Magnetic levitation separation supporting device for satellite load cabin
Magnetic levitation separation supporting device for satellite load cabin
- Neue Suche nach: QIN YUNFEI
- Neue Suche nach: WANG HUA
- Neue Suche nach: LIU XIAOFEI
- Neue Suche nach: WU CHEN
- Neue Suche nach: XU YIXING
- Neue Suche nach: QIN YUNFEI
- Neue Suche nach: WANG HUA
- Neue Suche nach: LIU XIAOFEI
- Neue Suche nach: WU CHEN
- Neue Suche nach: XU YIXING
The invention provides a magnetic levitation separation supporting device for a satellite load cabin. The magnetic levitation separation supporting device comprises a main supporting frame, an upper supporting leg, a lower supporting leg, a left supporting leg and a right supporting leg, wherein the upper supporting leg, the lower supporting leg, the left supporting leg and the right supporting leg are perpendicularly arranged at the upper end, the lower end, the left end and the right end of the main supporting frame respectively. A first air floating cushion mounting column and a second air floating cushion mounting column are arranged on the lower supporting leg, the outline of the main supporting frame is of an octagonal structure, and third air floating cushion mounting columns which are arranged in the same direction as the first air floating cushion mounting column and the second air floating cushion mounting column are arranged on the end side of the lower end of the main supporting frame. The device can simulate a load cabin body when a satellite is subjected to a magnetic levitation test, is used for supporting the load cabin after being connected with the air floatation cushion, can perform gravity unloading support when the satellite load cabin is subjected to magnetic levitation separation, is stable and reliable in unloading process, improves the magnetic levitation separation efficiency of the satellite load cabin, improves the support rigidity of the satellite load cabin, and reduces the cost. The device has the advantages of simple structure, small deformation, safety, reliability and the like.
本发明提供了一种用于卫星载荷舱磁浮分离支撑装置，包括主支撑架以及分别垂直布置在所述主支撑架上端、下端、左端、右端的上支撑腿、下支撑腿、左支撑腿、右支撑腿；所述下支撑腿上设置有第一气浮垫安装柱、第二气浮垫安装柱，所述主支撑架的轮廓呈八边形结构且在下端的端侧设置有分别与第一气浮垫安装柱、第二气浮垫安装柱同向布置的第三气浮垫安装柱。本发明可在卫星进行磁浮试验时模拟载荷舱体，与气浮垫连接后用于支撑载荷舱，可在卫星载荷舱磁浮分离时进行重力卸载支撑，卸载过程稳定可靠，提高了卫星载荷舱磁浮分离的效率，提高了卫星载荷舱的支撑刚度，具有结构简单、变形量小、安全可靠等优点。
Dokumentinformationen
Magnetic levitation separation supporting device for satellite load cabin
用于卫星载荷舱磁浮分离支撑装置
2023-05-16
Patent
Elektronische Ressource
Chinesisch
| IPC: | B64G Raumfahrt , COSMONAUTICS |
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