CN117697370A - High-automation cabin butt joint device - Google Patents
High-automation cabin butt joint device Download PDFInfo
- Publication number
- CN117697370A CN117697370A CN202410160438.XA CN202410160438A CN117697370A CN 117697370 A CN117697370 A CN 117697370A CN 202410160438 A CN202410160438 A CN 202410160438A CN 117697370 A CN117697370 A CN 117697370A
- Authority
- CN
- China
- Prior art keywords
- docking
- ring
- station
- cabin
- frame body
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 210000001503 joint Anatomy 0.000 title claims abstract description 13
- 238000003032 molecular docking Methods 0.000 claims abstract description 152
- 230000007246 mechanism Effects 0.000 claims abstract description 63
- 238000010586 diagram Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
Landscapes
- Automatic Assembly (AREA)
Abstract
The invention provides a high-automation cabin docking device, which relates to the technical field of aerospace and comprises a frame body, a docking mechanism and a driving mechanism, wherein the frame body is provided with two support columns, a docking ring is arranged between the two support columns by the docking mechanism, the docking ring is provided with a first axis, the docking mechanism is provided with a first station and a second station, when the docking mechanism is positioned at the first station, the extending direction of the first axis is in a vertical direction, when the docking mechanism is positioned at the second station, the extending direction of the first axis is in a horizontal direction, when the docking mechanism is positioned at the first station, the docking mechanism is hung up and vertically placed at the top of an inventory cabin of a warehouse and placed in the docking ring to finish the receiving of the inventory cabin, and when the docking mechanism is switched from the first station to the second station, the docking ring drives the inventory cabin to be positioned horizontally and can be docked with a fixed cabin; compared with the prior art, the invention does not need to lift the two ends of the stock cabin section to be placed on the circular arc-shaped supporting plate after being horizontally placed, and only the top end of the stock cabin section is lifted, so that the efficiency of cabin section butt joint is improved.
Description
Technical Field
The invention relates to the technical field of aerospace, in particular to a high-automation cabin butt joint device.
Background
In the aerospace field, along with the rapid development of automatic manufacturing and assembling technology in China, the automatic assembling and docking technology of a cabin is taken as one of key technologies, when cabin products are assembled, the cabin needs to be taken out of a warehouse, transported to a fixed cabin, docked with the transported cabin, and the fixed cabin is horizontally fixed, so that the existing transportation and docking device is mainly provided with an upward arc-shaped supporting plate, the cabin is fixed in an opening mode, the cabin is guaranteed to be kept in a stable horizontal state during transportation and docking, and during actual assembly, the cabin in the warehouse is vertically placed for storage, so that when the cabin is transported, the top end of the cabin needs to be lifted, the bottom end of the cabin is lifted, and then the cabin is placed on the arc-shaped supporting plate of a transportation device after being adjusted to be horizontal, and is transported.
In the prior art, in the transportation process of the stock cabin, the stock cabin needs to be lifted, and the installation and the release of the lifting appliance need to be manually participated, so that the overall efficiency of transportation and butt joint is reduced.
Disclosure of Invention
In view of the foregoing drawbacks or shortcomings of the prior art, the present invention is directed to a highly automated bay docking device for docking an inventory bay with a fixed bay, the fixed bay having an axis in a first direction, comprising:
the frame body comprises two support columns distributed and arranged along a second direction, a first space is formed between the two support columns, and the second direction is perpendicular to the first direction;
the docking mechanism comprises a docking ring, the docking ring is arranged in the first space, two ends of the docking ring along the second direction are respectively connected with the support columns, the docking ring is provided with a first axis, the docking mechanism is provided with a first station and a second station, when the docking mechanism is positioned at the first station, the extension direction of the first axis is a third direction, the third direction is perpendicular to the second direction and the first direction, and the first station is used for receiving the inventory cabin section; when the first station is positioned at the second station, the extension direction of the first axis is the first direction; the second station is used for butting the stock cabin section placed in the butting ring with the fixed cabin section;
the driving mechanism is used for switching the docking mechanism between the first station and the second station.
According to the technical scheme provided by the embodiment of the invention, the docking mechanism further comprises an angle adjusting assembly arranged in the first space and used for driving the docking ring and the inventory cabin to rotate by taking the first axis as the center when the docking mechanism is positioned at the second station.
According to the technical scheme provided by the embodiment of the invention, the angle adjusting assembly comprises the first ring body which is arranged outside the docking ring and is coaxially arranged with the docking ring, a first power part is arranged on the side, away from the docking ring, of the first ring body, and the first power part drives the first ring body to rotate by taking the first axis as the center so as to drive the docking ring and the inventory cabin section to synchronously rotate.
According to the technical scheme provided by the embodiment of the invention, the driving mechanism comprises a first driving assembly arranged on the supporting column, the first driving assembly comprises two connecting shafts arranged on two sides of the first ring body along the second direction, the direction of the extension line of the axis of the connecting shafts is the second direction, and the first driving assembly is used for driving the docking ring to rotate by taking the axis of the connecting shafts as the center.
According to the technical scheme provided by the embodiment of the invention, the first driving assembly further comprises two shaft seats sleeved outside the connecting shafts, the two shaft seats are respectively arranged on one sides of the corresponding support columns, a third motor is arranged on one side of the shaft seats, and the third motor drives each connecting shaft to rotate.
According to the technical scheme provided by the embodiment of the invention, the docking mechanism further comprises a height adjusting assembly arranged on the supporting column and used for adjusting the docking ring and the inventory cabin section to move along the third direction when the docking mechanism is in the second station.
According to the technical scheme provided by the embodiment of the invention, the height adjusting assembly comprises a sliding block connected with the shaft seat and a second power part arranged on the supporting column, wherein the second power part is used for driving the sliding block to move along the third direction and driving the angle adjusting assembly, the docking ring and the inventory cabin section to synchronously move.
According to the technical scheme provided by the embodiment of the invention, the frame body further comprises a first rectangular frame body arranged at the bottom ends of the two support columns and a second rectangular frame body arranged at the first rectangular frame body and far away from the support column ends, and a leveling assembly is arranged between the first rectangular frame body and the second rectangular frame body and used for limiting the extension direction of the support columns to be the third direction.
According to the technical scheme provided by the embodiment of the invention, the leveling assembly comprises four first studs in threaded connection with the first rectangular frame body, each first stud is respectively arranged at the bottom ends of four corners of the first rectangular frame body, each first stud is far away from the first rectangular frame body end and is in threaded connection with the second rectangular frame body, the direction of the axis extension line of each first stud is the third direction, and when the first stud rotates, the first rectangular frame body and the second rectangular frame body are driven to be far away from or close to each other.
According to the technical scheme provided by the embodiment of the invention, the driving mechanism comprises a second driving assembly arranged at the bottom end of the second rectangular frame body and used for driving the frame body to move on a first plane, and the first plane is perpendicular to the third direction.
In summary, the invention provides a high-automation cabin docking device, which comprises a frame body, a docking mechanism and a driving mechanism, wherein the frame body is provided with two support columns, the docking mechanism is provided with a docking ring between the two support columns, the docking ring is provided with a first axis, the docking mechanism is provided with a first station and a second station, when the docking mechanism is positioned at the first station, the extending direction of the first axis is in a vertical direction, when the docking mechanism is positioned at the second station, the extending direction of the first axis is in a horizontal direction, when the docking mechanism is positioned at the first station, the docking mechanism is lifted and vertically placed at the top of an inventory cabin of a warehouse and placed in the docking ring, so that the inventory cabin is completed, and when the docking mechanism is switched from the first station to the second station, the docking ring drives the inventory cabin to be positioned horizontally and can be docked with a fixed cabin; compared with the prior art, the invention has the advantages that the two ends of the stock cabin section are not required to be lifted to be placed on the circular arc-shaped supporting plate after being horizontally placed, only the top end of the stock cabin section is required to be lifted, the time for manually installing and dismantling the lifting appliance is reduced, and the butt joint efficiency of the cabin section is improved.
Drawings
Fig. 1 is a schematic structural diagram of a high automation cabin docking device according to an embodiment of the present invention;
FIG. 2 is a partially enlarged schematic illustration of region B of FIG. 1;
FIG. 3 is an enlarged schematic view of a portion of the area A of FIG. 1;
fig. 4 is a schematic structural diagram of pins and tooth grooves of a high-automation cabin butt joint device according to an embodiment of the present invention;
fig. 5 is a schematic structural diagram of a first ring body and a second ring body of a high-automation cabin docking device according to an embodiment of the present invention;
FIG. 6 is a schematic structural view of a slider and an extension portion of a high automation bay docking device according to an embodiment of the present invention;
fig. 7 is a schematic structural diagram of a second motor and a screw rod of a high-automation cabin docking device according to an embodiment of the present invention;
fig. 8 is a schematic structural diagram of a leveling assembly of a high automation cabin docking device according to an embodiment of the present invention.
The text labels in the figures are expressed as:
1. a frame body; 11. a support column; 12. a first rectangular frame; 13. a second rectangular frame; 14. cross ribs;
2. a leveling assembly; 21. a first nut; 22. a second nut; 23. a first stud; 24. screwing the block;
3. a docking mechanism; 31. a docking collar; 32. locking the screw hole; 33. a second stud; 34. lengthening the sleeve;
4. an angle adjustment assembly; 41. a first ring body; 42. a second ring body; 43. a first bearing; 44. a first motor; 45. a first disc; 46. a pin; 47. a second disc; 48. tooth slots;
5. a height adjustment assembly; 51. a second motor; 52. a screw rod; 53. a slide block; 54. an extension; 55. a screw nut; 56. a limit groove;
6. a first drive assembly; 61. a connecting shaft; 62. a shaft seat; 63. a third motor; 64. a second bearing;
7. a second drive assembly; 71. a first nalm wheel; 72. and a second Nahm wheel.
Detailed Description
The invention is described in further detail below with reference to the drawings and examples. It is to be understood that the specific embodiments described herein are merely illustrative of the invention and are not limiting of the invention. It should be noted that, for convenience of description, only the portions related to the invention are shown in the drawings.
It should be noted that, without conflict, the embodiments of the present invention and features of the embodiments may be combined with each other. The invention will be described in detail below with reference to the drawings in connection with embodiments.
As mentioned in the background art, to the problems in the prior art, a high automation cabin section interfacing apparatus for stock cabin section and fixed cabin section butt joint, the axis direction of fixed cabin section is first direction, wherein, first direction is fore-and-aft direction, includes:
the frame body 1, wherein the frame body 1 comprises two support columns 11 distributed and arranged along a second direction, a first space is formed between the two support columns 11, the second direction is perpendicular to the first direction, and the second direction is a left-right direction;
the docking mechanism 3, the docking mechanism 3 includes a docking ring 31, the docking ring 31 is disposed in the first space, two ends along the second direction are respectively connected with the support columns 11, the docking ring 31 has a first axis, the docking mechanism 3 has a first station and a second station, when the docking mechanism is located at the first station, an extension direction of the first axis is a third direction, the third direction is perpendicular to the second direction and the first direction, and the first station is used for receiving the inventory cabin; when the first station is positioned at the second station, the extension direction of the first axis is the first direction; the second station is used for docking the stock cabin section placed in the docking ring 31 with the fixed cabin section; the third direction is a vertical direction, and the stock cabin is also vertically placed when being stored, so when the docking mechanism 3 is at the first station, the top of the stock cabin is lifted and placed in the docking ring 31, and then the stock cabin is fixed, thereby completing the purpose of receiving the stock cabin, optionally, as shown in fig. 5, the docking ring 31 has an L-shaped cross section, a plurality of locking screw holes 32 are circumferentially distributed in an array on the side wall attached to the stock cabin, each locking screw hole 32 is internally and spirally connected with a second stud 33, and one end of each second stud 33 is rotated to be abutted against the outer wall of the stock cabin, thereby guaranteeing the stability of the stock cabin after being received; in addition, after the first axis is adjusted to be in a horizontal state, the stock cabin section is also adjusted to be in a horizontal state and can be in butt joint with the fixed cabin section;
the driving mechanism is used for switching the docking mechanism 3 between the first station and the second station, wherein the driving mechanism has a function of driving the docking ring 31 to rotate and adjust, so that the docking ring 31 swings from a vertical state to a horizontal state, the first axis is further adjusted from the vertical direction to the front-back direction, the storage cabin section swings to the horizontal state along with the docking ring 31 after being received, and the driving mechanism also has a function of moving the docking device from a warehouse to a docking site, so that the stock cabin section is received from the warehouse and is moved to the docking site to finish docking;
as shown in fig. 1, in the use process, when the docking mechanism 3 is at the first station, the docking ring 31 drives the stock cabin to be placed horizontally and can dock with the fixed cabin by lifting the top of the stock cabin vertically placed in the warehouse and placing the stock cabin into the docking ring 31, so that the stock cabin is received; compared with the prior art, the invention has the advantages that the two ends of the stock cabin section are not required to be lifted to be placed on the circular arc-shaped supporting plate after being horizontally placed, only the top end of the stock cabin section is required to be lifted, the time for manually installing and detaching the lifting appliance is reduced, and the butt joint efficiency of the cabin section is improved.
In a preferred embodiment, the docking mechanism 3 further includes an angle adjustment assembly 4 disposed in the first space for driving the docking ring 31 and the inventory bay to rotate about the first axis when the docking mechanism 3 is in the second position;
as shown in fig. 1 and fig. 5, the angle adjusting assembly 4 rotates the stock cabin segment to enable the connecting piece on the stock cabin segment to be overlapped with the connecting piece on the fixed cabin segment, after the connecting pieces of the stock cabin segment and the fixed cabin segment are fixed, the butt joint is completed, the butt joint ring 31 is released from fixing the stock cabin segment, and the stock cabin segment can be switched back to the first station.
In a preferred embodiment, the angle adjusting assembly 4 includes a first ring body 41 disposed outside the docking ring 31 and coaxially disposed with the docking ring 31, a first power portion is disposed on a side of the first ring body 41 away from the docking ring 31, and the first power portion drives the first ring body 41 to rotate around a first axis, so as to drive the docking ring 31 and the inventory cabin to rotate synchronously;
as shown in fig. 3, fig. 4 and fig. 5, a plurality of circumferentially arrayed tooth grooves 48 are formed in the edge of the first ring body 41, a second ring body 42 is coaxially arranged on the side, away from the docking ring 31, of the first ring body 41 through a first bearing 43, the first power part comprises a first motor 44 arranged on the second ring body 42, a first disc 45 is sleeved outside an output shaft of the first motor 44, a plurality of circumferentially arrayed pins 46 are arranged at the end, away from the first motor 44, of the first disc 45, the first motor 44 can drive the first disc 45 to rotate, and drives each pin 46 to rotate around the axis of the first disc 45, and each pin 46 is meshed with the tooth groove 48 in the rotation process of each pin 46 to drive the first ring body 41 to rotate, wherein the cross section of each pin 46 is circular, so that the pins can be fully attached to the tooth grooves 48, the back clearance in meshing process is reduced, the rotation angle of the first ring body 41 is higher in precision, in addition, each pin 46 is provided with a second disc 45 at the end, and the pins 46 are further connected with the second disc 47 in a stable manner; optionally, the first bearing 43 is a crossed roller bearing, and the crossed roller bearing has an inner ring, an outer ring and crossed rollers, the outer ring is connected with the first ring body 41, the inner ring is connected with the second ring body 42, and the first ring body 41 can stably rotate under the drive of the first power part through the crossed rollers; an extension sleeve 34 is arranged in the first ring body 41, and the extension sleeve 34 can increase the contact surface between the docking device and the stock cabin section, so that the unstable condition caused by the contact between the docking ring 31 and the stock cabin section is avoided.
In a preferred embodiment, the driving mechanism includes a first driving assembly 6 disposed on the support column 11, the first driving assembly 6 includes two connecting shafts 61 disposed on two sides of the first ring body 41 along the second direction, an axis extension line direction of the connecting shafts 61 is the second direction, and the first driving assembly 6 is configured to drive the docking ring 31 to rotate about an axis of the connecting shafts 61;
as shown in fig. 5 and 6, when the docking mechanism 3 is at the first station, the docking ring 31 receives the stock cabin, and at this time, the first driving assembly 6 drives the docking ring 31 to rotate around the axis of the connecting shaft 61, so that the first axis is switched from the vertical direction to the front-rear direction, and the docking ring 31 drives the stock cabin to be adjusted to the front-rear direction, so that the stock cabin is convenient to be subsequently docked with the fixed cabin.
In a preferred embodiment, the first driving assembly 6 further includes two shaft seats 62 sleeved outside the connecting shafts 61, the two shaft seats 62 are respectively disposed on one side of the corresponding supporting columns 11, a third motor 63 is disposed on one side of the shaft seats 62, and the third motor 63 drives each connecting shaft 61 to rotate;
as shown in fig. 1, 5 and 6, two connecting shafts 61 are respectively disposed at left and right ends of the second ring 42, the second ring 42 and the first bearing 43 are connected with the first ring 41 through the second ring 42 and the first bearing 43, the third motor 63 drives the connecting shaft 61 to rotate, and under the support of the shaft seat 62, the second ring 42 is driven to rotate around the axis of the connecting shaft 61, and because the second ring 42, the first ring 41 and the docking ring 31 are coaxially disposed, the first axis can be driven to switch in the vertical direction and the front and rear direction, in addition, a second bearing 64 is disposed in the shaft seat 62, the connecting shaft 61 is connected with the shaft seat 62 through the second bearing 64, so as to ensure that the connecting shaft 61 is stably autorotated, and optionally, the second bearing 64 is an angular contact ball bearing, which can bear radial load and axial load simultaneously, can satisfy the axial stress formed by the connecting shaft 61, and can also support the connecting shaft 61 and each component disposed on the connecting shaft 61 to form a higher radial stability.
In a preferred embodiment, the docking mechanism 3 further comprises a height adjustment assembly 5 provided on the support column 11 for adjusting the movement of the docking ring 31 and the inventory bay in the third direction when the docking mechanism 3 is in the second station;
as shown in fig. 1, 6 and 7, before docking, the heights of the docking ring 31 and the inventory cabin segment in the vertical direction need to be adjusted, so that the first axis and the axis of the fixed cabin segment are positioned on the same straight line, thereby facilitating the alignment of the inventory cabin segment with the center of the fixed cabin segment, and further docking is performed after the angle of the inventory cabin segment is adjusted by the angle adjusting component 4.
In a preferred embodiment, the height adjusting assembly 5 includes a slider 53 connected to the axle seat 62, and a second power unit disposed on the support column 11, where the second power unit is configured to drive the slider 53 to move along the third direction, so as to drive the angle adjusting assembly 4, the docking ring 31, and the inventory cabin to move synchronously;
as shown in fig. 5 and fig. 6, the second power portion includes a second motor 51 disposed at the top end of the support column 11, a screw rod 52 is coaxially disposed at an output shaft end of the second motor 51, a screw rod nut 55 is sleeved in the middle of the screw rod 52, a limit groove 56 is disposed on the support column 11 near the side of the slider 53, the slider 53 extends toward the screw rod nut 55 to form an extension portion 54, the extension portion 54 passes through the limit groove 56 and is connected with the screw rod nut 55, and further the second motor 51 drives the screw rod 52 to rotate, the extension portion 54 is acted by the limit groove 56, so that the screw rod nut 55 does not rotate synchronously with the screw rod 52, and then the screw rod nut 55 moves up and down along a vertical direction under the action of threads of the screw rod 52, and drives the slider 53 to move through the extension portion 54, so as to realize a function of adjusting the height of the docking ring 31.
In a preferred embodiment, the frame 1 further includes a first rectangular frame 12 disposed at bottom ends of the two support columns 11, and a second rectangular frame 13 disposed at a position where the first rectangular frame 12 is far away from the support columns 11, and a leveling component 2 is disposed between the first rectangular frame 12 and the second rectangular frame 13, for limiting the extending direction of the support columns 11 to be the third direction;
as shown in fig. 1 and 2, by the leveling assembly 2, it is ensured that the extending direction of the support column 11 is always vertical, so that each mechanism on the support column 11 can adjust the height, angle and axis position of the stock cabin, and the situation that the stock cabin and the docking ring 31 cannot be aligned with the fixed cabin is avoided.
In a preferred embodiment, the leveling assembly 2 includes four first studs 23 screwed to the first rectangular frame 12, each first stud 23 is respectively disposed at four bottom ends of the first rectangular frame 12, each first stud 23 is far away from the end of the first rectangular frame 12 and is screwed to the second rectangular frame 13, the direction of an axis extension line of each first stud 23 is the third direction, and when the first stud 23 rotates, the first rectangular frame 12 and the second rectangular frame 13 are driven to be far away from or close to each other;
as shown in fig. 2, the bottom ends of four corners of the first rectangular frame 12 are provided with first nuts 21, the top ends of four corners of the second rectangular frame 13 are provided with second nuts 22, two ends of the first stud 23 are respectively in threaded connection with the first nuts 21 and the second nuts 22, one of the first studs 23 is rotated, through the action of threads, the angles of the first rectangular frame 12 and the second rectangular frame 13 corresponding to the first stud 23 are mutually far away or close, and further, by adjusting four corners of the first rectangular frame 12, the adjustment of the levelness of the first rectangular frame 12 is realized, in addition, a screwing block 24 is sleeved in the middle of the first stud 23, so that the first stud 23 is convenient to rotate, the first rectangular frame 12 and the second rectangular frame 13 are respectively provided with a through hole, and when the first stud 23 and the first stud 23 are mutually close to each other, two ends of the first stud 23 can stretch into the through holes, the adjustment range is increased, optionally, as shown in fig. 8, the adjustment assembly further comprises the first rectangular frame 12, the first stud 23 is further provided with the first stud 23, and the first stud 23 is accurately arranged at the position, and the first stud 23 is more accurate, and the distance is increased, and the first stud 23 is prevented from being damaged, and the distance is increased.
In a preferred embodiment, the driving mechanism includes a second driving component 7 disposed at the bottom end of the second rectangular frame 13, for driving the frame 1 to move on a first plane, where the first plane is perpendicular to the third direction;
as shown in fig. 1 and 8, the bottom ends of four corners of the second rectangular frame 13 are provided with first nano wheels 71, the characteristics of the nano wheels serving as omni-directional wheels can be used for driving the second rectangular frame 13 to move at multiple angles and zero radius, so that the whole device can be conveniently driven to move from the warehouse to the docking site, the function of receiving the stock cabin from the warehouse and moving to the docking site to complete docking is realized, in addition, the inside of the second rectangular frame 13 is provided with cross ribs 14 for improving the strength of the second rectangular frame 13, and the bottom surface of the second rectangular frame 13 close to the end of the cross ribs 14 and the central bottom surface of the cross ribs 14 are provided with second nano wheels 72 for assisting the movement of the first nano wheels 71, so that a plurality of fulcra with a first plane are provided, the situation that the whole device is easily damaged by supporting the four first nano wheels 71 is avoided, wherein the first plane is the ground formed after concrete pouring;
when the docking device is used, the docking mechanism 3 is at the first station, the docking ring 31 is vertically upwards, the in-warehouse hoisting tool is started, the vertically placed stock cabin section is vertically hoisted, the axis of the stock cabin section is moved to be positioned on the same line with the first axis, the stock cabin section is lowered into the docking ring 31, the second stud 33 is screwed to enable the second stud 33 to abut against and fix the stock cabin section, the stock cabin section is further completed to be received, when the docking mechanism 3 is switched from the first station to the second station, the second driving assembly 7 of the driving mechanism firstly moves along the ground through the first Nam wheel 71 and the second Nam wheel 72, the whole docking device is moved from the warehouse to the docking site, then, the first driving assembly 6 drives the docking ring 31 and the stock cabin section to rotate by the connecting shaft 61 under the driving of the third motor 63, the first axis is rotated to the front-rear direction from the vertical direction, the first axis and the fixed cabin section are in the front-rear direction, and then the second station is reached, at this time, the heights of the docking ring 31 and the stock cabin section in the vertical direction are adjusted and adjusted by the height adjusting assembly 5, so that the axes of the first axis and the fixed cabin section are positioned on the same straight line, and then the angle adjusting assembly 4 rotates the docking ring 31 and the stock cabin section, so that the connecting piece on the stock cabin section coincides with the connecting piece on the fixed cabin section, and the docking is completed after the connecting pieces of the docking ring and the stock cabin section are fixed.
The principles and embodiments of the present invention have been described herein with reference to specific examples, the description of which is intended only to facilitate an understanding of the method of the present invention and its core ideas. The foregoing is merely illustrative of the preferred embodiments of this invention, and it is noted that there is objectively no limit to the specific structure disclosed herein, since numerous modifications, adaptations and variations can be made by those skilled in the art without departing from the principles of the invention, and the above-described features can be combined in any suitable manner; such modifications, variations and combinations, or the direct application of the inventive concepts and aspects to other applications without modification, are contemplated as falling within the scope of the present invention. The above description is only illustrative of the preferred embodiments of the present invention and of the principles of the technology employed.
Claims (10)
1. A high automation cabin section interfacing apparatus for stock cabin section and fixed cabin section butt joint, the axis direction of fixed cabin section is first direction, its characterized in that includes:
the frame body (1), the frame body (1) comprises two support columns (11) distributed and arranged along a second direction, a first space is formed between the two support columns (11), and the second direction is perpendicular to the first direction;
the docking mechanism (3), the docking mechanism (3) comprises a docking ring (31), the docking ring (31) is arranged in the first space, two ends along the second direction are respectively connected with the support columns (11), the docking ring (31) is provided with a first axis, the docking mechanism (3) is provided with a first station and a second station, when the docking mechanism is positioned at the first station, the extension direction of the first axis is a third direction, the third direction is perpendicular to the second direction and the first direction, and the first station is used for receiving the stock cabin; when the first station is positioned at the second station, the extension direction of the first axis is the first direction; the second station is used for docking the stock cabin section placed in the docking ring (31) with the fixed cabin section;
the driving mechanism is used for switching the docking mechanism (3) between the first station and the second station.
2. The high automation bay docking device of claim 1, wherein the docking mechanism (3) further comprises an angle adjustment assembly (4) disposed within the first space for driving the docking ring (31) and the inventory bay to rotate about the first axis when the docking mechanism (3) is in the second station.
3. The high-automation cabin segment docking device according to claim 2, wherein the angle adjusting assembly (4) comprises a first ring body (41) which is arranged outside the docking ring (31) and is coaxial with the docking ring (31), a first power part is arranged on the side, away from the docking ring (31), of the first ring body (41), and the first power part drives the first ring body (41) to rotate by taking a first axis as a center so as to drive the docking ring (31) and the stock cabin segment to synchronously rotate.
4. A high automation cabin segment docking device according to claim 3, characterized in that the driving mechanism comprises a first driving component (6) arranged on the supporting column (11), the first driving component (6) comprises two connecting shafts (61) arranged on two sides of the first ring body (41) along the second direction, the axis extension line direction of the connecting shafts (61) is the second direction, and the first driving component (6) is used for driving the docking ring (31) to rotate by taking the axis of the connecting shafts (61) as the center.
5. The high automation cabin segment docking device according to claim 4, wherein the first driving assembly (6) further comprises two shaft seats (62) sleeved outside the connecting shafts (61), the two shaft seats (62) are respectively arranged on one side of the corresponding supporting column (11), a third motor (63) is arranged on one side of the shaft seats (62), and the third motor (63) drives each connecting shaft (61) to rotate.
6. The high automation bay docking device of claim 5, wherein the docking mechanism (3) further comprises a height adjustment assembly (5) provided on the support column (11) for adjusting movement of the docking ring (31) and the inventory bay in the third direction when the docking mechanism (3) is in the second station.
7. The high automation class docking device of claim 6, wherein the height adjustment assembly (5) includes a slider (53) coupled to the axle seat (62), and a second power portion disposed on the support post (11) for driving the slider (53) to move in the third direction, driving the angle adjustment assembly (4), the docking ring (31), and the inventory class to move synchronously.
8. The high automation cabin segment docking device according to claim 1, wherein the frame body (1) further comprises a first rectangular frame body (12) arranged at the bottom ends of the two support columns (11), and a second rectangular frame body (13) arranged at the end, far away from the support columns (11), of the first rectangular frame body (12), and a leveling component (2) is arranged between the first rectangular frame body (12) and the second rectangular frame body (13) and used for limiting the extending direction of the support columns (11) to be the third direction.
9. The high automation cabin segment docking device according to claim 8, wherein the leveling assembly (2) comprises four first studs (23) in threaded connection with the first rectangular frame body (12), each first stud (23) is respectively arranged at the bottom ends of four corners of the first rectangular frame body (12), each first stud (23) is far away from the end of the first rectangular frame body (12) and is in threaded connection with the second rectangular frame body (13), the axis extension line direction of each first stud (23) is in the third direction, and when the first stud (23) rotates, the first rectangular frame body (12) and the second rectangular frame body (13) are driven to be far away from or close to each other.
10. The high automation bay docking device of claim 9, wherein the drive mechanism comprises a second drive assembly (7) provided at a bottom end of the second rectangular frame (13) for driving the frame (1) to move on a first plane, the first plane being perpendicular to the third direction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202410160438.XA CN117697370A (en) | 2024-02-05 | 2024-02-05 | High-automation cabin butt joint device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202410160438.XA CN117697370A (en) | 2024-02-05 | 2024-02-05 | High-automation cabin butt joint device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN117697370A true CN117697370A (en) | 2024-03-15 |
Family
ID=90157291
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202410160438.XA Pending CN117697370A (en) | 2024-02-05 | 2024-02-05 | High-automation cabin butt joint device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN117697370A (en) |
Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103062348A (en) * | 2013-01-02 | 2013-04-24 | 北京工业大学 | Anti-backlash transmission comprising trochoid gears and roll pins with conical teeth |
| CN103062334A (en) * | 2013-01-02 | 2013-04-24 | 北京工业大学 | Anti-backlash transmission comprising trochoid gears and roll pins with conical teeth |
| CN104097789A (en) * | 2014-06-25 | 2014-10-15 | 湖北航天技术研究院总体设计所 | Embedded type cabin section axial horizontal butt joint device and embedded type cabin section axial horizontal butt joint method |
| CN204123035U (en) * | 2014-09-25 | 2015-01-28 | 湖北三江航天红阳机电有限公司 | The section trimming of a kind of cabin and docking transporter |
| CN106584437A (en) * | 2016-12-31 | 2017-04-26 | 中国工程物理研究院激光聚变研究中心 | Seven-freedom-degree series-parallel docking platform |
| CN106826180A (en) * | 2017-04-01 | 2017-06-13 | 齐骥 | Manual butt joint assembly quality of gas suspension |
| JP2017207009A (en) * | 2016-05-18 | 2017-11-24 | 株式会社東芝 | Vertical inversion jig for cabin upper half of vacuum turbine, and vertical inversion method for cabin upper half of vacuum turbine |
| CN109129349A (en) * | 2018-09-19 | 2019-01-04 | 燕山大学 | Six degree of freedom posture adjustment docking platform |
| CN109318210A (en) * | 2018-11-26 | 2019-02-12 | 燕山大学 | The main passive compliance posture adjustment docking platform of thirteen-degree-of-freedom and its flexible docking method |
| CN215795054U (en) * | 2021-05-21 | 2022-02-11 | 北京凌空天行科技有限责任公司 | Multifunctional combined type universal bracket |
| CN217667578U (en) * | 2022-05-07 | 2022-10-28 | 德阳六合能源材料有限公司 | Aeroengine test run installation interfacing apparatus |
| CN115609535A (en) * | 2022-10-14 | 2023-01-17 | 沈阳航天新光集团有限公司 | Quick butt joint dismounting device of cabin section |
| CN115848963A (en) * | 2022-12-07 | 2023-03-28 | 中国科学院沈阳自动化研究所 | Operation rack for assembling large cabin pieces |
-
2024
- 2024-02-05 CN CN202410160438.XA patent/CN117697370A/en active Pending
Patent Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103062348A (en) * | 2013-01-02 | 2013-04-24 | 北京工业大学 | Anti-backlash transmission comprising trochoid gears and roll pins with conical teeth |
| CN103062334A (en) * | 2013-01-02 | 2013-04-24 | 北京工业大学 | Anti-backlash transmission comprising trochoid gears and roll pins with conical teeth |
| CN104097789A (en) * | 2014-06-25 | 2014-10-15 | 湖北航天技术研究院总体设计所 | Embedded type cabin section axial horizontal butt joint device and embedded type cabin section axial horizontal butt joint method |
| CN204123035U (en) * | 2014-09-25 | 2015-01-28 | 湖北三江航天红阳机电有限公司 | The section trimming of a kind of cabin and docking transporter |
| JP2017207009A (en) * | 2016-05-18 | 2017-11-24 | 株式会社東芝 | Vertical inversion jig for cabin upper half of vacuum turbine, and vertical inversion method for cabin upper half of vacuum turbine |
| CN106584437A (en) * | 2016-12-31 | 2017-04-26 | 中国工程物理研究院激光聚变研究中心 | Seven-freedom-degree series-parallel docking platform |
| CN106826180A (en) * | 2017-04-01 | 2017-06-13 | 齐骥 | Manual butt joint assembly quality of gas suspension |
| CN109129349A (en) * | 2018-09-19 | 2019-01-04 | 燕山大学 | Six degree of freedom posture adjustment docking platform |
| CN109318210A (en) * | 2018-11-26 | 2019-02-12 | 燕山大学 | The main passive compliance posture adjustment docking platform of thirteen-degree-of-freedom and its flexible docking method |
| CN215795054U (en) * | 2021-05-21 | 2022-02-11 | 北京凌空天行科技有限责任公司 | Multifunctional combined type universal bracket |
| CN217667578U (en) * | 2022-05-07 | 2022-10-28 | 德阳六合能源材料有限公司 | Aeroengine test run installation interfacing apparatus |
| CN115609535A (en) * | 2022-10-14 | 2023-01-17 | 沈阳航天新光集团有限公司 | Quick butt joint dismounting device of cabin section |
| CN115848963A (en) * | 2022-12-07 | 2023-03-28 | 中国科学院沈阳自动化研究所 | Operation rack for assembling large cabin pieces |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101254858B (en) | Lifting device for shift carrying | |
| CN105479129A (en) | Carrying and docking assembly for large-size heavy-load cylindrical workpieces | |
| CN105750860A (en) | Stent vehicle for mounting solar battery plate | |
| CN102102986B (en) | Roundness/cylindricality measurement workbench capable of automatically regulating center and inclination | |
| CN206511555U (en) | A kind of lifting body and AGV dolly | |
| CN117697370A (en) | High-automation cabin butt joint device | |
| CN117399881B (en) | Vertical butt joint device for web plate and wing plate during assembly of large-scale steel crane beam | |
| CN210478979U (en) | Intermediate shaft temporary support for shafting alignment | |
| CN114770107B (en) | Engine arrow installing equipment and engine arrow installing method | |
| CN218362990U (en) | Steel construction mounting structure for building manufacture | |
| CN108726459B (en) | Three-dimensional segmentation turns over with upset platform system | |
| CN109264628A (en) | AGV lifts alignment system | |
| CN105252199B (en) | Polyhedron rotation welding tool commonly used for multiple vehicle bodies | |
| CN211028638U (en) | Tunnel type welding system | |
| CN208471497U (en) | Three dimensional unit is turned over overturning platform | |
| CN205629692U (en) | Heavy tower crane festival assembling table | |
| CN110884511A (en) | Piggyback transport vehicle | |
| CN219548377U (en) | Building template capable of being assembled and used | |
| CN117324861B (en) | Medium-pressure container processing device and processing method | |
| CN114248241B (en) | Six-degree-of-freedom satellite control moment gyro mounting equipment | |
| CN117190802A (en) | Landing leg installation and butt joint combination device and installation and butt joint method | |
| CN216549462U (en) | Lifting mechanism for unmanned forklift | |
| CN111992967B (en) | Bearing pedestal with adjustable structure | |
| CN113602332B (en) | Integrated transfer device | |
| CN114776043B (en) | Auxiliary installation device for assembled building construction |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |