Abstract: A ventilation system for a wide bodied aircraft with pressurization cabin which includes: a compressor apparatus with a heat exchanger for drawing air in from an input reservoir and for generating an excess pressure in at least one output reservoir, several air outlets in the pressurization cabin which are connected to the output reservoir of the compressor apparatus, and at least one suction air intake pipe in the pressurization cabin wherein the volume flow through at least one of the air outlets is adjusted each time by a volume flow control member, as well as to a method for manufacturing a ventilation system of this type.

Abstract: A holding system for fixing a line assembly includes a fixing band, and a fixing band retaining element, which is arranged on the line assembly and comprises at least one guiding element for receiving the fixing band, the fixing band retaining element comprising two ends, one end being provided with at least one or more cavities or recesses, into which the other end can be plugged or hooked.

Abstract: A device (10) for connecting two duct elements (12, 14) and a baffle (34) in an aircraft air conditioning system may include first (30) and second (32) connecting flanges each connected to one of the two duct elements (12, 14), and at least one connecting element (38) formed on the first connecting flange (30) which interacts with at least one corresponding connecting element (40) formed on the second connecting flange (32) to establish the connection of the two duct elements (12, 14) and the baffle (34). The first (30) and/or second connecting flange (32) has/have an opening (44) for receiving the baffle (34), which is substantially disc-shaped and formed with at least one air passage (46, 48). The baffle (34) serves to control the flow of at least one air stream flowing through the connected duct elements (12, 14).

Abstract: The invention relates to a device (10) for connecting two duct elements (12, 14) and a baffle (34) in an aircraft air conditioning system. The device (10) comprises a first (30) and a second connecting flange (32) which are in each case connected to one of the two duct elements (12, 14) to be connected. Further, at least one connecting means (38) is formed on the first connecting flange (30), which means interacts with at least one corresponding connecting means (40) formed on the second connecting flange (32) to establish the connection of the two duct elements (12, 14) and the baffle (34). The first (30) and/or second connecting flange (32) has/have an opening (44) for receiving the baffle (34), which is substantially disc-shaped and formed with at least one air passage (46, 48). In this respect the baffle (34) serves to control the flow of at least one air stream flowing through the connection.

Abstract: A ventilation system for a wide bodied aircraft with pressurisation cabin which includes: a compressor apparatus with a heat exchanger for drawing air in from an input reservoir and for generating an excess pressure in at least one output reservoir, several air outlets in the pressurisation cabin which are connected to the output reservoir of the compressor apparatus, and at least one suction air intake pipe in the pressurisation cabin wherein the volume flow through at least one of the air outlets is adjusted each time by a volume flow control member, as well as to a method for manufacturing a ventilation system of this type.

Abstract: A holding system for fixing a line assembly includes a fixing band, and a fixing band retaining element, which is arranged on the line assembly and comprises at least one guiding element for receiving the fixing band, the fixing band retaining element comprising two ends, one end being provided with at least one or more cavities or recesses, into which the other end can be plugged or hooked.