Part transfer device for aircraft production
By designing a device suitable for the transfer of aircraft parts, and using connecting components and suction cups for fixation, the problem of traditional transfer devices requiring multiple devices to work together is solved, thus achieving efficient and low-cost transfer of parts.
Patent Information
- Application Number
- CN202520136756.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-20
- Publication Date
- 2025-11-25
- Estimated Expiration
- 2035-01-20
AI Technical Summary
When traditional transfer devices are used to transfer aircraft parts, some parts are too large and require multiple devices or hoisting equipment, which increases production costs.
A transfer device comprising a first transfer housing, a connecting housing, a moving component, a fixing component, and a suction cup is designed. By adjusting the distance between the components and using the suction cup for fixation, stable transfer of parts of different volumes can be achieved.
This reduces the cost of transferring parts during aircraft production and improves transfer efficiency and stability.
Smart Images
Figure CN223590770U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to aircraft production technical field, concretely is a kind of spare parts transfer device for aircraft production. BACKGROUND
[0002] Aircraft can make us reach destination faster, save a lot of time, compared with the slow progress of land transport, aircraft can fly across thousands of miles within hours, thereby save several hours of journey time, aircraft can help us more efficiently complete work, they can quickly transport people and goods to destination, so that the whole process is more efficient, which is very helpful for the material transportation, personnel transfer and other aspects needing efficiency and rapid response, aircraft production needs to use transfer device, to transport wing, engine, propeller, fuselage and other spare parts used in aircraft production.
[0003] However, the traditional transfer device has the following shortcomings:
[0004] In the process of transferring aircraft parts by the traditional transfer device, some aircraft parts are too large in size, and multiple transfer devices need to be used to cooperate or hoisting equipment to complete the transfer, which increases the production cost of aircraft. UTILITY MODEL CONTENT
[0005] The utility model aims at providing a spare parts transfer device for aircraft production to solve the problem that, in the process of transferring aircraft parts by the traditional transfer device, some aircraft parts are too large in size, and multiple transfer devices need to be used to cooperate or hoisting equipment to complete the transfer, which increases the production cost of aircraft.
[0006] To achieve the above purpose, the utility model provides the following technical scheme: a spare parts transfer device for aircraft production, comprising a first transfer machine shell, one end of the first transfer machine shell is slidably connected with a connecting machine shell, one end of the connecting machine shell is slidably connected with a second transfer machine shell, four corners of the bottom end of the first transfer machine shell and four corners of the bottom end of the second transfer machine shell are all fixedly installed with a moving assembly, a connecting assembly is installed between the two sides of the first transfer machine shell and the two sides of the second transfer machine shell, a fixed assembly is fixedly installed at the top end of the first transfer machine shell and the top end of the second transfer machine shell, the connecting assembly comprises a first positioning table and a first angle rod, the top end of the first positioning table is rotatably connected with one end of the first angle rod, the other end of the first angle rod is rotatably connected with a second angle rod, one end of the second angle rod is rotatably connected with a second positioning table.
[0007] Preferably, the middle of the second angle rod is provided with a direction shell, the inside of the direction shell is slidably connected with an extension rod, one end of the extension rod is provided with a suction cup, one side of the first positioning table is fixedly connected with a first transfer machine shell, one side of the second positioning table is fixedly connected with a second transfer machine shell, the user rotates the direction shell along the second angle rod, and the user slides the extension rod along the direction shell, so that the suction cup is firmly adsorbed on the first angle rod, and the user twists the screw through the direction shell to fix the extension rod in the direction shell.
[0008] Preferably, the two fixing assemblies each include a fixing table and two vertical plates, the top of the fixing table is fixedly connected with the bottom of the two vertical plates, respectively, the middle of one of the vertical plates is fixedly provided with a mounting shell, the inside of the mounting shell is threadedly connected with a lead screw, one end of the lead screw is rotatably connected with a clamping plate slidably connected with the fixing table, the user rotates the lead screw, the threads on the surface of the lead screw and the threads on the inner wall of the mounting shell are matched with each other, so that the lead screw rotates and translates relative to the mounting shell, and the lead screw pushes the clamping plate from one side, and the clamping plate and the vertical plate cooperate with each other to clamp and fix the parts produced by the aircraft.
[0009] Preferably, the two ends of one side of the clamping plate are fixedly provided with sliding rods slidably connected with adjacent vertical plates, and the surface of the clamping plate and the surface of the two vertical plates are paved with rubber plates, the bottom of one of the fixing tables is fixedly connected with a first transfer machine shell, and the bottom of the other fixing table is fixedly connected with a second transfer machine shell, during the sliding of the clamping plate along the fixing table, the sliding rods slide relative to the vertical plates, thereby improving the stability of the clamping plate and the vertical plate opposite to the clamping plate in clamping the parts produced by the aircraft.
[0010] Preferably, the eight moving assemblies each include a moving shell and a moving wheel, the bottom of the moving shell is fixedly connected with the top of the moving wheel, the top of the moving shell is provided with a damping groove, the bottom of the inner wall of the damping groove is fixedly provided with a spring damper, and the top of the spring damper is fixedly provided with a length rod extending to the outside. After the moving wheel contacts the ground and generates friction, the moving wheel rotates after being subjected to friction, thereby facilitating the transfer of the aircraft parts by the transfer machine shell. When the transfer is to a bumpy section, the length rod slides relative to the damping groove, and the length rod extrudes the spring damper from the top, and the spring damper buffers the bumping force received.
[0011] Preferably, the top of four of the length rods is fixedly connected with the first transfer machine shell, and the top of the other four length rods is fixedly connected with the second transfer machine shell, and the two sides of the four length rods connected with the first transfer machine shell and the two sides of the other four length rods connected with the second transfer machine shell are fixedly provided with reinforcing plates. The moving assemblies are respectively installed on the first transfer machine shell and the second transfer machine shell through the length rods, the installation of the reinforcing plates increases the connection area of the length rods and the transfer machine shell, and the stability of the installation of the moving assemblies is increased.
[0012] Preferably, the surface of the first transfer machine shell and the surface of the second transfer machine shell are fixedly installed with a push-pull plate, and the opposite sides of the two push-pull plates are fixedly installed with handles, and the user holds the handles to pull the transfer device from one side of the first transfer machine shell or one side of the second transfer machine shell.
[0013] Compared with the prior art, the beneficial effects of the utility model are that: through setting the connecting assembly, the first transfer machine shell, the second transfer machine shell and the connecting machine shell, the user adjusts the relative distance among the three according to the actual specifications of the aircraft parts to be transferred, and then the user fixes the relative positions of the first angle rod and the second angle rod through the deflection direction shell and the extension rod, indirectly fixes the transfer volume, and facilitates the transfer device to transfer aircraft parts of different volumes, thereby reducing the production cost of the aircraft. BRIEF DESCRIPTION OF DRAWINGS
[0014] Figure 1 It is a side view of the utility model;
[0015] Figure 2 It is a sectional view of the moving assembly of the utility model;
[0016] Figure 3 It is a side view of the connecting assembly of the utility model;
[0017] Figure 4 It is a side view of the fixing assembly of the utility model.
[0018] In the drawing: 1, first transfer machine shell; 2, push-pull plate; 3, handle; 4, fixing assembly; 41, fixing table; 42, vertical plate; 43, clamping plate; 44, sliding rod; 45, screw rod; 46, installation shell; 47, rubber plate; 5, connecting machine shell; 6, second transfer machine shell; 7, moving assembly; 71, moving shell; 72, length rod; 73, reinforcing plate; 74, spring shock absorber; 75, shock absorbing groove; 76, moving wheel; 8, connecting assembly; 81, first positioning table; 82, first angle rod; 83, second angle rod; 84, second positioning table; 85, direction shell; 86, extension rod; 87, suction cup. DETAILED DESCRIPTION
[0019] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model.
[0020] Please refer to Figures 1-4The utility model provides a kind of spare part transfer device for aircraft production, including first transfer casing 1, one end of first transfer casing 1 is slidably connected with connecting casing 5, one end of connecting casing 5 is slidably connected with second transfer casing 6, four corners of first transfer casing 1 bottom end and four corners of second transfer casing 6 bottom end are all fixedly installed with moving assembly 7, connecting assembly 8 is installed between the two sides of first transfer casing 1 and the two sides of second transfer casing 6, the top of first transfer casing 1 and the top of second transfer casing 6 are all fixedly installed with fixed assembly 4, connecting assembly 8 includes first positioning table 81 and first angle lever 82, the top of first positioning table 81 is rotatably connected with one end of first angle lever 82, the other end of first angle lever 82 is rotatably connected with second angle lever 83, one end of second angle lever 83 is rotatably connected with second positioning table 84.
[0021] The middle part of second angle lever 83 is installed with direction shell 85, extension rod 86 is slidably connected inside direction shell 85, one end of extension rod 86 is installed with suction disc 87, one side of first positioning table 81 is fixedly connected with first transfer casing 1, one side of second positioning table 84 is fixedly connected with second transfer casing 6, user rotates direction shell 85 along second angle lever 83, and user slides extension rod 86 along direction shell 85, so that suction disc 87 is firmly adsorbed on first angle lever 82, user twists screw through direction shell 85, and extension rod 86 is fixed in direction shell 85.
[0022] Two fixed assemblies 4 all include fixed table 41 and two vertical plates 42, the two sides of the top of fixed table 41 are fixedly connected with the bottom of two vertical plates 42 respectively, the middle part of one of vertical plates 42 is fixedly installed with mounting shell 46, screw rod 45 is threadedly connected inside mounting shell 46, one end of screw rod 45 is rotatably connected with clamping plate 43 slidably connected with fixed table 41, user rotates screw rod 45, the thread on the surface of screw rod 45 and the thread on the inner wall of mounting shell 46 are matched with each other, so that screw rod 45 rotates and translates relative to mounting shell 46, and screw rod 45 pushes clamping plate 43 from one side, and clamping plate 43 cooperates with vertical plate 42 to clamp and fix the spare part of aircraft production.
[0023] The two ends of one side of clamping plate 43 are all fixedly installed with sliding rod 44 slidably connected with adjacent vertical plate 42, the surface of clamping plate 43 and the surface of two vertical plates 42 are all paved with rubber plate 47, the bottom of one of fixed table 41 is fixedly connected with first transfer casing 1, the bottom of another fixed table 41 is fixedly connected with second transfer casing 6, in the process that clamping plate 43 slides along fixed table 41, sliding rod 44 slides relative to vertical plate 42, to improve the stability that clamping plate 43 and vertical plate 42 opposite clamp the spare part of aircraft production.
[0024] The eight moving assemblies 7 each comprise a moving shell 71 and a moving wheel 76, the bottom end of the moving shell 71 is fixedly connected with the top end of the moving wheel 76, the top end of the moving shell 71 is provided with a damping groove 75, the bottom end of the inner wall of the damping groove 75 is fixedly installed with a spring damper 74, the top end of the spring damper 74 is fixedly installed with a length rod 72 extending to the outside, the moving wheel 76 is in friction with the ground after being in contact with the ground, the moving wheel 76 rotates after being subjected to friction, so that the transfer machine shell is convenient for transferring the aircraft parts, when the transfer is to a bumpy road section, the length rod 72 slides relative to the damping groove 75, and the length rod 72 extrudes the spring damper 74 from the top, and the spring damper 74 buffers the bumping force received.
[0025] The top end of four length rods 72 is fixedly connected with the first transfer machine shell 1, and the top end of the other four length rods 72 is fixedly connected with the second transfer machine shell 6, the two sides of the four length rods 72 connected with the first transfer machine shell 1 and the two sides of the other four length rods 72 connected with the second transfer machine shell 6 are each fixedly installed with a reinforcing plate 73, the moving assembly 7 is installed on the first transfer machine shell 1 and the second transfer machine shell 6 through the length rod 72, and the installation of the reinforcing plate 73 increases the connection area of the length rod 72 and the transfer machine shell, and increases the stability of the installation of the moving assembly 7.
[0026] The surface of the first transfer machine shell 1 and the surface of the second transfer machine shell 6 are each fixedly installed with a push-pull plate 2, the side away from each other of the two push-pull plates 2 is each fixedly installed with a handle 3, the user holds the handle 3 with the hand, pulls the transfer device from one side of the first transfer machine shell 1 or pulls the transfer device from one side of the second transfer machine shell 6.
[0027] In use, the user slides the connecting shell 5 along the first transfer machine shell 1 and the second transfer machine shell 6, then the user rotates the direction shell 85 along the second angle rod 83, and the user slides the length rod 86 along the direction shell 85, so that the suction disc 87 is firmly adsorbed on the first angle rod 82, the user twists the screw through the direction shell 85 to fix the length rod 86 in the direction shell 85, the first angle rod 82 and the second angle rod 83 cooperate with each other to adjust the distance between the first transfer machine shell 1 and the second transfer machine shell 6, then the user fixes the aircraft parts, the user rotates the lead screw 45, the threads on the surface of the lead screw 45 are matched with the threads on the inner wall of the installation shell 46, so the lead screw 45 rotates and translates relative to the installation shell 46, and the lead screw 45 pushes the clamping plate 43 from one side, and the clamping plate 43 and the vertical plate 42 cooperate with each other to clamp and fix the aircraft parts, the user holds the handle 3 with the hand, pulls the transfer device from one side of the first transfer machine shell 1 or pulls the transfer device from one side of the second transfer machine shell 6, to complete the transfer of the aircraft parts.
[0028] Although the utility model has been explained in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions recorded in the foregoing embodiments or make equivalent replacement to part of the technical features, and any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the utility model shall be included in the protection scope of the utility model.
Claims
1. A component transfer device for aircraft manufacturing, comprising a first transfer housing (1), characterized in that: One end of the first transfer housing (1) is slidably connected to a connecting housing (5), and one end of the connecting housing (5) is slidably connected to a second transfer housing (6). Movable components (7) are fixedly installed at the four corners of the bottom of the first transfer housing (1) and the four corners of the bottom of the second transfer housing (6). Connecting components (8) are installed between the two sides of the first transfer housing (1) and the two sides of the second transfer housing (6). Fixing components (4) are fixedly installed at the top of the first transfer housing (1) and the top of the second transfer housing (6). The connecting component (8) includes a first positioning platform (81) and a first angle rod (82). The top of the first positioning platform (81) is rotatably connected to one end of the first angle rod (82). The other end of the first angle rod (82) is rotatably connected to a second angle rod (83). One end of the second angle rod (83) is rotatably connected to a second positioning platform (84).
2. The component transfer device for aircraft production according to claim 1, characterized in that: A direction shell (85) is installed in the middle of the second angle rod (83). An extension rod (86) is slidably connected inside the direction shell (85). A suction cup (87) is installed at one end of the extension rod (86). One side of the first positioning platform (81) is fixedly connected to the first transfer housing (1), and one side of the second positioning platform (84) is fixedly connected to the second transfer housing (6).
3. The component transfer device for aircraft production according to claim 1, characterized in that: Both of the fixing components (4) include a fixing platform (41) and two upright plates (42). The top two sides of the fixing platform (41) are fixedly connected to the bottom ends of the two upright plates (42). A mounting shell (46) is fixedly installed in the middle of one of the upright plates (42). A screw rod (45) is threaded inside the mounting shell (46). One end of the screw rod (45) is rotatably connected to a clamping plate (43) that is slidably connected to the fixing platform (41).
4. The aircraft manufacturing parts transfer device according to claim 3, characterized in that: Both ends of one side of the clamping plate (43) are fixedly installed with sliding rods (44) that are slidably connected to the adjacent upright plate (42). The surface of the clamping plate (43) and the surfaces of the two upright plates (42) are covered with rubber plates (47). The bottom end of one of the fixed platforms (41) is fixedly connected to the first transfer machine housing (1), and the bottom end of the other fixed platform (41) is fixedly connected to the second transfer machine housing (6).
5. A component transfer device for aircraft production according to claim 1, characterized in that: Each of the eight moving components (7) includes a moving shell (71) and a moving wheel (76). The bottom end of the moving shell (71) is fixedly connected to the top end of the moving wheel (76). A shock-absorbing groove (75) is provided at the top end of the moving shell (71). A spring shock absorber (74) is fixedly installed at the bottom end of the inner wall of the shock-absorbing groove (75). A long rod (72) extending to the outside is fixedly installed at the top end of the spring shock absorber (74).
6. A component transfer device for aircraft production according to claim 5, characterized in that: The top ends of four of the length rods (72) are fixedly connected to the first transfer housing (1), and the top ends of the other four length rods (72) are fixedly connected to the second transfer housing (6). Reinforcing plates (73) are fixedly installed on both sides of the connection between the four length rods (72) and the first transfer housing (1) and on both sides of the connection between the other four length rods (72) and the second transfer housing (6).
7. A component transfer device for aircraft production according to claim 1, characterized in that: Push-pull plates (2) are fixedly installed on the surface of the first transfer housing (1) and the surface of the second transfer housing (6), and handles (3) are fixedly installed on the opposite sides of the two push-pull plates (2).