Method of repairing damage to a thermoplastic composite element
AssigneePolskie Zaklady Lotnicze Spolka Z Orgraniczona Odpowiedzialnoscia
InventorsAdam Dworak, Aleksander Banas, Janusz Madry, Jaroslaw Sienicki, Marcin Glodzik
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Abstract
The disclosed embodiments relate to a method for repairing a damage to a thermoplastic composite element, in particular an aircraft component, wherein a socket is milled at the site of damage to the thermoplastic composite element. Then, in the socket a patch is formed from a thermosetting material containing a reinforcing phase of fabric layers and a matrix of thermosetting resin, the patch having a shape and size corresponding to the socket geometry. In the next step, the patch is cured, and finally the cured patch is glued into the socket by means of an adhesive.
Claims9
A method of repairing damage to a thermoplastic composite element, comprising milling a socket at a site of damage to the thermoplastic composite element, then in said socket, forming a patch from a thermosetting material containing a reinforcing phase of fabric layers and a matrix of thermosetting resin, said patch having a shape and a size corresponding to a socket geometry, curing the patch and finally gluing the cured patch into the socket by means of an adhesive, wherein in the step of forming the patch in the socket, the following are placed sequentially:
- a separating layer in a form of a film or a separating agent;
- sections of fabric layers constituting the reinforcing phase of fabric layers of the thermosetting material, impregnated with a matrix of thermosetting resin, whereby a number of the sections of fabric layers, their total thickness as well as a shape and size of individual sections corresponds to the geometry of the socket;
- and
- then covering the prepared patch successively with:
- a perforated separating foil, an absorbing fabric, a separating foil, a heating blanket, a breathable fabric and a vacuum foil, and an entire repair package thus formed is sealed to a surface of the thermoplastic composite element being repaired by a sealing tape.
Dependencies are inferred from the claim text.