Aerospace heat flow sensor and heat flow correction method based on double temperature difference compensation

• Main Authors: YAO JIE, ZHU YANDAN, GUO YIJUN, ZHANG HAOYUAN, QIU BO, SHI YOU'AN, JIANG BO, ZENG LEI
• Format: Patent
• Language: Chinese; English
• Published: 26.01.2024
• Subjects: MEASURING; MEASURING QUANTITY OF HEAT; MEASURING TEMPERATURE; PHYSICS; TESTING; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR

The invention discloses a spaceflight heat flow sensor and a heat flow correction method based on double temperature difference compensation. The spaceflight heat flow sensor comprises a first heat sink, a second heat sink and a metal plate. The first heat sink and the second heat sink are arranged...