Adjusting device

Abstract

The utility model belongs to the technical field of technological equipment for aircraft manufacturing, and discloses an adjusting device. The adjusting device is used for assembling and adjusting the aircraft wing slat and the sliding rail, and in the assembling and adjusting process, the slat and the sliding rail are adjusted through an eccentric bushing and connected through a bolt. The adjusting device comprises a main body, an adjusting groove is formed in the main body, the eccentric bushing is sleeved with the adjusting groove, and the eccentric bushing is driven to rotate and adjust by rotating the main body; a boss is arranged on the bottom wall of the adjusting groove and can be placed in a groove in the head of the bolt so as to limit rotation of the bolt. According to the utility model, two tools such as a sleeve tool and a bolt fixing clamp are not needed, and one person can complete the operation, so that the matching difficulty is reduced, the loosening risk and the risk of possibly damaging assembling personnel and products are avoided, the convenience is improved, and the problems of poor coordination and low safety are avoided; on the other hand, the adjusting device is simple and reliable in structure, and operation efficiency, installation quality and economic benefits can be improved.

Description

Technical Field

[0001] This utility model relates to the field of process equipment technology for aircraft manufacturing, and in particular to an adjustment device. Background Technology

[0002] The installation of the leading edge slat control surface of an aircraft wing refers to first connecting the slat to the rail with bolts, then conducting joint debugging to ensure that the aerodynamic step of the slat meets the design requirements, and finally locking the debugged slat rail to complete the installation of the slat.

[0003] Specifically, the joint adjustment of the slats is achieved by adjusting the eccentric bushing set on the slide rail to change the height of the slats. During the adjustment at the assembly site, a combination of bolt fixing fixture and sleeve tool is required. First, the sleeve is placed on the eccentric bushing of the slide rail, and the eccentric bushing is adjusted by rotating the sleeve. Then, the bolt fixing fixture is used to fix the bolt head, thereby completing the locking at the other end of the bolt to achieve the adjustment of the slat attitude.

[0004] The current assembly process often requires two people to operate the socket tool and the bolt fixing fixture respectively. Due to the large weight of the two tools, it is difficult for two people to work together, the safety is low, and the two operators need to have a high degree of coordination, which is not convenient. Utility Model Content

[0005] The purpose of this invention is to provide an adjustment device to solve the problems of high difficulty in multi-person cooperation, poor coordination, inconvenient operation, and low safety in the existing installation of aircraft wing leading edge slat control surfaces.

[0006] To achieve this objective, the present invention adopts the following technical solution:

[0007] An adjustment device for assembling and adjusting an aircraft wing slat and a slide rail, wherein the slat and the slide rail are adjusted via an eccentric bushing and connected by bolts, comprising:

[0008] The main body has an adjustment groove, which is fitted onto the eccentric bushing. The eccentric bushing is rotated by rotating the main body. The bottom wall of the adjustment groove has a boss, which can be placed in the groove of the bolt head to restrict the rotation of the bolt.

[0009] As an alternative to the adjustment device, one side of the main body is recessed inward to form the adjustment groove, which is in clearance fit with the eccentric bushing.

[0010] As an alternative to the adjustment device, the cross-sectional shape of the adjustment groove matches the shape of the mating part of the eccentric bushing.

[0011] As an alternative to the adjustment device, the adjustment groove is a prismatic groove adapted to the eccentric bushing.

[0012] As an alternative to the adjustment device, the opening of the adjustment groove is transitioned by an arc surface.

[0013] As an alternative adjustment device, the boss and the main body are an integral structure.

[0014] As an alternative to the adjustment device, the boss has a strip-shaped structure.

[0015] As an alternative adjustment device, the length of the boss is matched with the length of the groove in the bolt head.

[0016] As an alternative to the adjustment device, the main body is provided with a connecting part on the other side of the adjustment groove, the connecting part being used to cooperate with a clamping tool to restrict the rotation of the main body.

[0017] As an alternative to the adjustment device, the connecting part is a prismatic boss.

[0018] Beneficial effects:

[0019] In this invention, when the adjusting device is in use, the adjusting groove is first fastened onto the eccentric bushing. The main body is then rotated, causing the adjusting groove to rotate. After the eccentric bushing is adjusted, the boss is placed in the groove of the bolt head, restricting bolt rotation. The nut is then tightened on the other side of the bolt to lock it in place. This adjusting device eliminates the need for both socket tools and bolt clamps during the installation of aircraft wing leading-edge slat control surfaces. One person can complete the installation, reducing the difficulty of multi-person operation, avoiding the risk of loosening during tightening, and preventing potential damage to assembly personnel and products. It improves convenience and avoids problems of poor coordination and low safety. Furthermore, this adjusting device has a simple and reliable structure, improving operational efficiency, installation quality, and economic benefits. Attached Figure Description

[0020] Figure 1 This is a first-view structural schematic diagram of the adjustment device provided in this embodiment of the utility model;

[0021] Figure 2 This is a schematic diagram of the second-view structure of the adjustment device provided in an embodiment of the present invention.

[0022] In the picture:

[0023] 100. Main body; 110. Adjustment groove; 111. Boss; 120. Connecting part. Detailed Implementation

[0024] The present invention will now be described in further detail with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the present invention and not intended to limit it. Furthermore, it should be noted that, for ease of description, the accompanying drawings show only the parts relevant to the present invention, not the entire structure.

[0025] In the description of this utility model, unless otherwise explicitly specified and limited, the terms "connected," "linked," and "fixed" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral part; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; they can refer to the internal communication of two components or the interaction between two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0026] In this invention, unless otherwise explicitly specified and limited, "above" or "below" the second feature can include direct contact between the first and second features, or contact between the first and second features through another feature between them. Furthermore, "above," "over," and "on top" of the second feature includes the first feature directly above or diagonally above the second feature, or simply indicates that the first feature is at a higher horizontal level than the second feature. "Below," "below," and "under" the second feature includes the first feature directly below or diagonally below the second feature, or simply indicates that the first feature is at a lower horizontal level than the second feature.

[0027] In the description of this embodiment, the terms "upper," "lower," "right," etc., refer to the orientation or positional relationship shown in the accompanying drawings. They are used only for ease of description and simplification of operation, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model. In addition, the terms "first" and "second" are only used for distinction in description and have no special meaning.

[0028] Please see the appendix Figure 1 and attached Figure 2 This embodiment relates to an adjustment device for assembling and adjusting the slats and rails of an aircraft wing. During the assembly and adjustment process, the slats and rails are adjusted by an eccentric bushing and connected by bolts.

[0029] The adjustment device includes a main body 100, on which an adjustment groove 110 is provided. The adjustment groove 110 is fitted onto the eccentric bushing. The eccentric bushing is rotated by rotating the main body 100. A boss 111 is provided on the bottom wall of the adjustment groove 110. The boss 111 can be placed in the groove of the bolt head to restrict the rotation of the bolt.

[0030] Specifically, the main body 100 has a cylindrical block structure, with its diameter slightly larger than its height. An adjustment groove 110 is provided on the main body 100. When this adjustment device is in use, the adjustment groove 110 is first fastened onto the eccentric bushing. Rotating the main body 100 causes the adjustment groove 110 to rotate. It should be noted that during the rotation of the main body 100, the boss 111 is not placed in the groove of the bolt head. Therefore, when the eccentric bushing rotates, the bolt remains relatively stationary. After the position of the eccentric bushing is adjusted, the bolt is slightly rotated at a certain angle on the side away from the head so that the boss 111 can be placed in the groove of the bolt head. A certain force can be applied to the bolt head to restrict its rotation. Then, the nut is tightened on the other side of the bolt to lock the entire bolt and prevent it from rotating.

[0031] With this adjustment device, the installation of slat control surfaces on the leading edge of aircraft wings can be completed by one person without the need for both a sleeve tool and a bolt fixing clamp. This reduces the difficulty of coordination for multiple operators, avoids the risk of loosening during the tightening process, and eliminates the risk of damage to assembly personnel and products. It improves convenience and avoids problems of poor coordination and low safety. On the other hand, this adjustment device has a simple and reliable structure, which can improve operating efficiency, installation quality, and economic benefits.

[0032] Optionally, one side of the main body 100 is recessed inward to form an adjustment groove 110, which is clearance-fitted with the eccentric bushing.

[0033] In this embodiment, the adjustment groove 110 and the eccentric bushing are fitted together to ensure that the main body 100 can be easily fitted when the eccentric bushing is installed, thereby improving the operating efficiency.

[0034] Optionally, the cross-sectional shape of the adjusting groove 110 is matched with the shape of the mating part of the eccentric bushing.

[0035] In this embodiment, the mating part of the eccentric bushing has a prism structure, specifically a hexagonal prism. Adaptively, the cross-sectional shape of the adjusting groove 110 is also a hexagonal structure. That is, the adjusting groove 110 is a hexagonal prism groove adapted to the mating structure of the eccentric bushing. Of course, in other embodiments, the cross-sectional shape of the adjusting groove 110 can also be other polygonal structures to adapt to the shape of the mating part of the eccentric bushing.

[0036] Furthermore, the opening of the adjusting groove 110 is transitioned by an arc surface.

[0037] In this embodiment, the edges of the groove opening of the adjustment groove 110 are all connected with arc surfaces, which can ensure that the main body 100 can be fitted with the eccentric bushing more smoothly and without jamming.

[0038] Optionally, the boss 111 and the main body 100 are an integral structure.

[0039] In this embodiment, the boss 111 can be integrally cast or directly milled inside the adjusting groove 110. Of course, in other embodiments, the boss 111 can also be welded or threaded onto the bottom wall of the adjusting groove 110. The specific forming method can be selected according to the difficulty and cost of processing.

[0040] Optionally, the boss 111 has a strip-shaped structure.

[0041] The head of a bolt is usually provided with a slotted groove. To accommodate the slotted groove, the boss 111 is also a slotted strip structure. At the same time, the width of the boss 111 is smaller than that of the slotted groove to ensure a clearance fit between the two.

[0042] Alternatively, the length of the boss 111 matches the length of the groove in the bolt head.

[0043] In this embodiment, the length of the boss 111 is slightly smaller than the length of the groove in the bolt head to avoid the length of the boss 111 being too small compared to the length of the groove in the bolt head. This prevents stress concentration between the boss 111 and the groove when the bolt is tightened on the other side, thus avoiding damage to the bolt during the tightening process and ensuring the stability of the bolt during the assembly process.

[0044] Optionally, a connecting portion 120 is provided on the other side of the main body 100 opposite to the adjustment groove 110. The connecting portion 120 is used to cooperate with a clamping tool to limit the rotation of the main body 100.

[0045] In this embodiment, a connecting part 120 protrudes from the other side of the main body 100. A fixed-force wrench can be used as the clamping tool to ensure stable clamping of the connecting part 120, thereby limiting the rotation of the main body 100.

[0046] Furthermore, the connecting part 120 is a prism-shaped boss.

[0047] In this embodiment, the connecting part 120 is a hexagonal prism-shaped boss that is inserted into the fixed-force wrench, thereby restricting the rotation of the main body 100.

[0048] It should be noted that a series of adjustment devices of different specifications can be adaptively designed according to the specific dimensions and specifications of the eccentric bushing and bolts. In the actual assembly process, the corresponding size adjustment device can be selected as needed, which further improves the versatility of this adjustment device.

[0049] Obviously, the above embodiments of this utility model are merely examples for clearly illustrating the present utility model, and are not intended to limit the implementation of the present utility model. Those skilled in the art can make various obvious changes, readjustments, and substitutions without departing from the protection scope of this utility model. It is neither necessary nor possible to exhaustively describe all embodiments here. Any modifications, equivalent substitutions, and improvements made within the spirit and principles of this utility model should be included within the protection scope of the claims of this utility model.

Claims

1. An adjustment device for the assembly adjustment of a slat and a track of an aircraft wing, between which a slat and a track are adjusted by means of an eccentric bushing and connected by means of a bolt, characterized in that Comprise: The main body (100) is provided with an adjusting groove (110) on the main body (100), the adjusting groove (110) is sleeved on the eccentric bushing, and the eccentric bushing is adjusted by rotating the main body (100); The bottom wall of the adjusting groove (110) is provided with a boss (111), and the boss (111) can be placed in the groove of the bolt head to limit the rotation of the bolt.

2. The adjustment device of claim 1, wherein The side of the main body (100) is recessed inward to form the adjusting groove (110), and the adjusting groove (110) is gap-fitted with the eccentric bushing.

3. The adjustment device of claim 1, wherein, The cross-sectional shape of the adjusting groove (110) matches the shape of the matching part of the eccentric bushing.

4. The adjustment device of claim 3, wherein, The adjusting groove (110) is a prismatic groove suitable for the eccentric bushing.

5. The adjustment device of claim 1, wherein, The notch of the adjusting groove (110) is transitioned by a circular arc surface.

6. The adjustment device of claim 1, wherein, The boss (111) and the main body (100) are of an integral structure.

7. The adjustment device of claim 1, wherein The boss (111) is a strip structure.

8. The adjustment device of claim 7, wherein, The length of the boss (111) matches the length of the groove of the bolt head.

9. The adjustment device according to any one of claims 1-8, characterized in that The other side of the main body (100) relative to the adjusting groove (110) is provided with a connecting part (120), and the connecting part (120) is used for cooperating with a clamping tool to limit the rotation of the main body (100).

10. The adjustment device of claim 9, wherein, The connecting part (120) is a prismatic boss.

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