System and method for inspecting an acoustic liner of an aircraft engine
AssigneePratt & Whitney Canada Corp.
InventorsJeremy GONZALEZ, Jong PARK
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AssigneePratt & Whitney Canada Corp.
InventorsJeremy GONZALEZ, Jong PARK
Estimating the term…
A method for inspecting an acoustic liner positioned in an inner cavity of a component of an aircraft engine includes: emitting, through a drain hole of the component and through a section of the acoustic liner to be inspected, a sound signal having an initial intensity; capturing, via a sound capture device positioned inside the inner cavity, a transmitted intensity of the sound signal following its transmission through the section of the acoustic liner to be inspected; and determining a loss in signal intensity through the section of the acoustic liner to be inspected by comparing the transmitted intensity to the initial intensity. Upon detecting that the loss in signal intensity is within a predetermined loss in signal intensity envelope for the acoustic liner, an indication that the acoustic liner is acceptable is emitted.
A method for inspecting an acoustic liner in an aircraft engine, the acoustic liner positioned in an inner cavity of a component of the aircraft engine, the method comprising:
A system for inspecting an acoustic liner in an aircraft engine, the acoustic liner positioned in an inner cavity of a component of the aircraft engine, the system comprising:
A system for inspecting an acoustic liner mounted in a component of an aircraft engine, the acoustic liner formed at least partially of a porous material, the system comprising:
Dependencies are inferred from the claim text.