Patent ID: 11891953
Assignee: RTX CORPORATION
Field: Transport (Mechanical engineering)
Classification: CPC B  F | IPC B  F

Claim 12:
13. An aircraft system comprising:
a propulsor assembly disposed in an aircraft structure;
an inlet duct assembly configured to communicate airflow to the propulsor assembly, the inlet duct assembly comprising an inlet opening through a bottom outer surface of the aircraft structure;
a first heat exchanger assembly disposed in the inlet duct assembly and in thermal communication with an inlet airflow flowing through the inlet duct assembly; and
a skin heat exchanger assembly disposed along the bottom outer surface of the aircraft structure in thermal communication with the bottom outer surface of the aircraft structure and in fluid communication with the first heat exchanger assembly such that a working fluid is communicated therebetween, wherein the skin heat exchanger assembly is offset relative to the inlet duct assembly and the first heat exchanger assembly.