CN218621365U - Novel split type lift aircraft nose - Google Patents

Abstract

The utility model relates to a novel split type lift aircraft nose, which comprises a fixed base, a supporting seat, lift power unit, the direction subassembly, the backplate, the connecting plate, the lift aircraft nose, the back pivot, back gear drive subassembly, middle pivot, preceding gear drive subassembly and front rotary shaft, fixing base the place ahead erection bracing seat, supporting seat the place ahead installation direction subassembly, backplate the place ahead fixed mounting connecting plate, connecting plate below fixed mounting lift, lift power unit drive lift aircraft nose oscilaltion, the lift aircraft nose can be in low position work and also can be in high position work, it also is favorable to processing thicker shoes to get the material after finishing to be favorable to processing, simultaneously in order to guarantee the sewing needle department of power transmission to the aircraft nose, the back pivot is through back gear drive subassembly, middle pivot, pivot before mutually supporting drive of preceding gear drive subassembly rotates, gear drive is stable reliable can in time order about the preceding pivot rotation, it is very convenient to use, practicality and flexibility are all very strong, satisfy production actual demand.

Description

Novel split type lift aircraft nose

Technical Field

The utility model relates to a shoes manufacture equipment field, concretely relates to novel split type lift aircraft nose of interior wiring machine.

Background

Interior line machine, be used for to sports shoes, shoes such as playshoes carry out the equipment of sideline processing, in the numerous component parts of interior line machine, the aircraft nose belongs to more important part, the aircraft nose of interior line machine all is fixed integral type structure in the existing market, the aircraft nose is integrative with fixing base lug connection, the defect of this kind of fixed integral type structure lies in, the position of aircraft nose can not be adjusted, inconvenient material of getting on the one hand, on the other hand also does not benefit to the thick shoes of processing, it is not convenient to use, in addition, because the aircraft nose of traditional aircraft nose is integrative with the fixing base lug connection, only need a pivot that extends to the aircraft nose by the fixing base can transmit power and pass the aircraft nose, if the aircraft nose is the components of a whole that can function independently structure with the fixing base, how to guarantee power transmission also be the problem of considering.

SUMMERY OF THE UTILITY MODEL

There are above-mentioned defects to prior art, the utility model aims to solve the technical problem that how solve interior wiring machine's fixed integral type structure aircraft nose provides a novel split type lift aircraft nose for this reason, and concrete technical scheme is as follows:

the utility model provides a novel split type lift aircraft nose, which comprises a fixed base, a supporting seat, lift power unit, the direction subassembly, the backplate, the connecting plate, the lift aircraft nose, the back pivot, back gear drive subassembly, middle pivot, preceding gear drive subassembly and preceding pivot, fixing base the place ahead erection bracing seat, installation lift power unit above the supporting seat, supporting seat the place ahead installation direction subassembly, direction subassembly the place ahead installation backplate, backplate the place ahead fixed mounting connecting plate, connecting plate below fixed mounting lift aircraft nose, lift power unit drive lift aircraft nose oscilaltion, the back pivot is located the fixing base, the back pivot is rotated through the middle pivot of back gear drive subassembly drive, the middle pivot is rotated through the preceding pivot of preceding gear drive subassembly drive, preceding pivot is located the lift aircraft nose.

As a preferred scheme, back gear drive assembly includes back gear mounting panel, back first gear, back second gear, back third gear, preceding gear drive assembly includes preceding gear mounting panel, preceding first gear, preceding second gear and preceding third gear, back gear mounting panel fixed mounting is in fixing base the place ahead, back gear mounting panel the place ahead is rotated first gear after the installation, back second gear, back third gear, back first gear meshes the back respectively, back third gear, first gear behind the back pivot front end cartridge, gear mounting panel before the installation of lift aircraft nose rear, first gear before the installation is rotated to preceding gear mounting panel rear, preceding second gear, preceding third gear, preceding second gear meshes preceding first gear respectively, preceding third gear, first gear before the preceding pivot rear end cartridge, third gear behind the preceding third gear of middle pivot front end cartridge.

As a preferred scheme of the utility model, lift power unit includes cylinder and connector, supporting seat top installation cylinder, and the piston rod of cylinder stretches out the supporting seat downwards, the piston rod lower extreme erection joint head of cylinder, connector lower extreme erection joint board.

As a preferred scheme of the utility model, the direction subassembly includes slide rail and slider, two slide rails of supporting seat the place ahead fixed mounting, the vertical setting of slide rail, a plurality of sliders of slide rail the place ahead sliding connection, slider the place ahead fixed mounting backplate.

As a preferred scheme of the utility model, lift aircraft nose top installation presses the material cylinder, and lift aircraft nose side rotates the installation and presses the material foot, presses the material cylinder drive to press the material foot lifting.

Has the advantages that: the elevating power mechanism drives the elevating machine head to ascend and descend, the elevating machine head can be in low position work and also can be in high position work, it also is favorable to processing thicker shoes to get the material after finishing processing, simultaneously in order to guarantee the sewing needle department of power transmission to the aircraft nose, the back pivot is through back gear drive subassembly, the middle pivot, the pivot is rotated before the drive of mutually supporting of preceding gear drive subassembly, the pivot is rotated before gear drive is reliable and stable can in time order about, it is very convenient to use, practicality and flexibility are all very strong, satisfy production actual demand.

Drawings

Fig. 1 is a perspective view of the present invention;

fig. 2 is an exploded view of the present invention;

fig. 3 is a perspective view of the rear rotary shaft, the rear gear transmission assembly, the middle rotary shaft, the front gear transmission assembly and the front rotary shaft of the present invention;

fig. 4 is a perspective view of the rear rotary shaft, the rear gear assembly, the intermediate rotary shaft, the front gear assembly and the front rotary shaft of the present invention matching with another viewing angle;

fig. 5 is a perspective view of the lifting mechanism of the present invention.

Detailed Description

The following description of the embodiments of the present invention will be made with reference to the accompanying drawings:

in the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the indicated position or element must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.

In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected" and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood as appropriate by those of ordinary skill in the art.

As shown in fig. 1-3, a novel split type lift aircraft nose, including fixing base 1, a support base 2, lift power unit 3, direction subassembly 4, backplate 5, connecting plate 6, lift aircraft nose 7, back pivot 8, back gear drive subassembly 9, middle pivot 10, preceding gear drive subassembly 11 and preceding pivot 12, fixing base 1 the place ahead erection bracing seat 2, lift power unit 3 is installed to supporting seat 2 top, 2 the place ahead erection bracing subassembly 4 of supporting seat, 4 the place ahead erection backplate 5 of direction subassembly, backplate 5 can take place the relative position change with supporting seat 2 through direction subassembly 4, backplate 5 the place ahead fixed mounting connecting plate 6, connecting plate 6 below fixed mounting lift aircraft nose 7, lift power unit 3 drive lift aircraft nose 7 oscilaltion, back pivot 8 is located fixing base 1, back pivot 8 passes through back gear drive subassembly 9 drive middle pivot 10 and rotates, middle pivot 10 rotates through preceding pivot 12 of front gear drive subassembly 11 drive, preceding pivot 12 is located lift aircraft nose 7.

Because the machine head and the fixed seat of the traditional machine head are directly connected into a whole, the power can be transmitted only by one rotating shaft extending from the fixed seat to the machine head. And the utility model discloses a fixing base 1 and lift aircraft nose 7 are the components of a whole that can function independently structure, in order to guarantee power transmission, as shown in fig. 3 and 4, back gear drive assembly 9 includes back gear mounting panel 91, back first gear 92, back second gear 93, back third gear 94, preceding gear drive assembly 11 includes preceding gear mounting panel 111, preceding first gear 112, preceding second gear 113 and preceding third gear 114, back gear mounting panel 91 fixed mounting is in fixing base 1 the place ahead, first gear 92 after the installation is rotated to back gear mounting panel 91 the place ahead, back second gear 93, back third gear 94, back second gear 93 meshes back first gear 92 respectively, back third gear 94, first gear 92 behind the 8 front end cartridge of back pivot, lift aircraft nose 7 rear installation front gear mounting panel 111, preceding first gear 112 is rotated to preceding gear mounting panel 111 rear installation, preceding second gear 113, preceding third gear 114, preceding second gear 113 meshes preceding first gear 112 respectively, preceding third gear 113, preceding pivot 12 rear end cartridge gear 112, third gear 94 is installed to middle pivot front end cartridge before 10 rear end cartridge. The rear rotating shaft 8 drives the rear first gear 92 to rotate, the rear first gear 92 drives the rear second gear 93 to rotate, the rear second gear 93 drives the rear third gear 94 to rotate, the rear third gear 94 drives the middle rotating shaft 10 to rotate, the middle rotating shaft 10 drives the front third gear 114 to rotate, the front third gear 114 drives the front second gear 113 to rotate, the front second gear 113 drives the front first gear 112 to rotate, the front first gear 112 drives the front rotating shaft 12 to rotate, bearings are respectively arranged between the middle rotating shaft 10 and the rear gear mounting plate 91 and between the middle rotating shaft 10 and the front gear mounting plate 111, when the elevator head ascends, the front gear mounting plate 111 can rotate around the middle rotating shaft 10, and power transmission cannot be influenced.

As shown in fig. 5, the lifting power mechanism 3 includes a cylinder 31 and a connector 32, the cylinder 31 is installed above the support seat 2, a piston rod of the cylinder 31 extends downward out of the support seat 2, the connector 32 is installed at a lower end of a piston rod of the cylinder 31, the connector 32 is in an inverted T shape, a connecting plate 6 is installed at a lower end of the connector 32, the guide assembly 4 includes a slide rail 41 and a slider 42, two slide rails 41 are fixedly installed in front of the support seat 2, the slide rails 41 are vertically arranged, a plurality of sliders 42 are slidably connected in front of the slide rails 41, a backboard 5 is fixedly installed in front of the slider 42, when the piston rod of the cylinder 31 extends and retracts, the cylinder 31 drives the connecting plate 6 to move up and down, the connecting plate 6 drives the backboard 5, the lifting machine head 7 to move up and down, and the backboard 5 realizes more accurate up and down vertical motion under the cooperation of the slide rails 41 and the sliders 42.

Specifically, a material pressing cylinder 14 is installed above the lifting machine head 7, a material pressing pin 15 is rotatably installed on the side of the lifting machine head 7, and the material pressing cylinder 14 drives the material pressing pin 15 to rotate around a mounting point to lift, so that automatic material pressing is achieved.

The above description is provided for the purpose of describing the present invention in more detail with reference to the preferred embodiments, and it should not be construed that the present invention is limited to these descriptions, and it will be apparent to those skilled in the art that the present invention can be implemented in many ways without departing from the spirit and scope of the present invention.

Claims (5)

1. The utility model provides a novel split type lift aircraft nose, includes the fixing base, its characterized in that: still include the supporting seat, lift power unit, the direction subassembly, the backplate, the connecting plate, the lift aircraft nose, the back pivot, back gear drive subassembly, middle pivot, preceding gear drive subassembly and preceding pivot, fixing base the place ahead erection bracing seat, lift power unit is installed to the supporting seat top, supporting seat the place ahead installation direction subassembly, direction subassembly the place ahead installation backplate, backplate the place ahead fixed mounting connecting plate, connecting plate below fixed mounting lift aircraft nose, lift power unit drive lift aircraft nose oscilaltion, the back pivot is located the fixing base, the back pivot is rotated through the middle pivot of back gear drive subassembly drive, the middle pivot is rotated through the preceding pivot of preceding gear drive subassembly drive, preceding pivot is located the lift aircraft nose.

2. The novel split type lifting machine head as claimed in claim 1, characterized in that: the rear gear transmission assembly comprises a rear gear mounting plate, a rear first gear, a rear second gear and a rear third gear, the front gear transmission assembly comprises a front gear mounting plate, a front first gear, a front second gear and a front third gear, the rear gear mounting plate is fixedly mounted in front of the fixing seat, the rear first gear, the rear second gear and the rear third gear are rotatably mounted in front of the rear gear mounting plate, the rear second gear is respectively meshed with the rear first gear and the rear third gear, the rear first gear is inserted at the front end of the rear rotating shaft, the front gear mounting plate is mounted behind the lifting machine head, the front first gear, the front second gear and the front third gear are rotatably mounted behind the front gear mounting plate, the front second gear is respectively meshed with the front first gear and the front third gear, the front first gear is inserted at the rear end of the front rotating shaft, and the rear third gear is inserted at the front end of the middle rotating shaft and the rear third gear is inserted at the front end of the rear rotating shaft.

3. The novel split type lifting machine head as claimed in claim 1, characterized in that: the lifting power mechanism comprises an air cylinder and a connector, the air cylinder is installed above the supporting seat, a piston rod of the air cylinder extends downwards out of the supporting seat, the connector is installed at the lower end of the piston rod of the air cylinder, and a connecting plate is installed at the lower end of the connector.

4. The novel split type lifting machine head as claimed in claim 1, characterized in that: the guide assembly comprises a slide rail and a slide block, the two slide rails are fixedly mounted in front of the supporting seat, the slide rail is vertically arranged, the slide rail is connected with the slide blocks in front in a sliding mode, and the back plate is fixedly mounted in front of the slide block.

5. The novel split type lifting machine head as claimed in claim 1, characterized in that: the material cylinder is pressed in lift aircraft nose top installation, and lift aircraft nose side rotates the installation and presses the material foot, presses the material cylinder drive to press the material foot lifting.

Images