A thrust reverser (130) of a nacelle (100) may include an translating sleeve (134) and an inner fixed structure (132) a pressure relief assembly (420). A pressure relief mechanism may include a pressure relief door (522) coupled via a hinge (524) and a latch (622) to the inner fixed structure (132). The pressure relief assembly (420) may limit deflections between the thrust reverser (134) and a pylon (140) in response to a burst duct. The pressure relief door (522) may release from the latch (622) automatically in response to an over pressurization event.
PRESSURE RELIEF ASSEMBLY
DRUCKENTLASTUNGSANORDNUNG
ENSEMBLE DE DÉCHARGE DE PRESSION
2022-08-03
Patent
Electronic Resource
English
Pressure relief assembly and a valve assembly that uses the pressure relief assembly
European Patent Office | 2025
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