A structural panel for an aircraft nacelle may comprise a first skin, a second skin, and a core sandwiched between them. A disbond may be present between the first skin and the core. A plurality of layers of blueprint film adhesive may be positioned over the disbond. The structural panel may be vacuum bagged, and the blueprint film adhesive may be heated. The blueprint film adhesive may flow through perforations in the first skin and bond the first skin to the core.
SANDWICH PANEL DISBOND REPAIR
2018-01-18
Patent
Electronic Resource
English
IPC: | B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
British Library Online Contents | 1992
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