CN-224227145-U - Surface hardening treatment device for aviation parts

Abstract

The utility model relates to the technical field of surface treatment of aviation parts, in particular to a surface hardening treatment device for aviation parts. The utility model provides an aviation part surface hardening treatment device which can enable a gear part and a laser heat processor to reversely rotate and improve the uniformity and consistency of gear hardening. The surface hardening treatment device for the aviation parts comprises a base, a first motor, a bevel gear and the like, wherein the upper side of the right part of the base is connected with the first motor, and the output shaft of the first motor is connected with the bevel gear. According to the utility model, the first motor is started to drive the bevel gear to move in a meshing way, the rotating shaft is driven to rotate, so that the rotating frame and the rotating table rotate reversely, and the laser heat processor is started to carry out surface hardening treatment on the gear part, so that the gear part and the laser heat processor can rotate reversely, and the effect of improving the uniformity and consistency of gear hardening is achieved.

Inventors

• SUN RULING

Assignees

• 九江恒川机电科技有限公司

Dates

Publication Date

20260512

Application Date

20250616

Claims (6)

1. 1. The utility model provides an aviation spare part case hardening processing apparatus, a serial communication port, including base (1), first motor (2), bevel gear (3), pivot (4), swivel mount (5), processing unit and place the subassembly, base (1) right part upside is connected with first motor (2), be connected with bevel gear (3) on the output shaft of first motor (2), base (1) middle part rotation type is connected with pivot (4), pivot (4) lower part also is connected with bevel gear (3), pivot (4) upper portion rotation type is connected with bevel gear (3), two adjacent bevel gear (3) intermeshing, pivot (4) upper portion rotation type is connected with swivel mount (5), bevel gear (3) of upside are connected with swivel mount (5), be equipped with on swivel mount (5) and carry out the processing unit of case hardening processing to aviation spare part, be equipped with on pivot (4) and place the subassembly that can place aviation spare part.
2. 2. The surface hardening treatment device for aviation components according to claim 1, further comprising rollers (6), wherein the left and right parts of the rotating frame (5) are respectively connected with an upper roller (6) and a lower roller (6) in a rotating manner, and the two rollers (6) on the lower side are respectively in contact fit with the base (1).
3. 3. The surface hardening treatment device for aviation components according to claim 1, wherein the treatment assembly comprises a screw rod (7), a sliding block (8), an electric push rod (9) and a laser heat processor (10), the screw rod (7) is rotationally connected to the right part of the rotating frame (5), the sliding block (8) is connected to the screw rod (7) in a threaded manner, the sliding block (8) is slidably connected with the rotating frame (5), the electric push rod (9) is connected to the upper side of the sliding block (8), and the laser heat processor (10) is connected to the telescopic end of the electric push rod (9).
4. 4. A surface hardening treatment device for aeronautical parts according to claim 3, characterised in that the right side of the screw (7) is provided with a grip.
5. 5. The surface hardening treatment device for aviation components according to claim 1, wherein the placement assembly comprises a rotary table (11), a rotary table (12), a second motor (13), a common gear (14) and an adjusting rod (15), the rotary table (11) is connected to the upper side of the rotary shaft (4), rollers (6) on the upper side are in contact fit with the rotary table (11), the rotary table (12) is rotatably connected to the upper side of the middle part of the rotary table (11), the second motor (13) is connected to the lower part of the rotary table (11), the common gear (14) is connected to an output shaft of the second motor (13), the common gear (14) is also connected to the rotary table (12), the common gear (14) is meshed with each other, and a plurality of adjusting rods (15) are connected between the rotary table (11) and the rotary table (12) in a sliding mode.
6. 6. The surface hardening treatment device for aviation components according to claim 5, wherein the adjusting rods (15) are provided with soft cushions.

Description

Surface hardening treatment device for aviation parts Technical Field The utility model relates to the technical field of surface treatment of aviation parts, in particular to a surface hardening treatment device for aviation parts. Background In aviation components, particularly critical components such as gears, the gear surface is typically hardened to ensure that the gear remains high in hardness, wear resistance and fatigue resistance under extreme operating conditions. The existing surface hardening treatment device for aviation parts generally fixes a gear on a workbench, and then enables a laser heat processor to emit laser to harden the surface of the gear, but the gear is usually fixed when hardening treatment is carried out, and the surface of the gear is only treated through rotation of the laser heat processor, so that hardening uniformity and consistency are difficult to ensure. Therefore, an aeronautical part surface hardening treatment device capable of reversely rotating a gear part and a laser heat processor and improving the uniformity and consistency of gear hardening is now developed. Disclosure of utility model In order to overcome the defect that the existing surface hardening treatment device for aviation parts is difficult to ensure hardening uniformity and consistency by only treating the surface of a gear through rotation of a laser heat processor when the gear is hardened, the utility model provides the surface hardening treatment device for aviation parts, which can enable the gear part and the laser heat processor to reversely rotate and improve the hardening uniformity and consistency of the gear. The technical scheme includes that the surface hardening treatment device for the aviation components comprises a base, a first motor, bevel gears, rotating shafts, rotating frames, treatment assemblies and placement assemblies, wherein the upper side of the right part of the base is connected with the first motor, the bevel gears are connected to output shafts of the first motor, the middle part of the base is rotatably connected with the rotating shafts, the lower part of the rotating shafts is also connected with the bevel gears, the upper parts of the rotating shafts are rotatably connected with the bevel gears, the adjacent two bevel gears are meshed with each other, the upper parts of the rotating shafts are rotatably connected with the rotating frames, the bevel gears on the upper sides of the rotating shafts are connected with the rotating frames, the treatment assemblies capable of carrying out surface hardening treatment on the aviation components are arranged on the rotating frames, and the placement assemblies capable of placing the aviation components are arranged on the rotating shafts. More preferably, the rotary rack further comprises rollers, wherein the left part and the right part of the rotary rack are both rotationally connected with an upper roller and a lower roller, and the two rollers at the lower side are both in contact fit with the base. More preferably, the processing assembly comprises a screw rod, a sliding block, an electric push rod and a laser heat processor, the right part of the rotating frame is rotationally connected with the screw rod, the screw rod is connected with the sliding block in a threaded manner, the sliding block is connected with the rotating frame in a sliding manner, the upper side of the sliding block is connected with the electric push rod, and the telescopic end of the electric push rod is connected with the laser heat processor. More preferably, the right side of the screw rod is provided with a handle. More preferably, place the subassembly including revolving stage, rotary disk, second motor, ordinary gear and regulation pole, the pivot upside is connected with the revolving stage, and the gyro wheel of upside all contacts the cooperation with the revolving stage, and the revolving stage middle part upside rotation is connected with the rotary disk, and the revolving stage lower part is connected with the second motor, is connected with ordinary gear on the second motor output shaft, also is connected with ordinary gear on the rotary disk, ordinary gear intermeshing, sliding connection has a plurality of regulation poles between revolving stage and the rotary disk. More preferably, soft cushions are arranged on the adjusting rods. Compared with the prior art, the utility model has the advantages that the first motor is started to drive the bevel gear to move in a meshing way to drive the rotating shaft to rotate, so that the rotating frame and the rotating table reversely rotate, and the laser heat processor is started to carry out surface hardening treatment on the gear part, thereby achieving the effects of reversely rotating the gear part and the laser heat processor and improving the uniformity and consistency of gear hardening. Drawings Fig. 1 is a schematic perspective view of the present utility model. Fig. 2 is a sche