Three-period minimal surface phase change heat exchanger for on-board intermittent high heat flux density surface heat dissipation
By introducing a three-period minimal surface structure and a cooperative perturbation structure into the phase change heat exchanger, the heat exchange process of the three fluids is optimized, solving the thermal management problem of high heat flux density and pulsed operating frequency of airborne equipment, and achieving the effect of rapid heat storage and release.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- DALIAN UNIV OF TECH
- Filing Date
- 2025-06-12
- Publication Date
- 2026-06-02
AI Technical Summary
Existing three-fluid phase change heat exchangers lack synergistic optimization of the three-layer flow space in airborne equipment, resulting in insufficient heat storage and release rates, making it difficult to effectively meet the high heat flux density and pulsed operating frequency requirements of airborne equipment.
The phase change heat exchanger, which adopts a three-period minimal curved surface structure and a cooperative perturbation structure design, constructs a continuous and efficient heat conduction path by encapsulating phase change materials in the hot fluid channel and setting a perturbation skeleton in the cold fluid channel that is cooperatively matched with the hot side structure, thereby improving heat exchange efficiency.
It significantly improves the heat exchange area and efficiency between the heat fluid and the phase change material, enabling rapid heat absorption and release of the phase change material, and is suitable for efficient heat dissipation of intermittent high heat flux density surfaces on airborne surfaces.
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Figure CN120667962B_ABST