US Patent:
20110043382, Feb 24, 2011
Inventors:
Zhennong Wang - Renton WA, US
International Classification:
G08B 21/00
Abstract:
Systems and methods for aircraft cabin noise analysis are disclosed. In one embodiment, a method includes receiving a first request for an aircraft cabin noise analysis, wherein the request comprises a plurality of flight parameters associated with a first flight mission, retrieving, from a computer readable memory, a plurality of noise parameters associated with the plurality of flight parameters for the first flight mission, determining a total noise exposure parameter associated with the first flight mission, generating an output comprising the total noise exposure on a user interface, and generating a warning on a user interface when the total noise exposure exceeds a threshold. In some embodiments, the monitored system may be implemented in a computing system or as logic instructions recorded on a computer readable medium.