The invention is related to an aircraft door, and, more particularly, to a mounting system for a pressure seal of an aircraft door. Mounting system 107 may include outer skin 101, pressure seal 103, clamping component 104, pressure seal fastener 105 having a head and a threaded shank, nut 106, mounting support 102 having clearance hole 160 that is adapted to prevent a rotational and axial movement of pressure seal fastener 105, and mounting support fasteners 120. Mounting support fasteners 120 removably attach mounting support 102 to outer skin 101. The head of the pressure seal fastener 105 is connected to the mounting support 102 such that a rotational and axial movement of the pressure seal fastener 105 is prevented. Nut 106 is removably attached to the threaded shank of pressure seal fastener 105, thereby removably clamping pressure seal 103 between clamping component 104 and mounting support 102.
A MOUNTING SYSTEM FOR A PRESSURE SEAL OF AN AIRCRAFT DOOR
MONTAGESYSTEM FÜR EINE DRUCKDICHTUNG EINER FLUGZEUGTÜR
SYSTÈME DE MONTAGE POUR UN JOINT DE PRESSION D'UNE PORTE D'AÉRONEF
2021-08-11
Patent
Electronic Resource
English
European Patent Office | 2024
|European Patent Office | 2024
|European Patent Office | 2024
|