Pressure bulkhead apparatus (102) is disclosed. An example bulkhead apparatus includes a frame (202, 308) and a plurality of beams (312) radially spaced relative to a longitudinal axis (306) of the frame. A beam (312, 404) from the plurality of beams has a first end (314) and a second end (316). A beam end assembly (324) couples the second end of the beam and a stringer (206, 302, 304, 410, 412) of a fuselage (104). The beam end assembly enables the second end of the beam to move relative to at least one of the frame or the stringer.
PRESSURE BULKHEAD APPARATUS
DRUCKSCHOTTVORRICHTUNG
APPAREIL DE CLOISON DE PRESSURISATION
2018-12-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |