary filter layer and of said secondary filter layer is insert-fitted to a first fixing frame; andeach of said unitary filters of said tertiary filter layer is insert-fitted to a second fixing frame. 19. The gas turbine intake air filter unit as set forth in claim 1, further comprising:a weather louver for integrating and refracting intake air flow located at an upstream side of said primary filter layer. 20. The gas turbine intake air filter unit as set forth in claim 19, whereinsaid weather louver is formed so as to cover said upstream end opening of said intake duct in a bag shape.