CN210085695U - A locating component for aircraft nose - Google Patents
A locating component for aircraft nose Download PDFInfo
- Publication number
- CN210085695U CN210085695U CN201920552860.4U CN201920552860U CN210085695U CN 210085695 U CN210085695 U CN 210085695U CN 201920552860 U CN201920552860 U CN 201920552860U CN 210085695 U CN210085695 U CN 210085695U
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- China
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- guide rail
- roller
- gyro wheel
- aircraft nose
- head assembly
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Abstract
The utility model mainly relates to a locating component for aircraft nose, including the guide rail, on the base was located to the guide rail, the guide rail included first guide rail and second guide rail, aircraft nose subassembly installation was between first guide rail and second guide rail, both ends all are equipped with gyro wheel one and gyro wheel two respectively about the aircraft nose subassembly, the aircraft nose subassembly passes through gyro wheel one, gyro wheel two is connected with the guide rail cooperation and realizes the installation, gyro wheel one is used for carrying on spacingly to the aircraft nose subassembly fore-and-aft direction, gyro wheel two is used for spacing to the aircraft nose subassembly upper and lower direction, the aircraft nose subassembly adopts the roll fit with the guide rail to be connected. This design simple structure has sufficient stable support and spacing effect to the aircraft nose, is difficult to deposition, easy clearance, has guaranteed that the aircraft nose can stable reciprocating motion on the guide rail, has improved the life of machine, and easy maintenance has improved the economic benefits of enterprise greatly.
Description
Technical Field
The utility model relates to a locating component for aircraft nose belongs to knitting machine technical field.
Background
The flat knitting machine is used for knitting articles such as knitted gloves and socks, the front and back symmetry is provided with the head guide rail in two bases of the flat knitting machine, the head guide rail is mainly used for the front and back heads to support and limit the guide, the existing head guide rail is complex in structure, during operation, the head is stressed greatly, the guide rail supports and limits the heads insufficiently, the head guide rail is easy to accumulate dust and hair in a rail groove and is not easy to clean, the head is unstable when reciprocating on the guide rail, shaking and other phenomena occur, corresponding parts are abraded, the service life of the machine is greatly shortened, the maintenance is troublesome, the repair cost is high, and the economic benefit of an enterprise is influenced.
SUMMERY OF THE UTILITY MODEL
In order to solve the problem, the utility model provides a locating component for aircraft nose, this design simple structure has sufficient stable support and spacing effect to the aircraft nose, is difficult to deposition, easy clearance, has guaranteed that the aircraft nose can stable reciprocating motion on the guide rail, has improved the life of machine, and easy maintenance has improved the economic benefits of enterprise greatly.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a locating component for aircraft nose, including the guide rail, the guide rail is located on the base, the guide rail includes first guide rail and second guide rail, aircraft nose subassembly installs between first guide rail and second guide rail, both ends all are equipped with gyro wheel one and gyro wheel two respectively about the aircraft nose subassembly, the aircraft nose subassembly passes through gyro wheel one, gyro wheel two is connected with the guide rail cooperation and realizes the installation, gyro wheel one is used for spacing aircraft nose subassembly fore-and-aft direction, gyro wheel two is used for spacing to the aircraft nose subassembly upper and lower direction, the aircraft nose subassembly adopts the roll fit to be connected with the guide rail.
The machine head component is characterized in that first fixing seats are symmetrically arranged at one end of the machine head component, at least two first rolling wheels are arranged on the first fixing seats, a pair of first guide rails of the rolling wheels are clamped and installed in a matched mode, a second rolling wheel is arranged on the side edge of the first fixing seat, and the second rolling wheel is installed in a matched mode in contact with the first guide rails.
The other end of the machine head assembly is symmetrically provided with a second fixing seat, a first roller is arranged on the second fixing seat, the first roller is installed in a matched mode with the second guide rail, a second roller is arranged on the side edge of the second fixing seat, and the second roller is installed in a contact matched mode with the second guide rail.
The first guide rail is of a T-shaped or L-shaped structure.
The machine head component is characterized in that a third fixing seat is arranged at one end of the machine head component, first rollers are symmetrically arranged at the lower end of the third fixing seat, the first rollers are installed in a matched mode with the first guide rail, second rollers are symmetrically arranged on the side edge of the third fixing seat, and the second rollers are installed in a contact matched mode with the first guide rail.
The other end of the machine head assembly is symmetrically provided with a first roller and a second roller, the first roller is installed in a matched mode with the second guide rail, a reserved hole is formed in the other end of the machine head assembly, the second roller is installed in the reserved hole, and the second roller is installed in a matched mode with the second guide rail in a contact mode.
The first guide rail, the second guide rail and the head assembly can be replaced mutually or installed in the same connecting mode.
The utility model discloses following beneficial effect has:
the utility model provides a locating component for aircraft nose, including the guide rail, the guide rail is located on the base, the guide rail includes first guide rail and second guide rail, aircraft nose subassembly installs between first guide rail and second guide rail, both ends all are equipped with gyro wheel one and gyro wheel two about the aircraft nose subassembly respectively, aircraft nose subassembly passes through gyro wheel one, gyro wheel two is connected with the guide rail cooperation and realizes the installation, gyro wheel one is used for spacing aircraft nose subassembly fore-and-aft direction, gyro wheel two is used for spacing the upper and lower direction to the aircraft nose subassembly, aircraft nose subassembly adopts the roll fit to be connected with the guide rail, frictional force has been reduced, this design simple structure, there are enough stable support and spacing effect to the aircraft nose, be difficult to the deposition, easy clearance, the aircraft nose can stable reciprocating motion on the guide rail has been guaranteed, the life of machine has been improved, convenient maintenance, the economic benefits of enterprise.
Drawings
Fig. 1 is a perspective structural view of a first embodiment of the present invention;
FIG. 2 is a partial perspective view of an embodiment of the present invention;
fig. 3 is a perspective view of the present invention from another perspective view of fig. 2;
fig. 4 is a perspective structural view of a second embodiment of the present invention;
fig. 5 is a left side view of the second embodiment of the present invention.
Reference numbers in the figures: 1. a guide rail; 11. a first guide rail; 12. a second guide rail; 2. a first roller; 3. a second roller; 4. a first fixed seat; 5. a second fixed seat; 6. a base; 7. a head assembly; 8. a third fixed seat; 9. holes are reserved.
Detailed Description
As shown in fig. 1, 2, 3, 4, 5, a positioning assembly for a machine head comprises a guide rail 1, the guide rail 1 is arranged on a base 6, the guide rail 1 comprises a first guide rail 11 and a second guide rail 12, a machine head assembly 7 is arranged between the first guide rail 11 and the second guide rail 12, a first roller 2 and a second roller 3 are respectively arranged at the upper end and the lower end of the machine head assembly 7, the machine head assembly 7 is matched and connected with the guide rail through the first roller 2 and the second roller 3 to realize installation, the first roller 2 is used for limiting the front and rear direction of the machine head assembly 7, the second roller 3 is used for limiting the up and down direction of the machine head assembly 7, the machine head assembly 7 is connected with the guide rail 1 in a rolling fit manner to reduce friction force, the design structure is simple, the machine head has enough stable supporting and limiting effects, dust and hair are not easy to accumulate, the cleaning is easy, and the machine head can stably, the service life of the machine is prolonged, the maintenance is convenient, and the economic benefit of enterprises is greatly improved.
The first embodiment is as follows:
as shown in fig. 1, 2 and 3, a first fixing seat 4 is symmetrically arranged at one end of the head assembly 7, at least two first rollers 2 are arranged on the first fixing seat 4, the first rollers 2 are installed on the first guide rail 11 in a front-back clamping and matching mode, a second roller 3 is arranged on the side edge of the first fixing seat 4, and the second roller 3 is installed in a contact and matching mode with the first guide rail 11.
The other end of the machine head assembly 7 is symmetrically provided with a second fixing seat 5, a first roller 2 is arranged on the second fixing seat 5, the first roller 2 is installed in a matched mode with the second guide rail 12, a second roller 3 is arranged on the side edge of the second fixing seat 5, and the second roller 3 is installed in a contact matched mode with the second guide rail 12.
The first guide rail 11 is one of a T-shaped or L-shaped structure.
Example two:
as shown in fig. 4 and 5, a third fixing seat 8 is arranged at one end of the head assembly 7, first rollers 2 are symmetrically arranged at the lower end of the third fixing seat 8, the first rollers 2 are installed in a matched manner with the first guide rail 11, second rollers 3 are symmetrically arranged on the side edges of the third fixing seat 8, and the second rollers 3 are installed in a contact and matched manner with the first guide rail 11.
The other end of the head assembly 7 is symmetrically provided with a first roller 2 and a second roller 3, the first roller 2 is installed in a matching mode with the second guide rail 12, the other end of the head assembly 7 is provided with a preformed hole 9, the second roller 3 is installed in the preformed hole 9, and the second roller 3 is installed in a contact matching mode with the second guide rail 12.
The connection modes of the first guide rail 11, the second guide rail 12 and the handpiece assembly 7 can be replaced mutually, or the same connection mode is selected for installation.
Claims (7)
1. The utility model provides a locating component for aircraft nose, includes the guide rail, and on the base was located to the guide rail, its characterized in that: the guide rail includes first guide rail and second guide rail, and head assembly installs between first guide rail and second guide rail, and both ends all are equipped with gyro wheel one and gyro wheel two respectively about the head assembly, and head assembly passes through gyro wheel one, gyro wheel two is connected with the guide rail cooperation and realizes the installation, and gyro wheel one is used for spacing head assembly fore-and-aft direction, and gyro wheel two is used for spacing head assembly upper and lower direction, and head assembly and guide rail adopt the roll fit to be connected.
2. A positioning assembly for a handpiece, as set forth in claim 1, wherein: the machine head component is characterized in that first fixing seats are symmetrically arranged at one end of the machine head component, at least two first rolling wheels are arranged on the first fixing seats, the rolling wheels are clamped and installed in a matched mode through a pair of first guide rails, rolling wheels second are arranged on the side edges of the first fixing seats, and the rolling wheels second are installed in a matched mode through contact with the first guide rails.
3. A positioning assembly for a handpiece, as set forth in claim 1, wherein: the other end of the machine head assembly is symmetrically provided with a second fixing seat, a first roller is arranged on the second fixing seat, the first roller is installed in a matched mode with the second guide rail, a second roller is arranged on the side edge of the second fixing seat, and the second roller is installed in a contact matched mode with the second guide rail.
4. A positioning assembly for a handpiece, as set forth in claim 2, wherein: the first guide rail is of a T-shaped or L-shaped structure.
5. A positioning assembly for a handpiece, as set forth in claim 1, wherein: the machine head component is characterized in that a third fixing seat is arranged at one end of the machine head component, first rollers are symmetrically arranged at the lower end of the third fixing seat, the first rollers are installed in a matched mode with the first guide rail, second rollers are symmetrically arranged on the side edge of the third fixing seat, and the second rollers are installed in a contact matched mode with the first guide rail.
6. A positioning assembly for a handpiece, as set forth in claim 1, wherein: the other end of the machine head assembly is symmetrically provided with a first roller and a second roller, the first roller is installed in a matched mode with the second guide rail, a reserved hole is formed in the other end of the machine head assembly, the second roller is installed in the reserved hole, and the second roller is installed in a matched mode with the second guide rail in a contact mode.
7. A positioning assembly for a handpiece, as claimed in any one of claims 1, 2, 3, 5, 6, wherein: the connection modes of the first guide rail, the second guide rail and the handpiece component can be replaced mutually, or the same connection mode is selected for installation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920552860.4U CN210085695U (en) | 2019-04-23 | 2019-04-23 | A locating component for aircraft nose |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920552860.4U CN210085695U (en) | 2019-04-23 | 2019-04-23 | A locating component for aircraft nose |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210085695U true CN210085695U (en) | 2020-02-18 |
Family
ID=69475308
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920552860.4U Active CN210085695U (en) | 2019-04-23 | 2019-04-23 | A locating component for aircraft nose |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210085695U (en) |
-
2019
- 2019-04-23 CN CN201920552860.4U patent/CN210085695U/en active Active
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