De-icing device for gas turbine engine

The attachment element has a nacelle (30) and an annular tube element (31) that are connected with each other by a fastening unit, such that relative movement between nacelle and annular tuber element is ensured. Two struts are arranged at specific angle with each other such that end regions of struts are respectively fastened at nacelle and annular tube element. The struts are bent in resilient manner and arranged in the form of flat metal strips. Specific end region of strut is connected to tube element by using a carrier element. An independent claim is included for a snow and ice removal device of gas turbine engine mounted in aircraft.