Patent ID: 9085368
Filing Date: 2015-07-21
Classification: B64D

Abstract:
1. A system for air conditioning an aircraft cabin in an aircraft, the system comprising: a central mixer and first and second local mixers, the first and second local mixers being formed separate from each other and being positioned at different locations in the aircraft, an air conditioning unit connected to the central mixer in order to supply the central mixer with air at a desired low temperature, a first recirculation system which is designed to remove recirculation air from a first aircraft cabin region and which is connected to the central mixer in order to lead the recirculation air from the first aircraft cabin region into the central mixer, and a second recirculation system which is designed to remove recirculation air from a second aircraft cabin region and which is connected to the first local mixer and the second local mixer in order to lead the recirculation air from the second aircraft cabin region into the first local mixer and the second local mixer, the first and second local mixers each being connected to the central mixer in order to supply mixed air from the central mixer into the first and second local mixers, the second recirculation system further comprising: