Method of reducing the gap between a liner and a turbine distributor of a turbojet engine

摘要: A method of reducing the gap between a liner and turbine distributor turbojet engine. The allows for improvement seal on inside high pressure at lower platform. includes steps of: applying protective deposit to part external surface liner, before carrying out filling by diffusion brazing distributor. deposit, preferably anti-adherent ceramic, makes it possible braze avoid fixing onto platform level. also has applications engines.