CN220093796U - Horizontal machining center for aviation hydraulic oil tank - Google Patents
Horizontal machining center for aviation hydraulic oil tank Download PDFInfo
- Publication number
- CN220093796U CN220093796U CN202320401877.6U CN202320401877U CN220093796U CN 220093796 U CN220093796 U CN 220093796U CN 202320401877 U CN202320401877 U CN 202320401877U CN 220093796 U CN220093796 U CN 220093796U
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- China
- Prior art keywords
- oil tank
- hydraulic oil
- aviation hydraulic
- strip
- machining center
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- 239000010720 hydraulic oil Substances 0.000 title claims abstract description 30
- 238000007789 sealing Methods 0.000 claims description 3
- 238000003754 machining Methods 0.000 abstract description 3
- 239000000428 dust Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000003028 elevating effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- Supply Devices, Intensifiers, Converters, And Telemotors (AREA)
Abstract
The utility model discloses a horizontal machining center for an aviation hydraulic oil tank, which comprises a strip-shaped base with a control box, wherein the upper end surface of the strip-shaped base is provided with a strip-shaped groove, two screws are arranged in the strip-shaped groove in parallel up and down, two ends of the two screws are respectively and rotatably connected with the inner wall of the strip-shaped groove, two servo motors for respectively controlling the two screws are fixedly arranged in the control box, machining openings for communicating the strip-shaped groove are formed in the strip-shaped base, two movable seats are symmetrically arranged in the strip-shaped groove, the two movable seats are respectively and slidably sleeved on the two screws, the two movable seats are respectively in threaded connection with the two screws, two L-shaped seats are symmetrically and fixedly arranged at the upper ends of the two movable seats, two clamping tools are symmetrically arranged between the two L-shaped seats, and the two clamping tools are respectively and rotatably connected with the two L-shaped seats through two rotating shafts. The utility model can realize the functions of fast clamping the aviation hydraulic oil tank and conveniently adjusting the orientation position of the aviation hydraulic oil tank, and is convenient and fast to use.
Description
Technical Field
The utility model relates to the technical field related to aviation hydraulic oil tank processing, in particular to a horizontal processing center for an aviation hydraulic oil tank.
Background
Most of hydraulic oil tanks of the existing aviation hydraulic elevator for aircraft maintenance are of a cuboid or cylindrical independent structure arranged on an elevating table top. This oil tank often adopts horizontal machining center to carry out processing operation when carrying out processing, but is carrying out the in-process of processing to aviation hydraulic tank, needs to stabilize and carries out the centre gripping, and the in-process of centre gripping probably needs to change aviation hydraulic tank's position according to the processing purpose moreover, and further still need change aviation hydraulic tank's orientation, in order to adapt to present processing demand moreover, still need have the effect of quick clamping, and present horizontal machining center can not satisfy these demands.
For this purpose, we propose a horizontal machining center for aviation hydraulic oil tanks to solve the above problems.
Disclosure of Invention
The utility model aims to solve the defects in the prior art, and provides a horizontal machining center for an aviation hydraulic oil tank.
In order to achieve the above purpose, the present utility model adopts the following technical scheme:
a horizontal machining center for an aviation hydraulic tank, comprising: the strip-shaped base with the control box, strip-shaped base up end is provided with the bar recess, be provided with two screw rods from top to bottom in the bar recess side by side, two the both ends of screw rod all rotate with the bar recess inner wall and be connected, two servo motor of two screw rods of control box internal fixed mounting respectively, be provided with the processing opening of intercommunication bar recess on the bar base, the symmetry is provided with two in the bar recess and removes the seat, two it establishes at two screw rods to remove the equal slip cap of seat, two remove the seat respectively with two screw rod threaded connection, two it is provided with two L type seats to remove seat upper end symmetry, two the symmetry is provided with two centre gripping frock between the L type seat, two centre gripping frock rotates with two L type seats respectively through two pivots and is connected.
Preferably, a driving motor is fixedly installed on one of the L-shaped seats, and the output end of the driving motor penetrates through the L-shaped seat and is fixedly connected with the rotating shaft in a coaxial manner.
Preferably, one of them L type seat upside level is fixed and is provided with the crossbearer, vertically run through on the crossbearer and be provided with the hydraulic telescoping rod, hydraulic telescoping rod lower extreme corresponds and fixedly connected with brake block with the pivot position.
Preferably, a storage cavity is arranged in the control box, a suction inlet which is communicated with the storage cavity and the strip-shaped groove is arranged on the control box, an air pump is fixedly arranged on the side wall of the control box, the air pump is communicated with the storage cavity through a short pipe, and a filter screen is fixedly arranged in the short pipe in a sealing way.
Preferably, the clamping tool comprises a fixing piece, two sliding rods are symmetrically and fixedly arranged on the fixing piece, a moving piece is arranged on the two sliding rods in a sliding sleeve mode, a threaded short rod is connected to the fixing piece in a rotating mode, the threaded short rod is sleeved with the moving piece in a threaded mode, and a rotating handle is fixedly connected to one end, away from the fixing piece, of the threaded short rod in a coaxial mode.
Preferably, the fixed part and the movable part are both machined to a shape corresponding to that of the aviation hydraulic oil tank.
Compared with the prior art, the utility model has the beneficial effects that: the horizontal machining center can realize the functions of quickly clamping the aviation hydraulic oil tank and conveniently adjusting the orientation position of the aviation hydraulic oil tank, the aviation hydraulic oil tank is placed on the strip-shaped base and is placed between the two L-shaped seats, the two L-shaped seats can be controlled to move through the work of the two servo motors, the two L-shaped seats are close to the aviation hydraulic oil tank, then the two L-shaped seats can be clamped and fixed through clamping tools on the L-shaped seats, then the two L-shaped seats synchronously move to a machining opening position, the subsequent machining of the aviation hydraulic oil tank can be facilitated, and the positions can be quickly clamped and conveniently changed; one of the L-shaped seats is provided with a hydraulic telescopic rod and pushes the brake pad to prop against the rotating shaft to fix the aviation hydraulic oil tank, after the hydraulic telescopic rod is loosened, the aviation hydraulic oil tank can be rotated through a servo motor on the other L-shaped seat to change the direction so as to facilitate processing, and generated fine scraps can be collected during processing, so that the hydraulic telescopic rod is convenient and rapid to use as a whole.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is a schematic perspective view of another view of the present utility model;
fig. 3 is a schematic perspective view of a clamping tool according to the present utility model.
In the figure:
1 bar base, 2 control box, 3 screw rods, 4 servo motor, 5 remove seat, 6L type seat, 7 centre gripping frock, 8 pivot, 9 driving motor, 10 crossbearer, 11 hydraulic telescoping rod, 12 aspiration pump, 13 nozzle stub, 71 mounting, 72 slide bar, 73 moving part, 74 screw thread quarter butt, 75 rotating handle.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments.
Referring to fig. 1 to 3, a horizontal machining center for an aviation hydraulic oil tank includes:
the strip-shaped base 1 with the control box 2 adopts a common box body and base structure, a strip-shaped groove is formed in the upper end face of the strip-shaped base 1 and used for installing a subsequent moving structure, specifically, two screws 3 are arranged in the strip-shaped groove in parallel up and down, two ends of the two screws 3 are rotationally connected with the inner wall of the strip-shaped groove, two servo motors 4 for respectively controlling the two screws 3 are fixedly arranged in the control box 2, the two servo motors 4 can respectively control the two screws 3 to rotate, a PLC controller is arranged in the control box 2 and used for controlling in the prior art, and details are omitted;
in aviation hydraulic tank's course of working, because the processing demand probably needs to change aviation hydraulic tank's orientation, consequently, be provided with the processing opening of intercommunication bar recess on bar base 1 and make things convenient for aviation hydraulic tank to rotate, simultaneously in order to carry out the centre gripping to aviation hydraulic tank and fix, the symmetry is provided with two in the bar recess and removes seat 5, two are removed seat 5 and are all slided the cover and establish at two screw rods 3, two remove seat 5 respectively with two screw rods 3 threaded connection, two are removed seat 5 upper end symmetry and are fixedly provided with two L type seat 6, two L type seat 6 between the symmetry be provided with two centre gripping frock 7, two centre gripping frock 7 rotate with two L type seat 6 respectively through two pivot 8 and are connected, work through two servo motor 4, can change the position of two removal seats 5, thereby can realize that control two centre gripping frock 7 keep away from or be close to aviation hydraulic tank and drive aviation hydraulic tank after the centre gripping is fixed and remove.
Meanwhile, in order to realize the rotation of the aviation hydraulic oil tank after clamping, a driving motor 9 is fixedly arranged on one L-shaped seat 6, the output end of the driving motor 9 penetrates through the L-shaped seat 6 and is fixedly connected with the rotating shaft 8 in a coaxial way, and the driving motor 9 works to drive the aviation hydraulic oil tank to rotate so as to change the direction of the aviation hydraulic oil tank; in order to guarantee the steadiness when not needing to rotate, the horizontal fixed crossbearer 10 that is provided with in one of them L type seat 6 upside level, the vertical hydraulic telescoping rod 11 that runs through is provided with on the crossbearer 10, hydraulic telescoping rod 11 lower extreme corresponds and fixedly connected with brake block with pivot 8 position, and hydraulic telescoping rod 11 supports the brake block and realizes spacing fixed action in pivot 8.
In can appearing the fine dust and fall into the bar recess in carrying out the course of working to aviation hydraulic tank, inconvenient cleaning is provided with the storage cavity for this in control box 2, be provided with the sunction inlet of intercommunication storage cavity and bar recess on the control box 2, fixedly be provided with aspiration pump 12 on the control box 2 lateral wall, aspiration pump 12 passes through nozzle stub 13 and storage cavity intercommunication, nozzle stub 13 internal seal is fixed and is provided with the filter screen, can inhale the storage cavity with the fine dust in the bar recess in through aspiration pump 12 work, reach clean effect, can set up the sealing door of intercommunication storage cavity on control box 2 and make things convenient for follow-up clearance.
For clamping and fixing of an aviation hydraulic oil tank, specifically, the clamping tool 7 comprises a fixing piece 71, two sliding rods 72 are symmetrically and fixedly arranged on the fixing piece 71, a moving piece 73 is sleeved on the two sliding rods 72 in a sliding mode, a threaded short rod 74 is rotationally connected to the fixing piece 71, the moving piece 73 is sleeved on the threaded short rod 74 in a threaded mode, a rotating handle 75 is fixedly connected to one end, far away from the fixing piece 71, of the threaded short rod 74 in a coaxial mode, the threaded short rod 74 can be driven to rotate through rotation of the rotating handle 75, vertical movement of the moving piece 73 is controlled through a threaded structure, and therefore stable clamping is achieved; simultaneously, the fixed part 71 and the movable part 73 are processed to be in a shape corresponding to the aviation hydraulic oil tank so as to be convenient and stable to clamp.
The foregoing is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical scheme of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.
Claims (6)
1. Horizontal machining center for aviation hydraulic tank, characterized by comprising: the strip base (1) with control box (2), strip base (1) up end is provided with the bar recess, be provided with two screw rods (3) from top to bottom in the bar recess side by side, two the both ends of screw rod (3) all rotate with the bar recess inner wall and be connected, fixed mounting has two servo motor (4) of controlling two screw rods (3) respectively in control box (2), be provided with the processing opening of intercommunication bar recess on strip base (1), the symmetry is provided with two in the bar recess and removes seat (5), two remove seat (5) all the slip cap and establish at two screw rods (3), two remove seat (5) respectively with two screw rod (3) threaded connection, two remove seat (5) upper end symmetry fixed two L type seat (6), two between L type seat (6) symmetry be provided with two centre gripping frock (7), two centre gripping (7) rotate with two L type seat (6) respectively through two pivot (8).
2. The horizontal machining center for the aviation hydraulic oil tank according to claim 1, wherein a driving motor (9) is fixedly installed on one of the L-shaped seats (6), and an output end of the driving motor (9) penetrates through the L-shaped seat (6) and is fixedly connected with the rotating shaft (8) in a coaxial mode.
3. The horizontal machining center for the aviation hydraulic oil tank according to claim 1, wherein a transverse frame (10) is horizontally and fixedly arranged on the upper side of one L-shaped seat (6), a hydraulic telescopic rod (11) is vertically and penetratingly arranged on the transverse frame (10), and a brake pad is correspondingly and fixedly connected to the lower end of the hydraulic telescopic rod (11) in position with a rotating shaft (8).
4. The horizontal machining center for the aviation hydraulic oil tank according to claim 1, wherein a storage cavity is formed in the control box (2), a suction inlet communicated with the storage cavity and the strip-shaped groove is formed in the control box (2), an air pump (12) is fixedly arranged on the side wall of the control box (2), the air pump (12) is communicated with the storage cavity through a short pipe (13), and a filter screen is fixedly arranged in the short pipe (13) in a sealing mode.
5. The horizontal machining center for an aviation hydraulic oil tank according to claim 1, wherein the clamping tool (7) comprises a fixing piece (71), two sliding rods (72) are symmetrically and fixedly arranged on the fixing piece (71), a moving piece (73) is arranged on the two sliding rods (72) in a sliding sleeve mode, a threaded short rod (74) is rotatably connected to the fixing piece (71), the moving piece (73) is arranged on the threaded short rod (74) in a threaded sleeve mode, and a rotating handle (75) is fixedly connected to one end, away from the fixing piece (71), of the threaded short rod (74) in a coaxial mode.
6. The horizontal machining center for an aviation hydraulic oil tank according to claim 5, wherein the fixed member (71) and the moving member (73) are each machined to a shape corresponding to that of the aviation hydraulic oil tank.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320401877.6U CN220093796U (en) | 2023-03-07 | 2023-03-07 | Horizontal machining center for aviation hydraulic oil tank |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320401877.6U CN220093796U (en) | 2023-03-07 | 2023-03-07 | Horizontal machining center for aviation hydraulic oil tank |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220093796U true CN220093796U (en) | 2023-11-28 |
Family
ID=88845918
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320401877.6U Active CN220093796U (en) | 2023-03-07 | 2023-03-07 | Horizontal machining center for aviation hydraulic oil tank |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220093796U (en) |
-
2023
- 2023-03-07 CN CN202320401877.6U patent/CN220093796U/en active Active
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