CN213080881U - Gear machine head of integrated numerical control machine tool - Google Patents

Abstract

The utility model relates to a digit control machine tool technical field just discloses gear aircraft nose of integral type digit control machine tool, which comprises a motor, the other end of motor output shaft is provided with the belt, just the belt with motor drive connects, belt top inboard is provided with the belt pulley, just the belt pulley with belt drive connects, the inside right side of belt pulley is provided with the axis of rotation, just the axis of rotation with belt pulley fixed connection. This gear aircraft nose of integral type digit control machine tool, through setting up the solid fixed ring of safety cover and safety cover, the safety cover passes through the fixture block and installs the inside at the solid fixed ring of safety cover, add man-hour to the part at processing machine head, fix the solid fixed ring of safety cover in the right-hand member outside of processing aircraft nose, then install the safety cover in the solid fixed ring's of safety cover inside, avoid processing aircraft nose when adding the gear head and produce the fracture and fly away, the security of processing environment has been improved, consequently, the practicality of the gear aircraft nose of this digit control machine.

Description

Gear machine head of integrated numerical control machine tool

Technical Field

The utility model relates to a digit control machine tool technical field, the gear aircraft nose of specific formula digit control machine tool as an organic whole.

Background

The numerical control machine tool is a digital control machine tool for short, and is an automatic machine tool equipped with a program control system, said control system can logically process and decode the program defined by control code or other symbolic instruction, and can use coded digital representation, and can utilize information carrier to input it into numerical control device, and can utilize the numerical control device to give out various control signals to control the action of machine tool so as to automatically machine the part according to the form and size required by drawing.

At present, the processing aircraft nose of current digit control machine tool is adding the processing and probably producing the fracture to the part, leads to cracked tooth head to fly away easily, probably causes on-the-spot operating personnel to receive the injury, consequently needs to improve the gear aircraft nose of this digit control machine tool.

SUMMERY OF THE UTILITY MODEL

The utility model provides a not enough to prior art, the utility model provides a gear aircraft nose of integral type digit control machine tool possesses the security that improves the processing link and is convenient for carry out the advantage dismantled to the safety cover, and the processing aircraft nose of having solved current digit control machine tool is adding the part and is adding and probably producing the fracture, leads to cracked tooth head to fly away easily, probably causes the operating personnel on site to receive the injury, consequently needs to carry out the modified problem to the gear aircraft nose of this digit control machine tool.

The utility model provides a following technical scheme: the gear head of the integrated numerical control machine tool comprises a motor, a belt is arranged at the other end of an output shaft of the motor and is in transmission connection with the motor, a belt pulley is arranged on the inner side of the top end of the belt and is in transmission connection with the belt, a rotating shaft is arranged on the right side inside the belt pulley and is fixedly connected with the belt pulley, a fixed shaft is arranged on the outer side of the rotating shaft and is movably connected with the rotating shaft, a mounting ring is arranged on the right side outside the fixed shaft and is detachably connected with the fixed shaft, a telescopic rod is arranged on the right side of the mounting ring and is movably connected with the mounting ring, a protective cover fixing ring is arranged on the right side of the telescopic rod and is fixedly connected with the telescopic rod, a bottom rod is arranged on the right side of the mounting ring, just the sill bar with collar fixed connection, the spout has been seted up in the sill bar outside, the axis of rotation right-hand member outside is provided with the processing aircraft nose, just the processing aircraft nose with the connection can be dismantled to the axis of rotation, the solid fixed ring inboard of safety cover is provided with the safety cover, just the safety cover with the solid fixed ring of safety cover can be dismantled and be connected.

Preferably, the motor and the pulley are rotatably connected through the rotating shaft.

Preferably, the number of the bottom rods is two, and the two bottom rods are symmetrically fixed at the front end and the rear end of the right side of the mounting ring.

Preferably, the shape of the protective cover fixing ring is semicircular, and the protective cover fixing ring and the bottom rod are in sliding connection through the sliding groove.

Preferably, the protective cover outside is provided with the fixture block, just the fixed ring of protective cover with the protective cover passes through the connection can be dismantled to the fixture block.

Preferably, an extension spring is arranged inside the telescopic rod and fixedly connected with the telescopic rod.

Compared with the prior art, the utility model discloses possess following beneficial effect:

1. this gear aircraft nose of integral type digit control machine tool, through setting up the solid fixed ring of safety cover and safety cover, the safety cover passes through the fixture block and installs the inside at the solid fixed ring of safety cover, add man-hour to the part at processing machine head, fix the solid fixed ring of safety cover in the right-hand member outside of processing aircraft nose, then install the safety cover in the solid fixed ring's of safety cover inside, avoid processing aircraft nose when adding the gear head and produce the fracture and fly away, the security of processing environment has been improved, consequently, the practicality of the gear aircraft nose of this digit control machine.

2. This gear aircraft nose of integral type digit control machine tool, through setting up telescopic link and spout, when needs use the safety cover, with the solid fixed ring of safety cover pass through telescopic link and spout to the right-hand member outside of processing aircraft nose, when not using, with the solid fixed ring of safety cover accomodate through telescopic link and spout can, consequently increased the practicality of the gear aircraft nose of this digit control machine tool.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic side view of the protective cover of the present invention;

fig. 3 is a schematic view of the telescopic rod structure of the present invention.

In the figure: 1. a telescopic rod; 2. a protective cover fixing ring; 3. processing a machine head; 4. a bottom bar; 5. a chute; 6. a motor; 7. a belt; 8. a belt pulley; 9. a rotating shaft; 10. a fixed shaft; 11. a mounting ring; 12. a protective cover; 13. a telescoping spring.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-3, the gear machine head of the integrated numerical control machine tool comprises a motor 6, a belt 7 is arranged at the other end of an output shaft of the motor 6, the belt 7 is in transmission connection with the motor 6, a belt pulley 8 is arranged at the inner side of the top end of the belt 7, the belt pulley 8 is in transmission connection with the belt 7, the motor 6 is in rotation connection with the belt pulley 8 through a rotation shaft 9, the rotation shaft 9 is arranged at the right side inside the belt pulley 8, the rotation shaft 9 is fixedly connected with the belt pulley 8, a fixed shaft 10 is arranged at the outer side of the rotation shaft 9, the fixed shaft 10 is movably connected with the rotation shaft 9, a mounting ring 11 is arranged at the right side outside the fixed shaft 10, the mounting ring 11 is detachably connected with the fixed shaft 10, a telescopic rod 1 is arranged at the right side of the mounting, the solid fixed ring 2's of safety cover shape is semi-circular, and solid fixed ring 2 of safety cover and sill bar 4 pass through 5 sliding connection of spout, 11 right sides of collar are close to 1 bottom of telescopic link and are provided with sill bar 4, and sill bar 4 and 11 fixed connection of collar, sill bar 4 is provided with two, two 4 symmetries of sill bar are fixed at the front and back both ends on the 11 right sides of collar, spout 5 has been seted up in the sill bar 4 outside, the 9 right-hand members of axis of rotation outside is provided with processing aircraft nose 3, and processing aircraft nose 3 can dismantle with axis of rotation 9 and be connected, solid fixed ring 2 inboard of safety cover is provided with safety cover 12, and safety cover 12 can dismantle with solid fixed ring 2 of safety cover and be connected, and solid fixed ring 2 of safety cover and safety cover 12 can dismantle the connection through.

The during operation, when using safety cover 12, with the solid fixed ring of safety cover 2 remove to the right-hand member outside of processing aircraft nose 3 through telescopic link 1 and spout 5, then install safety cover 12 in the solid fixed ring of safety cover 2's inside through the fixture block, avoid processing aircraft nose 3 when adding the gear head and produce the fracture and rush away, the security of processing environment has been improved, for the circular telegram of motor 6, motor 6 drives belt pulley 8 through belt 7 and rotates, belt pulley 8 drives processing aircraft nose 3 through axis of rotation 9 and rotates and process the part.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. Gear aircraft nose of integral type digit control machine tool, including motor (6), its characterized in that: the other end of the output shaft of the motor (6) is provided with a belt (7), the belt (7) is in transmission connection with the motor (6), the belt (7) is provided with a belt pulley (8) on the inner side of the top end, the belt pulley (8) is in transmission connection with the belt (7), the right side inside the belt pulley (8) is provided with a rotating shaft (9), the rotating shaft (9) is fixedly connected with the belt pulley (8), the outer side of the rotating shaft (9) is provided with a fixed shaft (10), the fixed shaft (10) is movably connected with the rotating shaft (9), the right side outside the fixed shaft (10) is provided with a mounting ring (11), the mounting ring (11) is detachably connected with the fixed shaft (10), the right side of the mounting ring (11) is provided with a telescopic rod (1), and the telescopic rod (1) is movably connected with the mounting ring (11), telescopic link (1) right side is provided with the solid fixed ring of safety cover (2), just the solid fixed ring of safety cover (2) with telescopic link (1) fixed connection, collar (11) right side is close to telescopic link (1) bottom is provided with sill bar (4), just sill bar (4) with collar (11) fixed connection, spout (5) have been seted up in the sill bar (4) outside, axis of rotation (9) right-hand member outside is provided with processing aircraft nose (3), just processing aircraft nose (3) with the connection can be dismantled in axis of rotation (9), the solid fixed ring of safety cover (2) inboard is provided with safety cover (12), just safety cover (12) with the solid fixed ring of safety cover (2) can be dismantled and be connected.

2. The gear head of an integrated numerical control machine tool according to claim 1, characterized in that: the motor (6) and the belt pulley (8) are rotationally connected through the rotating shaft (9).

3. The gear head of an integrated numerical control machine tool according to claim 1, characterized in that: the two bottom rods (4) are symmetrically fixed at the front end and the rear end of the right side of the mounting ring (11).

4. The gear head of an integrated numerical control machine tool according to claim 1, characterized in that: the shape of the protective cover fixing ring (2) is semicircular, and the protective cover fixing ring (2) is connected with the bottom rod (4) in a sliding mode through the sliding groove (5).

5. The gear head of an integrated numerical control machine tool according to claim 1, characterized in that: the outer side of the protective cover (12) is provided with a clamping block, and the protective cover fixing ring (2) and the protective cover (12) are detachably connected through the clamping block.

6. The gear head of an integrated numerical control machine tool according to claim 1, characterized in that: the telescopic rod (1) is internally provided with a telescopic spring (13), and the telescopic spring (13) is fixedly connected with the telescopic rod (1).

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