CN116161234A - Gesture adjusting mechanism capable of reducing equipment height - Google Patents

Gesture adjusting mechanism capable of reducing equipment height Download PDF

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Publication number
CN116161234A
CN116161234A CN202310284298.2A CN202310284298A CN116161234A CN 116161234 A CN116161234 A CN 116161234A CN 202310284298 A CN202310284298 A CN 202310284298A CN 116161234 A CN116161234 A CN 116161234A
Authority
CN
China
Prior art keywords
axis
screw rod
guide rail
seat
sliding
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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
Application number
CN202310284298.2A
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Chinese (zh)
Inventor
腾欢
张光宇
李向东
宋泽生
田李明
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chengdu Jiuxi Robot Technology Co ltd
Original Assignee
Chengdu Jiuxi Robot Technology Co ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Chengdu Jiuxi Robot Technology Co ltd filed Critical Chengdu Jiuxi Robot Technology Co ltd
Priority to CN202310284298.2A priority Critical patent/CN116161234A/en
Publication of CN116161234A publication Critical patent/CN116161234A/en
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor

Abstract

The invention discloses a gesture adjusting mechanism for reducing equipment height, which comprises a supporting seat, a sliding table, a transverse moving table, a longitudinal moving installation seat, a mounting plate, a Z-axis transmission screw rod, an X-axis transmission screw rod, a Y-axis transmission screw rod and a guide rail assembly, and is characterized in that the sliding table is movably connected to the supporting seat through the guide rail assembly, and a Z-axis nut seat of the Z-axis transmission screw rod is connected with the side edge of the sliding table; the X-axis transmission screw rod is movably connected to the sliding table through a guide rail assembly, and an X-axis nut seat of the X-axis transmission screw rod is connected with the bottom of the transverse sliding table; the vertical moving installation seat is vertically arranged at the upper end of the transverse moving platform, the installation plate is movably connected to the vertical moving platform through the guide rail assembly, and the Y-axis nut seat of the Y-axis transmission screw rod is connected with the bottom of the installation plate. The invention solves the technical problems of low precision and overhigh device in the prior art by reducing the equipment height of the gesture adjusting mechanism.

Description

Gesture adjusting mechanism capable of reducing equipment height
Technical Field
The invention relates to the field of attitude adjustment in aircraft assembly, in particular to an attitude adjustment mechanism for reducing equipment height.
Background
The aircraft assembly is a task which needs the cooperation of multiple departments to be completed, in order to better ensure the interchangeability and coordination of the butt joint of the aircraft fuselage and the wings, the assembly process of the fuselage and the wing parts needs no stress, the aircraft structure is prevented from being damaged due to the installation with stress, the safety is better ensured, and the safety flight coefficient of the aircraft is improved.
The assembly of current wing butt joint still adopts traditional hoist and mount and artifical supplementary assembly mostly, and the digitization degree is lower relatively, also can't realize flexible assembly, causes the butt joint precision of assembly low, and assembly platform stability is poor to current appearance mechanism of adjusting generally adds up for each axle of X axle, Y axle and Z axle, and overall structure is bigger, and initial height is too high.
Disclosure of Invention
The invention aims to provide a gesture adjusting mechanism capable of reducing equipment height so as to solve the technical problems of low precision and overhigh device in the prior art.
In order to achieve the above purpose, the invention provides a gesture adjusting mechanism for reducing equipment height, which comprises a supporting seat, a sliding table, a transverse moving table, a longitudinal moving installation seat, a mounting plate, a Z-axis transmission screw rod, an X-axis transmission screw rod, a Y-axis transmission screw rod, a servo motor, a grating ruler, a self-locking speed reducer and a guide rail assembly, and is characterized in that the sliding table is movably connected to the supporting seat through the guide rail assembly, the Z-axis transmission screw rod is installed in the vertical direction of the supporting seat, and a Z-axis nut seat of the Z-axis transmission screw rod is connected with the side edge of the sliding table; the X-axis transmission screw rod is movably connected to the sliding table through a guide rail assembly, and an X-axis nut seat of the X-axis transmission screw rod is connected with the bottom of the transverse sliding table; the vertical moving installation seat is vertically arranged at the upper end of the transverse moving platform, the upper end of the vertical moving installation seat is provided with a Y-axis transmission screw rod and an installation plate, the installation plate is movably connected to the vertical moving platform through a guide rail assembly, and a Y-axis nut seat of the Y-axis transmission screw rod is connected with the bottom of the installation plate; the output end of the servo motor is connected with a self-locking speed reducer, the servo motor provides driving for the self-locking speed reducer, and the self-locking speed reducer is connected with the execution tail ends of the Z-axis transmission screw rod, the X-axis transmission screw rod and the Y-axis transmission screw rod respectively through a coupler; the grating ruler is arranged on the side edge of the working direction of the guide rail assembly, the grating ruler records the walking displacement of the positioner in the sliding block, data are fed back to the control system, and the control system feeds back position data to the servo motor for position detection control.
Further, the guide rail assembly comprises a Z-axis sliding rail, an X-axis sliding rail, a Y-axis sliding rail and a plurality of sliding blocks, the sliding blocks are respectively movably connected to the Z-axis sliding rail, the X-axis sliding rail and the Y-axis sliding rail, the sliding blocks can linearly slide on the Z-axis sliding rail, the X-axis sliding rail and the Y-axis sliding rail, the Z-axis sliding rail is arranged on the side edge of the supporting seat, the X-axis sliding rail is arranged at the upper end of the sliding table, the Y-axis sliding rail is arranged at the upper end of the longitudinally-moving installation seat, and the X-axis sliding rail and the Y-axis sliding rail are vertically arranged.
Further, the supporting seat is a supporting structure formed by splicing and welding steel plates, a plurality of lightening holes are formed in the supporting seat, a buffer block is arranged at the bottom of the supporting seat, a parking assembly is arranged on the other side edge of the supporting seat, and the parking assembly consists of parking support legs and a servo electric cylinder.
Further, the Z-axis transmission screw rod consists of a Z-axis screw rod and a Z-axis nut seat, the Z-axis screw rod is arranged on the support seat through a screw rod support seat, the Z-axis nut seat is sleeved on the Z-axis screw rod, and the Z-axis nut seat is connected with the side edge of the sliding table; two sides of the sliding table are connected with the sliding blocks on the Z-axis sliding rail.
Further, the X-axis transmission screw rod consists of an X-axis screw rod and an X-axis nut seat, the X-axis screw rod is installed on the sliding table through a screw rod supporting seat, the X-axis nut seat is sleeved on the X-axis screw rod, the X-axis nut seat is connected with the bottom of the transverse moving seat, and two sides of the bottom of the transverse moving table are connected with sliding blocks on the X-axis sliding rail.
Further, the Y-axis transmission screw rod consists of a Y-axis screw rod and a Y-axis nut seat, the Y-axis screw rod is arranged at the upper end of the longitudinally moving installation seat through a screw rod supporting seat, the Y-axis nut seat is sleeved on the Y-axis screw rod, and the Y-axis nut seat is connected with the bottom of the installation plate; the two sides of the bottom of the mounting plate are connected with the sliding blocks on the Y-axis sliding rail.
Further, the mounting positions of the guide rail assemblies are provided with drag chains and protective covers.
Further, the drag chain is respectively arranged at the side positions of the Z-axis sliding rail, the X-axis sliding rail and the Y-axis sliding rail, and the installation direction of the drag chain is consistent with the working direction of the guide rail system; the protection casing is installed respectively in the bottom of Z axle slide rail, the one side that X axle slide rail is close to the supporting seat and the both sides of Y axle slide rail, and the protection casing adopts organ formula elasticity protection casing.
Based on the technical scheme, the invention can produce the following beneficial effects:
(1) According to the gesture adjusting mechanism for reducing the equipment height, the grating ruler is arranged on the side edge of the working direction of the guide rail assembly, the grating ruler records the walking displacement of the positioner in the sliding block, data are fed back to the control system, the control system feeds back position data to the servo motor for position detection control, the whole numerical control system enters a closed loop measuring link, and the repeated positioning accuracy is 0.02mm.
(2) According to the gesture adjusting mechanism for reducing the equipment height, the sliding table is arranged in the vertical direction of the supporting seat, the height of the supporting seat is used for the sliding height of the sliding table on the Z axis, and the gesture adjusting mechanism is reduced in height.
Drawings
FIG. 1 is a schematic diagram of an embodiment of the present invention;
FIG. 2 is a top view of the structure of an embodiment of the present invention;
FIG. 3 is a schematic view of a Z-axis transmission screw structure according to an embodiment of the present invention;
in the figure: 1. a support base; 2. a sliding table; 3. a traversing table; 4. longitudinally moving the mounting seat; 5. a mounting plate; 6. z-axis transmission screw rod; 7. X-axis transmission screw rod; 8. Y-axis transmission screw rod; 9. a Z-axis sliding rail; 10. an X-axis sliding rail; 11. a Y-axis sliding rail; 12. a slide block; 13. a servo motor; 14. a drag chain; 15. a grating ruler; 16. a self-locking speed reducer; 17. a protective cover; 18. a parking assembly.
Detailed Description
For a better understanding of the objects, structures and functions of the present invention, a gesture adjusting mechanism for reducing the height of equipment according to the present invention will be described in further detail with reference to the accompanying drawings.
In the description of the present invention, it should be noted that the terms "center", "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the apparatus or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
As shown in fig. 1-3, the gesture adjusting mechanism for reducing the equipment height comprises a supporting seat 1, a sliding table 2, a transverse moving table 3, a longitudinal moving installation seat 4, an installation plate 5, a Z-axis transmission screw rod 6, an X-axis transmission screw rod 7, a Y-axis transmission screw rod 8, a servo motor 13, a grating ruler 15, a self-locking speed reducer 16 and a guide rail assembly, and is characterized in that the sliding table 2 is movably connected to the supporting seat 1 through the guide rail assembly, the Z-axis transmission screw rod 6 is installed in the vertical direction of the supporting seat 1, and a Z-axis nut seat of the Z-axis transmission screw rod 6 is connected with the side edge of the sliding table 2; the X-axis transmission screw rod 7 is movably connected to the sliding table 2 through a guide rail assembly, and an X-axis nut seat of the X-axis transmission screw rod 7 is connected with the bottom of the transverse moving table 3; the longitudinal moving installation seat 4 is vertically arranged at the upper end of the transverse moving platform 3, a Y-axis transmission screw rod 8 and an installation plate 5 are arranged at the upper end of the longitudinal moving installation seat 4, the installation plate 5 is movably connected to the longitudinal moving platform 4 through a guide rail assembly, and a Y-axis nut seat of the Y-axis transmission screw rod 8 is connected with the bottom of the installation plate 5; the output end of the servo motor 13 is connected with a self-locking speed reducer 16, the servo motor 13 provides driving for the self-locking speed reducer 16, and the self-locking speed reducer 16 is connected with the execution ends of the Z-axis transmission screw rod 6, the X-axis transmission screw rod 7 and the Y-axis transmission screw rod 8 respectively through a coupler; the grating ruler 15 is arranged on the side edge of the working direction of the guide rail assembly, the grating ruler 15 records the walking displacement of the positioner in the sliding block 12, data are fed back to the control system, and the control system feeds back position data to the servo motor 13 for position detection control.
The guide rail assembly comprises a Z-axis slide rail 9, an X-axis slide rail 10, a Y-axis slide rail 11 and a plurality of sliding blocks 12, wherein the sliding blocks 12 are respectively and movably connected to the Z-axis slide rail 9, the X-axis slide rail 10 and the Y-axis slide rail 11, the sliding blocks 12 can linearly slide on the Z-axis slide rail 9, the X-axis slide rail 10 and the Y-axis slide rail 11, the Z-axis slide rail 9 is arranged on the side edge of the supporting seat 1, the X-axis slide rail 10 is arranged at the upper end of the sliding table 2, the Y-axis slide rail 11 is arranged at the upper end of the longitudinally moving installation seat 4, and the X-axis slide rail 10 and the Y-axis slide rail 11 are vertically arranged.
The supporting seat 1 is a supporting structure formed by splicing and welding steel plates, a plurality of lightening holes are formed in the supporting seat 1, a buffer block is arranged at the bottom of the supporting seat 1, a parking assembly 18 is arranged on the other side edge of the supporting seat 1, and the parking assembly 18 consists of parking support legs and a servo electric cylinder.
The Z-axis transmission screw rod 6 consists of a Z-axis screw rod and a Z-axis nut seat, the Z-axis screw rod is arranged on the supporting seat 1 through a screw rod supporting seat, the Z-axis nut seat is sleeved on the Z-axis screw rod, and the Z-axis nut seat is connected with the side edge of the sliding table 2; the two sides of the sliding table 2 are connected with a sliding block 12 on the Z-axis sliding rail 9.
The X-axis transmission screw rod 7 consists of an X-axis screw rod and an X-axis nut seat, the X-axis screw rod is installed on the sliding table 2 through a screw rod supporting seat, the X-axis nut seat is sleeved on the X-axis screw rod, the X-axis nut seat is connected with the bottom of the transverse moving seat 3, and two sides of the bottom of the transverse moving table 3 are connected with sliding blocks 12 on the X-axis sliding rail 10.
The Y-axis transmission screw rod 8 consists of a Y-axis screw rod and a Y-axis nut seat, the Y-axis screw rod is arranged at the upper end of the longitudinal movement installation seat 4 through a screw rod supporting seat, the Y-axis nut seat is sleeved on the Y-axis screw rod, and the Y-axis nut seat is connected with the bottom of the installation plate 5; the two sides of the bottom of the mounting plate 5 are connected with a sliding block 12 on a Y-axis sliding rail 11.
The structure of the X-axis transmission screw rod 7 and the Y-axis transmission screw rod 8 is the same as that of the Z-axis transmission screw rod 6, and both the X-axis transmission screw rod and the Y-axis transmission screw rod are shown in fig. 3.
The mounting plate 5 is provided with a high-precision ball locking device for airplane assembly butt joint, the gesture adjusting mechanisms are distributed at four corners of the underframe, and multi-gesture adjustment can be carried out in the butt joint process of the wing and the airplane body to ensure that hole sites are aligned quickly.
The Z-axis transmission screw rod 6, the X-axis transmission screw rod 7 and the Y-axis transmission screw rod 8 adopt ball screws, the lead error of the ball screws is not more than 0.008mm within any 300mm, the outer diameter of the ball screws is phi 32mm, the nuts are pre-tightened by double nuts, and the maximum dynamic load is about 2T.
The mounting locations of the track assemblies are provided with a tow chain 14 and a protective cover 17.
The servo motor 13 provides driving for the self-locking speed reducer 16, the self-locking speed reducer 16 is connected with the execution tail ends of the Z-axis transmission screw rod 6, the X-axis transmission screw rod 7 and the Y-axis transmission screw rod 8 respectively through a coupler, and the self-locking speed reducer 16 drives the Z-axis transmission screw rod 6, the X-axis transmission screw rod 7 and the Y-axis transmission screw rod 8 to rotate.
The drag chain 14 is respectively arranged at the side positions of the Z-axis sliding rail 9, the X-axis sliding rail 10 and the Y-axis sliding rail 11, and the installation direction of the drag chain 14 is consistent with the working direction of the guide rail system; the protection cover 17 is respectively arranged at the bottom of the Z-axis sliding rail 9, one side of the X-axis sliding rail 10 close to the supporting seat 1 and two sides of the Y-axis sliding rail 11, and the protection cover 17 adopts an organ type elastic protection cover.
The drag chain 14 is provided to retract various wires.
The organ type elastic protective cover is flexible in sliding, convenient to detach and relatively large in compression, and can be quickly detached and installed when maintenance and overhaul are needed.
The grating ruler 15 is arranged on the side edge of the working direction of the guide rail assembly, the grating ruler 15 records the walking displacement of the positioner in the sliding block 12, data are fed back to the control system, the control system feeds back position data to the servo motor 13 for position detection control, the whole numerical control system enters a closed loop measurement link, and the repeated positioning accuracy is 0.02mm.
The maximum resolution of the grating scale 15 is 0.5 μm; the precision grade is +/-5 mu m, and the protection grade is IP53; the absolute output is S422/TLL comp.
The specific operation method of the invention comprises the following steps:
the grating ruler 15 accurately records the walking position of the positioner of the sliding block 12, the existing position data is accurately fed back to the control system, the control system feeds back the position parameters to the servo motor 13 for position detection control, and the whole numerical control system enters a closed-loop measurement link.
The servo motor 13 drives the self-locking speed reducer 16 to enable the Z-axis transmission screw rod 6, the X-axis transmission screw rod 7 and the Y-axis transmission screw rod 8 to rotate, and enable the sliding table 2, the transverse sliding table 2 and the mounting plate 5 on the Z-axis nut seat, the X-axis nut seat and the Y-axis nut seat to slide linearly on the guide rail assembly.
It will be understood that the invention has been described with respect to certain embodiments and that various changes and equivalents may be made to those features and embodiments without departing from the spirit and scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.

Claims (8)

1. The utility model provides a reduce and equip appearance mechanism of height, includes supporting seat (1), slip table (2), sideslip platform (3), indulges and moves mount pad (4), mounting panel (5), Z axle transmission lead screw (6), X axle transmission lead screw (7), Y axle transmission lead screw (8), servo motor (13), grating chi (15), auto-lock speed reducer (16) and guide rail subassembly, its characterized in that, slip table (2) are through guide rail subassembly swing joint on supporting seat (1), and the vertical direction at supporting seat (1) is installed in Z axle transmission lead screw (6), and the Z axle nut seat of Z axle transmission lead screw (6) is connected with the side of slip table (2); the X-axis transmission screw rod (7) is movably connected to the sliding table (2) through a guide rail assembly, and an X-axis nut seat of the X-axis transmission screw rod (7) is connected with the bottom of the transverse moving table (3); the longitudinal moving installation seat (4) is vertically arranged at the upper end of the transverse moving table (3), a Y-axis transmission screw rod (8) and an installation plate (5) are arranged at the upper end of the longitudinal moving installation seat (4), the installation plate (5) is movably connected to the longitudinal moving table (4) through a guide rail assembly, and a Y-axis nut seat of the Y-axis transmission screw rod (8) is connected with the bottom of the installation plate (5); the output end of the servo motor (13) is connected with a self-locking speed reducer (16), the servo motor (13) provides driving for the self-locking speed reducer (16), and the self-locking speed reducer (16) is connected with the execution tail ends of the Z-axis transmission screw rod (6), the X-axis transmission screw rod (7) and the Y-axis transmission screw rod (8) respectively through a coupler; the grating ruler (15) is arranged on the side edge of the working direction of the guide rail assembly, the grating ruler (15) records walking displacement of the positioner in the sliding block (12), data are fed back to the control system, and the control system feeds back position data to the servo motor (13) for position detection control.
2. The gesture adjusting mechanism for reducing equipment height according to claim 1, wherein the guide rail assembly is composed of a Z-axis guide rail (9), an X-axis guide rail (10), a Y-axis guide rail (11) and a plurality of sliding blocks (12), the sliding blocks (12) are respectively movably connected to the Z-axis guide rail (9), the X-axis guide rail (10) and the Y-axis guide rail (11), the sliding blocks (12) can linearly slide on the Z-axis guide rail (9), the X-axis guide rail (10) and the Y-axis guide rail (11), the Z-axis guide rail (9) is arranged on the side edge of the supporting seat (1), the X-axis guide rail (10) is arranged at the upper end of the sliding table (2), the Y-axis guide rail (11) is arranged at the upper end of the longitudinally moving installation seat (4), and the X-axis guide rail (10) and the Y-axis guide rail (11) are vertically arranged.
3. The gesture adjusting mechanism for reducing equipment height according to claim 1, wherein the supporting seat (1) is a supporting structure formed by splicing steel plates, a plurality of lightening holes are formed in the supporting seat (1), a buffer block is arranged at the bottom of the supporting seat (1), a parking assembly (18) is arranged at the other side edge of the supporting seat (1), and the parking assembly (18) consists of parking support legs and a servo electric cylinder.
4. The gesture adjusting mechanism for reducing the equipment height according to claim 1, wherein the Z-axis transmission screw rod (6) consists of a Z-axis screw rod and a Z-axis nut seat, the Z-axis screw rod is arranged on the supporting seat (1) through a screw rod supporting seat, the Z-axis nut seat is sleeved on the Z-axis screw rod, and the Z-axis nut seat is connected with the side edge of the sliding table (2); two side edges of the sliding table (2) are connected with sliding blocks (12) on the Z-axis sliding rail (9).
5. The gesture adjusting mechanism for reducing equipment height according to claim 1, wherein the X-axis transmission screw rod (7) is composed of an X-axis screw rod and an X-axis nut seat, the X-axis screw rod is installed on the sliding table (2) through a screw rod supporting seat, the X-axis nut seat is sleeved on the X-axis screw rod, the X-axis nut seat is connected with the bottom of the traversing seat (3), and two sides of the bottom of the traversing seat (3) are connected with sliding blocks (12) on the X-axis sliding rail (10).
6. The gesture adjusting mechanism for reducing equipment height according to claim 1, wherein the Y-axis transmission screw rod (8) consists of a Y-axis screw rod and a Y-axis nut seat, the Y-axis screw rod is arranged at the upper end of the longitudinally moving installation seat (4) through a screw rod supporting seat, the Y-axis nut seat is sleeved on the Y-axis screw rod, and the Y-axis nut seat is connected with the bottom of the installation plate (5); the two sides of the bottom of the mounting plate (5) are connected with a sliding block (12) on the Y-axis sliding rail (11).
7. A reduced equipment height attitude adjustment mechanism according to claim 1, wherein the mounting locations of the rail assemblies are provided with a drag chain (14) and a protective cover (17).
8. The gesture adjusting mechanism for reducing the equipment height according to claim 7, wherein the drag chain (14) is respectively arranged at the side positions of the Z-axis sliding rail (9), the X-axis sliding rail (10) and the Y-axis sliding rail (11), and the installation direction of the drag chain (14) is consistent with the working direction of the guide rail system; the protection cover (17) is respectively arranged at the bottom of the Z-axis sliding rail (8), one side of the X-axis sliding rail (10) close to the supporting seat (1) and two sides of the Y-axis sliding rail (11), and the protection cover (17) adopts an organ type elastic protection cover.
CN202310284298.2A 2023-03-22 2023-03-22 Gesture adjusting mechanism capable of reducing equipment height Pending CN116161234A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202310284298.2A CN116161234A (en) 2023-03-22 2023-03-22 Gesture adjusting mechanism capable of reducing equipment height

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202310284298.2A CN116161234A (en) 2023-03-22 2023-03-22 Gesture adjusting mechanism capable of reducing equipment height

Publications (1)

Publication Number Publication Date
CN116161234A true CN116161234A (en) 2023-05-26

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Application Number Title Priority Date Filing Date
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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060180704A1 (en) * 2005-02-01 2006-08-17 The Boeing Company Mandrel segment loader
CN107186498A (en) * 2017-05-23 2017-09-22 浙江大学 A kind of five-shaft numerical control drilling lathe for aircraft wing box numeric terminal
CN109955049A (en) * 2019-03-20 2019-07-02 燕山大学 A kind of vertical posture adjusting system can be used for large-scale assembly
CN112475935A (en) * 2020-11-18 2021-03-12 广东普拉迪科技股份有限公司 Five-axis numerical control machining center with high-rigidity transmission chain structure
CN113305772A (en) * 2021-04-27 2021-08-27 成都飞机工业(集团)有限责任公司 Auxiliary docking device for aircraft component and operation method thereof
CN114476116A (en) * 2022-01-27 2022-05-13 成都九系机器人科技有限公司 Flexible butt joint system for large helicopter assembly

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060180704A1 (en) * 2005-02-01 2006-08-17 The Boeing Company Mandrel segment loader
CN107186498A (en) * 2017-05-23 2017-09-22 浙江大学 A kind of five-shaft numerical control drilling lathe for aircraft wing box numeric terminal
CN109955049A (en) * 2019-03-20 2019-07-02 燕山大学 A kind of vertical posture adjusting system can be used for large-scale assembly
CN112475935A (en) * 2020-11-18 2021-03-12 广东普拉迪科技股份有限公司 Five-axis numerical control machining center with high-rigidity transmission chain structure
CN113305772A (en) * 2021-04-27 2021-08-27 成都飞机工业(集团)有限责任公司 Auxiliary docking device for aircraft component and operation method thereof
CN114476116A (en) * 2022-01-27 2022-05-13 成都九系机器人科技有限公司 Flexible butt joint system for large helicopter assembly

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