CN214134896U - Pentahedron machining center aircraft nose fixing device - Google Patents
Pentahedron machining center aircraft nose fixing device Download PDFInfo
- Publication number
- CN214134896U CN214134896U CN202023018989.9U CN202023018989U CN214134896U CN 214134896 U CN214134896 U CN 214134896U CN 202023018989 U CN202023018989 U CN 202023018989U CN 214134896 U CN214134896 U CN 214134896U
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- China
- Prior art keywords
- fixedly connected
- shell
- machining center
- fixing device
- aircraft nose
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- Expired - Fee Related
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- 238000012423 maintenance Methods 0.000 abstract description 8
- 238000003754 machining Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a pentahedron machining center aircraft nose fixing device, comprising a base plate, the equal fixedly connected with cylinder in both sides at bottom plate top, the top fixedly connected with slide bar of cylinder, the left side fixedly connected with riser at slide bar top, the right side fixedly connected with electric telescopic handle of riser, electric telescopic handle's right side fixedly connected with sliding sleeve, the bottom fixedly connected with casing of sliding sleeve, the axis department of casing bottom is provided with the aircraft nose body, the front and the equal fixedly connected with stopper in the back of aircraft nose body. The utility model discloses a cooperation of riser, electric telescopic handle, sliding sleeve, casing, aircraft nose body, first spring, limiting plate, spliced pole, movable rod, dead lever, stopper, link, spacing, second spring and baffle has solved current pentahedron machining center aircraft nose very troublesome when dismantling to inconvenient later maintenance, the inconvenient problem of using.
Description
Technical Field
The utility model relates to the technical field of machinery, specifically be a pentahedron machining center aircraft nose fixing device.
Background
The pentahedron machining center has the characteristics of high efficiency and high precision, complex machining can be completed by clamping a workpiece once, and the pentahedron machining center can be suitable for machining of modern dies such as automobile parts and airplane structural parts, but the machine head of the existing pentahedron machining center is very troublesome in disassembly, inconvenient in later maintenance and inconvenient in use.
SUMMERY OF THE UTILITY MODEL
Solves the technical problem
Not enough to prior art, the utility model provides a pentahedron machining center aircraft nose fixing device possesses the advantage of being convenient for maintain, has solved current pentahedron machining center aircraft nose very troublesome when dismantling to inconvenient later maintenance, the inconvenient problem of using.
Technical scheme
In order to achieve the above object, the utility model provides a following technical scheme: a pentahedron machining center aircraft nose fixing device comprises a bottom plate, wherein both sides of the top of the bottom plate are fixedly connected with air cylinders, the top of the air cylinder is fixedly connected with a slide bar, the left side of the top of the slide bar is fixedly connected with a vertical plate, the right side of the vertical plate is fixedly connected with an electric telescopic rod, the right side of the electric telescopic rod is fixedly connected with a sliding sleeve, the bottom of the sliding sleeve is fixedly connected with a shell, a central shaft at the bottom of the shell is provided with an aircraft nose body, the front side and the back side of the aircraft nose body are fixedly connected with limit blocks, the central shaft at the front side of the inner cavity of the shell is fixedly connected with a first spring, the back side of the first spring is fixedly connected with a limit plate, the top of the limit plate is movably connected with a movable rod, the back side of the movable rod is movably connected with a fixed rod, and the bottoms of the limit plate and the fixed rod penetrate to the bottom of the shell, the rear side cover at casing top is equipped with the link, the positive fixedly connected with spacing of link, the top fixedly connected with second spring of spacing, the top and the casing fixed connection of second spring.
Preferably, the bottom of the front side of the inner cavity of the shell is fixedly connected with a connecting column, and the rear side of the connecting column is movably connected with the limiting plate.
Preferably, the inner cavity of the fixing rod is slidably connected with a supporting rod, and the rear side of the supporting rod is fixedly connected with the shell.
Preferably, the top of the rear side of the inner cavity of the shell is provided with a sliding groove, and the inner cavity of the sliding groove is in sliding connection with the connecting frame.
Preferably, the surface of the sliding rod is in sliding connection with the sliding sleeve, and the two sides of the bottom of the shell are fixedly connected with the baffle plates.
Advantageous effects
Compared with the prior art, the utility model provides a pentahedron machining center aircraft nose fixing device possesses following beneficial effect:
1. the utility model discloses when the aircraft nose body need be maintained, only need upwards stimulate the link, the link drives spacing frame and removes, keep away from behind the dead lever when spacing frame, can pull the bottom of limiting plate to the front side, make the limiting plate use the spliced pole to rotate as the centre of a circle, thereby the top of limiting plate can drive the movable rod and remove, the movable rod drives the dead lever and removes, can make limiting plate and dead lever keep away from the stopper, thereby accomplish the dismantlement, also can install through above-mentioned step fast after the maintenance, it is very troublesome when dismantling to have solved current pentahedron machining center aircraft nose, thereby inconvenient later maintenance, the inconvenient problem of using.
2. The utility model discloses a set up the spliced pole, stabilized the work of limiting plate, avoided the limiting plate can't carry out work, through setting up the bracing piece, stabilized the work of dead lever, carried out the balanced support to the dead lever, through setting up the spout, stabilized the work of link, carried out the balanced support to the link.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the side view structure of the shell of the present invention in a sectional view;
fig. 3 is an enlarged schematic view of a portion a in fig. 2 according to the present invention.
In the figure: 1. a base plate; 2. a cylinder; 3. a slide bar; 4. a vertical plate; 5. an electric telescopic rod; 6. a sliding sleeve; 7. a housing; 8. a handpiece body; 9. a first spring; 10. a limiting plate; 11. connecting columns; 12. a movable rod; 13. fixing the rod; 14. a limiting block; 15. a connecting frame; 16. a limiting frame; 17. a second spring; 18. and a baffle plate.
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.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end", 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 device or element to be referred must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted", "provided", "connected", and the like are to be construed broadly, such as "connected", which may be 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 in specific cases to those skilled in the art.
The utility model discloses a bottom plate 1, cylinder 2, slide bar 3, riser 4, electric telescopic handle 5, sliding sleeve 6, casing 7, aircraft nose body 8, first spring 9, limiting plate 10, spliced pole 11, movable rod 12, dead lever 13, stopper 14, link 15, spacing 16, second spring 17 and 18 parts of baffle are the general standard or the part that technical staff in the field knows, its structure and principle all are that this technical staff all can learn through technical manual or learn through conventional experimental method.
Referring to fig. 1-3, a pentahedral machining center head fixing device comprises a bottom plate 1, wherein both sides of the top of the bottom plate 1 are fixedly connected with air cylinders 2, the top of the air cylinder 2 is fixedly connected with a slide bar 3, the left side of the top of the slide bar 3 is fixedly connected with a vertical plate 4, the right side of the vertical plate 4 is fixedly connected with an electric telescopic rod 5, the right side of the electric telescopic rod 5 is fixedly connected with a sliding sleeve 6, the bottom of the sliding sleeve 6 is fixedly connected with a shell 7, the surface of the slide bar 3 is slidably connected with the sliding sleeve 6, both sides of the bottom of the shell 7 are fixedly connected with baffles 18, a head body 8 is arranged at the middle shaft at the bottom of the shell 7, the front and the back of the head body 8 are fixedly connected with limit blocks 14, a first spring 9 is fixedly connected at the middle shaft at the front side of the inner cavity of the shell 7, a limit plate 10 is fixedly connected at the back of the first spring 9, a connecting column 11 is fixedly connected at the bottom of the front side of the inner cavity of the shell 7, the rear side of the connecting column 11 is movably connected with the limiting plate 10, the working of the limiting plate 10 is stabilized by arranging the connecting column 11, the failure of the limiting plate 10 in working is avoided, the top of the limiting plate 10 is movably connected with a movable rod 12, the rear side of the movable rod 12 is movably connected with a fixed rod 13, the inner cavity of the fixed rod 13 is slidably connected with a supporting rod, the rear side of the supporting rod is fixedly connected with the shell 7, the working of the fixed rod 13 is stabilized by arranging the supporting rod, the fixed rod 13 is balanced and supported, the bottoms of the limiting plate 10 and the fixed rod 13 penetrate through to the bottom of the shell 7, the connecting frame 15 is sleeved at the rear side of the top of the shell 7, the top of the rear side of the inner cavity of the shell 7 is provided with a sliding groove, the inner cavity of the sliding groove is slidably connected with the connecting frame 15, the working of the connecting frame 15 is stabilized by arranging the sliding groove, the connecting frame 15 is balanced and supported, the limiting frame 16 is fixedly connected with the front side of the connecting frame 15, the top of the limiting frame 16 is fixedly connected with a second spring 17, and the top of the second spring 17 is fixedly connected with the shell 7.
When the device is used, the electric telescopic rod 5 is controlled by the external controller to work, the electric telescopic rod 5 drives the sliding sleeve 6 to move, the sliding sleeve 6 drives the shell 7 to move, the shell 7 drives the machine head body 8 to move, after the device is moved to a working position, the machine head body 8 and the air cylinder 2 are controlled by the external controller to work, the machine head body 8 works, meanwhile, the air cylinder 2 drives the sliding rod 3 to move, the sliding rod 3 drives the sliding sleeve 6 to move, the sliding sleeve 6 drives the shell 7 to move, the shell 7 drives the machine head body 8 to move, and then the device can work, when the machine head body 8 needs maintenance, only the connecting frame 15 needs to be pulled upwards, the connecting frame 15 drives the limiting frame 16 to move, after the limiting frame 16 is far away from the fixed rod 13, the bottom of the limiting plate 10 can be pulled forwards, so that the limiting plate 10 rotates by taking the connecting column 11 as the center of a circle, thereby limiting plate 10's top can drive movable rod 12 and remove, movable rod 12 drives dead lever 13 and removes, can make limiting plate 10 and dead lever 13 keep away from stopper 14, thereby accomplish the dismantlement, also can install fast through above-mentioned step after the maintenance, it is very troublesome when dismantling to have solved current pentahedron machining center aircraft nose, thereby inconvenient later maintenance, the problem of inconvenient use, the peripheral hardware controller is the PLC controller in this application, and simultaneously, two wiring ends of peripheral hardware controller are connected with power plug through the wire, and adopt commercial power to supply power in this application.
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 (5)
1. The utility model provides a pentahedron machining center aircraft nose fixing device, includes bottom plate (1), its characterized in that: the improved electric hair dryer is characterized in that cylinders (2) are fixedly connected to two sides of the top of the bottom plate (1), slide rods (3) are fixedly connected to the tops of the cylinders (2), vertical plates (4) are fixedly connected to the left sides of the tops of the slide rods (3), electric telescopic rods (5) are fixedly connected to the right sides of the vertical plates (4), sliding sleeves (6) are fixedly connected to the right sides of the electric telescopic rods (5), a shell (7) is fixedly connected to the bottom of the sliding sleeves (6), a nose body (8) is arranged at a middle shaft at the bottom of the shell (7), limiting blocks (14) are fixedly connected to the front side and the back side of the nose body (8), first springs (9) are fixedly connected to the middle shaft at the front side of an inner cavity of the shell (7), limiting plates (10) are fixedly connected to the back side of the first springs (9), and movable rods (12) are movably connected to the tops of the limiting plates (10), the rear side swing joint of movable rod (12) has dead lever (13), the bottom of limiting plate (10) and dead lever (13) all runs through to the bottom of casing (7), the rear side cover at casing (7) top is equipped with link (15), the positive fixedly connected with spacing (16) of link (15), the top fixedly connected with second spring (17) of spacing (16), the top and casing (7) fixed connection of second spring (17).
2. The pentahedral machining center head fixing device of claim 1, wherein: the bottom fixedly connected with spliced pole (11) of casing (7) inner chamber front side, the rear side and limiting plate (10) swing joint of spliced pole (11).
3. The pentahedral machining center head fixing device of claim 1, wherein: the inner cavity of the fixing rod (13) is connected with a supporting rod in a sliding mode, and the rear side of the supporting rod is fixedly connected with the shell (7).
4. The pentahedral machining center head fixing device of claim 1, wherein: the top of the rear side of the inner cavity of the shell (7) is provided with a sliding groove, and the inner cavity of the sliding groove is connected with the connecting frame (15) in a sliding manner.
5. The pentahedral machining center head fixing device of claim 1, wherein: the surface of the sliding rod (3) is connected with the sliding sleeve (6) in a sliding manner, and the two sides of the bottom of the shell (7) are fixedly connected with baffle plates (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023018989.9U CN214134896U (en) | 2020-12-15 | 2020-12-15 | Pentahedron machining center aircraft nose fixing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023018989.9U CN214134896U (en) | 2020-12-15 | 2020-12-15 | Pentahedron machining center aircraft nose fixing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214134896U true CN214134896U (en) | 2021-09-07 |
Family
ID=77587215
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023018989.9U Expired - Fee Related CN214134896U (en) | 2020-12-15 | 2020-12-15 | Pentahedron machining center aircraft nose fixing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214134896U (en) |
-
2020
- 2020-12-15 CN CN202023018989.9U patent/CN214134896U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 215000 No. 96, Wangxian Road, DONGBANG Town, Changshu, Suzhou, Jiangsu Patentee after: Suzhou juntie CNC Machinery Co.,Ltd. Address before: 215539 Building 1, No.1, Kaicheng Road, Zhitang Town, Changshu City, Suzhou City, Jiangsu Province Patentee before: Suzhou juntie Machinery Co.,Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210907 |