A blanket (110) for insulating an aircraft structure (190) comprises an insulating portion (112), comprising a first edge (111) and a second edge (113), perpendicular to the first edge (111). The blanket (110) also comprises a tab portion (114), extending from the insulating portion (112), and a formable coupler (116), attached to the insulating portion (112). The tab portion (114) is thinner than the insulating portion (112). The insulating portion (112) fully overlaps the formable coupler (116). The formable coupler (116) is parallel to the second edge (113) of the insulating portion (112) and is perpendicular to the first edge (111) of the insulating portion (112).
BLANKETS FOR INSULATING AIRCRAFT STRUCTURES AND INSULATED AIRCRAFT ASSEMBLIES
2022-01-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Blankets for insulating aircraft structures and insulated aircraft assemblies
European Patent Office | 2024
|Flammability Test Method for Aircraft Comfort Blankets
SAE Technical Papers | 2022
Flammability Test Method for Aircraft Comfort Blankets
SAE Technical Papers | 2016
Bonded Lockstitch for Insulating Blankets
NTRS | 1984
|Aircraft bay blankets that provide enhanced drainage features
European Patent Office | 2020
|