The development of TiAl intermetallics is mainly motivated by the potential of weight savings due to their low density. The latter ranges between 3.6 g cm -3 for c-TiAl [1] and 4.3 g cm -3 for a 2 -Ti 3 Al [1,2] whereas those of nickel-based super alloys or steels, used in structural applications, are close to 8 g cm -3 (e.g. 8.3 g cm -3 for single crystal Ni-base alloy [3] ). These materials possess good mechanical properties comparable to nickel base super alloys, even at high temperature. This fact proposes them as serious candidates for the use in high temperature applications such as air-foils in turbine engines for aeronautic applications, or rotors for turbochargers as well as exhaust valves for the automotive industry. However, it is known that the degradation of the mechanical properties of TiAl base alloys due to environmental embrittlement resulting from high temperature oxidation is still a critical issue for industry if titanium aluminide alloys are chosen as a substitute for Ni-based superalloys. Especially, this point is true for the aeronautical industry where materials have to face severe thermal cyclic as well as environmental service conditions. Indeed high temperature oxidation of TiAl base alloys leads to the formation of a (Al 2 O 3 / TiO 2 /TiN) mixed oxide scale which is non protective for long term service. [4] In order to improve the oxidation resistance of titanium aluminides, several studies on surface treatments have been performed (alloying with a third element, overlay coatings, pre-oxidation, anodisation, metallic ion implantation of third elements) and were reviewed by Yang et al. [2] Such surface modifications improve the oxidation resistance but the benefit remains limited with time and is not always obvious for thermocyclic conditions. Moreover, thick coatings may modify the mechanical properties of the alloy by the formation of brittle phases at the alloy surface. It should be emphasized that with all the previous treatments, no long term (over thousands of hours) effect was observed.An interesting alternative consists in the surface treatment by halogens. [5,6] Two models have been proposed to explain the beneficial effect of halogens applied to TiAl alloys although halogens are usually known to be strong corrosive agents for metals especially in the temperature range of interest: [7] Lattice Doping Model Taniguchi [8] proposed the "lattice doping model" in which it is postulated that two chlorine anions could annihilate an oxygen vacancy in the oxide scale. However results from direct implantation of chlorine into the oxide scale by Schumacher et al. [9] did not sustain this hypothesis.
Gas Phase Transport ModelAs an alternative to the lattice doping model a new model called "gas phase transport model" was proposed and progressively ascertained. [6,[10][11][12] This model assumes that the presence of a well defined amount of halogen in the metal subsurface zone leads to the preferential formation of aluminium halides which diffuse in outward direction into voids or cavities ...