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AssigneeSafran Nacelles
InventorsYanhaël Labat, Laurent Ruban, Philippe Leroux, Arnaud Cammage, Tony Miossec, Charles-Antoine Lampaert, Jean-Philippe Joret, Alexis Yves-Marie Loncle, Mathieu David
Estimating the term…
This device for attaching a heat shield to an aircraft panel comprises a first attachment element associated with the heat shield, a second attachment element associated with the aircraft panel, and a metal wire forming a loop. At least one of said attachment elements is provided with means for retaining said loop, said loop being closed by a braking member at the ends of said loop, intended for bringing said attachment elements together; the loop abutting respectively in the middle portion one of the attachment elements and at the braking member on the other attachment element. The loop is set apart from the heat shield and from the aircraft panel, and passes outside the heat shield and the aircraft panel.
Device for attaching a heat shield to an aircraft panel, comprising a first attachment element associated with the heat shield, a second attachment element associated with the aircraft panel and a wire forming a loop, wherein at least one of said first and second attachment elements is provided with retention means for retaining said loop, said loop being closed by a braking member of the ends of said loop for bringing said attachment elements together, said loop abutting respectively in a middle portion thereof on one of said attachment elements and at the level of the braking member on the other of said attachment elements, said loop being set apart from said heat shield and said aircraft panel, said loop passing outside said heat shield and said aircraft panel, said attachment elements extending from said aircraft panel and said heat shield in a direction opposite to a contact area between said aircraft panel and said heat shield.
Dependencies are inferred from the claim text.