CN2880358Y - Mould for assembling lighter - Google Patents
Mould for assembling lighter Download PDFInfo
- Publication number
- CN2880358Y CN2880358Y CN 200620090387 CN200620090387U CN2880358Y CN 2880358 Y CN2880358 Y CN 2880358Y CN 200620090387 CN200620090387 CN 200620090387 CN 200620090387 U CN200620090387 U CN 200620090387U CN 2880358 Y CN2880358 Y CN 2880358Y
- Authority
- CN
- China
- Prior art keywords
- lighter
- mould
- core
- deck
- main body
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Lighters Containing Fuel (AREA)
Abstract
The utility model relates to a mould for lighter assembly. The mould includes a bottom plate, a main clamp seat to fix the lighter and a head clamp seat for installing the lighting head alternately assembled on both sides of the bottom plate, and an actuating component used on the jacking lighter and enabling the jacking lighter to move to the head clamp seat. The mould is featured with simple structure and very convenient operation. Collision between the lighting head and the lighter can be avoided in assembly, and the collision may lead to damage.
Description
Technical field:
The utility model relates to a kind of mould with mechanical mode assembling lighter.
Background technology:
Lighter particularly pulls out wheeled lighter and normally is made up of fuselage and two discrete parts of rotor of being used for carrying liquid part, and fuselage and rotor are to combine by the mode of socket joint.Yet, in the prior art, usually adopt artificial assembling lighter, be to waste time and energy and manually assemble the problem that lighter at first reflects, secondly be operating efficiency is very low, also improve the cost of manufacture of lighter simultaneously.
For this reason, to be called " lighter porous type assembly jig " be exactly a solution that is proposed at the manually-operated problem to the name of No. 2452641 Granted publications of Chinese patent.This assembly jig comprises rotor cross section identical and the lower bolster and the sheet rubber that is used to adjust its height the one-tenth column distribution with lighter, and the cope match-plate pattern superimposed with lower bolster, be provided with the guide-track groove that is parallel to each other and slide block is housed in the bottom surface of cope match-plate pattern opposite end.Its meaning is to want to utilize a plurality of lighter of the disposable assembling of mechanical mode.With regard to mechanical type assembling fuselage and these two parts of rotor, in assembling process, putting fuselage and rotor in the mould needs most times of whole assembly program, be that groundwork is in the program of putting, simultaneously because height and equipment that assembling lighter in a row also needs to adjust fuselage or rotor with sheet rubber are put the pressure that adds to mould, so, at packaging efficiency, adopt single assembling and in a row assemble and there is no big difference, but, the mould structure and the operating process relative complex of assembling in a row, cost of manufacture is higher, and plant equipment is also had higher requirement.
Summary of the invention:
The purpose of this utility model provides a kind of mould that is used to assemble lighter, utilizes the very convenient operation of this kind mould assembling lighter.
The mould that the utility model proposed is used to assemble lighter has a base plate, be separately installed with the main body deck that is used for fixing the lighter fuselage in the both sides of this base plate at interval predeterminedly and be used to install the head deck of its rotor, and the actuating assembly that is used for pushing tow lighter fuselage and it can be moved towards head deck direction.
The central region of described main body deck is provided with the storage tank that the external diameter of internal diameter and lighter fuselage is complementary, and is respectively arranged with a recess at the middle part of two sidewalls of this storage tank.
Described head deck has the outer cover that is connected with base plate, in this outer cover core component is installed, and this core component and be provided with towards the end that makes main body deck direction is used to limit the chamber of the rotor position of lighter.Described core component have external core and be connected by rod member with this external core and the inner core-body of preset distance at interval, and be installed in elastomeric element on the rod member between external core and the inner core-body.Be provided with two manholes in the described external core, and be respectively arranged with a clear opening and a tapped through hole in the inner core-body and with two corresponding positions of manhole, and make the rod member that passes clear opening extend the end face of inner core-body.
Described actuating assembly comprise a shell body and be installed in this shell body and with its inner surface drive link movingly, and be installed in drive link and extend return spring on the shell body part.Described drive link is provided with push plate near the end face of main body deck, and also is provided with a stroke limit bolt at drive link near on push plate one end.
The mould employing and fuselage and identical respectively main body deck and the head deck of rotor shape that are used to assemble lighter that the utility model proposed, its structure is simple relatively, when assembling, as long as fuselage and rotor are placed on respectively in separately the deck, it can be fitted together by actuating assembly pushing tow fuselage, so operation is very easy to utilize this kind mould assembling lighter; In addition, the telescopic inner core-body that adopts in the described core component can play the effect of buffering in assembling process, damages because of bump in the time of can avoiding rotor to contact with fuselage.
Description of drawings:
Accompanying drawing 1 is a surface structure schematic diagram of assembling the utility model being used to of proposing an embodiment of mould of lighter;
Accompanying drawing 2 is view sub-anatomies of head deck 3 among Fig. 1.
The specific embodiment:
Referring to Fig. 1, this figure provides that the utility model proposes is used to assemble the overall appearance structure of an embodiment of mould of lighter.This mould comprises base plate 1 and the main body deck 2, head deck 3 and the actuating assembly 4 that are installed on this base plate 1.
Described base plate 1 is the plate of a rectangle basically, and the surface is equipped with head deck 3, main body deck 2 and actuating assembly 4 successively thereon.Wherein, head deck 3 is used for the splendid attire rotor, and main body deck 2 is used for the splendid attire fuselage, and actuating assembly 4 is the parts that are used for the pushing tow fuselage, and headward deck 3 directions of fuselage are moved to realize assembling.
The central region of main body deck 2 is provided with the storage tank 21 that the external diameter of internal diameter and lighter fuselage is complementary, the fuselage of lighter can be placed in the storage tank 21, middle part at two sidewalls of storage tank 21 is respectively arranged with a recess 22, and this recess 22 is mainly used in fuselage from lighter to storage tank 21 that place or take out.
Actuating assembly 4 comprise a shell body 41 and be installed in this shell body 41 and with its inner surface drive link 42 movingly, extends on shell body 41 parts at drive link 42 return spring 43 is installed, and end is provided with push plate 44 within it.When the end of external force pushing tow drive link 42, drive link 42 can move towards the direction of main body deck 2, push plate 44 moves to the storage tank 21 interior directions that the fuselage of lighter can be pushed head deck 3 of main body deck 2, and then realize fuselage and rotor are fitted together, in order to limit the displacement of push plate 44, on drive link 42 and near push plate 44 1 ends, be provided with a stroke limit bolt 45.
Referring to Fig. 2, this figure provides the overall appearance structure of 3 one embodiment of head deck.Head deck 3 has the outer cover 31 that is connected with base plate, in this outer cover 31 core component is installed.Core component comprises external core 32 and inner core-body 33, external core 32 be axially disposed within two manholes 36, and the axial and manhole 36 corresponding positions of inner core-body 33 are provided with a clear opening 37 and a tapped through hole 38, rod member 34 links together external core 32 and inner core-body 33 through manhole 36 and clear opening 37, and extend inner core-body 33, and rod member 39 by manhole 36 and tapped through hole 38 with the fixed-site between external core 32 and the inner core-body 33.The elastomeric element 35 that is made of spring all is installed on rod member 34 and rod member 39.Inner core-body 33 is provided with the chamber (figure does not provide) that is used for limiting the rotor position in the end towards the direction of main body deck 2.
Claims (7)
1, a kind of mould that is used to assemble lighter, it is characterized in that: this mould has a base plate, be separately installed with the main body deck that is used for fixing the lighter fuselage in the both sides of this base plate at interval predeterminedly and be used to install the head deck of its rotor, and the actuating assembly that is used for pushing tow lighter fuselage and it can be moved towards head deck direction.
2, mould according to claim 1 is characterized in that: the central region of described main body deck is provided with the storage tank that the external diameter of internal diameter and lighter fuselage is complementary, and is respectively arranged with a recess at the middle part of two sidewalls of this storage tank.
3, mould according to claim 1, it is characterized in that: described head deck has the outer cover that is connected with base plate, in this outer cover core component is installed, this core component and be provided with towards the end that makes main body deck direction is used to limit the chamber of the rotor position of lighter.
4, mould according to claim 3 is characterized in that: described core component have external core and be connected by rod member with this external core and the inner core-body of preset distance at interval, and be installed in elastomeric element on the rod member between external core and the inner core-body.
5, mould according to claim 4, it is characterized in that: be provided with two manholes in the described external core, and be respectively arranged with a clear opening and a tapped through hole in the inner core-body and with two corresponding positions of manhole, and make the rod member that passes clear opening extend the end face of inner core-body.
6, mould according to claim 1 is characterized in that: described actuating assembly comprise a shell body and be installed in this shell body and with its inner surface drive link movingly, and be installed in drive link and extend return spring on the shell body part.
7 moulds according to claim 6 is characterized in that: described drive link is provided with push plate near the end face of main body deck, and also is provided with a stroke limit bolt at drive link near on push plate one end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620090387 CN2880358Y (en) | 2006-04-14 | 2006-04-14 | Mould for assembling lighter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620090387 CN2880358Y (en) | 2006-04-14 | 2006-04-14 | Mould for assembling lighter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2880358Y true CN2880358Y (en) | 2007-03-21 |
Family
ID=37880196
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200620090387 Expired - Fee Related CN2880358Y (en) | 2006-04-14 | 2006-04-14 | Mould for assembling lighter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2880358Y (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106584107A (en) * | 2017-01-16 | 2017-04-26 | 中山市显东电器有限公司 | Lighter head automatic assembly equipment |
-
2006
- 2006-04-14 CN CN 200620090387 patent/CN2880358Y/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106584107A (en) * | 2017-01-16 | 2017-04-26 | 中山市显东电器有限公司 | Lighter head automatic assembly equipment |
| CN106584107B (en) * | 2017-01-16 | 2023-08-11 | 中山市显东电器有限公司 | Automatic assembling equipment for lighter head |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20070321 Termination date: 20140414 |