Airtight box positioning tool
By designing the airtight box positioning tool, precise positioning is achieved using the guide rail and slide chute structure, and preventing offsets through the coordination of the lead screw and the clamp block, the problem of positioning difficulties and offsets during the installation of the airtight box is solved, and the installation is improved Efficiency and product quality.
Patent Information
- Application Number
- CN202421087582.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-17
- Publication Date
- 2025-02-07
- Estimated Expiration
- 2034-05-17
AI Technical Summary
In airtight aircraft, it is difficult to accurately locate the airtight box during installation, resulting in easy leakage and positioning offset during hole making, affecting the margins of the rivets and the position of other parts, increasing the installation difficulty and risk.
An airtight box positioning tool is designed, including positioning components and tensioning components. The precise positioning of the airtight box is achieved through the guide rail and the sliding groove structure, and the matching of the lead screw and the clamp block ensures that the airtight box is during the installation process. No offset.
It effectively improves the installation efficiency of the airtight box, avoids the deviation of the airtight box during the hole making process, ensures the accuracy of the rivet margin and the correct position of other parts, and improves product quality.
Smart Images

Figure CN222430535U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the technical field of aviation manufacturing technology structure assembly, and relates to a tool used for positioning an airtight box. Background Art
[0002] In order to ensure that the internal system equipment can be connected to the outside, a certain number of airtight boxes need to be installed on an airtight aircraft. Currently, airtight boxes are installed on jigs during the aircraft assembly stage. Due to the limitations of the jigs, the airtight boxes are difficult to position during the installation process, and often require two operators to collaborate on the installation on both sides of the airtight box. The inner operator is responsible for positioning the airtight box, and the outer operator is responsible for making holes and locating pins. However, during the hole making process, the inner operator is prone to force loss, which leads to the positioning offset of the airtight box. If the operator does not correct it, the final installation position of the airtight box will deviate, resulting in insufficient rivet margins, which affects the position of the parts installed together with the airtight box.
[0003] At the same time, in order to improve the performance of the aircraft, there are cases where the airtight box is moved or added to the delivered aircraft. At this time, due to the small construction space on the aircraft, the positioning of the airtight box requires two operators to work closely inside and outside the aircraft, which greatly increases the difficulty. Utility Model Content
[0004] Technical problem solved by the utility model: The utility model overcomes the shortcomings of the prior art and is designed to provide an airtight box positioning tool aimed at the problems existing in the above-mentioned prior art. Its purpose is to use the tool to solve the positioning problem of the original airtight box during the installation process, so as to reduce the installation difficulty of the airtight box and the insufficient rivet margin caused by the offset of the airtight box during the hole making process, thereby improving the installation efficiency of the airtight box and ensuring product quality.
[0005] The technical solution of this utility model:
[0006] A positioning tool for an airtight box comprises a positioning component and a tensioning component, wherein the positioning component comprises a guide rail 1, the bottom surface of the guide rail is a plane, matched with the surface of an aircraft skin, and a slide groove is arranged inside the guide rail 1; the tensioning component comprises a connecting strip 2, sliders 3 are arranged at both ends of the connecting strip 2, the sliders 3 are slidably arranged in the slide groove of the guide rail 1, a groove is opened in the middle part of the connecting strip 2 along its length direction, a lead screw 5 vertically passes through the groove in the middle part of the connecting strip 2, a clamping block 4 is arranged on the top of the lead screw 5, the clamping block 4 is threadedly matched with the upper end of the lead screw 5, a stopper 6 is arranged at the lower end of the lead screw 5, and the stopper length 6 is greater than the aperture of the mounting hole at the bottom of the airtight box.
[0007] Furthermore, a rubber pad 7 is provided on the ground of the guide rail 1 .
[0008] Furthermore, both ends of the connecting bar 2 are connected to the slider 3 via connecting columns 8 respectively.
[0009] Furthermore, the upper end of the screw rod 5 is threaded, and the lower end is provided with a pin hole.
[0010] Furthermore, the lower end of the lead screw 5 is square and matches with the square hole in the center of the stopper 6. A pin rod 10 is arranged in the pin rod hole at the lower end of the lead screw 5, and the pin rod 10 limits the stopper 6 from moving downward.
[0011] Furthermore, a rubber pad 9 with holes is provided on the upper surface of the stopper 6 .
[0012] Furthermore, a threaded hole is formed in the middle of the clamping block 4 , which matches with the thread on the upper end of the screw rod 5 .
[0013] Furthermore, the guide rail 1 is an aluminum profile, and its surface is anodized; the connecting bar 2 is an aluminum profile, and its surface is anodized; the slider 3, the block 4, and the connecting column 8 are all aluminum alloy parts; the screw rod 5 is made of steel and is hard chrome treated.
[0014] Beneficial effects of the utility model:
[0015] The utility model provides an airtight box positioning tool, which has the advantages of greatly ensuring and improving the installation efficiency of the airtight box, and can also avoid the deviation of the airtight box during the hole making process. It is easy to use, can not only improve the installation efficiency of the airtight box, but also ensure product quality. BRIEF DESCRIPTION OF THE DRAWINGS
[0016] Figure 1 This is a schematic diagram of the airtight box positioning tooling structure;
[0017] Figure 2 Schematic diagram of the use of the airtight box positioning tooling on the machine;
[0018] Among them: 1. Guide rail, 2. Connecting strip, 3. Slider, 4. Block, 5. Screw, 6. Stopper, 7. Rubber pad, 8. Connecting column, 9. Rubber pad with hole, 10. Pin rod. DETAILED DESCRIPTION
[0019] The present invention will be further described below in conjunction with the accompanying drawings:
[0020] like Figure 1 As shown, the utility model proposes to provide an airtight box positioning tool, which mainly includes a positioning component and a tensioning component; wherein the fixing component includes 2 guide rails 1 and 2 rubber pads 7; the tensioning component includes 1 clamping block 4, 1 connecting strip 2, 2 sliders 3, 2 connecting columns 8, 1 screw rod 5, 1 stopper 6, 1 rubber pad with holes 9, and 1 pin rod 10.
[0021] In the positioning assembly, the guide rail 1 is an aluminum profile, and the surface is anodized and oxidized. There is a convex groove inside it, which mainly provides a sliding track for the slider 3 and limits one degree of freedom of the slider 3; the rubber pad 7 is a rubber material, and its main function is to protect the aircraft skin and prevent the aircraft skin from being crushed by the guide rail 1. In the positioning assembly, the length of the guide rail 1 can be changed according to the length of the required positioning airtight box to achieve a wider range of applications; the length of the rubber pad 7 varies according to the length of the guide rail 1, and the contact surface between the guide rail 1 and the aircraft skin is fully covered.
[0022] In the tensioning assembly, the block 4 is an aluminum alloy part with a threaded hole in the middle, which matches the thread of the screw rod; the connecting bar 2 is an aluminum profile, and the surface is anodized and oxidized, and there is a groove inside it, which mainly provides a sliding track for the screw rod 5, while making the screw rod 5 have only one degree of freedom; the slider 3 is an aluminum alloy part, which mainly slides in the guide rail 1; the connecting column 8 is an aluminum alloy part, and its main function is to connect the slider 3 and the connecting bar 2; the screw rod 5 is made of steel material and hard chrome treated, with a thread on the upper end and a pin hole on the lower end; the stopper 6 is an aluminum alloy part, with a square hole in the middle, which is square with the cross-section of the lower end of the screw rod, and the end has a pin hole and matches the pin rod 10; the pin rod 10 is an aluminum alloy part, which is mainly used to limit the movement of the stopper 6; the perforated rubber pad 9 is made of rubber material, and its main function is to protect the airtight box and prevent the airtight box from being crushed by the stopper 6. In the tensioning assembly, the length of the connecting strip 2 can be changed according to the width of the required positioning airtight box to achieve a wider range of applications; the number of tensioning assemblies can be changed according to the length of the airtight box and the number of holes on the airtight box.
[0023] When working, first select the length of the guide rail 1, rubber pad 7, connecting strip 2 and the number of tensioning components according to the length and width of the airtight box and the number of holes on the airtight box. Combine the positioning component with the connecting strip 2, slider 3 and connecting column 8, and position the positioning component on the aircraft skin to ensure that the rubber pad 7 fits the aircraft skin; then pass the lead screw 5 through the groove in the middle of the connecting strip 2, the lower end of the lead screw 5 penetrates into the airtight box and extends from the mounting hole at the bottom of the airtight box, and then install the stopper 6 at the bottom of the lead screw 5, so that the upper surface of the stopper 6 contacts the bottom surface of the airtight box 9, and then install the clamping block 4 at the upper end of the lead screw 5. When in use, rotate the clamping block 4, and when the length of the stopper 6 is greater than the aperture of the mounting hole at the bottom of the airtight box, the tensioning component pulls the airtight box upward, and the airtight box is simultaneously subjected to the downward pressure of the positioning component, ensuring the positioning of the airtight box.
[0024] The utility model greatly improves the installation efficiency of the airtight box, can also avoid the deviation of the airtight box during the hole making process, is easy to use, can improve the installation efficiency of the airtight box, and can ensure product quality.
Claims
1. An airtight box positioning tool, characterized in that: It includes a positioning component and a tensioning component. The positioning component includes a guide rail. The bottom surface of the guide rail is a plane and cooperates with the surface of the aircraft skin. A slide groove is arranged inside the guide rail. The tensioning component includes a connecting strip. Slide blocks are arranged at both ends of the connecting strip. The slide blocks are slidably arranged in the slide groove of the guide rail. A groove is opened in the middle part of the connecting strip along its length direction. The lead screw vertically passes through the groove in the middle part of the connecting strip. A clamping block is arranged on the top of the lead screw. The clamping block cooperates with the upper end thread of the lead screw. A stop block is arranged at the lower end of the lead screw. The length of the stop block is greater than the aperture of the mounting hole at the bottom of the airtight box.
2. The airtight box positioning tool according to claim 1, characterized in that: The guide rail floor is provided with a rubber pad.
3. The airtight box positioning tool according to claim 1, characterized in that: Both ends of the connecting strip are connected to the slider through connecting columns.
4. The airtight box positioning tool according to claim 1, characterized in that: The upper end of the screw rod is provided with threads, and the lower end is provided with a pin hole.
5. The airtight box positioning tool according to claim 4, characterized in that: The lower end of the lead screw is square and matches with the square hole in the center of the stopper. A pin is arranged in the pin hole at the lower end of the lead screw to limit the downward movement of the stopper.
6. The airtight box positioning tool according to claim 5, characterized in that: A rubber pad with holes is arranged on the upper surface of the stopper.
7. The airtight box positioning tool according to claim 1, characterized in that: A threaded hole is provided in the middle of the clamping block, which matches with the thread on the upper end of the screw rod.
8. The airtight box positioning tool according to claim 1, characterized in that: The guide rail is an aluminum profile with an anodized surface. The connecting strip is an aluminum profile with an anodized surface. The slider, block and connecting column are all aluminum alloy parts. The lead screw is made of steel and hard chrome treated.