Abstract: Example systems and methods for integrating an air-cooled oil cooler into an inlet frame of an engine are provided. An example gas turbine engine comprises an inlet frame including an inlet plenum at a first end of an inlet frame flow path, the inlet frame defining an airflow entrance to a compressor; the compressor to provide an airflow through the inlet frame; a pump to circulate a fluid; a plurality of struts supporting the inlet frame flow path; and a fluid core connected to the pump and built at least partially into the inlet frame of the gas turbine engine, the fluid core to route the fluid through the inlet plenum.

Abstract: Power consumption that occurs in response to software errors may be reduced. In one example a system tracks a number of occurrences a first set of code causes a system to perform one or more reset actions, determines whether the number of occurrences exceeds a threshold, and selects a second set of code to execute in place of the first set of code, if the quantity exceeds the threshold.

Abstract: Power consumption that occurs in response to software errors may be reduced. In one example a system tracks a number of occurrences a first set of code causes a system to perform one or more reset actions, determines whether the number of occurrences exceeds a threshold, and selects a second set of code to execute in place of the first set of code, if the quantity exceeds the threshold.