Fluid evacuating device for e.g. tapping line of aircraft's engine, has rupture zone located at or beyond aerodynamic surface and permitting disintegration of part of evacuating device in case of impact

摘要

The device (28) has a rupture zone (32) for permitting disintegration of a part of the device in case of impact. The rupture zone is located at or beyond an aerodynamic surface (S) and separates a separable part and a fixed part. The zone has a connection unit placed between the separable part and the fixed part. The unit has a connection finger connected with the fixed part and adapted to a housing for being received in the separable part.