Abstract: A system and a method for promoting improved air flow through a cooling tower and reduced inner air pressure losses caused by rain in the rain zone of a cooling tower. Aerodynamic modules are mounted on the lower edge of the cooling tower shell in order to deflect the downward-flowing air about the lower edge of the tower shell and into the rain zone. The aerodynamic modules can be modularly mounted, can be replaced, and do not affect the statics of the tower shell. Aerodynamic modules can also be built on the base area to deflect the incoming air over any obstacles. Troughs or dripping elements can also promote flow by reducing the rain falling in an outer area.

Abstract: A system and a method for promoting improved air flow through a cooling tower and reduced inner air pressure losses caused by rain in the rain zone of a cooling tower. Aerodynamic modules are mounted on the lower edge of the cooling tower shell in order to deflect the downward-flowing air about the lower edge of the tower shell and into the rain zone. The aerodynamic modules can be modularly mounted, can be replaced, and do not affect the statics of the tower shell. Aerodynamic modules can also be built on the base area to deflect the incoming air over any obstacles. Troughs or dripping elements can also promote flow by reducing the rain falling in an outer area.

Abstract: A coupling apparatus (4) for connecting two rotatable shafts (2a, 3a) of a turbocompressor (1) includes a first and a second coupling part (4a, 4b) which form part of the shaft (2a, 3a) or are designed for firm connection to one end section of the shafts (2a, 3a) each. A third coupling part (4c) is designed in disc-shape and is arranged between the first and the second coupling part (4a, 4b). The first, second and third coupling part (4a, 4b, 4c) are firmly connectable to one another. The third coupling part (4c) has a section (41) which projects beyond the first or second coupling part (4a, 4b) in the radial direction and is designed as a bearing disc of an axial bearing (7).

Abstract: A coupling apparatus (4) for connecting two rotatable shafts (2a, 3a) of a turbocompressor (1) includes a first and a second coupling part (4a, 4b) which form part of the shaft (2a, 3a) or are designed for firm connection to one end section of the shafts (2a, 3a) each. A third coupling part (4c) is designed in disc-shape and is arranged between the first and the second coupling part (4a, 4b). The first, second and third coupling part (4a, 4b, 4c) are firmly connectable to one another. The third coupling part (4c) has a section (41) which projects beyond the first or second coupling part (4a, 4b) in the radial direction and is designed as a bearing disc of an axial bearing (7).