CN212703793U - Machine head lifting structure of pipe bending machine - Google Patents
Machine head lifting structure of pipe bending machine Download PDFInfo
- Publication number
- CN212703793U CN212703793U CN202021527091.1U CN202021527091U CN212703793U CN 212703793 U CN212703793 U CN 212703793U CN 202021527091 U CN202021527091 U CN 202021527091U CN 212703793 U CN212703793 U CN 212703793U
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- fixedly connected
- bending machine
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- 238000005452 bending Methods 0.000 title claims abstract description 27
- 230000007246 mechanism Effects 0.000 claims description 6
- 230000003028 elevating effect Effects 0.000 abstract description 26
- 230000000694 effects Effects 0.000 abstract description 8
- 230000008901 benefit Effects 0.000 abstract description 5
- 238000000034 method Methods 0.000 description 5
- 238000010276 construction Methods 0.000 description 2
- 238000005034 decoration Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000002035 prolonged effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- 230000001603 reducing effect Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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- Bending Of Plates, Rods, And Pipes (AREA)
Abstract
The utility model discloses a aircraft nose elevation structure of bending machine, which comprises a housin, the top fixedly connected with operation panel of casing, the left side at operation panel top is provided with the framework, the inner chamber of framework is provided with the elevating platform, the top of elevating platform runs through to the top of framework, the top on elevating platform right side is provided with the aircraft nose body, the bottom on framework inner chamber right side is provided with the drive case, the inner chamber of drive case is provided with elevating system. The utility model discloses a setting of casing, operation panel, framework, elevating platform, aircraft nose body, drive box, elevating system, sliding seat, pull rod, movable block, spout, slide, sliding sleeve and traveller has reached the advantage of being convenient for to adjust, has solved current bending machine aircraft nose elevating system and has been convenient for adjust not, can influence the lift effect of aircraft nose, can't satisfy user's demand, has reduced the lift efficiency of aircraft nose, can influence the problem that later stage bending machine used.
Description
Technical Field
The utility model relates to a bending machine technical field specifically is a aircraft nose elevation structure of bending machine.
Background
The pipe bender can be roughly divided into a numerical control pipe bender, a hydraulic pipe bender and the like, is mainly used for electric power construction, highway construction, pipeline laying and repairing in the aspects of boilers, bridges, ships, furniture, decoration and the like, has the advantages of multiple functions, reasonable structure, simplicity in operation and the like, can be used as a hydraulic jack by using an oil cylinder besides the pipe bending function, has the characteristics of low price and convenience in use relative to numerical control pipe bending equipment, and occupies the leading product position in the domestic pipe bender market.
Present bending machine aircraft nose elevating system not convenient to adjust can influence the lift effect of aircraft nose, can't satisfy user's demand, has reduced the lift efficiency of aircraft nose, can influence the use of later stage bending machine.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a aircraft nose elevation structure of bending machine possesses the advantage of being convenient for to adjust, has solved current bending machine aircraft nose elevating system and has not been convenient for adjust, can influence the lift effect of aircraft nose, can't satisfy user's demand, has reduced the lift efficiency of aircraft nose, can influence the problem that later stage bending machine used.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a aircraft nose elevation structure of bending machine, includes the casing, the top fixedly connected with operation panel of casing, the left side at operation panel top is provided with the framework, the inner chamber of framework is provided with the elevating platform, the top of elevating platform runs through to the top of framework, the top on elevating platform right side is provided with the aircraft nose body, the bottom on framework inner chamber right side is provided with the drive case, the inner chamber of drive case is provided with elevating system, elevating system includes the motor, the front of motor and the positive fixed connection of drive case inner chamber, the output fixedly connected with pivot of motor, the surface of pivot is provided with the gear, the bottom of gear runs through to the bottom of drive case and has meshed the rack board, the bottom of rack board and the bottom fixed connection of drive case inner chamber.
Preferably, the back of the rotating shaft is sleeved with a bearing seat, and the back of the bearing seat is fixedly connected with the back of the inner cavity of the driving box.
Preferably, the back of the rotating shaft is sleeved with a bearing seat, and the back of the bearing seat is fixedly connected with the back of the inner cavity of the driving box.
Preferably, the top of framework inner chamber both sides has all been seted up the spout, the inner chamber sliding connection of spout has the slide, the bottom of slide and the top fixed connection of movable block, the top of slide and the bottom fixed connection of elevating platform.
Preferably, the fixed surface of gear is connected with tooth one, the inboard fixedly connected with of rack board and the tooth two that tooth one cooperation was used, the equal fixedly connected with stopper that the gear cooperation was used in both sides at rack board top.
Preferably, the equal fixedly connected with sliding sleeve in front and the back of drive case, the inner chamber sliding connection of sliding sleeve has the traveller, the both sides of traveller all are provided with the limiting plate, and the outside of limiting plate and the both sides of drive case inner chamber front side and the both sides fixed connection of rear side.
Preferably, a support is arranged at the top of the left side of the shell, an operating device is arranged on one side, away from the shell, of the support, box doors are arranged on two sides of the front side of the shell through hinges, and handles are arranged on the inner sides of the front sides of the box doors.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a setting of casing, operation panel, framework, elevating platform, aircraft nose body, drive box, elevating system, sliding seat, pull rod, movable block, spout, slide, sliding sleeve and traveller has reached the advantage of being convenient for to adjust, has solved current bending machine aircraft nose elevating system and has been convenient for adjust not, can influence the lift effect of aircraft nose, can't satisfy user's demand, has reduced the lift efficiency of aircraft nose, can influence the problem that later stage bending machine used.
2. The utility model discloses a set up the bearing frame, the stable effect of rotation has been played to the countershaft, stability when having increased the pivot rotation, prevent that the pivot from appearing rocking problem when work is used, through setting up slide and spout, it is more smooth and easy to make the elevating platform in the inside gliding of framework, the friction between elevating platform and the framework has been reduced, the life of elevating platform and framework has been prolonged, mutually support through setting up sliding sleeve and traveller, play the effect that reduces the friction to drive case and framework, drive case and framework have been solved because frictional force is too big when using, the phenomenon of damage appears.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a sectional view of the frame structure of the present invention;
fig. 3 is a top view of the driving box and the lifting mechanism of the present invention.
In the figure: 1. a housing; 2. an operation table; 3. a frame body; 4. a lifting platform; 5. a handpiece body; 6. a drive box; 7. a lifting mechanism; 71. an electric motor; 72. a rotating shaft; 73. a gear; 74. a rack plate; 8. a movable seat; 9. a pull rod; 10. a movable block; 11. a chute; 12. a slide plate; 13. a sliding sleeve; 14. a slide column.
Detailed Description
In order to make the technical solution of the present invention better understood, the present invention is described in detail below with reference to the accompanying drawings, and the description of the present invention is only exemplary and explanatory, and should not be construed as limiting the scope of the present invention.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.
It should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like refer to the orientation or positional relationship shown in the drawings, or the orientation or positional relationship that the utility model is usually placed when in use, and are used for convenience of description and simplification of description, but do not refer to or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another and are not to be construed as indicating or implying relative importance.
Furthermore, the terms "horizontal", "vertical", "overhang" and the like do not imply that the components are required to be absolutely horizontal or overhang, but may be slightly inclined. For example, "horizontal" merely means that the direction is more horizontal than "vertical" and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; 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.
Referring to fig. 1-3, a machine head lifting structure of a pipe bending machine includes a housing 1, the top of the housing 1 is fixedly connected with an operation table 2, the left side of the top of the operation table 2 is provided with a frame 3, an inner cavity of the frame 3 is provided with a lifting table 4, the top of the lifting table 4 penetrates through the top of the frame 3, the top of the right side of the lifting table 4 is provided with a machine head body 5, the bottom of the right side of the inner cavity of the frame 3 is provided with a driving box 6, the inner cavity of the driving box 6 is provided with a lifting mechanism 7, the lifting mechanism 7 includes a motor 71, the front of the motor 71 is fixedly connected with the front of the inner cavity of the driving box 6, the output end of the motor 71 is fixedly connected with a rotating shaft 72, the surface of the rotating shaft 72 is provided with a gear 73, the bottom of the gear 73;
the back of the rotating shaft 72 is sleeved with a bearing seat, the back of the bearing seat is fixedly connected with the back of the inner cavity of the driving box 6, and the bearing seat is arranged, so that the rotating shaft 72 is stably rotated, the stability of the rotating shaft 72 in rotation is improved, and the problem that the rotating shaft 72 shakes during working and use is solved;
the top of the driving box 6 is fixedly connected with a movable seat 8, the top of the movable seat 8 is movably connected with a pull rod 9 through a movable shaft, and one side of the pull rod 9, which is far away from the movable seat 8, is movably connected with a movable block 10 through the movable shaft;
the top parts of the two sides of the inner cavity of the frame body 3 are respectively provided with a sliding groove 11, the inner cavity of the sliding groove 11 is connected with a sliding plate 12 in a sliding manner, the bottom part of the sliding plate 12 is fixedly connected with the top part of the movable block 10, the top part of the sliding plate 12 is fixedly connected with the bottom part of the lifting table 4, the sliding table 4 can slide more smoothly in the frame body 3 by arranging the sliding plate 12 and the sliding groove 11, the friction between the lifting table 4 and the frame body 3 is reduced, and the service lives of the lifting table 4 and the frame body 3 are prolonged;
the surface of the gear 73 is fixedly connected with a first tooth, the inner side of the rack plate 74 is fixedly connected with a second tooth matched with the first tooth, and two sides of the top of the rack plate 74 are fixedly connected with limit blocks matched with the gear 73;
the front and the back of the driving box 6 are fixedly connected with sliding sleeves 13, the inner cavity of the sliding sleeve 13 is connected with sliding columns 14 in a sliding manner, limiting plates are arranged on two sides of each sliding column 14, the outer sides of the limiting plates are fixedly connected with two sides of the front side and two sides of the rear side of the inner cavity of the driving box 6, the sliding sleeves 13 and the sliding columns 14 are arranged to be matched with each other, so that the friction reducing effect is achieved on the driving box 6 and the frame body 3, and the phenomenon that the driving box 6 and the frame body 3 are damaged due to overlarge friction force when in use is solved;
the left top of casing 1 is provided with the support, and the support is kept away from one side of casing 1 and is provided with operating means, the positive both sides of casing 1 all are provided with the chamber door through the hinge, and the positive inboard of chamber door is provided with the handle, through casing 1, operation panel 2, framework 3, elevating platform 4, aircraft nose body 5, drive box 6, elevating system 7, the sliding seat 8, pull rod 9, movable block 10, spout 11, slide 12, the setting of sliding sleeve 13 and traveller 14, the advantage of being convenient for adjust has been reached, it is not convenient for adjust to have solved current bending machine aircraft nose elevating system, can influence the lift effect of aircraft nose, can't satisfy user's demand, the lift efficiency of aircraft nose has been reduced, can influence the problem that later stage bending machine used.
During the use, the user opens motor 71 through external controller, motor 71 drives gear 73 through pivot 72 and bearing frame and rotates, through setting up the bearing frame, the effect of rotational stabilization has been played to pivot 72, stability when pivot 72 rotates has been increased, prevent that pivot 72 from appearing the problem of rocking when the work is used, gear 73 and rack plate 74 meshing drive box 6 and remove, drive box 6 drives movable seat 8 through the supplementary of sliding sleeve 13 and traveller 14 and removes, movable seat 8 drives slide 12 through pull rod 9 and movable block 10 and removes, slide 12 drives elevating platform 4 rebound through the supplementary of spout 11, elevating platform 4 drives aircraft nose body 5 and adjusts, and easy operation is convenient.
The standard parts used in this application document all can be purchased from the market, and can be customized according to the record of description and drawings, the concrete connection mode of each part all adopts conventional means such as mature bolt, rivet, welding among the prior art, machinery, part and equipment all adopt conventional model among the prior art, the control mode is automatic control through the controller, the control circuit of controller can realize through technical staff's simple programming in this field, belong to the common general knowledge in this field, and the utility model discloses mainly be used for protecting mechanical device, so the utility model discloses no longer explain control mode and circuit connection in detail, and the peripheral controller that mentions in the description can play the control role for the electrical components that this article mention, and this peripheral controller is conventional known equipment.
It should be noted that, in this document, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
The principles and embodiments of the present invention have been explained herein using specific examples, which are presented only to assist in understanding the methods and their core concepts. It should be noted that there are infinite specific structures due to the limited character expressions, and it will be apparent to those skilled in the art that various improvements, decorations or changes can be made without departing from the principles of the present invention, and the technical features can be combined in a suitable manner; the application of these modifications, variations or combinations, or the application of the concepts and solutions of the present invention in other contexts without modification, is not intended to be considered as a limitation of the present invention.
Claims (7)
1. The utility model provides a aircraft nose elevation structure of bending machine, includes casing (1), its characterized in that: the top of the shell (1) is fixedly connected with an operation table (2), the left side of the top of the operation table (2) is provided with a frame body (3), an inner cavity of the frame body (3) is provided with a lifting table (4), the top of the lifting table (4) penetrates through the top of the frame body (3), the top on the right side of the lifting table (4) is provided with a machine head body (5), the bottom on the right side of the inner cavity of the frame body (3) is provided with a driving box (6), the inner cavity of the driving box (6) is provided with a lifting mechanism (7), the lifting mechanism (7) comprises a motor (71), the front of the motor (71) is fixedly connected with the front of the inner cavity of the driving box (6), the output end of the motor (71) is fixedly connected with a rotating shaft (72), the surface of the rotating shaft (72) is provided with a gear (73), the bottom of the gear (73) penetrates through, the bottom of the rack plate (74) is fixedly connected with the bottom of the inner cavity of the driving box (6).
2. The head lifting structure of a bending machine according to claim 1, wherein: the back of the rotating shaft (72) is sleeved with a bearing seat, and the back of the bearing seat is fixedly connected with the back of the inner cavity of the driving box (6).
3. The head lifting structure of a bending machine according to claim 1, wherein: the top fixedly connected with sliding seat (8) of drive case (6), there is pull rod (9) at the top of sliding seat (8) through loose axle swing joint, one side of sliding seat (8) is kept away from in pull rod (9) and has movable block (10) through loose axle swing joint.
4. The head lifting structure of a bending machine according to claim 1, wherein: sliding grooves (11) are formed in the tops of two sides of an inner cavity of the frame body (3), sliding plates (12) are connected to the inner cavities of the sliding grooves (11) in a sliding mode, the bottoms of the sliding plates (12) are fixedly connected with the tops of the movable blocks (10), and the tops of the sliding plates (12) are fixedly connected with the bottoms of the lifting tables (4).
5. The head lifting structure of a bending machine according to claim 1, wherein: the surface fixed connection of gear (73) has tooth one, the inboard fixedly connected with of rack board (74) uses with tooth one cooperation tooth two, the equal fixedly connected with stopper that uses of gear (73) cooperation in both sides at rack board (74) top.
6. The head lifting structure of a bending machine according to claim 1, wherein: the front and the back of drive case (6) equal fixedly connected with sliding sleeve (13), the inner chamber sliding connection of sliding sleeve (13) has traveller (14), the both sides of traveller (14) all are provided with the limiting plate, and the both sides of the outside of limiting plate and drive case (6) inner chamber front side and the both sides fixed connection of rear side.
7. The head lifting structure of a bending machine according to claim 1, wherein: the portable multifunctional portable electronic device is characterized in that a support is arranged at the left top of the shell (1), an operating device is arranged on one side, away from the shell (1), of the support, box doors are arranged on the two front sides of the shell (1) through hinges, and handles are arranged on the inner sides of the front sides of the box doors.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021527091.1U CN212703793U (en) | 2020-07-29 | 2020-07-29 | Machine head lifting structure of pipe bending machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021527091.1U CN212703793U (en) | 2020-07-29 | 2020-07-29 | Machine head lifting structure of pipe bending machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212703793U true CN212703793U (en) | 2021-03-16 |
Family
ID=74910153
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021527091.1U Expired - Fee Related CN212703793U (en) | 2020-07-29 | 2020-07-29 | Machine head lifting structure of pipe bending machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212703793U (en) |
-
2020
- 2020-07-29 CN CN202021527091.1U patent/CN212703793U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210316 |