Patent ID: 6024639
Filing Date: 2000-02-15
Classification: B64D,Y02T

Abstract:
An injector air outlet adapted to be connected to an air supply duct in an aircraft having an aircraft interior space therein, said injector air outlet comprisinga housing wall with an injector mixing chamber therein,a primary air supply channel having a primary air inlet adapted to be connected to the air supply duct of the aircraft and a primary air outlet that opens into said mixing chamber,a secondary air channel having a secondary air inlet adapted to open into the interior space of the aircraft and a secondary air outlet that opens into said mixing chamber,said primary air outlet and said secondary air outlet forming an injector nozzle,a mixed air outlet that is connected to said mixed air chamber and passes out through said housing wall and that is adapted to open into the interior space of the aircraft, anda sensor unit including at least one of a temperature sensor and a smoke sensor arranged within said secondary air channel.