A ratchet wrench for dismounting the bolts of a helicopter collector ring
Patent Information
- Application Number
- CN202522121225.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-10-06
- Publication Date
- 2026-08-28
- Estimated Expiration
- 2035-10-06
AI Technical Summary
[0002]直升机主桨的集流环顶部通常与位于客舱顶部的加温线缆保护罩通过螺栓固定,螺栓上有U形卡槽,在使用通用拆卸工具安装或拆卸直升机主桨集流环上的固定螺栓时容易打滑,不便于拆卸和安装,因此,本实用新型提供一种能够快速拆卸集流环螺栓的棘轮扳手
[0010]本实用新型针对直升机主桨集流环固定螺栓上有U形卡槽,通用拆卸工具安装或拆卸时易打滑、不便于操作的问题,该棘轮扳手通过可拆卸连接的拆卸头,利用其卡接端设置的U形卡块,可精准卡接螺栓,有效避免打滑,实现快速、便捷地拆卸和安装集流环螺栓。同时,连接头与拆卸头通过方形槽和弹性卡接结构含弹性件、定位珠及定位卡槽实现可靠连接与定位,方便拆卸头的更换以适应不同需求。
Smart Images

Figure CN224688884U_ABST
Abstract
Claims
1. A ratchet wrench suitable for removing helicopter manifold bolts, characterized in that, The device includes a ratchet handle (1), a connector (2), and a disassembly head (3). The ratchet handle (1) is provided with a connector (2). The disassembly head (3) has a square groove (4) at its connecting end. The connecting end of the disassembly head (3) is detachably connected to the ratchet handle (1) through the square groove (4). The disassembly head (3) has a snap-fit groove (5) at its snap-fit end. A U-shaped snap-fit block (6) for snapping bolts is provided inside the snap-fit groove (5).
2. A ratchet wrench for removing helicopter manifold bolts according to claim 1, characterized in that, The four inner walls of the square groove (4) are provided with positioning slots (7) along the axial direction. The positioning slots (7) are arc-shaped grooves.
3. A ratchet wrench for removing helicopter manifold bolts according to claim 2, characterized in that, The connector (2) is provided with an elastic snap-fit structure that can correspond to any positioning slot (7). The elastic snap-fit structure includes an installation slot, an elastic element (8) and a positioning bead (9). The installation slot is horizontally opened on the outside of the connector (2). The elastic element (8) and the positioning bead (9) are both installed on the inside of the installation slot. The elastic element (8) can be fitted into the positioning slot (7). The two ends of the elastic element (8) are fixedly connected to the installation slot and the positioning bead (9) respectively. The elastic element (8) is used to connect the connector (2) and the disassembly head (3) by pressing the positioning bead (9) into the positioning slot (7).
4. A ratchet wrench for removing helicopter manifold bolts according to claim 1, characterized in that, The disassembly head (3) is made of quenched 42CrMo stainless steel.