Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Airplane covering cap limiting lock structure and using method
The aircraft covering cap limiting lock structure comprises an upper lock body, a lower lock body and a lock pin, a fixed upper lock body lug piece is arranged on the upper lock body, concentric lock cylinder through holes with the same diameter are formed in the upper lock body lug piece and the upper lock body, and a groove-shaped structure gap allowing the lower lock body lug piece to slide in and out smoothly is formed between the upper lock body lug piece and the upper lock body. A gap of the groove-shaped structure is vertical and passes through the lock cylinder through hole; lock cylinder through holes which are concentric and equal in diameter are also formed in the lower lock body lug piece and the lower lock body, a same groove-shaped structure gap allowing the upper lock body lug piece to smoothly slide in and out is formed between the lower lock body lug piece and the lower lock body, and after the upper lock body and the lower lock body are combined, the lock cylinder through holes of the upper lock body and the lower lock body are coaxial. The upper lock body lug is embedded into a gap of the groove-shaped structure of the lower lock body, the lower lock body lug is embedded into a gap of the groove-shaped structure of the upper lock body, and the lock pin is embedded into a lock cylinder through hole of the upper lock body and a lock cylinder through hole of the lower lock body.
一种飞机口盖限位锁结构及使用方法，含有上锁体、下锁体和锁销，上锁体上设有固定的上锁体耳片，上锁体耳片和上锁体上布置同心且直径相等的锁芯通过孔，上锁体耳片和上锁体之间设置可供下锁体耳片顺畅滑入滑出的槽状结构间隙，该槽状结构间隙垂直并通过锁芯通过孔；下锁体耳片和下锁体上同样布置同心且直径相等的锁芯通过孔，下锁体耳片和下锁体之间设置可供上锁体耳片顺畅滑入滑出的同样的槽状结构间隙，上锁体和下锁体结合后，上锁体和下锁体的锁芯通过孔同轴，上锁体耳片嵌入下锁体的槽状结构间隙中，下锁体耳片嵌入上锁体的槽状结构间隙中，锁销镶嵌在上锁体和下锁体的锁芯通过孔中。
Airplane covering cap limiting lock structure and using method
The aircraft covering cap limiting lock structure comprises an upper lock body, a lower lock body and a lock pin, a fixed upper lock body lug piece is arranged on the upper lock body, concentric lock cylinder through holes with the same diameter are formed in the upper lock body lug piece and the upper lock body, and a groove-shaped structure gap allowing the lower lock body lug piece to slide in and out smoothly is formed between the upper lock body lug piece and the upper lock body. A gap of the groove-shaped structure is vertical and passes through the lock cylinder through hole; lock cylinder through holes which are concentric and equal in diameter are also formed in the lower lock body lug piece and the lower lock body, a same groove-shaped structure gap allowing the upper lock body lug piece to smoothly slide in and out is formed between the lower lock body lug piece and the lower lock body, and after the upper lock body and the lower lock body are combined, the lock cylinder through holes of the upper lock body and the lower lock body are coaxial. The upper lock body lug is embedded into a gap of the groove-shaped structure of the lower lock body, the lower lock body lug is embedded into a gap of the groove-shaped structure of the upper lock body, and the lock pin is embedded into a lock cylinder through hole of the upper lock body and a lock cylinder through hole of the lower lock body.
一种飞机口盖限位锁结构及使用方法，含有上锁体、下锁体和锁销，上锁体上设有固定的上锁体耳片，上锁体耳片和上锁体上布置同心且直径相等的锁芯通过孔，上锁体耳片和上锁体之间设置可供下锁体耳片顺畅滑入滑出的槽状结构间隙，该槽状结构间隙垂直并通过锁芯通过孔；下锁体耳片和下锁体上同样布置同心且直径相等的锁芯通过孔，下锁体耳片和下锁体之间设置可供上锁体耳片顺畅滑入滑出的同样的槽状结构间隙，上锁体和下锁体结合后，上锁体和下锁体的锁芯通过孔同轴，上锁体耳片嵌入下锁体的槽状结构间隙中，下锁体耳片嵌入上锁体的槽状结构间隙中，锁销镶嵌在上锁体和下锁体的锁芯通过孔中。
Airplane covering cap limiting lock structure and using method
一种飞机口盖限位锁结构及使用方法
LI YAO (Autor:in) / ZHAO SHUJUN (Autor:in) / MENG LIPING (Autor:in) / LI XINGFU (Autor:in) / LI YUNFEI (Autor:in)
09.08.2024
Patent
Elektronische Ressource
Chinesisch
Covering cap lock and covering cap structure comprising same
| Europäisches Patentamt | 2020