一种航空轮胎胎面复合材料挤出装置

Abstract

本实用新型涉及轮胎加工的技术领域，特别是涉及一种航空轮胎胎面复合材料挤出装置，其能够对加入的大块物料进行粉碎，加快后续加热融化效率，使物料进行完全冷却，便于后续操作；包括熔融箱、挤出机本体、底板、支撑杆、粉碎部件、喷洒组件、冷却组件、输送导向部件和清理部件，熔融箱的输入端连接有粉碎部件，熔融箱的输出端与挤出机本体连接，熔融箱底部前后对称安装有支撑杆，支撑杆安装在底板顶端，冷却组件安装在底板顶部，冷却组件顶部右侧安装有喷洒组件，冷却组件内部安装有输送导向部件，冷却组件左侧输出端安装有清理部件。

Claims

1. An aircraft tire tread composite extrusion apparatus characterized by, The device includes a melting chamber (1), an extruder body (2), a base plate (9), support rods (10), a crushing component, a spraying component, a cooling component, a conveying and guiding component, and a cleaning component. The input end of the melting chamber (1) is connected to the crushing component, and the output end of the melting chamber (1) is connected to the extruder body (2). Support rods (10) are symmetrically installed at the bottom of the melting chamber (1). The support rods (10) are installed at the top of the base plate (9). The cooling component is installed at the top of the base plate (9). A spraying component is installed on the right side of the top of the cooling component. A conveying and guiding component is installed inside the cooling component. A cleaning component is installed at the output end on the left side of the cooling component.

2. An apparatus for extruding a tread compound for an aircraft tire as set forth in claim 1, wherein, The crushing component includes a feeding box (3), multiple vertical rods (4), a feed hopper (5), a drive motor (6), a drive shaft (7), and multiple sets of crushing blades (8). The output end of the feeding box (3) is connected to the input end of the melting box (1). The bottom of the feeding box (3) is connected to the top of the melting box (1) through multiple vertical rods (4). The feed hopper (5) is installed on the left side of the top of the feeding box (3). The drive motor (6) is installed on the top of the feeding box (3). The output end of the drive motor (6) passes through the top of the feeding box (3) and is installed on the drive shaft (7). Multiple sets of crushing blades (8) are installed on the drive shaft (7).

3. An apparatus for extruding a tread compound for an aircraft tire as set forth in claim 1, wherein, The cooling assembly includes a water tank (11), a support arm (12), a first guide roller (18), and a second guide roller (19). The water tank (11) is installed on the top of the base plate (9). The first guide roller (18) is rotatably installed on the right side inside the water tank (11). The second guide roller (19) is rotatably installed on the lower side inside the water tank (11). An outlet is opened on the upper part of the left side wall of the water tank (11). The top right side of the water tank (11) is connected to the extruder body (2) through the support arm (12).

4. An apparatus for extruding a tread compound for an aircraft tire as set forth in claim 3, wherein, The spraying assembly includes a cooling shroud (13), an upper spray pipe (14), a lower spray pipe (15), a water pump (16), and a water pipe (17). The cooling shroud (13) is installed on the upper right side of the water tank (11). The upper spray pipe (14) is installed on the upper part of the cooling shroud (13), and the lower spray pipe (15) is installed on the lower part of the cooling shroud (13). Multiple spray heads are installed on the upper spray pipe (14) and the lower spray pipe (15). The water pump (16) is installed on the right side wall of the water tank (11) and communicates with its interior. The output end of the water pump (16) is connected to the water pipe (17), and the output end of the water pipe (17) is connected to the input end of the upper spray pipe (14) and the lower spray pipe (15).

5. An apparatus for extruding a tread compound for an aircraft tire as set forth in claim 3, wherein, The conveying guide component includes two extension blocks (20), two slide rods (21), two sliders (22), two springs (23), a conveying roller (24), and two outlet rollers (25). The two extension blocks (20) are installed at the front and rear ends on the left side inside the water tank (11). A sliding groove is provided on the extension block (20). The slide rods (21) are installed in the sliding grooves. The sliders (22) are slidably installed on the outer wall of the slide rods (21). The springs (23) are fitted on the upper outer wall of the slide rods (21). The conveying rollers (24) are rotatably installed between the two sliders (22). The two outlet rollers (25) are rotatably installed at the outlet of the water tank (11).

6. An apparatus for extruding a tread compound for an aircraft tire as set forth in claim 3, wherein, The cleaning components include a cleaning groove (26), two sets of guide rods (27), two sets of push plates (28), two sets of clamping springs (29), and two scrapers (30). The cleaning groove (26) is installed on the upper left side wall of the water tank (11). The cleaning groove (26) has symmetrical sliding grooves at both ends. The guide rods (27) are installed in the sliding grooves. The push plates (28) are slidably installed on the outer walls of the two guide rods (27) at both ends. The scrapers (30) are symmetrically installed on the opposite side of the two push plates (28).

7. An apparatus for extruding a tread compound for an aircraft tire as set forth in claim 3, wherein, It also includes a liquid level sensor (31), which is installed inside the water tank (11).

Images