| 摘要 |
<p>Connection of elements (1) which form part of aeronautical structures, with said elements (1) being made from composite material, with other thermoplastic or reinforced thermoplastic elements (2) also pertaining to aeronautical structures, with said element (1) comprising at least one part of its structure made from thermoplastic material, with said part of thermoplastic material being arranged on the structure of the most superficial element (1) of composite material, with respect to the thermoplastic or reinforced thermoplastic element (2) with which it is to be connected, in such a way that the connection between the elements (1,2) is made by means of ultrasound welding without fusion, applying pressure and heat through friction of the surfaces of the elements to be connected (1,2) obtaining in this way a permanent connection of elements (1,2) making its extraction possible at the same time.</p> |
