THERMAL MANAGEMENT SYSTEM (TMS), AIRCRAFT AND SYSTEM

摘要

THERMAL MANAGEMENT SYSTEM (TMS), AIRCRAFT AND SYSTEM. A thermal management system (TMS) (200) includes a motor thermal chamber (304) configured to transmit heat from a propulsive thermal motor (20) to a pumped heat transfer fluid, a motor exhaust thermal chamber (206). ) coupled in flow communication with the engine thermal chamber, the engine exhaust thermal chamber configured to transmit heat from a propulsive thermal motor exhaust to the pumped heat transfer fluid, a bypass valve (208) coupled in parallel with the engine exhaust thermal chamber, the selectable bypass valve to modulate a flow of the heat transfer fluid pumped through the thermal engine exhaust thermal chamber, and a plurality of additional thermal chambers, for each of a plurality of loads of a vehicle coupled in flow communication with at least one of the engine thermal chambers and exhaust thermal chambers each of the plurality of additional flow controllable thermal chambers using a shaping valve.