Patent ID: 7278208

Claim:
A method of replacing an abradable portion on the casing of a turbojet fan, the turbojet including a rotary portion, the rotary portion comprising a shaft including a fan stage attached to its front end, the fan stage comprising a hub supporting a plurality of blades, the turbojet also comprising an annular fan casing surrounding the fan stage, said fan casing comprising an inside wall against which a likewise annular abradable portion is bonded, the surface of the abradable portion opposite from its bonding surface being referred to as its sealing surface, the fan casing including a plurality of fixing points, the fan stage having previously been removed, the method comprising: a) removing a worn abradable portion; b) preparing a new abradable portion; c) applying adhesive to the bonding surfaces of the new abradable portion and of the fan casing, said bonding surfaces having previously been cleaned; d) applying the abradable portion against the inside wall of the new fan casing; e) putting an inside heating belt into place against the sealing surface of the new abradable portion, the inside heating belt completely covering the new abradable portion; f) putting holding sectors into place against the inside heating belt, each holding sector including an inflatable bladder, the new abradable portion and the inside heating belt being sandwiched in full between the fan casing and the bladders, the holding sectors themselves being held in place by a plurality of straps attached to the fan casing by the fixing points; g) connecting the bladders to a common source of air under pressure and connecting the inside heating belt to a regulated electrical power supply, pressurizing the bladders, and heating the adhesive in application of a cycle of temperature and pressure conditions that is adapted to the adhesive used and to the thermal conductivity of the fan casing; and h) cooling and removing the holding sectors and the inside heating belt.