Cabin butt-joint assembly auxiliary tool
By designing buffer components and ranging structures for auxiliary tooling for module docking and assembly, the problem of structural damage during module docking was solved, resulting in improved safety and convenient movement control.
Patent Information
- Application Number
- CN202520073011.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-13
- Publication Date
- 2026-01-16
- Estimated Expiration
- 2035-01-13
AI Technical Summary
During the docking process, the lack of a buffer structure led to damage to the structure of the compartment and its internal equipment.
Design an auxiliary tooling for docking and assembly of compartments, including a buffer assembly and a ranging structure. The buffer assembly consists of a first fixing block, a lug plate, a guide ring, a guide rod, a limit block, a damper, and a helical spring, which is used to absorb and disperse impact energy. The ranging structure monitors the distance between compartments through a laser rangefinder.
It effectively reduces or eliminates impact and vibration during docking, improves safety, and facilitates control of the module movement speed.
Smart Images
Figure CN223806540U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to cabin section butt joint technical field, concretely is a kind of cabin section butt joint assembly auxiliary tool. BACKGROUND
[0002] In the cabin section butt joint process, the contact and collision between two cabin sections, and the cabin section butt joint section lacks buffer structure in prior art, which can cause cabin section structure and its internal equipment damage.
[0003] Therefore, we propose a kind of cabin section butt joint assembly auxiliary tool. UTILITY MODEL CONTENTS
[0004] (One) technical problem solved
[0005] In view of the deficiencies of the prior art, the utility model provides a kind of cabin section butt joint assembly auxiliary tool, can effectively absorb and disperse impact energy during butt joint process, improves safety and other advantages, can effectively solve the problems in the background art.
[0006] (Two) technical scheme
[0007] To achieve the above-mentioned purpose, the technical scheme adopted by the utility model is as follows: a kind of cabin section butt joint assembly auxiliary tool, including buffer assembly, the buffer assembly includes first fixed block, ear plate, guide ring, guide rod, first limit block, damper, spiral spring, second limit block and installation cavity, and the front end of the outer surface of the upper end of the first fixed block is fixedly installed with ranging structure, the ranging structure includes second fixed block and laser range finder, the second fixed block is fixedly installed on the front end of the outer surface of the upper end of the first fixed block.
[0008] Preferably, the ear plate is fixedly installed on the left and right ends of the rear end of the outer surface of the upper and lower sides of the first fixed block.
[0009] Preferably, the laser range finder is fixedly installed on the second fixed block.
[0010] Preferably, the installation cavity is opened in the inside of the first fixed block, the number of guide ring and guide rod is two groups, two groups of guide ring are fixedly installed on the upper and lower sides of the outer surface of the front end of the first fixed block, and the guide rod penetrates the guide ring.
[0011] Preferably, the two groups of guide rods are fixedly installed between the rear end outer surface of the first limiting block and the front end outer surface of the second limiting block, and the damper, the spiral spring and the second limiting block are located in the mounting cavity, the damper is fixedly installed between the middle portion of the mounting cavity away from the guide ring and the middle portion of the outer surface of one side of the second limiting block, the spiral spring is movably sleeved on the outer wall of the damper, one end of the outer surface of the spiral spring is fixedly connected with one end of the mounting cavity, and the other end of the outer surface of the spiral spring is fixedly connected with the outer surface of one side of the second limiting block.
[0012] Preferably, the outer wall of the second limiting block and the mounting cavity are in sliding connection, one side of the outer surface of the second limiting block is elastically connected with one end of the mounting cavity through the damper and the spiral spring, and the outer wall of the guide rod and the guide ring are in sliding connection.
[0013] (Three) beneficial effects
[0014] Compared with the prior art, the utility model provides a cabin section butt joint assembly auxiliary tool, has the following beneficial effects:
[0015] 1、This cabin section butt joint assembly auxiliary tool, through the buffer assembly that sets, reduce or eliminate the impact and vibration that produces in the butt joint process, improve security.
[0016] 2、This cabin section butt joint assembly auxiliary tool, through the ranging structure that sets up, be convenient for monitoring the spacing between cabin section, be convenient for to control the speed of cabin section on the guide rail moves. BRIEF DESCRIPTION OF DRAWINGS
[0017] Figure 1 It is the overall structure schematic diagram of the utility model a cabin section butt joint assembly auxiliary tool.
[0018] Figure 2 It is the structure schematic diagram of the utility model a cabin section butt joint assembly auxiliary tool buffer assembly.
[0019] Figure 3 It is the structure schematic diagram of the utility model a cabin section butt joint assembly auxiliary tool ranging structure.
[0020] Figure 4 It is the side view sectional drawing of the utility model a cabin section butt joint assembly auxiliary tool buffer assembly.
[0021] In the drawing: 1, buffer assembly;2, ranging structure;3, first fixed block;4, lug plate;5, guide ring;6, guide rod;7, first limiting block;8, second fixed block;9, laser range finder;10, damper;11, spiral spring;12, second limiting block;13, mounting cavity. DETAILED DESCRIPTION
[0022] To make the technical means, creative features, objectives and effects of this utility model easier to understand, the present utility model will be further described below in conjunction with specific embodiments.
[0023] This embodiment is an auxiliary tooling for module docking and assembly.
[0024] like Figures 1-4 As shown, it includes a buffer assembly 1, which includes a first fixing block 3, an ear plate 4, a guide ring 5, a guide rod 6, a first limiting block 7, a damper 10, a coil spring 11, a second limiting block 12, and a mounting cavity 13. A ranging structure 2 is fixedly installed on the front end of the upper outer surface of the first fixing block 3. The ranging structure 2 includes a second fixing block 8 and a laser rangefinder 9. The second fixing block 8 is fixedly installed on the front end of the upper outer surface of the first fixing block 3.
[0025] Ear plates 4 are fixedly installed on the left and right ends of the rear end of the upper and lower outer surfaces of the first fixed block 3; laser rangefinder 9 is fixedly installed on the second fixed block 8; mounting cavity 13 is opened inside the first fixed block 3; there are two sets of guide rings 5 and guide rods 6; the two sets of guide rings 5 are fixedly installed on the upper and lower sides of the front outer surface of the first fixed block 3, and the guide rods 6 pass through the guide rings 5; the two sets of guide rods 6 are fixedly installed between the rear outer surface of the first limiting block 7 and the front outer surface of the second limiting block 12, and the damper 10, coil spring 11 and the second limiting block 12 are all located in the mounting cavity 13; the damper 10 is fixedly installed... The helical spring 11 is movably sleeved on the outer wall of the damper 10, located between the middle of the end of the mounting cavity 13 away from the guide ring 5 and the middle of the outer surface of one side of the second limiting block 12. One end of the outer surface of the helical spring 11 is fixedly connected to one end of the mounting cavity 13, and the other end of the outer surface of the helical spring 11 is fixedly connected to one side of the outer surface of the second limiting block 12. The outer wall of the second limiting block 12 is slidably connected to the mounting cavity 13, and one side of the outer surface of the second limiting block 12 is elastically connected to one end of the mounting cavity 13 through the damper 10 and the helical spring 11. The outer wall of the guide rod 6 is slidably connected to the guide ring 5.
[0026] It needs to be explained that the utility model is a kind of cabin section butt joint assembly auxiliary tool, the buffer assembly 1 and range finding structure 2 being set, the impact force and vibration can be generated in the contact and collision between two cabin sections during cabin section butt joint process, in order to slow down this impact, protect cabin section structure and its internal equipment, buffer assembly 1 is installed in the main impact area of butt joint, these areas include the vicinity of butt joint port, the connecting place between cabin sections etc., when cabin section is butt jointed, first limit block 7 is extruded, first limit block 7 drives guide rod 6 to slide along guide ring 5, guide rod 6 drives second limit block 12 to extrude damper 10 and helical spring 11 in the inside of first fixed block 3, by being set damper 10 and helical spring 11, can play the role of buffering and shock absorption, improve safety, by being set laser range finder 9, it is convenient to monitor the spacing between cabin sections, it is convenient to remind staff to control the speed of cabin section moving on guide rail in time.
[0027] It needs to be explained that, in this document, relational terms such as first and second and the like can be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises", "comprising", or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but can include other elements not expressly listed or inherent to such process, method, article, or apparatus. An element proceeded by "comprises... a" does not, without more constraints, exclude the existence of additional identical elements in the process, method, article, or apparatus that comprises the element.
[0028] The basic principle and main features of the utility model and the advantages of the utility model are shown and described above. It should be understood by those skilled in the art that the utility model is not limited by the above examples, and the above examples and descriptions in the specification are only to illustrate the principle of the utility model, and various changes and improvements can be made to the utility model without departing from the spirit and scope of the utility model, and these changes and improvements all fall within the scope of the utility model claimed.
Claims
1. A docking assembly aid for a cabin section, comprising a buffer assembly (1), characterized in that: The buffer assembly (1) comprises a first fixed block (3), an ear plate (4), a guide ring (5), a guide rod (6), a first limiting block (7), a damper (10), a spiral spring (11), a second limiting block (12) and a mounting cavity (13), and the front end of the outer surface of the upper end of the first fixed block (3) is fixedly installed with a distance measuring structure (2), the distance measuring structure (2) comprises a second fixed block (8) and a laser range finder (9), and the second fixed block (8) is fixedly installed on the front end of the outer surface of the upper end of the first fixed block (3).
2. The cabin section docking assembly aid tool of claim 1, wherein: The ear plate (4) is fixedly installed on the left and right ends of the rear end of the outer surface of the upper and lower sides of the first fixed block (3).
3. The midbody docking assembly aid of claim 2, wherein: The laser range finder (9) is fixedly installed on the second fixed block (8).
4. The midbody mating assembly aid of claim 3, wherein: The mounting cavity (13) is arranged in the first fixed block (3), the guide ring (5) and the guide rod (6) are both two groups, the two groups of guide rings (5) are fixedly installed on the upper and lower sides of the outer surface of the front end of the first fixed block (3), and the guide rods (6) penetrate through the guide rings (5).
5. The midbody mating assembly aid of claim 4, wherein: The two groups of guide rods (6) are fixedly installed between the rear end outer surface of the first limiting block (7) and the front end outer surface of the second limiting block (12), and the damper (10), the spiral spring (11) and the second limiting block (12) are located in the mounting cavity (13), the damper (10) is fixedly installed between the middle of the end of the mounting cavity (13) away from the guide ring (5) and the middle of the outer surface of one side of the second limiting block (12), the spiral spring (11) is movably sleeved on the outer wall of the damper (10), one end of the outer surface of the spiral spring (11) is fixedly connected with one end of the mounting cavity (13), and the other end of the outer surface of the spiral spring (11) is fixedly connected with the outer surface of one side of the second limiting block (12).
6. The midbody mating assembly aid of claim 5, wherein: The outer wall of the second limiting block (12) and the mounting cavity (13) are in sliding connection, one side of the outer surface of the second limiting block (12) is elastically connected with one end of the mounting cavity (13) through the damper (10) and the spiral spring (11), and the outer wall of the guide rod (6) and the guide ring (5) are in sliding connection.