Auxiliary device for reaming butt joint of central wing of horizontal tail of helicopter
By designing auxiliary devices of the positioning frame and the supporting frame, the problem that the existing device cannot be fixed and flipped is solved, multi-angle reaming operation is realized, and the reaming efficiency and accuracy are improved.
Patent Information
- Application Number
- CN202422257938.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-09-14
- Publication Date
- 2025-09-12
- Estimated Expiration
- 2034-09-14
AI Technical Summary
The existing helicopter horizontal tail center wing butt joint reaming auxiliary device lacks fixing and flipping functions, resulting in inconvenience in reaming bolt holes at different positions.
An auxiliary device including a positioning frame and a supporting frame is designed. The positioning frame fixes the central wing through a flipping mechanism and an adjustable supporting structure, and provides a suitable reaming operation angle through multi-angle flipping.
The efficiency and accuracy of reaming operations are improved, and reaming operations of bolt holes in different positions are simplified.
Smart Images

Figure CN223325574U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the field of helicopter process equipment design, and in particular relates to an auxiliary device for reaming holes in a butt joint of a helicopter horizontal tail central wing. Background Art
[0002] The center wing of a helicopter's horizontal tail structure features a butt joint. Multiple bolt holes secure the joint to the center wing. These precision-designed bolt holes require reaming. The existing center wing butt joint reaming auxiliary bracket only provides simple support for the center wing, lacking either a fixed or tilting function. This makes it difficult to easily ream bolt holes in different locations. Utility Model Content
[0003] Purpose of the utility model: To propose an auxiliary device for reaming holes in the center wing butt joint of a helicopter horizontal tail, which is used to replace the original auxiliary bracket for reaming holes in the center wing butt joint, provide a suitable operating angle for reaming holes in bolt holes at different positions, and improve the efficiency of reaming operations.
[0004] Technical Solution
[0005] Provided is an auxiliary device for reaming a hole in a helicopter horizontal tail center wing butt joint, comprising: a positioning frame and a support frame;
[0006] The positioning frame is provided with a flip mechanism at both ends and is installed on the support frame through the flip mechanism; the positioning frame is used to position, support and fix the central wing of the horizontal tail.
[0007] The positioning frame includes a C-shaped frame, a single fork ear connection structure, and an adjustable support structure;
[0008] Both end surfaces of the C-shaped frame are inwardly installed with single-fork ear connection structures, which are used to connect with a set of double-fork ear structures of the central wing, thereby positioning and fixing the central wing;
[0009] Multiple sets of adjustable support structures are set on the C-shaped frame. When multiple sets are used simultaneously, they can also clamp the central wing, thereby further strengthening the fixation of the central wing.
[0010] A set of adjustable support structures includes an upper adjustable support structure and a lower adjustable support structure, both of which have the same structure; the adjustable support structure includes a fixed support, a rocker arm, a clamping screw, and a movable clamping block;
[0011] The rocker arm is installed on the C-shaped frame through a fixed support. One end of the rocker arm cooperates with the clamping screw, and the bottom end of the clamping screw is connected to the movable clamping block. The movable clamping block can rotate around the bottom end of the clamping screw and tilt at a small angle.
[0012] The auxiliary device also includes: a lateral support structure;
[0013] The lateral support structure includes a sleeve bracket, a compression screw, and a movable pressure plate;
[0014] The sleeve bracket is fixed to the outer wall of the C-shaped frame, and the pressing screw passes through the central threaded hole of the sleeve bracket and out of the inner wall of the C-shaped frame to be connected with the movable pressing plate;
[0015] The movable pressing plate can rotate around the exit end of the pressing screw and tilt at a small angle.
[0016] The turning mechanism is provided with a dividing plate for multi-angle turning and real-time fixation of the positioning frame.
[0017] Four sets of adjustable supports are provided at the bottom of the support frame for the stable placement of the device.
[0018] Beneficial effects:
[0019] This auxiliary device has a simple structure and is easy to operate, effectively supporting and securing the center fin of the horizontal tail. The device can be tilted at a fixed angle, providing multiple angles for reaming butt joints. This provides the appropriate operating angle for reaming bolt holes in different locations, improving reaming efficiency. BRIEF DESCRIPTION OF THE DRAWINGS
[0020] Figure 1 The utility model is a schematic structural diagram of an auxiliary device for reaming holes in a helicopter horizontal tail central wing butt joint, wherein: 1 is a positioning frame, and 2 is a support frame.
[0021] Figure 2 This is a schematic diagram of the positioning frame structure of the utility model Figure 1 .
[0022] Figure 3 This is a schematic diagram of the positioning frame structure of the utility model Figure 2 .
[0023] Figure 4 It is a schematic diagram of the support frame structure of the utility model.
[0024] Figure 5 It is a schematic diagram of an example of use of the present utility model. DETAILED DESCRIPTION
[0025] The utility model designs an auxiliary device for reaming holes in the butt joint of the central wing of the horizontal tail of a helicopter. The device can not only fix the central wing of the horizontal tail, but also realize multi-angle flipping and fixing, thereby providing a suitable operating angle for the reaming operation and improving the efficiency of the reaming operation.
[0026] The utility model provides an auxiliary device for reaming holes in the center wing butt joint of a helicopter horizontal tail. Figure 1 As shown, the main structural components of the device include a positioning frame and a supporting frame.
[0027] Positioning frame Figure 2 and Figure 3 As shown, it is used to position, support and secure the center wing of the horizontal tail.
[0028] The positioning frame is provided with a set of single-fork ear connection structures for connecting with a set of double-fork ear structures of the central wing, thereby positioning and fixing the central wing.
[0029] The positioning frame is equipped with multiple sets of adjustable support structures. When multiple sets are used simultaneously, they can also clamp the central wing, thereby further strengthening the fixation of the central wing.
[0030] Both ends of the positioning frame are provided with a turning mechanism, and a dividing plate is provided on the turning mechanism for multi-angle turning and real-time fixation of the positioning frame.
[0031] Support frame such as Figure 4 As shown, it is used to support the positioning frame and is fixedly connected to the flip mechanisms at both ends of the positioning frame.
[0032] The bottom of the support frame is provided with 4 sets of adjustable supports for the stable placement of the device.
[0033] The utility model is used as an example Figure 5 As shown, during use, the center fin of the horizontal stabilizer is placed on the device's positioning frame. Positioned using the forked lugs at each end, the fin is tightened using the positioning bolts and nuts. Multiple sets of adjustable supports on the positioning frame act simultaneously to further clamp the fin. Based on the location of the bolt holes to be reamed, the positioning frame is flipped to the appropriate angle and secured, and the reaming operation begins. After all bolt holes have been reamed, the center fin is removed, completing the device's use.
Claims
1. An auxiliary device for reaming a hole in a helicopter horizontal tail center wing butt joint, characterized in that: include: Positioning frame and support frame; The positioning frame is provided with a flip mechanism at both ends and is mounted on the support frame through the flip mechanism; The positioning frame is used to position, support and fix the center wing of the horizontal tail; The positioning frame includes a C-shaped frame, a single fork ear connection structure, and an adjustable support structure; Both end surfaces of the C-shaped frame are inwardly installed with single-fork ear connection structures, which are used to connect with a set of double-fork ear structures of the central wing, thereby positioning and fixing the central wing; Multiple sets of adjustable support structures are set on the C-shaped frame. When used simultaneously, multiple sets can also clamp the central wing, thereby further strengthening the fixation of the central wing.
2. The auxiliary device according to claim 1, characterized in that A set of adjustable support structures includes an upper adjustable support structure and a lower adjustable support structure, both of which have the same structure; the adjustable support structure includes a fixed support, a rocker arm, a clamping screw, and a movable clamping block; The rocker arm is installed on the C-shaped frame through a fixed support. One end of the rocker arm cooperates with the clamping screw, and the bottom end of the clamping screw is connected to the movable clamping block. The movable clamping block can rotate around the bottom end of the clamping screw and tilt at a small angle.
3. The auxiliary device according to claim 2, characterized in that Also includes: lateral support structure; The lateral support structure includes a sleeve bracket, a compression screw, and a movable pressure plate; The sleeve bracket is fixed to the outer wall of the C-shaped frame, and the pressing screw passes through the central threaded hole of the sleeve bracket and out of the inner wall of the C-shaped frame to be connected with the movable pressing plate; The movable pressing plate can rotate around the exit end of the pressing screw and tilt at a small angle.
4. The auxiliary device according to claim 1, characterized in that The turning mechanism is provided with a dividing plate for multi-angle turning and real-time fixation of the positioning frame.
5. The auxiliary device according to claim 1, characterized in that Four sets of adjustable supports are provided at the bottom of the support frame for the stable placement of the device.