Startup Characteristics and Thermal Instability of a Visual Loop Heat Pipe under Acceleration Force

Loop heat pipes are efficiently two-phase heat transfer devices in the field of aircraft thermal management. To investigate the startup behavior and thermal instability of loop heat pipes under acceleration force, this study designed a novel loop heat pipe featuring two visual compensation chambers and a visual condenser. Elevated acceleration experiments were conducted across for different heat loads, acceleration magnitudes, and directions. The heat load ranged from 30 W to 150 W, while the acceleration magnitude varies from 1g to 15g, with four acceleration directions (A, B, C, and D). The startup behavior, thermal instability, internal flow pattern, and phase distribution were analyzed systematically. The experimental results reveal that (ⅰ) the startup behaviors vary across the four acceleration directions.‌ In direction A, startup is more difficult due to additional resistance induced by acceleration force. In direction C, startup time generally decreases with increasing heat load and acceleration up to 7g. The longest startup time observed is 372 s at 30 W and 11g. (ⅱ) at high heat load, periodic temperature fluctuations are observed, particularly in directions B and C. Simultaneously, the vapor-liquid phase interface in the condenser exhibits periodic back-and-forth movement. (ⅲ) the visual DCCLHP exhibits a loss of temperature control under the combined influence of high heat loads and acceleration force, often accompanied by working fluid reverse flow, periodic temperature fluctuations, or wick dry-out.