Abstract: Systems and methods to fuse aviation-related data systems for comprehensive aircraft system health monitoring are provided. One example method includes obtaining, by one or more computing devices, fault data indicative of a plurality of fault indications provided by a first plurality of components of an aircraft. The method includes obtaining, by the one or more computing devices, condition indicators describing the respective operational conditions of a second plurality of components of the aircraft. The method includes fusing, by the one or more computing devices, the fault data with the condition indicators to form a comprehensive data set. The method includes identifying, by the one or more computing devices, one or more causes of the plurality of fault conditions based at least in part on the comprehensive data set. One example system includes a data fuser, a cause identifier, and an alert generator.

Abstract: A pacifier thermometer having one or more electrical sensors within the pacifier nipple and digital measurement and display units external to the nipple is provided. An insulating nipple core can be utilized to improve the speed and accuracy of sensor response. Two or more sensors along with digital logic selection of the highest constant reading can be used to avoid false low readings. Additional conventional features can be provided as well.