Captive balloon anchoring facility

• Main Authors: GONG WENTAO, HE ZEQING, ZHANG DONGHUI, ZHANG TAIHUA, LI YINGSI
• Format: Patent
• Language: Chinese; English
• Published: 02.07.2021
• Subjects: AIRCRAFT; AVIATION; COSMONAUTICS; LIGHTER-THAN AIR AIRCRAFT; PERFORMING OPERATIONS; TRANSPORTING

The embodiment of the invention provides a captive balloon anchoring facility. The captive balloon anchoring facility comprises a bearing main body, a revolving platform and a braking device. The revolving platform is configured to rotate relative to the bearing main body. The braking device is configured to brake the rotary platform to limit rotation of the revolving platform relative to the bearing main body. Due to the fact that the braking device brakes the revolving platform, rotation of the revolving platform relative to the bearing main body is limited, the rotating speed and the rotating and swinging intensity of the revolving platform can be reduced to a certain degree, and the risk brought by captive balloon anchoring facilities to operators is reduced. 本申请实施例提供一种系留气球锚泊设施，包括承载主体、回转平台以及制动装置。回转平台配置为能够相对于承载主体转动。制动装置配置为能够对回转平台制动以限制回转平台相对于承载主体转动。由于制动装置对回转平台制动，限制了回转平台相对于承载主体的转动，能够在一定程度上减缓回转平台的转动速度以及旋转摆动的剧烈程度，降低了系留气球锚泊设施给操作人员带来的风险。