CN215628151U

CN215628151U - Aircraft part heat treatment material device capable of conveniently taking materials

Info

Publication number: CN215628151U
Application number: CN202121619723.1U
Authority: CN
Inventors: 李光同
Original assignee: Nantong Fujitekaixiang Aviation Equipment Co ltd
Current assignee: Nantong Fujitekaixiang Aviation Equipment Co ltd
Priority date: 2021-07-15
Filing date: 2021-07-15
Publication date: 2022-01-25
Anticipated expiration: 2031-07-15

Abstract

The utility model discloses an airplane part heat treatment material device convenient for material taking, which aims at the problem of time and labor waste in material taking and provides the following technical scheme that the device comprises a skip car for loading workpieces, a reticular material basket which is parallel to the ground and is in sliding connection with the skip car for containing the workpieces, an opening for sliding the workpieces out of the reticular material basket, a limiting component which is connected with the skip car and is used for resisting and pushing the workpieces to move towards the opening, and a bearing component which is connected with the skip car and is used for loading the skip car for heat treatment, when the reticular charging basket is drawn out of the charging car, the limiting component can support the airplane parts of the reticular charging basket, and along with the pull of netted charging basket, spacing subassembly pushes away the aircraft part to the opening part, makes the aircraft part fall into the work piece of below and deposits in the basket, and whole process easy operation has made things convenient for the step of getting the material and depositing, has improved work efficiency.

Description

Aircraft part heat treatment material device capable of conveniently taking materials

Technical Field

The utility model relates to the technical field of heat treatment, in particular to a material taking device for airplane part heat treatment, which is convenient for material taking.

Background

When a large batch of small-sized workpieces are subjected to heat treatment, the workpieces are pushed into a hot furnace tray by a long rod in a manual mode, and the workpieces are manually taken out after heating is finished, so that time and labor are wasted in the whole process.

At present, chinese patent application No. 201520424263.5 discloses a material trolley for heat treatment of ring-shaped workpieces, and it is including the frame that has the chassis and set up the gyro wheel in the chassis below, is provided with a plurality of interlayers along vertical direction interval on the frame, and the interlayer is parallel to each other with the chassis, and the array is provided with the rectangle through-hole on the interlayer, and the ring-shaped workpiece passes rectangle through-hole, the periphery of ring-shaped workpiece with two minor face contacts of rectangle through-hole, and the diameter of ring-shaped workpiece is greater than the long limit length of rectangle through-hole during the use, place the ring-shaped workpiece in the rectangle through-hole on the interlayer, make its mutual isolation.

Although the material trolley for heat treatment of the ring-shaped workpiece solves the problem that a small workpiece is manually and directly fed into a heating furnace during heat treatment of the ring-shaped workpiece, the workpiece needs to be taken out and placed in a storage place after heat treatment is finished, if the workpiece is directly poured out, the workpiece is easy to fall off, and generally the workpiece is taken out from the material trolley one by one, so that the whole process is time-consuming and labor-consuming.

SUMMERY OF THE UTILITY MODEL

Aiming at the defects in the prior art, the utility model aims to provide the airplane part heat treatment material taking device which is convenient for taking materials and has the advantage of convenience in taking materials.

In order to achieve the purpose, the utility model provides the following technical scheme:

the utility model provides an aircraft part heat treatment material device of conveniently getting material, including the skip that is used for loading the work piece, still including be on a parallel with ground and with skip sliding connection is used for holding the netted charging basket of using of work piece, the netted opening that is used for the work piece roll-off of seting up with the charging basket, still include with the skip connect be used for keeping out and promote the work piece towards spacing subassembly that the opening removed, with the skip is connected and is used for loading the skip carries out the bearing component that heat treats.

Adopt above-mentioned technical scheme, the skip can transport aircraft parts, has replaced the step of artifical transport, and netted basket of using can hold aircraft parts, netted basket of using and skip sliding connection make things convenient for the drawing of net enclosing plate in the skip to put, and spacing subassembly can support when netted basket of using is taken out and promote the work piece court the opening removes, makes aircraft parts fall into the below work piece through pushing and deposits in the basket, has improved the efficiency of getting the material and depositing, and bearing assembly is used for loading the skip and carries out heat treatment, and after heat treatment finished, the skip shifted out, and next skip immigration bearing assembly carries out heat treatment, has improved work efficiency.

Further, the skip comprises a frame for loading workpieces, a net-shaped cover plate, a first slide way and a second slide way, wherein the net-shaped cover plate is attached to and fixed on the frame, the first slide way is horizontally fixed on the frame and is in sliding connection with the net-shaped charging basket, and the second slide way is horizontally fixed on the frame and is positioned below the first slide way.

By adopting the technical scheme, the reticular cover plate can prevent the aircraft parts from turning out of the reticular charging basket and falling off when the aircraft parts are subjected to heat treatment, the first slide way facilitates the drawing of the reticular charging basket, and the second slide way facilitates the extraction of the workpiece storage basket.

Further, spacing subassembly include with netted apron articulated baffle, be fixed in netted apron is used for restricting the baffle pivoted limiting plate, with netted apron rotate to be connected and with baffle lapped L shape dwang.

By adopting the technical scheme, the baffle can resist aircraft parts moving along with the net-shaped charging basket, the limiting plate can resist the baffle to continue rotating, the baffle is overlapped on the L-shaped rotating rod, and the L-shaped rotating rod can be rotated to control the retraction of the baffle.

Further, the bearing assembly comprises a support for loading the skip car, a track fixed on the support and connected with the skip car, and a lifting lug fixedly connected with the support.

By adopting the technical scheme, the track can facilitate the skip car to be transported to the support, and the lifting lug facilitates the rigging to hook the bearing component, so that the bearing component is lifted to be thermally treated in the heating furnace.

Further, the support with the skip is through first round pin hub connection.

By adopting the technical scheme, the first pin shaft can fix the position of the skip car in the support, so that the phenomenon that the skip car slides out of the support when the support is lifted is prevented.

Furthermore, the reticular cover plate is connected with the reticular material basket through a second pin shaft.

Adopt above-mentioned technical scheme, the position of netted charging basket in the skip can be fixed to the second round pin axle, prevents that the support from lifting by crane the emergence of the phenomenon of the netted charging basket of following the skip roll-off.

Furthermore, the reticular charging basket is fixedly connected with a drawing handle.

By adopting the technical scheme, the drawing handle is convenient for drawing the reticular charging basket.

Further, the opening of the net-shaped charging basket is provided with a ramp for sliding the workpiece.

By adopting the technical scheme, the ramp can guide the aircraft parts to slide out from the opening and fall into the workpiece storage basket below, so that the damage of the aircraft parts to workpieces caused by sliding is reduced.

In conclusion, the utility model has the following beneficial effects:

1. when the net-shaped charging basket is pulled out of the charging trolley, the limiting assembly can support airplane parts of the net-shaped charging basket, and the airplane parts are pushed to the opening by the limiting assembly along with the pulling of the net-shaped charging basket, so that the airplane parts fall into the workpiece storage basket below the limiting assembly, the whole process is simple to operate, the steps of taking and storing are facilitated, and the working efficiency is improved;

2. the bearing assembly can bear the skip car and lift the skip car into the hot furnace for heat treatment, and serves as a carrier of the skip car, so that the step of repeatedly taking and hanging the rigging when the skip car is directly lifted is avoided, and the working efficiency is improved;

3. the mesh cover plate is attached to the mesh charging basket, so that the aircraft parts can be prevented from falling off from the mesh charging basket, and the mesh charging basket has the advantage of preventing workpieces from falling off.

Drawings

Fig. 1 is a schematic structural view of the utility model;

fig. 2 is a schematic structural view of the skip car of the utility model;

FIG. 3 is a cross-sectional view of the middle stop assembly and the mesh basket of the present invention;

FIG. 4 is a schematic structural view of the load-bearing assembly of the present invention;

fig. 5 is a schematic diagram of the operation of the present invention.

In the figure: 1. a skip car; 11. a frame; 12. a mesh cover plate; 13. a first slideway; 14. a second slideway; 15. a roller; 16. a first connecting member; 17. a second connecting member; 2. a limiting component; 21. a baffle plate; 22. a limiting plate; 23. an L-shaped rotating rod; 24. a rotating sheet; 3. a net-shaped material basket; 31. a mesh floor; 32. using the side wall of the charging basket; 33. a ramp; 34. an opening; 35. a third connecting member; 36. a second pin shaft; 37. a pull handle; 4. a load bearing assembly; 41. a support; 42. a track; 43. lifting lugs; 44. a bracket opening; 45. a limit baffle; 46. a fourth connecting member; 47. a first pin.

Detailed Description

The present invention will be described in detail below with reference to the accompanying drawings and examples.

The present embodiment is only for explaining the present invention, and it is not limited to the present invention, and those skilled in the art can make modifications of the present embodiment without inventive contribution as needed after reading the present specification, but all of them are protected by patent law within the scope of the claims of the present invention.

The utility model provides an aircraft part heat treatment of conveniently getting material uses material device, as shown in figure 1 for conveniently take out the work piece, including the skip 1 that is used for loading the work piece, the netted charging basket 3 that is used for holding the work piece, be used for keeping out and promoting the spacing subassembly 2 that the work piece removed, be used for loading skip 1 and carry out the carrier assembly 4 that heat treats, netted charging basket 3 that is used is on a parallel with ground and with skip 1 sliding connection, spacing subassembly 2 is connected with skip 1, carrier assembly 4 is connected with skip 1.

Specifically, as shown in fig. 2, the skip 1 includes a frame 11 for loading a workpiece, a mesh-shaped cover plate 12 for covering a mesh-shaped basket 3 (see fig. 1), a first slide 13 for sliding the mesh-shaped basket 3, and a second slide 14 for sliding a workpiece storage box, the frame 11 is a rectangular frame, the frame 11 is connected to four rollers 15 for transporting the workpiece, a first connecting member 16 is fixedly connected to a lower portion of the frame 11, the first connecting member 16 is provided with through holes, the first connecting members 16 are four groups and are respectively located at four bottom corners of the frame 11, the mesh-shaped cover plate 12 is a square plate fixed to the frame 11, the mesh-shaped cover plate 12 is attached to a basket opening of the mesh-shaped basket 3, the mesh-shaped cover plate 12 is fixedly connected to the second connecting member 17, the connecting members are provided with through holes, the first slide 13 is a groove-shaped slide horizontally fixed to the frame 11 and located at two sides of the frame 11, the first slide 13 is slidably connected to the mesh-shaped basket 3, the net shape apron 12 is three groups and sets up along frame 11 vertical direction interval in this embodiment, and second slide 14 is the level and is fixed in frame 11 and is located the L type slide of frame 11 both sides, and second slide 14 is located the below of first slide 13.

As shown in fig. 3, the limiting component 2 includes a baffle 21 for resisting and pushing the workpiece to move, a limiting plate 22 for limiting rotation of the baffle 21, an L-shaped rotating rod 23 for retracting the baffle 21, the baffle 21 is a rectangular plate, the baffle 21 is hinged to the mesh-shaped cover plate 12, the baffle 22 can rotate around the mesh-shaped cover plate 12, the limiting plate 22 is a rectangular plate, the limiting plate 22 is fixed and perpendicular to the mesh-shaped cover plate 12, the L-shaped rotating rod 23 passes through a hole of the mesh-shaped cover plate 12 and is rotationally connected with the mesh-shaped cover plate 12, the baffle 21 is overlapped on the L-shaped rotating rod 23, and the L-shaped rotating rod 23 is fixedly connected with a rotating sheet 24 for conveniently rotating the L-shaped rotating rod 23.

As shown in fig. 3, the mesh-shaped basket 3 includes a mesh-shaped bottom plate 31, basket side walls 32 and a ramp 33 for sliding down the workpiece, the mesh-shaped bottom plate 31 is a square mesh plate, the basket side walls 32 are perpendicular to the mesh-shaped bottom plate 31 and fixedly connected with the mesh-shaped bottom plate 31 in a U-shape, the side of the mesh-shaped bottom plate 31, which is not provided with the basket side walls 32, is fixedly connected with the ramp 33, the mesh-shaped basket 3 is provided with an opening 34 for sliding out the workpiece, wherein the ramp 33 is in a mesh-shaped structure, the basket side walls 32 on the opposite side of the ramp 33 are fixedly connected with a third connecting member 35, the third connecting member 35 is provided with a through hole, the second connecting member 17 and the third connecting member 35 are connected through a second pin shaft 36, the basket side walls 32 on the opposite side of the ramp 33 are fixedly connected with a pull handle 37, and the pull handle 37 is in a U-shaped structure.

As shown in fig. 4, the carrier assembly 4 includes a bracket 41 for loading the skip 1, a rail 42 for facilitating movement of the skip 1 (see fig. 1), the lifting lugs 43 are used for driving the skip car 1 to lift, the support 41 is a rectangular frame capable of accommodating the skip car 1, one side of the side wall of the support 41 is provided with a support opening 44 through which the skip car 1 enters and exits, a limit baffle 45 is mounted on the support 41 on the opposite side of the support opening 44, the rail 42 is parallel to the ground and is fixedly connected with the support 41, the rail 42 extends towards the support opening 44, the lifting lugs 43 are mounted at the top end of the support 41, the lifting lugs 43 are annular, in the embodiment, 3 lifting lugs 43 are provided, the bottom of the support 41 is provided with a fourth connecting piece 46, the fourth connecting piece 46 is provided with a through hole, in the embodiment, the fourth connecting pieces 46 are provided in four groups, and the fourth connecting piece 46 is connected with the first connecting piece 16 through a first pin shaft 47 (see fig. 5).

The working process and principle of the embodiment are as follows:

as shown in fig. 3 and 5, when using the utility model, take out netted charging basket 3 along first slide 13, put into netted charging basket 3 with aircraft part, then push charging cart 1 with netted charging basket 3 along first slide 13, until second connecting piece 17 and third connecting piece 35 laminate each other, insert second round pin axle 36 and fix netted charging basket 3.

As shown in fig. 3 and 5, after each layer of mesh baskets 3 is completely fixed in the skip car 1, the skip car 1 is pushed to move towards the support opening 44 of the support 41, the skip car 1 moves along the track 42 until the skip car 1 contacts the limit baffle 45 in the support 41, at this time, the through holes of the first connecting piece 16 and the fourth connecting piece 46 are overlapped, the first pin 47 is inserted to fix the position of the skip car 1, then, the rigging drives the support 41 and the skip car 1 in the support 41 to ascend into the heating furnace through the lifting lug 43 for heat treatment, after the heating is completed, the support 41 and the skip car 1 start to descend to the surface of the machine for water washing and cooling, after the cooling is completed, the work storage basket is pushed into the skip car 1 along the second slide way 14, the rotating piece 24 is pulled to drive the L-shaped rotating rod 23, the baffle 21 overlapped on the L-shaped rotating rod 23 rotates under the action of gravity until the baffle 21 is perpendicular to the mesh cover plate 12, the mesh-shaped charging basket 3 is pulled out, the airplane parts are driven by the mesh-shaped charging basket 3 to move until the airplane parts abut against the baffle 21, the baffle plate 22 prevents the baffle 21 from continuing to rotate, the baffle 21 pushes the airplane parts to move along the opening 34 along with the movement of the mesh-shaped charging basket 3 and fall into the workpiece storage basket from the opening 34, and finally the workpiece storage basket is taken out.

The above description is only a preferred embodiment of the present invention, and the protection scope of the present invention is not limited to the above embodiments, and all technical solutions belonging to the idea of the present invention belong to the protection scope of the present invention. It should be noted that modifications and embellishments within the scope of the utility model may occur to those skilled in the art without departing from the principle of the utility model, and are considered to be within the scope of the utility model.

Claims

1. The utility model provides an aircraft part heat treatment of conveniently getting material uses material device, includes skip (1) that is used for loading the work piece, its characterized in that: the material loading device is characterized by further comprising a net-shaped material basket (3) which is parallel to the ground and is connected with the skip car (1) in a sliding mode and used for containing workpieces, an opening (34) used for sliding out the workpieces is formed in the net-shaped material basket (3), a limiting component (2) which is connected with the skip car (1) and used for resisting and pushing the workpieces to move towards the opening (34) and a bearing component (4) which is connected with the skip car (1) and used for loading the skip car (1) for heat treatment are further included.

2. The aircraft part heat treatment material taking device convenient to take materials as claimed in claim 1, characterized in that: the skip (1) comprises a frame (11) used for loading workpieces, a net-shaped cover plate (12) which is attached to and fixed on the frame (11) through a basket opening of the net-shaped charging basket (3), a first slide way (13) which is horizontally fixed on the frame (11) and is in sliding connection with the net-shaped charging basket (3), and a second slide way (14) which is horizontally fixed on the frame (11) and is positioned below the first slide way (13).

3. The aircraft part heat treatment material taking device convenient to take materials as claimed in claim 2, characterized in that: spacing subassembly (2) include with netted apron (12) articulated baffle (21), be fixed in netted apron (12) are used for restricting baffle (21) pivoted limiting plate (22), with netted apron (12) rotate to be connected and with baffle (21) lapped L shape dwang (23).

4. The aircraft part heat treatment material taking device convenient to take materials as claimed in claim 1, characterized in that: the bearing assembly (4) comprises a support (41) used for loading the skip car (1), a track (42) fixed on the support (41) and connected with the skip car (1), and a lifting lug (43) fixedly connected with the support (41).

5. The aircraft part heat treatment material taking device convenient to take materials as claimed in claim 4, wherein: the support (41) is connected with the skip car (1) through a first pin shaft (47).

6. The aircraft part heat treatment material taking device convenient to take materials as claimed in claim 2, characterized in that: the reticular cover plate (12) is connected with the reticular charging basket (3) through a second pin shaft (36).

7. The aircraft part heat treatment material device convenient for taking materials as claimed in any one of claims 1 to 6, is characterized in that: the reticular charging basket (3) is fixedly connected with a drawing handle (37).

8. The aircraft part heat treatment material device convenient for taking materials as claimed in any one of claims 1 to 6, is characterized in that: the opening (34) of the reticular charging basket (3) is provided with a ramp (33) for sliding the workpiece.