Assembly system and assembly method for cabin and protective sleeve

Abstract

The invention provides an assembling system and method for a cabin body and a protective sleeve, the assembling system for the cabin body and the protective sleeve comprises a rack, the cabin body, the protective sleeve, a first mounting assembly, a first driving assembly and at least one flaring mechanism, the first mounting assembly is arranged on the rack, and the first mounting assembly positions the cabin body to a preset angle; the protective sleeve and the cabin body are correspondingly arranged in the first horizontal direction, and an opening extending in the length direction of the protective sleeve is formed in the protective sleeve and faces downwards. The operation end of the flaring mechanism is arranged under the protective sleeve, the protective sleeve is arranged on the flaring mechanism in the first horizontal direction, and the flaring mechanism expands the diameter of the protective sleeve through the opening; the first driving assembly drives the first sliding table on the rack to move in the first horizontal direction so that the protective sleeve and the cabin can be assembled, the operation end faces upwards and corresponds to the opening, the flaring action on the protective sleeve is achieved, meanwhile, the protective sleeve is accurately positioned, the concentricity of the protective sleeve and the cabin is ensured, and follow-up accurate installation is facilitated.

Description

Technical Field

[0001] This invention relates to the field of automated assembly technology, and in particular to an assembly system and method for a cabin and a protective sleeve. Background Technology

[0002] In the aerospace, aviation, and high-end equipment manufacturing fields, the cabin serves as the core functional carrier, and its outer protective sleeve plays a crucial role in sealing, impact resistance, and corrosion prevention. The precision assembly quality of these two components directly determines the operational reliability, adaptability to extreme operating conditions, and service life of the entire equipment. These cabins and protective sleeves are often irregular conical structures. The assembly process requires multiple core steps, including cabin surface pretreatment, precise adhesive application, protective sleeve flaring and shaping, alignment and calibration, and fitting and fixing. If the relative positional deviation exceeds the allowable range, it can lead to localized stress concentration in the protective sleeve, sealing failure, and even component deformation under high-speed operation or high-pressure environments, directly threatening the overall performance and safety of the equipment. Therefore, the assembly precision of the cabin and protective sleeve is a key indicator for ensuring the core performance of the product.

[0003] Currently, the assembly of such irregularly shaped components in the industry still mainly relies on traditional manual operation. On the one hand, the manual alignment process lacks precise benchmarks and quantitative basis. Operators need to visually observe the alignment of the edges of the cabin and the protective cover, and adjust the placement angle and axial position of the protective cover by hand in an attempt to achieve concentric alignment. However, irregular conical structures do not have clear visual reference lines, and manual judgment is easily affected by factors such as light intensity and operator fatigue, making it difficult to identify subtle eccentric deviations. On the other hand, different operators have different levels of experience and visual judgment habits. Even for the same batch of cabins and protective covers, the assembly accuracy pass rate varies significantly between different operators. Moreover, the assembly accuracy of the same operator at different times will fluctuate due to changes in fatigue. After continuous operation, the incidence of eccentricity and tilting problems in the assembly will increase significantly, which cannot meet the requirements of aerospace, aviation and high-end equipment manufacturing fields for the stability and accuracy of cabin and protective cover assembly quality. Summary of the Invention

[0004] The purpose of this application is to provide an assembly system for a cabin and a protective sleeve, so as to solve the problem of low precision in the combination of the cabin and the protective sleeve in the prior art; in addition, the purpose of this application is also to provide an assembly method including the assembly system for the cabin and the protective sleeve.

[0005] To achieve this objective, the following technical solution is adopted in this application:

[0006] This application provides an assembly system for a cabin and a protective sleeve, comprising a frame, a cabin, a protective sleeve, a first mounting assembly, a first drive assembly, and at least one flaring mechanism, wherein:

[0007] The first mounting component is disposed at one end of the frame along the first horizontal direction, the cabin is disposed on the first mounting component along the first horizontal direction, the cabin is rotatably disposed on the first mounting component along its own axis, and the first mounting component is configured to support the cabin and drive the cabin to rotate to a preset angle.

[0008] The protective sleeve is correspondingly set to the cabin body along the first horizontal direction and the protective sleeve can be fitted onto the cabin body. The protective sleeve is provided with an opening extending along its own length direction, with the opening facing downward.

[0009] A first slide is provided on the frame, a flaring mechanism is provided on the first slide and spaced apart from the first mounting component along the first horizontal direction, the operating end of the flaring mechanism is located directly below the cabin along its own axis, a protective sleeve is provided on the flaring mechanism along the first horizontal direction, and the flaring mechanism is configured to enlarge the diameter of the protective sleeve through the opening.

[0010] The fixed end of the first drive assembly is mounted on the frame, and the drive end of the first drive assembly is connected to the first slide. The first drive assembly is configured to drive the first slide to reciprocate along a first horizontal direction.

[0011] Optionally, the cabin is configured as an irregular conical hollow structure, and the protective sleeve is configured as an irregular cone with the same shape as the cabin;

[0012] Each flaring mechanism includes a support plate, a support assembly, and at least one flaring assembly, wherein:

[0013] The protective sleeve is set on the support plate along the first horizontal direction with the opening facing downward. The fixed end of the flaring assembly is set on the support plate, and the operating end of the flaring assembly extends upward through the support plate and into the opening. The flaring assembly is configured to enlarge the opening.

[0014] The support assembly is disposed on the upper surface of the support plate and is configured to provide stable support for the protective sleeve on the support plate.

[0015] Optionally, the assembly system for the hull and protective casing may also include a testing mechanism and at least one adjustment mechanism, wherein:

[0016] The testing mechanism is located on one side of the protective sleeve extending along the first horizontal direction. The testing mechanism can move back and forth along the first horizontal direction. The testing mechanism is configured to test the in-situ status of the chamber and the protective sleeve and transmit deviation data information to the adjustment mechanism.

[0017] Each adjustment mechanism corresponds to a flaring mechanism. The adjustment mechanism is set on the first slide and is connected to the support plate. The adjustment mechanism is configured to receive information from the testing agency and adjust the concentricity of the protective sleeve and the cabin through the support plate.

[0018] Optionally, the flaring assembly includes a third drive assembly, a connecting plate, two baffles, a first gripper, a second gripper, and a transmission assembly, wherein:

[0019] Two baffles are parallel and spaced apart along the first horizontal direction on the bottom surface of the support plate, a connecting plate is set at the bottom end of the two baffles along the horizontal direction, and the first and second grippers are spaced apart between the two baffles along the second horizontal direction.

[0020] The fixed end of the third drive assembly is disposed on the connecting plate, and the drive end of the third drive assembly is connected to the first gripper and / or the second gripper. The third drive assembly is configured to drive the first gripper and / or the second gripper to move closer to or further away from each other.

[0021] Optionally, the adjustment mechanism includes two sets of adjustment components, which are spaced apart below the support plate along a second horizontal direction. Each set of adjustment components includes a second drive component, a first mounting plate, and a second mounting plate, wherein:

[0022] The second mounting plate is located directly below the first mounting plate. The first mounting plate is hinged to the support plate via a first hinge shaft, which extends along a first horizontal direction.

[0023] The fixed end of the second driving component is disposed on the second mounting plate, and the driving end of the second driving component is connected to the first mounting plate. The second driving component is configured to drive the second mounting plate to rise and fall.

[0024] Optionally, the adjustment assembly also includes a third mounting plate and a second hinge shaft. The third mounting plate is located directly below the second mounting plate and is hinged to the bottom surface of the second mounting plate via the second hinge shaft, which extends along a first horizontal direction.

[0025] Optionally, the adjusting assembly further includes at least one set of guide components, each set of guide components including a guide rod and a guide cylinder, wherein:

[0026] The second mounting plate has a perforation, the guide cylinder is set in the perforation in the vertical direction, and the first end of the guide rod along its own length direction is fixedly installed on the bottom surface of the first mounting plate. The guide rod is movably inserted into the guide cylinder.

[0027] Optionally, the adjustment assembly also includes two sets of first limiting components. The two sets of first limiting components are disposed on both sides of the protective sleeve extending along the first horizontal direction. Each set of first limiting components includes a support column, a fourth driving member, and a push plate. The support column is disposed vertically on the first slide. The fixed end of the fourth driving member is disposed on the support column. The driving end of the fourth driving member is connected to the push plate. The push plate is disposed close to the protective sleeve. The fourth driving member is configured to drive the baffle to move closer to or away from the protective sleeve along the second horizontal direction.

[0028] Optionally, the assembly system of the cabin and the protective sleeve also includes a fifth drive assembly, a second slide and an adhesive application mechanism. The second slide is mounted on the frame and located on one side of the first slide extending along the first horizontal direction. The adhesive application structure is mounted on the first side of the cabin extending along the first horizontal direction. The adhesive application mechanism is mounted on the second slide and is configured to apply adhesive to the surface of the cabin. The adhesive application mechanism and the detection mechanism are spaced apart along the first horizontal direction.

[0029] The fixed end of the fifth drive assembly is mounted on the frame, and the drive end of the fifth drive assembly is connected to the second slide. The fifth drive assembly is configured to drive the second slide to reciprocate along the first horizontal direction.

[0030] An assembly method, implemented through the aforementioned assembly system for the hull and protective sleeve, comprising the following steps for precise installation of the hull and protective sleeve:

[0031] The cabin is installed on the first mounting assembly along the first horizontal direction. The first mounting assembly drives the cabin to rotate along its own axis and position it at a preset angle. At the same time, the protective sleeve is placed on the support plate along the first horizontal direction with the opening facing down. The tops of the first and second grippers pass through the opening.

[0032] The detection mechanism moves back and forth along the first horizontal direction to detect the in-situ status and relative position of the detection chamber and the protective cover, generate concentricity deviation data and transmit it to the control mechanism;

[0033] The control mechanism controls the adjustment mechanism to operate, and drives the second mounting plate to rise and fall through the corresponding second driving component. Combined with the first hinge shaft driving the first mounting plate to rotate relative to the support plate, and the second hinge shaft driving the second mounting plate to rotate relative to the third mounting plate, the support plate is adjusted in spatial posture to ensure that the protective sleeve and the cabin are precisely coaxially set.

[0034] The third drive assembly drives the first and second grippers to move away from each other along the second horizontal direction via the transmission assembly, thereby expanding the opening and diameter of the protective sleeve to fit the size of the cabin.

[0035] The fifth drive component drives the second slide to move along the first horizontal direction, which in turn drives the glue application mechanism to apply glue evenly along a preset trajectory on the surface of the cabin.

[0036] The first drive assembly drives the first slide to move closer to the cabin along the first horizontal direction, so as to synchronously drive the protective sleeve to move closer to the cabin until the protective sleeve fits and is placed on the outside of the cabin.

[0037] Compared with the prior art, the assembly system for the cabin and protective sleeve proposed in this application has the following advantages:

[0038] 1) The first installation component drives the cabin to rotate along its own axis and position it at a preset angle, and the operating end of the flaring mechanism is positioned directly below the protective sleeve. By inserting the operating end into the opening of the protective sleeve, not only can the flaring action of the protective sleeve be realized, but the protective sleeve can also be accurately positioned at the same time to ensure the concentricity of the protective sleeve and the cabin, which is convenient for subsequent accurate installation.

[0039] 2) By integrating CNC rotary tables, robots, cylinders and other actuators, fully automated operations such as automatic glue application, automatic flaring, automatic posture adjustment and automatic splicing are realized, which greatly reduces manual intervention, ensures the consistency of production cycle and continuous operation capability, and significantly improves production efficiency.

[0040] 3) By setting up a movable detection mechanism, the relative position information of the cabin and the protective cover is obtained in real time. The concentricity deviation is converted into quantitative data. The attitude adjustment mechanism receives the detection data and corrects the attitude of the protective cover in real time to ensure the stability of the protective cover and the cabin during installation.

[0041] 4) Through the cooperation of the second driving component, the first mounting plate and the second mounting plate, the protective sleeve can be slightly rotated around a specific direction, improving the angle adjustment accuracy and thus ensuring the concentricity of the cabin and the protective sleeve. At the same time, by adding a second hinge shaft and a third mounting plate, the second mounting plate can be rotated around a specific direction. Combined with the rotation function of the first hinge shaft, the attitude adjustment of the protective sleeve in multiple vertical planes can be realized, further increasing the accuracy of the adjustment of the protective sleeve. Attached Figure Description

[0042] To more clearly illustrate and understand the technical solutions in the embodiments of this application, the accompanying drawings used in the background technology and embodiment descriptions of this application will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on the content of the embodiments of this application and these drawings without creative effort.

[0043] Figure 1 This is a three-dimensional structural diagram of the assembly system of the cabin and protective sleeve provided in the embodiments of this application;

[0044] Figure 2 This is a three-dimensional structural diagram of the adjustment mechanism of the assembly system for the cabin and protective sleeve provided in the embodiments of this application;

[0045] Figure 3 This is a front view of the adjustment mechanism of the assembly system for the cabin and protective sleeve provided in the embodiments of this application;

[0046] Figure 4 This is a three-dimensional structural diagram of the flared assembly of the hull and protective sleeve assembly system provided in the embodiments of this application;

[0047] Figure 5 This is a front view of the flared assembly of the hull and protective sleeve assembly system provided in the embodiments of this application;

[0048] Figure 6 This is a three-dimensional structural diagram of the first limiting component of the assembly system for the cabin and protective sleeve provided in the embodiments of this application;

[0049] Figure 7 This is a front view of the protective sleeve of the assembly system of the cabin and protective sleeve provided in the embodiments of this application;

[0050] Figure 8 This is a side view of the protective sleeve of the assembly system of the cabin and protective sleeve provided in the embodiments of this application;

[0051] Figure 9 This is a front view of the cabin of the assembly system for the cabin and protective sleeve provided in the embodiments of this application;

[0052] Figure 10 This is a side view of the cabin of the assembly system of the cabin and protective sleeve provided in the embodiments of this application. Detailed Implementation

[0053] To facilitate understanding of this application, a more complete description of the application will be provided below with reference to the accompanying drawings. Preferred embodiments of the application are shown in the drawings. However, the application can be implemented in many different forms and is not limited to the embodiments described herein. Rather, these embodiments are provided to provide a more thorough and complete understanding of the disclosure of this application. It should be noted that when a component is referred to as being "fixed to" another component, it can be directly on the other component or there may be an intermediate component. When a component is referred to as being "connected to" another component, it can be directly connected to the other component or there may be an intermediate component. The terms "vertical," "horizontal," "left," "right," and similar expressions used herein are for illustrative purposes only and do not represent the only possible implementations. Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs. The terminology used herein in the specification of this application is for the purpose of describing particular embodiments only and is not intended to be limiting of the application. The term "and / or" as used herein includes any and all combinations of one or more of the associated listed items.

[0054] Please see Figures 1 to 10 As shown in the figure, an assembly system for a cabin and a protective sleeve provided in this application embodiment includes a frame 3, a cabin 1, a protective sleeve 2, a first mounting assembly, a first drive assembly, and at least one flaring mechanism, wherein:

[0055] The first mounting component is positioned on the rack 3 along the first horizontal direction. Figure 1 At one end of the X direction, the cabin 1 is mounted on the first mounting assembly along the first horizontal direction. The cabin 1 is rotatably mounted on the first mounting assembly along its own axis. The first mounting assembly is configured to support the cabin 1 and drive the cabin 1 to rotate to a preset angle.

[0056] The protective sleeve 2 is correspondingly set to the cabin 1 along the first horizontal direction and the protective sleeve 2 can be fitted onto the cabin 1. The protective sleeve 2 is provided with an opening extending along its own length direction, with the opening facing downward.

[0057] A first slide 7 is provided on the frame 3. A flaring mechanism is provided on the first slide 7 and spaced apart from the first mounting component along the first horizontal direction. The operating end of the flaring mechanism is located directly below the cabin 1 along its own axis. The protective sleeve 2 is provided on the flaring mechanism along the first horizontal direction. The flaring mechanism is configured to enlarge the diameter of the protective sleeve 2 through the opening.

[0058] The fixed end of the first drive assembly is mounted on the frame 3, and the drive end of the first drive assembly is connected to the first slide 7. The first drive assembly is configured to drive the first slide 7 to reciprocate along the first horizontal direction.

[0059] Specifically, the first installation component includes a support block 4, a three-jaw chuck 5, and a positioning plate 6. The support block 4 is located on the frame 3 at the end away from the protective sleeve 2. The three-jaw chuck 5 is rotatably mounted on the support block 4 and faces the protective sleeve 2. The positioning plate 6 is fixedly mounted on the three-jaw chuck 5. The end of the cabin 1 with the larger diameter is fixedly mounted on the positioning plate 6 along the first horizontal direction. The positioning plate 6 is snapped into the cabin 1.

[0060] Specifically, a limit rod 8 is provided on the first slide 7. The limit rod 8 is fixedly installed in the vertical direction at the end of the first slide 7 away from the cabin 1, and the smaller diameter end of the protective sleeve 2 abuts against the limit rod 8.

[0061] Specifically, the assembly system for the hull and protective sleeve includes two flaring mechanisms spaced apart along the first horizontal direction, ensuring the stability and efficiency of the flaring.

[0062] Specifically, the first drive component is a linear module composed of a motor and a ball screw linear transmission pair.

[0063] Specifically, the frame 3 is welded from standard square tubing. Both sides of the frame 3 extending along the first horizontal direction are equipped with double doors, which not only provide stable support for the overall structure, but also provide storage space for electrical components.

[0064] Specifically, a cantilever control box 31 is installed on the frame 3 to facilitate manual operation and equipment debugging.

[0065] The first installation component drives the cabin 1 to rotate along its own axis and position it at a preset angle, and sets the operating end of the flaring mechanism directly below the protective sleeve 2. By inserting the operating end into the opening of the protective sleeve 2, not only can the flaring action of the protective sleeve 2 be realized, but the protective sleeve 2 can also be accurately positioned at the same time to ensure the concentricity of the protective sleeve 2 and the cabin 1, which is convenient for subsequent accurate installation.

[0066] In one embodiment, the cabin 1 is configured as an irregular conical hollow structure, and the protective sleeve 2 is configured as an irregular cone with the same shape as the cabin 1;

[0067] Each flaring mechanism includes a support plate 9, a support assembly, and at least one flaring assembly, wherein:

[0068] The protective sleeve 2 is set on the support plate 9 along the first horizontal direction with the opening facing downward. The fixed end of the flaring assembly is set on the support plate 9, and the operating end of the flaring assembly faces upward, passes through the support plate 9, and extends into the opening. The flaring assembly is configured to enlarge the opening.

[0069] The support assembly is disposed on the upper surface of the support plate 9 and is configured to provide stable support for the protective sleeve 2 on the support plate 9.

[0070] Specifically, each flaring mechanism includes two flaring components spaced apart along the first horizontal direction, further improving the stability and efficiency of the flaring operation.

[0071] Specifically, the support components include two along the second horizontal direction ( Figure 1 Support blocks 10 are spaced apart in the Y direction. Each support block 10 has an inclined support surface, which is inclined upward away from the opposite support block.

[0072] Specifically, the first horizontal direction is perpendicular to the second horizontal direction.

[0073] Through the cooperation of the support plate 9, the support assembly and the flaring mechanism, the protective sleeve 2 is provided with stable support, while the operating end of the flaring assembly acts directly on the edge of the opening, ensuring that the flaring direction is consistent with the opening extension direction, and avoiding deformation of the protective sleeve 2 caused by flaring offset.

[0074] In one embodiment, the assembly system for the hull and protective sleeve further includes a detection mechanism and at least one adjustment mechanism, wherein:

[0075] The detection mechanism is located on one side of the protective sleeve 2 extending along the first horizontal direction. The detection mechanism can move back and forth along the first horizontal direction. The detection mechanism is configured to detect the in-situ status of the chamber 1 and the protective sleeve 2 and transmit the deviation data information to the adjustment mechanism.

[0076] Each adjustment mechanism corresponds to a flaring mechanism. The adjustment mechanism is set on the first slide 7 and is connected to the support plate 9. The adjustment mechanism is configured to receive information from the testing agency and adjust the concentricity of the protective sleeve 2 and the cabin 1 through the support plate 9.

[0077] Specifically, a third slide 37 is provided on the frame 3. The third slide 37 can slide back and forth along the first horizontal direction, and the third slide 37 and the second slide 32 are spaced apart along the first horizontal direction.

[0078] Specifically, the detection mechanism includes a robotic arm 33, a sixth drive assembly 34, and a binocular camera 36. The sixth drive assembly 34 drives the third slide 37 to slide back and forth in the horizontal direction. The fixed end of the robotic arm 33 is set on the third slide 37, and the execution end of the robotic arm 33 is connected to the binocular camera 36. The binocular camera 36 is used to scan the cabin 1 and the protective cover 2, obtain the position coordinates, and transmit them to the control mechanism.

[0079] Specifically, the sixth drive component 34 is a linear module composed of a motor and a ball screw linear transmission pair.

[0080] Specifically, the assembly system for the cabin and protective casing includes two adjustment mechanisms.

[0081] By setting up a movable detection mechanism, the relative position information of the cabin 1 and the protective sleeve 2 is obtained in real time through scanning. The concentricity deviation is converted into quantitative data. The attitude adjustment mechanism receives the detection data and corrects the attitude of the protective sleeve 2 in real time, ensuring the stability of the protective sleeve 2 and the cabin 1 during the installation process.

[0082] In one embodiment, the flaring assembly includes a third drive assembly 20, a connecting plate, two baffles 26, a first gripper 25, a second gripper 24, and a transmission assembly, wherein:

[0083] Two baffles 26 are parallel and spaced apart along the first horizontal direction on the bottom surface of the support plate, a connecting plate is arranged at the bottom end of the two baffles 26 along the horizontal direction, and the first gripper 25 and the second gripper 24 are spaced apart between the two baffles 26 along the second horizontal direction.

[0084] The fixed end of the third drive assembly 20 is disposed on the connecting plate, and the drive end of the third drive assembly 20 is connected to the first gripper 25 and / or the second gripper 24. The third drive assembly 20 is configured to drive the first gripper 25 and / or the second gripper 24 to move closer to or further away from each other.

[0085] Specifically, the first horizontal direction is perpendicular to the second horizontal direction.

[0086] Specifically, the drive end of the third drive component 20 is connected to the first gripper 25 and the second gripper 24, and the third drive component 20 is configured to drive the first gripper 25 and the second gripper 24 to move closer to or further away from each other.

[0087] Specifically, the third drive component 20 is configured as the first cylinder, with the extension rod of the first cylinder facing upwards.

[0088] Specifically, the transmission assembly includes a lifting rod 21, a first connecting rod 22, a second connecting rod, a first hinge rod 23, and a second hinge rod, wherein:

[0089] The telescopic end of the first cylinder is connected to the lifting rod 21. The first connecting rod 22 and the second connecting rod are spaced apart along the second horizontal direction. Both the first connecting rod 22 and the second connecting rod are inclined outward. The bottom end of the first connecting rod 22 is hinged to the lifting rod 21. The top end of the first connecting rod 22 is hinged to the first end of the first hinge rod 23. The second end of the first hinge rod 23 is fixedly connected to the first gripper 25.

[0090] The first hinge rod 23 and the second hinge rod are spaced apart along the second horizontal direction. The bottom end of the second connecting rod is hinged to the lifting rod 21, the top end of the second connecting rod is hinged to the first end of the second hinge rod, and the second end of the second hinge rod is fixedly connected to the second gripper 24. The first gripper 25 and the second gripper 24 are staggered, and the corresponding hinge shafts all extend along the first horizontal direction, providing a transmission component with a simple structure and a high transmission ratio.

[0091] The first gripper 25 and the second gripper 24 are directly driven by the third drive component 20 to move closer or further apart, thereby achieving precise control of the flaring amplitude. At the same time, the structure is simple and the layout is compact, which improves the space utilization of the mechanism.

[0092] In one embodiment, the adjustment mechanism includes two sets of adjustment components, which are spaced apart below the support plate 9 along a second horizontal direction. Each set of adjustment components includes a second drive member 14, a first mounting plate 12, and a second mounting plate 17, wherein:

[0093] The second mounting plate 17 is located directly below the first mounting plate 12. The first mounting plate 12 is hinged to the support plate 9 via a first hinge shaft 11, which extends along a first horizontal direction.

[0094] The fixed end of the second driving member 14 is disposed on the second mounting plate 17, and the driving end of the second driving member 14 is connected to the first mounting plate 12. The second driving member 14 is configured to drive the second mounting plate 17 to rise and fall.

[0095] Specifically, the second driving component 14 is configured as a second cylinder, with the extension rod of the second cylinder facing upwards.

[0096] Specifically, the first slide 7 is provided with a clearance hole, and the bottom of the second cylinder passes through the clearance hole.

[0097] Through the cooperation of the second drive component 14, the first mounting plate 12 and the second mounting plate 17, the protective sleeve 2 can rotate slightly around a specific direction, improving the angle adjustment accuracy, thereby ensuring the concentricity of the cabin 1 and the protective sleeve 2.

[0098] In one embodiment, the adjustment assembly further includes a third mounting plate 19 and a second hinge shaft 18. The third mounting plate 19 is disposed directly below the second mounting plate 17 and is hinged to the bottom surface of the second mounting plate 17 via the second hinge shaft 18, which extends along a first horizontal direction.

[0099] Specifically, the third mounting plate 19 is fixedly mounted on the first slide 7.

[0100] By setting the second hinge shaft 18 and the third mounting plate 19, the second mounting plate 17 can rotate around a specific direction. Combined with the rotation function of the first hinge shaft 11, the posture adjustment of the protective sleeve 2 in multiple vertical planes is realized, further increasing the accuracy of the adjustment of the protective sleeve 2.

[0101] In one embodiment, the adjusting assembly further includes at least one set of guide components, each set of guide components including a guide rod 13 and a guide cylinder 15, wherein:

[0102] The second mounting plate 17 has a through hole, the guide cylinder 15 is arranged vertically in the through hole, and the first end of the guide rod 13 along its own length is fixedly installed on the bottom surface of the first mounting plate 12. The guide rod 13 is movably inserted into the guide cylinder 15.

[0103] Specifically, the adjustment assembly includes two sets of guide components spaced apart along a first horizontal direction.

[0104] The guide rod 13 and the guide cylinder 15 work together to limit the movement trajectory of the second mounting plate 17 relative to the first mounting plate 12, ensuring the smoothness of the guide sleeve angle adjustment process.

[0105] In one embodiment, the adjustment assembly further includes two sets of first limiting components, which are disposed on both sides of the protective sleeve 2 extending along a first horizontal direction. Each set of first limiting components includes a support column 28, a fourth driving member 27, and a push plate 30. The support column 28 is disposed vertically on the first slide table 7. The fixed end of the fourth driving member 27 is disposed on the support column 28. The driving end of the fourth driving member 27 is connected to the push plate 30. The push plate 30 is disposed close to the protective sleeve 2. The fourth driving member 27 is configured to drive the baffle 26 to move closer to or further away from the protective sleeve 2 along a second horizontal direction.

[0106] Specifically, the fourth drive component 27 is configured as the third cylinder, and the extension rod of the third cylinder is directed toward the protective sleeve 2 along the second horizontal direction.

[0107] Specifically, the telescopic rod of the third cylinder is connected to the push plate 30 via a universal damping ball joint 29, so that the push plate 30 can adaptively adjust its direction.

[0108] The cooperation of the support column 28, the fourth drive component 27 and the push plate 30 provides a first limiting component with a simple structure and stable support, which further ensures the stability of the protective sleeve 2 in the second horizontal direction.

[0109] In one embodiment, the assembly system of the cabin and the protective sleeve further includes a fifth drive assembly 38, a second slide 32 and an adhesive application mechanism. The second slide 32 is disposed on the frame 3 and located on the side of the first slide 7 extending along the first horizontal direction. The adhesive application structure is disposed on the first side of the cabin 1 extending along the first horizontal direction. The adhesive application mechanism is mounted on the second slide 32 and is configured to apply adhesive to the surface of the cabin 1. The adhesive application mechanism and the detection mechanism are spaced apart along the first horizontal direction.

[0110] The fixed end of the fifth drive assembly 38 is mounted on the frame 3, and the drive end of the fifth drive assembly 38 is connected to the second slide 32. The fifth drive assembly 38 is configured to drive the second slide 32 to reciprocate along the first horizontal direction.

[0111] Specifically, the fifth drive component 38 is a linear module composed of a motor and a ball screw linear transmission pair.

[0112] Specifically, the glue application mechanism includes a robotic arm 33 and a screw glue feeder 35. The fixed end of the robotic arm 33 is mounted on the second slide table 32, and the execution end of the robotic arm 33 is connected to the screw glue feeder 35. The screw glue feeder 35 is used to apply glue to the outer surface of the cabin 1.

[0113] The fifth drive component 38 drives the second slide 32 to move the glue application mechanism along a preset trajectory, replacing manual brushing, achieving precise control of the glue application trajectory, avoiding problems such as missed coating and uneven thickness, ensuring consistent glue application quality, and improving overall production efficiency.

[0114] An assembly method, implemented through the aforementioned assembly system for the cabin and protective sleeve, for the precise installation of the cabin 1 and the protective sleeve 2, includes the following steps:

[0115] The cabin 1 is installed on the first mounting assembly along the first horizontal direction. The first mounting assembly drives the cabin 1 to rotate along its own axis and position it at a preset angle. At the same time, the protective sleeve 2 is placed on the support plate 9 along the first horizontal direction with the opening facing down. The tops of the first claw 25 and the second claw 24 pass through the opening.

[0116] The detection mechanism moves back and forth along the first horizontal direction to detect the in-situ status and relative position of the detection chamber 1 and the protective sleeve 2, generate concentricity deviation data and transmit it to the control mechanism;

[0117] The control mechanism controls the adjustment mechanism to work, and drives the second mounting plate 17 to rise and fall through the corresponding second driving component 14. Combined with the first hinge shaft 11 driving the first mounting plate 12 to rotate relative to the support plate 9, and the second hinge shaft 18 driving the second mounting plate 17 to rotate relative to the third mounting plate 19, the support plate 9 is adjusted in spatial posture to ensure that the protective sleeve 2 and the cabin 1 are precisely coaxially set.

[0118] The third drive assembly 20 drives the first gripper 25 and the second gripper 24 to move away from each other in the second horizontal direction through the transmission assembly, so as to expand the opening and diameter of the protective sleeve 2 and adapt to the suit size of the cabin 1.

[0119] The fifth drive assembly 38 drives the second slide 32 to move along the first horizontal direction, thereby driving the glue application mechanism to apply glue evenly along the preset trajectory on the surface of the cabin 1.

[0120] The first drive assembly drives the first slide 7 to move closer to the cabin 1 along the first horizontal direction, so as to synchronously drive the protective sleeve 2 to move closer to the cabin 1 until the protective sleeve 2 fits and is placed on the outside of the cabin 1.

[0121] The above embodiments merely illustrate the basic principles and characteristics of this application. This application is not limited to the above examples. Various changes and modifications can be made to this application without departing from the spirit and scope thereof, and all such changes and modifications fall within the scope of this application as claimed. The scope of protection of this application is defined by the appended claims and their equivalents.

Claims

1. A system for assembling a pod and a protective cover, the system comprising: The cabin and the protective sleeve assembly system comprises a rack, a cabin, a protective sleeve, a first mounting assembly, a first driving assembly and at least one flaring mechanism, wherein: The first mounting assembly is arranged at one end of the rack along a first horizontal direction, the cabin is arranged on the first mounting assembly along the first horizontal direction, the cabin is rotatably arranged on the first mounting assembly along its axis direction, and the first mounting assembly is configured to support and rotate the cabin to a preset angle; The protective sleeve is arranged corresponding to the cabin along the first horizontal direction, and the protective sleeve is arranged on the cabin in a sleeved manner, the protective sleeve is provided with an opening extending along its length direction, and the opening faces downward; The rack is provided with a first sliding table, the flaring mechanism is arranged on the first sliding table and is arranged spaced apart from the first mounting assembly along the first horizontal direction, the operating end of the flaring mechanism is arranged directly below the cabin along its axis direction, the protective sleeve is arranged on the flaring mechanism along the first horizontal direction, and the flaring mechanism is configured to expand the diameter of the protective sleeve through the opening; The fixed end of the first driving assembly is arranged on the rack, the driving end of the first driving assembly is connected to the first sliding table, and the first driving assembly is configured to drive the first sliding table to reciprocate along the first horizontal direction.

2. The pod and shroud assembly of claim 1, wherein, The cabin is arranged as an irregular conical hollow structure, and the protective sleeve is arranged as an irregular conical body with the same shape as the cabin; Each group of the flaring mechanism comprises a support plate, a support assembly and at least one flaring assembly, wherein: The protective sleeve is arranged on the support plate along the first horizontal direction and the opening faces downward, the fixed end of the flaring assembly is arranged on the support plate, the operating end of the flaring assembly penetrates through the support plate and extends into the opening, and the flaring assembly is configured to expand the opening; The support assembly is arranged on the upper surface of the support plate, and the support assembly is configured to stably support the protective sleeve on the support plate.

3. The pod and shroud assembly of claim 2, wherein, The cabin and the protective sleeve assembly system further comprises a detection mechanism and at least one adjustment mechanism, wherein: The detection mechanism is arranged on one side of the protective sleeve extending along the first horizontal direction, the detection mechanism can reciprocate along the first horizontal direction, and the detection mechanism is configured to detect the in-place state of the cabin and the protective sleeve and transmit deviation data information to the adjustment mechanism; Each adjustment mechanism is arranged corresponding to one flaring mechanism, the adjustment mechanism is arranged on the first sliding table, the adjustment mechanism is connected with the support plate, and the adjustment mechanism is configured to accept the information of the detection mechanism and adjust the concentricity of the protective sleeve and the cabin through the support plate.

4. The pod and shroud assembly system of claim 3, wherein, The flaring assembly comprises a third driving assembly, a connecting plate, two baffles, a first clamping jaw, a second clamping jaw and a transmission assembly, wherein: Two baffles are arranged in parallel and spaced apart along a first horizontal direction on the bottom surface of the support plate, and the connecting plate is arranged at the bottom end of the two baffles along the horizontal direction. The fixed end of the third driving assembly is arranged on the connecting plate, and the driving end of the third driving assembly is connected to the first clamping jaw and / or the second clamping jaw. The third driving assembly is configured to drive the first clamping jaw and / or the second clamping jaw to move closer to or away from each other.

5. The pod and shroud assembly of claim 4, wherein, The funding mechanism includes two sets of adjustment assemblies, and each set of adjustment assembly is arranged below the support plate along the second horizontal direction. Each set of adjustment assembly includes a second driving member, a first mounting plate and a second mounting plate. The second mounting plate is located directly below the first mounting plate, and the first mounting plate is hingedly connected to the support plate through a first hinge shaft extending along the first horizontal direction. The fixed end of the second driving member is arranged on the second mounting plate, and the driving end of the second driving member is connected to the first mounting plate. The second driving member is configured to drive the second mounting plate to move up and down.

6. The pod and shroud assembly system of claim 5, wherein, The adjustment assembly further includes a third mounting plate and a second hinge shaft. The third mounting plate is arranged directly below the second mounting plate, and the third mounting plate is hingedly connected to the bottom surface of the second mounting plate through the second hinge shaft extending along the first horizontal direction.

7. The pod and boot assembly of claim 5, wherein, The adjustment assembly further includes at least one set of guide assembly, and each set of guide assembly includes a guide rod and a guide cylinder. The second mounting plate is provided with a through hole, and the guide cylinder is arranged in the through hole in a vertical direction. The first end of the guide rod along the length direction of the guide rod is fixedly installed on the bottom surface of the first mounting plate, and the guide rod is movably arranged in the guide cylinder.

8. The pod and boot assembly of claim 5, wherein, The adjustment assembly further includes two sets of first limiting assemblies. Each set of first limiting assembly is arranged on both sides of the protective sleeve extending along the first horizontal direction. Each set of first limiting assembly includes a support column, a fourth driving member and a push plate. The support column is arranged on the first sliding table in a vertical direction. The fixed end of the fourth driving member is arranged on the support column, and the driving end of the fourth driving member is connected to the push plate. The push plate is arranged close to the protective sleeve. The fourth driving member is configured to drive the baffles to move closer to or away from the protective sleeve along the second horizontal direction.

9. The pod and boot assembly of claim 3, wherein, The assembly system of the cabin and the protective sleeve further includes a fifth driving assembly, a second sliding table and a gluing mechanism. The second sliding table is arranged on the rack and located on one side of the first sliding table extending along the first horizontal direction. The gluing mechanism is arranged on the second sliding table. The gluing mechanism is configured to glue the surface of the cabin. The gluing mechanism and the detection mechanism are arranged spaced apart along the first horizontal direction. The fixed end of the fifth driving assembly is arranged on the rack, and the driving end of the fifth driving assembly is connected with the second sliding table. The fifth driving assembly is configured to drive the second sliding table to reciprocate along the first horizontal direction.

10. A method of assembly, characterized by, The assembly method is implemented by the assembly system of the cabin and the protective sleeve according to the cabin and the protective sleeve in claims 1-9, and is used for accurate installation of the cabin and the protective sleeve, and comprises the following steps: The cabin is installed on the first installation assembly along the first horizontal direction, the cabin is driven to rotate along the axis thereof to a preset angle by the first installation assembly, and the protective sleeve is placed on the support plate along the first horizontal direction with the opening downward and the top ends of the first clamping jaw and the second clamping jaw penetrating through the opening. The detection mechanism reciprocates along the first horizontal direction to detect the in-situ state and relative position of the cabin and the protective sleeve, generates concentricity deviation data and transmits the data to the control mechanism. The control mechanism controls the adjustment mechanism to work, drives the second installation plate to ascend and descend by the corresponding second driving member, drives the first installation plate to rotate relative to the support plate by the first hinged shaft, drives the second installation plate to rotate relative to the third installation plate by the second hinged shaft, and further drives the support plate to adjust the spatial posture, so as to ensure that the protective sleeve and the cabin are accurately coaxially arranged. The third driving assembly drives the first clamping jaw and the second clamping jaw to move away from each other along the second horizontal direction by the transmission assembly, so as to expand the opening and diameter of the protective sleeve and adapt the size of the cabin. The fifth driving assembly drives the second sliding table to move along the first horizontal direction, and drives the gluing mechanism to uniformly glue along the preset track of the cabin surface. The first driving assembly drives the first sliding table to move along the first horizontal direction and close to the cabin, so as to synchronously drive the protective sleeve to close to the cabin until the protective sleeve is attached and sleeved outside the cabin.

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