利索-全球专利检索

  1. 登录
  2. 注册
发明公开
CN107128796A 一种尾翼吊具 无效 - 驳回

一种尾翼吊具
摘要：
本发明公开了一种用于运载火箭尾翼安装的吊具。吊环与大卸扣、第一前吊带连接，所述吊环与大卸扣、第二后吊带连接；所述吊环与吊钩连接；所述前手拉葫芦与第一前吊带、前双耳吊环、第二前吊带连接，所述后手拉葫芦与第一后吊带、后双耳吊环、第二后吊带连接；所述第二前吊带穿过前双耳吊环固定孔，所述第二后吊带穿过后双耳吊环固定孔；所述前连接螺栓通过小卸扣与尾翼前吊点连接，所述后连接螺栓通过小卸扣与尾翼后吊点连接；所述前连接螺栓与尾翼前吊点之间安装垫片，所述后安装螺栓与尾翼后吊点之间安装垫片。
摘要（英）：

The invention discloses a lifting tool used for carrier rocket empennage mounting. A lifting ring is connected with a large shackle and a first front lifting belt. The lifting ring is connected with the large shackle and a second rear lifting belt. The lifting ring is connected with a lifting hook. A front chain block is connected with the first front lifting belt, a front double-lug lifting ring and a second front lifting belt, and a rear chain block is connected with a first rear lifting belt, a rear double-lug lifting ring and the second rear lifting belt. The second front lifting belt penetrates through a front double-lug lifting ring fixing hole, and the second rear lifting belt penetrates through a rear double-lug lifting ring fixing hole. A front connecting bolt is connected with the front lifting point of an empennage through a small shackle, and a rear connecting bolt is connected with a rear lifting point of the empennage through a small shackle. A gasket is mounted between the front connecting bolt and the front lifting point of the empennage, and a gasket is mounted between the rear connecting bolt and the rear lifting point of the empennage.

0/0