Air-conditioning system for aircraft
An air conditioning system, air system technology, applied in the direction of air handling equipment, aircraft parts, energy-saving panel measures, etc., can solve the problem of inability to provide air conditioning in the cabin, and achieve the effect of reducing structural costs
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[0029] figure 1 A schematic circuit diagram of the first preferred embodiment of the air conditioning system 10 is shown. The air conditioning system 10 is designed to be mirror-symmetrical along line A in the wiring diagram, that is, all basic components exist in a double-redundant manner. In the following, only the part of the air conditioning system 10 located on the left side of each figure is described, and the redundant right side part of the same design is only involved in the figure without a more detailed description.
[0030] Via a compression stage, as schematically illustrated by the bleed air source 12, high-pressure hot bleed air is extracted from a turbine unit (not shown). The extracted bleed air is supplied to the ozone converter 24 via the main bleed air line 20 and the branch bleed air line 22, from where the bleed air passes through another bleed air line section 26 to the main regulating valve 16 (FCV) and via the T line section 28 (T pipe) and another blee...
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