CN210589407U

CN210589407U - Rotary hair clipper

Info

Publication number: CN210589407U
Application number: CN201921105274.1U
Authority: CN
Inventors: 卢德刚
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-07-15
Filing date: 2019-07-15
Publication date: 2020-05-22
Anticipated expiration: 2029-07-15

Abstract

The utility model relates to a rotation type hair clipper, including the casing, the casing front end is equipped with blade subassembly, is equipped with in the casing to be used for driving the motor of blade subassembly work and is used for the power supply unit for the motor power supply, still including the switch that is used for controlling motor work, the casing including fuselage and the aircraft nose that the components of a whole that can function independently set up, the aircraft nose setting is at the fuselage front end, the aircraft nose can be for fuselage normal running fit. Adopt above-mentioned technical scheme, the utility model provides a rotation type hair clipper, it can change the angle of blade subassembly through rotating the aircraft nose, and then can satisfy the demand of pruning and different hairdressers to different positions, and it is more convenient to use, and is more practical.

Description

Rotary hair clipper

Technical Field

The utility model relates to a hair clipper, in particular to a rotary hair clipper.

Background

The existing hair clipper comprises a casing, wherein a blade assembly is arranged at the front end of the casing, a motor used for driving the blade assembly to work and a power supply unit used for supplying power to the motor are arranged in the casing, and a switch used for controlling the motor to work is further arranged on the casing. Because when pruning different positions, need change blade subassembly's angle, different barber's operation custom is different moreover, and the mode that leads to holding the casing is different, but, the hair clipper of this kind of structure, the integrative setting of casing can only hold the angle that the position changed blade subassembly through barber's own adjustment, and it uses inconveniently, and the practicality is poor.

Disclosure of Invention

The utility model aims at: in order to overcome the defects of the prior art, the utility model provides a rotation type hair clipper, it can change the angle of blade subassembly through rotating the aircraft nose, and then can satisfy the demand of pruning and different hairdressers to different positions, and it is more convenient to use, and is more practical.

The technical scheme of the utility model: the utility model provides a rotation type hair clipper, includes the casing, and the casing front end is equipped with blade subassembly, is equipped with in the casing to be used for the motor of drive blade subassembly work and is used for the power supply unit for the motor power supply, still including the switch that is used for controlling motor work, its characterized in that: the machine shell comprises a machine body and a machine head which are arranged in a split mode, the machine head is arranged at the front end of the machine body, the blade assembly is arranged at the front end of the machine head, and the machine head can be matched with the machine body in a rotating mode.

Adopt above-mentioned technical scheme, because blade subassembly sets up at the aircraft nose front end, the aircraft nose can be for fuselage normal running fit, can rotate the aircraft nose like this and change the angle of blade subassembly, and then can satisfy the demand of pruning and different hairdressers to different positions, it is more convenient to use, and is more practical.

The utility model discloses a further setting: the motor sets up in the aircraft nose, and the power supply unit sets up in the fuselage, and the switch setting all is equipped with the through wires hole on the fuselage, aircraft nose rear end and fuselage front end.

Adopt above-mentioned further setting, this kind of motor, power supply unit and switch setting mode, rationally distributed, the transmission between motor and the blade subassembly of can being convenient for is connected, moreover, the electricity of the power supply unit of being convenient for is connected.

The utility model discloses a further setting again: and a gear mechanism for controlling the rotation angle of the machine head is arranged between the machine head and the machine body.

Adopt above-mentioned further setting again, can carry out the gear location when the aircraft nose rotates different angles, it is more convenient to use.

The utility model discloses a still further set up: the aircraft nose front end be equipped with the go-between, the rear end of aircraft nose is equipped with the carousel, the carousel cup joints and rotatable fit with the go-between, the carousel front end still is equipped with spacing piece, spacing piece and fuselage fixed connection.

By adopting the above further arrangement, the turntable and the connecting ring are sleeved to realize the rotating fit of the machine body and the machine body, the structure is simple, the rotation is stable, and the spacing piece can prevent the machine head from being separated from the machine body.

The utility model discloses a still further set up: the gear mechanism comprises a gear block arranged at the front end of the machine body in a sliding mode, one end of the gear block is a locking end, a spring is arranged between the other end of the gear block and the machine body, and a plurality of gear grooves for enabling the locking end of the gear block to slide into are formed in the rotary disc around the center of the rotary disc.

By adopting the above further arrangement, when the gear block slides into the next gear groove from one gear groove, the spring is firstly compressed and then reset, and the gear mechanism is simple in structure and good in stability.

The utility model discloses a still further set up: the rotary disc is provided with an annular groove corresponding to the connecting ring, the connecting ring can be rotatably inserted into the annular groove, the gear block is arranged in the connecting ring, and the gear groove is formed in the inner ring surface of the rotary disc.

By adopting the above further arrangement, the whole structure is more compact, the layout is reasonable, and the stability is good.

The utility model discloses a still further set up: gear piece including locking piece and deflector, the fuselage front end is equipped with the guide way, the deflector slides and sets up in the guide way, the tip of locking piece is the toper and forms the locking end, guide way one side is equipped with the opening that supplies the locking piece business turn over, spring one end is contradicted with the deflector, the other end is contradicted with the inner wall of guide way opposite side.

By adopting the above further arrangement, the sliding of the gear block is more stable through the matching of the guide plate and the guide groove; the tapered locking end may facilitate movement of the block into and out of the notch.

The utility model discloses a still further set up: the gear blocks are symmetrically arranged, the springs and the guide grooves are arranged corresponding to the gear blocks, and the threading holes in the machine body are formed between the two guide grooves.

Adopt above-mentioned further setting again for stability is better when the aircraft nose rotates, and the through wires hole setting on the fuselage is between two guide ways, and the structure is compacter.

The utility model discloses a still further set up: the machine head comprises a left shell and a right shell which are arranged in a split mode, the left shell is fixedly connected with the right shell, and the rotary table is arranged at the rear end of the left shell.

By adopting the above further arrangement, the connection between the machine head and the machine body and the installation of each part in the machine head can be facilitated.

The utility model discloses a still further set up: the blade subassembly including moving blade and quiet blade, the moving blade can slide relative to quiet blade, is connected with the transmission shaft on the output shaft of motor, the relative output shaft eccentric settings of transmission shaft is equipped with the drive groove on the moving blade, the transmission shaft extends to the drive inslot, the motor rotates and drives the moving blade through transmission shaft, drive groove and slide.

By adopting the above further arrangement, the motor rotates, the motor output shaft drives the transmission shaft to rotate, and the transmission shaft is eccentrically arranged relative to the output shaft and can be matched with the inner wall of the transmission groove to drive the movable blade to slide and the fixed blade to be matched to realize shearing operation.

Drawings

FIG. 1 is an overall block diagram of an embodiment of the present invention;

FIG. 2 is a view showing an internal structure of a handpiece according to an embodiment of the present invention;

FIG. 3 is a view of the front structure of the body according to an embodiment of the present invention;

FIG. 4 is a rear end structure diagram of a turntable according to an embodiment of the present invention;

FIG. 5 is a front structure diagram of a turntable according to an embodiment of the present invention;

FIG. 6 is a block diagram of a gear shift in an embodiment of the present invention;

FIG. 7 is a view of the installation structure of the spacing piece according to the embodiment of the present invention;

FIG. 8 is a view showing the internal structure of the body according to the embodiment of the present invention;

fig. 9 is a structural diagram after the utility model is rotated by 180 degrees.

Detailed Description

As shown in fig. 1-9, a rotary hair clipper comprises a casing 1, a blade assembly 2 is arranged at the front end of the casing 1, a motor 3 for driving the blade assembly 2 to work and a power supply unit 4 for supplying power to the motor 3 are arranged in the casing 1, the power supply unit 4 comprises a battery 41, a circuit board 42 and a switch 5 for controlling the motor 3 to work, the motor 3, the switch 5 and the battery 41 are all connected with the circuit board 42, the switch 5 can adopt a press switch, a slide switch or an induction switch, etc., the casing 1 comprises a machine body 11 and a machine head 12 which are separately arranged, the machine head 12 is arranged at the front end of the machine body 11, the blade assembly 2 is arranged at the front end of the machine head 12, the machine head 12 can be rotatably matched with the machine body 11, a gear mechanism 6 for controlling the rotation angle of the machine head 12 is further arranged between the machine head 12 and the machine body 11, the motor, the power supply unit 4 is arranged in the machine body 11, the switch 5 is arranged on the machine body 11, and the rear end of the machine head 12 and the front end of the machine body 11 are provided with threading holes.

The utility model discloses in the concrete embodiment, fuselage 11 front end be equipped with go-between 111, the rear end of aircraft nose 12 is equipped with carousel 120, the hole of carousel 120 forms the through wires hole, carousel 120 cup joints and rotatable fit with go-between 111, the carousel 120 front end still is equipped with spacing piece 7, spacing piece 7 is through bolt fixed connection with fuselage 11, certainly also can adopt modes such as buckles fixed. The gear mechanism 6 comprises a gear block 61 arranged at the front end of the machine body 11 in a sliding manner, one end of the gear block 61 is a locking end 610, a spring 62 is arranged between the other end of the gear block 61 and the machine body 11, and a plurality of gear grooves 63 for the locking ends of the gear block 61 to slide into are arranged on the rotary disc 120 around the center thereof; an annular groove 1201 is arranged on the rotary disc 120 corresponding to the connecting ring 111, the connecting ring 111 is rotatably inserted into the annular groove 1201, the gear block 61 is arranged in the connecting ring 111, and the gear groove 63 is arranged on the inner ring surface of the rotary disc 120. The gear block 61 includes a locking block 611 and a guide plate 612, the front end of the body 11 is provided with a guide groove 112, the guide plate 612 is slidably disposed in the guide groove 112, the end of the locking block 611 is tapered to form a locking end 610, one side of the guide groove 112 is provided with an opening 1121 for the locking block 6 to go in and out, one end of the spring 62 abuts against the guide plate 612, and the other end abuts against the inner wall of the other side of the guide groove 112. In the embodiment of the present invention, the gear block 61 is symmetrically provided with two, the spring 62 and the guide groove 112 are provided with two corresponding gear blocks 61, and the threading hole 110 on the body 11 is provided between the two guide grooves 112. The utility model discloses in the concrete embodiment, only set up two gears, initial gear and rotatory 180 degrees gears, of course, can set up more gears as required, like 45 degrees gears, 90 degrees gears etc.

The machine head 12 comprises a left shell 121 and a right shell 122 which are arranged in a split mode, the left shell 121 and the right shell 122 are fixedly connected through bolts, the rotary table 120 is arranged at the rear end of the left shell 121, the blade assembly 2 comprises a movable blade 21 and a fixed blade 22, the movable blade 21 can slide relative to the fixed blade 22, a transmission shaft 23 is connected to an output shaft 31 of the motor 3, the transmission shaft 23 is eccentrically arranged relative to the output shaft 31, a transmission groove 211 is formed in the movable blade 21, the transmission shaft 23 extends into the transmission groove 211, and the motor 3 rotates to drive the movable blade 21 to slide through the transmission shaft 23 and the transmission groove 211.

Claims

1. The utility model provides a rotation type hair clipper, includes the casing, and the casing front end is equipped with blade subassembly, is equipped with in the casing to be used for the motor of drive blade subassembly work and is used for the power supply unit for the motor power supply, still including the switch that is used for controlling motor work, its characterized in that: the machine shell comprises a machine body and a machine head which are arranged in a split mode, the machine head is arranged at the front end of the machine body, the blade assembly is arranged at the front end of the machine head, and the machine head can be matched with the machine body in a rotating mode.

2. The rotary hair clipper according to claim 1, wherein: the motor sets up in the aircraft nose, and the power supply unit sets up in the fuselage, and the switch setting all is equipped with the through wires hole on the fuselage, aircraft nose rear end and fuselage front end.

3. The rotary hair clipper according to claim 1 or 2, wherein: and a gear mechanism for controlling the rotation angle of the machine head is arranged between the machine head and the machine body.

4. The rotary hair clipper of claim 3, wherein: the aircraft nose front end be equipped with the go-between, the rear end of aircraft nose is equipped with the carousel, the carousel cup joints and rotatable fit with the go-between, the carousel front end still is equipped with spacing piece, spacing piece and fuselage fixed connection.

5. The rotary hair clipper of claim 4, wherein: the gear mechanism comprises a gear block arranged at the front end of the machine body in a sliding mode, one end of the gear block is a locking end, a spring is arranged between the other end of the gear block and the machine body, and a plurality of gear grooves for enabling the locking end of the gear block to slide into are formed in the rotary disc around the center of the rotary disc.

6. The rotary hair clipper of claim 5, wherein: the rotary disc is provided with an annular groove corresponding to the connecting ring, the connecting ring can be rotatably inserted into the annular groove, the gear block is arranged in the connecting ring, and the gear groove is formed in the inner ring surface of the rotary disc.

7. The rotary hair clipper according to claim 5 or 6, wherein: gear piece including locking piece and deflector, the fuselage front end is equipped with the guide way, the deflector slides and sets up in the guide way, the tip of locking piece is the toper and forms the locking end, guide way one side is equipped with the opening that supplies the locking piece business turn over, spring one end is contradicted with the deflector, the other end is contradicted with the inner wall of guide way opposite side.

8. The rotary hair clipper of claim 7, wherein: the gear blocks are symmetrically arranged, the springs and the guide grooves are arranged corresponding to the gear blocks, and the threading holes in the machine body are formed between the two guide grooves.

9. The rotary hair clipper according to claim 4, 5 or 6, wherein: the machine head comprises a left shell and a right shell which are arranged in a split mode, the left shell is fixedly connected with the right shell, and the rotary table is arranged at the rear end of the left shell.

10. The rotary hair clipper of claim 9, wherein: the blade subassembly including moving blade and quiet blade, the moving blade can slide relative to quiet blade, is connected with the transmission shaft on the output shaft of motor, the relative output shaft eccentric settings of transmission shaft is equipped with the drive groove on the moving blade, the transmission shaft extends to the drive inslot, the motor rotates and drives the moving blade through transmission shaft, drive groove and slide.