Nozzle structure of air jet loom
By using the rotating cap, sealing ring and auxiliary block design in the nozzle structure, the problems of inconvenient gas leakage and direction adjustment in the existing nozzle structure are solved, and the nozzle is easily installed and the effect of preventing skew is achieved.
Patent Information
- Application Number
- CN202421117345.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-22
- Publication Date
- 2025-02-14
- Estimated Expiration
- 2034-05-22
AI Technical Summary
The existing nozzle structure is threaded, resulting in gas leakage after long-term use and is inconvenient to adjust the direction.
The rotating cap and sealing ring design is adopted to reduce the rotation amplitude of the nozzle when installed by rotating cap, and avoid gas leakage through the sealing ring. At the same time, the nozzle is limited by the auxiliary block to prevent deflection.
It realizes convenient installation and direction adjustment of the nozzle, avoids gas leakage, and prevents deflection when the nozzle rotates.
Smart Images

Figure CN222476903U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the field of nozzle structures, and more specifically to a nozzle structure of an air jet loom. Background Art
[0002] When a jet loom is in use, a nozzle is generally used to spray air onto the fabric. Existing nozzles are generally connected together by threads. Long-term use of threaded connections may cause nozzle gas leakage and easily make it inconvenient to adjust the direction of the nozzle. For this reason, we propose a nozzle structure for a jet loom. Utility Model Content
[0003] 1. Technical issues to be solved
[0004] In view of the problems existing in the prior art, the purpose of the utility model is to provide a nozzle structure for a jet loom, which is convenient for installing the nozzle by rotating the cap and reducing the rotation amplitude of the nozzle during installation, and convenient for avoiding gas leakage through the sealing ring. At the same time, the nozzle is limited by the auxiliary block to prevent the nozzle from being deflected when rotating.
[0005] 2. Technical solution
[0006] To solve the above problems, the utility model adopts the following technical solutions.
[0007] A nozzle structure of an air jet loom, comprising a docking block, a side wall of the docking block being threadedly connected with symmetrically arranged bolts, a docking tube being installed on the side wall of the docking block, both ends of the docking tube being rotatably connected with a rotating cap, a side wall of the rotating cap being installed with a limiting ring, and two symmetrically arranged auxiliary blocks being installed on the lower end of the docking block;
[0008] It also includes a nozzle, two ends of which are equipped with two symmetrically arranged auxiliary shafts, the auxiliary shafts are rotatably connected to adjacent auxiliary blocks, the rotating cap is threadedly connected to the nozzle, and the side wall of the nozzle is equipped with symmetrically arranged retaining blocks, the retaining blocks are slidably connected to adjacent auxiliary blocks.
[0009] Furthermore, the butt joint includes two mounting blocks and a bellows, and mounting blocks are installed at both ends of the bellows to facilitate the rotation of the bellows to adapt to the nozzle.
[0010] Furthermore, a sealing ring is installed at the upper end of the nozzle, and docking grooves are opened at both ends of the mounting block. The sealing ring is engaged with the docking groove, and the gap when the nozzle is docked with the docking tube is reduced by the sealing ring to avoid gas leakage.
[0011] Furthermore, the mounting block is provided with a rotation groove, and the limiting ring is rotatably connected to the rotation groove to facilitate the rotation of the rotating cap.
[0012] Furthermore, the auxiliary block is provided with an auxiliary hole, the auxiliary shaft is rotatably connected to the auxiliary hole, the docking block is provided with a threaded hole, and the side wall of the bolt is provided with a thread matching the inner wall of the threaded hole, so as to facilitate the nozzle to rotate with the auxiliary shaft as the axis.
[0013] 3. Beneficial effects
[0014] Compared with the prior art, the advantages of the present invention are:
[0015] (1) The utility model facilitates the installation of the nozzle by rotating the cap and reduces the rotation range of the nozzle during installation, thereby facilitating the prevention of gas leakage through the sealing ring. At the same time, the nozzle is limited by the auxiliary block to prevent the nozzle from being deflected during rotation. BRIEF DESCRIPTION OF THE DRAWINGS
[0016] Figure 1 It is a structural sectional view of the utility model;
[0017] Figure 2 This is the structural front view of the utility model;
[0018] Figure 3 for Figure 1 A magnified schematic diagram of the middle part;
[0019] Figure 4 It is a structural side view of the utility model.
[0020] Description of the numbers in the figure:
[0021] 1. Docking block; 2. Bolt; 3. Docking tube; 4. Rotating cap; 5. Limiting ring; 6. Auxiliary block; 7. Nozzle; 8. Auxiliary shaft; 9. Retaining block; 10. Sealing ring. DETAILED DESCRIPTION
[0022] The following will combine the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all the embodiments. All other embodiments obtained by ordinary technicians in this field without creative work based on the embodiments in the utility model belong to the scope of protection of the utility model.
[0023] In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "top / bottom" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific position, be constructed and operated in a specific position, and therefore cannot be understood as limiting the present invention. In addition, the terms "first" and "second" are used for descriptive purposes only, and cannot be understood as indicating or implying relative importance.
[0024] In the description of the present utility model, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "provided with", "set / connected", "connected", etc. should be understood in a broad sense. For example, "connected" can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances.
[0025] Example 1: Please refer to Figure 1 , Figure 2 , Figure 3 and Figure 4 , a nozzle structure of an air jet loom, comprising a docking block 1, a side wall of the docking block 1 is threadedly connected with a symmetrically arranged bolt 2, a side wall of the docking block 1 is installed with a docking pipe 3, both ends of the docking pipe 3 are rotatably connected with a rotating cap 4, a side wall of the rotating cap 4 is installed with a limiting ring 5, and the lower end of the docking block 1 is installed with two symmetrically arranged auxiliary blocks 6;
[0026] It also includes a nozzle 7, two ends of the nozzle 7 are equipped with two symmetrically arranged auxiliary shafts 8, the auxiliary shafts 8 are rotatably connected to the adjacent auxiliary blocks 6, the rotating cap 4 is threadedly connected to the nozzle 7, and the side walls of the nozzle 7 are equipped with symmetrically arranged retaining blocks 9, and the retaining blocks 9 are slidably connected to the adjacent auxiliary blocks 6.
[0027] The butt joint pipe 3 includes two mounting blocks and a bellows. Mounting blocks are mounted on both ends of the bellows to facilitate the rotation of the bellows to adapt to the nozzle 7.
[0028] A sealing ring 10 is installed at the upper end of the nozzle 7, and docking grooves are provided at both ends of the mounting block. The sealing ring 10 is engaged with the docking grooves to reduce the gap when the nozzle 7 is docked with the docking tube 3 to avoid gas leakage.
[0029] The mounting block is provided with a rotation groove, and the limiting ring 5 is rotatably connected to the rotation groove to facilitate the rotation of the rotating cap 4.
[0030] The auxiliary block 6 is provided with an auxiliary hole, and the auxiliary shaft 8 is rotatably connected to the auxiliary hole. The side walls of the auxiliary shaft 8 and the inner walls of the auxiliary hole are frosted to increase the friction between the auxiliary hole and the auxiliary shaft 8 and prevent the auxiliary shaft 8 from being easily rotated by external force. The docking block 1 is provided with a threaded hole, and the side wall of the bolt 2 is provided with a thread that matches the inner wall of the threaded hole, so that the nozzle 7 can rotate with the auxiliary shaft 8 as the axis.
[0031] When in use, a technician in this field uses bolts 2 to install the docking block 1, then connects the gas pipe to the mounting block above the docking block 1, and uses the rotating cap 4 to connect it, and then spirally rotates the rotating cap 4 below the docking block 1, so as to facilitate the connection of the docking tube 3 to the nozzle 7, and makes the sealing ring 10 snap into the docking groove, so as to facilitate the subsequent rotation of the nozzle 7. The bellows adapts to the rotation amplitude of the nozzle 7. At this time, the retaining block 9 is against the inner wall of the auxiliary block 6, so as to facilitate the limiting of the nozzle 7. The utility model facilitates the installation of the nozzle 7 by the rotating cap 4, and reduces the rotation amplitude of the nozzle 7 during installation, and facilitates the avoidance of gas leakage through the sealing ring 10. At the same time, the nozzle 7 is limited by the auxiliary block 6 to prevent the nozzle 7 from deflecting when rotating.
[0032] The above is only a preferred specific implementation method of the utility model, but the protection scope of the utility model is not limited to it. Any technician familiar with the technical field within the technical scope disclosed by the utility model and any equivalent replacement or change based on the technical solution and improved concept of the utility model shall be included in the protection scope of the utility model.
Claims
1. A nozzle structure of an air jet loom, comprising a docking block (1), the side wall of the docking block (1) being threadedly connected with symmetrically arranged bolts (2), characterized in that: The side wall of the docking block (1) is provided with a docking tube (3), both ends of the docking tube (3) are rotatably connected with a rotating cap (4), the side wall of the rotating cap (4) is provided with a limit ring (5), and the lower end of the docking block (1) is provided with two symmetrically arranged auxiliary blocks (6); It also comprises a nozzle (7), two ends of the nozzle (7) are provided with two symmetrically arranged auxiliary shafts (8), the auxiliary shafts (8) are rotatably connected to adjacent auxiliary blocks (6), the rotating cap (4) is threadedly connected to the nozzle (7), and the side wall of the nozzle (7) is provided with symmetrically arranged retaining blocks (9), the retaining blocks (9) are slidably connected to adjacent auxiliary blocks (6).
2. The nozzle structure of an air jet loom according to claim 1, characterized in that: The butt-joint pipe (3) comprises two mounting blocks and a bellows, and mounting blocks are mounted on both ends of the bellows.
3. The nozzle structure of an air jet loom according to claim 2, characterized in that: A sealing ring (10) is installed at the upper end of the nozzle (7), and docking grooves are provided at both ends of the mounting block, and the sealing ring (10) is clamped in the docking grooves.
4. The nozzle structure of an air jet loom according to claim 2, characterized in that: The mounting block is provided with a rotation groove, and the limiting ring (5) is rotationally connected to the rotation groove.
5. The nozzle structure of an air jet loom according to claim 1, characterized in that: The auxiliary block (6) is provided with an auxiliary hole, the auxiliary shaft (8) is rotatably connected to the auxiliary hole, the docking block (1) is provided with a threaded hole, and the side wall of the bolt (2) is provided with a thread matching the inner wall of the threaded hole.