CN212096244U - Strutting arrangement is used in maintenance of aviation spare part - Google Patents
Strutting arrangement is used in maintenance of aviation spare part Download PDFInfo
- Publication number
- CN212096244U CN212096244U CN201922381624.3U CN201922381624U CN212096244U CN 212096244 U CN212096244 U CN 212096244U CN 201922381624 U CN201922381624 U CN 201922381624U CN 212096244 U CN212096244 U CN 212096244U
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- plate
- roof
- support rod
- rod
- strutting arrangement
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Abstract
The utility model discloses a strutting arrangement is used in aviation spare part maintenance relates to maintenance tool technical field, specifically is a strutting arrangement is used in aviation spare part maintenance, which comprises a base, the top fixed mounting of base has the cover shell, the inside fixed mounting of cover shell has the telescopic link, the outer wall of cover shell is provided with the rotating turret, the inside rotation of rotating turret is connected with side branch, the top of telescopic link runs through the inside of cover shell and extends to the outside of cover shell, the telescopic link is located the one end fixedly connected with mounting panel in the cover shell outside, the sliding tray has been seted up to the bottom of mounting panel. This strutting arrangement is used in aviation spare part maintenance is through setting up branch roof around the crown plate to utilize the cradling piece to support to divide the roof, thereby enlarged this strutting arrangement's support area, supported the position all around of spare part through dividing the roof to use, improved this strutting arrangement and supported the stability of spare part support.
Description
Technical Field
The utility model relates to a repair tools technical field specifically is a strutting arrangement is used in aviation spare part maintenance.
Background
When aviation spare part is maintained, the volume of spare part is great a bit, and the scope that most strutting arrangement's holding surface can support is less, consequently support spare part that can not be fine, traditional strutting arrangement's holding surface is the plane board mostly, the size of fixed mounting rear plane board can't change, consequently, when the plane board is great, the space that occupies is great, it is inconvenient with the transportation, when the plane board is less, can't satisfy spare part's supporting role again.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art, the utility model provides an aviation spare part is strutting arrangement for maintenance has solved the problem that proposes in the above-mentioned background art.
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a supporting device for maintaining aviation parts comprises a base, a sleeve shell is fixedly arranged above the base, a telescopic rod is fixedly arranged inside the sleeve shell, a rotating frame is arranged on the outer wall of the sleeve shell, a side supporting rod is rotatably connected inside the rotating frame, the top end of the telescopic rod penetrates through the inside of the sleeve shell and extends to the outside of the sleeve shell, a mounting plate is fixedly connected to one end, located outside the sleeve shell, of the telescopic rod, a sliding groove is formed in the bottom of the mounting plate, one end, far away from the sleeve shell, of the side supporting rod is slidably sleeved inside the sliding groove, a guide rod is fixedly connected to the center of the top of the mounting plate, a spring is arranged above the guide rod, two ends of the spring are respectively and fixedly connected with the guide rod and a ring top plate, an annular groove is formed in the side face of the ring top plate, a, one end of the support rod, which is far away from the separation top plate, is rotatably connected to the top of the mounting plate.
Optionally, the cradling piece includes first vaulting pole, second vaulting pole and limiting plate, the both ends of first vaulting pole rotate with the outer wall and the second vaulting pole of branch roof respectively and are connected, the one end that first vaulting pole was kept away from to the second vaulting pole is rotated and is connected the top at the mounting panel, the below fixedly connected with limiting plate of second vaulting pole, the limiting plate extends to the below of first vaulting pole.
Optionally, the number of the branch top plates is four, the branch top plates are respectively located on the side faces of the ring top plates, branch rods located on the outer sides of the support rods are fixedly mounted above the mounting plate, and the top ends of the branch rods are rotatably connected with the support rods.
Optionally, the sub-top plate is triangular, two mutually perpendicular side surfaces of the sub-top plate are respectively provided with a clamping plate and a clamping groove, and the clamping grooves and the clamping plates arranged on the same side of the two adjacent sub-top plates are mutually clamped.
Optionally, the bottom of the branch top plate is slidably connected with a guide rail, and one end of the guide rail, which is far away from the branch top plate, is slidably sleeved on the side surface of the annular top plate.
Optionally, walking wheels are arranged below the base, and the deformation length of the spring is the height value between the top of the annular top plate and the top of the branch top plate.
The utility model provides an aviation spare part is strutting arrangement for maintenance possesses following beneficial effect:
1. this strutting arrangement is used in aviation spare part maintenance is through setting up branch roof around the crown plate to utilize the cradling piece to support to divide the roof, thereby enlarged this strutting arrangement's support area, supported the position all around of spare part through dividing the roof to use, improved this strutting arrangement and supported the stability of spare part support.
2. This strutting arrangement is used in aviation spare part maintenance, through the draw-in groove and the joint of each other of cardboard of adjacent branch roof side, guaranteed that this strutting arrangement roof can not scatter when accomodating to divide the inside of roof joint in the annular through processing, effectively reduced the space that this strutting arrangement occupy, this strutting arrangement's of being convenient for carry the transportation, improved this strutting arrangement's practicality.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a top view of the present invention.
In the figure: 1. a base; 2. a housing; 3. a telescopic rod; 4. mounting a plate; 5. a side strut; 6. a guide bar; 7. a spring; 8. a top ring plate; 9. a ring groove; 10. a card slot; 11. a support rod; 1101. a first stay bar; 1102. a second stay bar; 1103. a limiting plate; 12. clamping a plate; 13. a guide rail; 14. separating rods; 15. and (4) dividing the top 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.
Referring to fig. 1 to 2, the present invention provides a technical solution: a supporting device for maintaining aviation parts comprises a base 1, a sleeve 2 is fixedly mounted above the base 1, a telescopic rod 3 is fixedly mounted inside the sleeve 2, a rotating frame is arranged on the outer wall of the sleeve 2, a side supporting rod 5 is rotatably connected inside the rotating frame, the side supporting rod 5 is used for supporting a mounting plate 4, the stability of the mounting plate 4 when the telescopic rod 3 extends and retracts is ensured, the top end of the telescopic rod 3 penetrates through the inside of the sleeve 2 and extends to the outer side of the sleeve 2, the mounting plate 4 is fixedly connected to one end, located outside the sleeve 2, of the telescopic rod 3, the bottom of the mounting plate 4 is provided with a sliding groove, one end, far away from the sleeve 2, of the side supporting rod 5 is slidably sleeved inside the sliding groove, a guide rod 6 is fixedly connected to the center of the top of the mounting plate 4, a spring 7 is arranged above the guide rod 6, the spring, thereby make the top of crown plate 8 and the top of dividing crown plate 15 keep flushing, be convenient for support spare part, spring 7's both ends difference fixedly connected with guide arm 6 and crown plate 8, annular 9 has been seted up to the side of crown plate 8, and annular 9's inside joint has branch roof 15, divides the middle part of roof 15 below to rotate and is connected with cradling piece 11, and cradling piece 11 keeps away from the one end rotation connection at mounting panel 4 of dividing crown plate 15.
The support rod 11 comprises a first support rod 1101, a second support rod 1102 and a limiting plate 1103, two ends of the first support rod 1101 are respectively rotatably connected with the outer wall of the top separating plate 15 and the second support rod 1102, one end, far away from the first support rod 1101, of the second support rod 1102 is rotatably connected above the mounting plate 4, the limiting plate 1103 is fixedly connected below the second support rod 1102, the limiting plate 1103 extends to the lower portion of the first support rod 1101, and the limiting plate 1103 is used for preventing the first support rod 1101 from rotating towards the other direction of the second support rod 1102, so that the first support rod 1101 and the second support rod 1102 are kept stable when being parallel.
Wherein, divide the quantity of roof 15 to be four and be located the side of ring roof 8 respectively, the top fixed mounting of mounting panel 4 has the branch pole 14 that is located the support bar 11 outside, divides pole 14 to be used for supporting support bar 11, guarantees support bar 11 and divides the support dynamics of roof 15, divides the top and the support bar 11 of pole 14 to rotate and is connected, rotates to connect the rotation that is used for adapting to support bar 11.
The sub-top plate 15 is triangular, two mutually perpendicular side surfaces of the sub-top plate 15 are respectively provided with a clamping plate 12 and a clamping groove 10, and the clamping grooves 10 and the clamping plates 12 arranged on the same side of the two adjacent sub-top plates 15 are mutually clamped.
Wherein, divide the bottom sliding connection of roof 15 to have guide rail 13, guide rail 13 is used for guaranteeing to divide the track that roof 15 removed, avoids dividing roof 15 moving direction mistake, perhaps misplaces when the inside of injecting annular 9 and leads to unable accomodating, and guide rail 13 keeps away from the one end sliding sleeve who divides roof 15 and connects in the side of crown plate 8.
Wherein, the below of base 1 is provided with the walking wheel, and the deformation length of spring 7 is the height value between the top of crown plate 8 to the top of branch roof 15, and spring 7 mainly used when supporting spare part for the top of crown plate 8 keeps flushing with the top of dividing roof 15, and when using up this strutting arrangement, spring 7 upwards promotes crown plate 8, makes and divides roof 15 can insert the inside of annular 9.
In summary, in the aviation component maintenance supporting device, when in use, firstly, the supporting device is moved to the lower part of the component, or the component is placed on the top of the ring top plate 8 of the supporting device, secondly, the top end of the telescopic rod 3 is extended to push the mounting plate 4 and the ring top plate 8 to move upwards so as to support the component, when the mounting plate 4 moves upwards, the side supporting rod 5 rotates around the side surface of the casing 2, the upper end of the side supporting rod 5 moves inwards along the bottom of the mounting plate 4, secondly, the ring top plate 15 is pulled outwards along the guide rail 13 from the inside of the ring top plate 8, the first supporting rod 1101 and the second supporting rod 1102 are kept straight in the same direction, the first supporting rod 1101 is clamped on the top of the limiting plate 1103, so that the first supporting rod 1101 cannot rotate downwards, and finally, when the ring top plate 8 contacts with the component and moves upwards, the ring top plate 8 moves downwards, the guide rail 13 slides along the side surface of the ring top plate 8, the guide rod 6 is compressed, and the ring top plate 8 is kept flush with the top of the branch top plate 15.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. The utility model provides a strutting arrangement is used in maintenance of aviation spare part, includes base (1), its characterized in that: a sleeve shell (2) is fixedly mounted above the base (1), a telescopic rod (3) is fixedly mounted inside the sleeve shell (2), a rotating frame is arranged on the outer wall of the sleeve shell (2), a side supporting rod (5) is rotatably connected inside the rotating frame, the top end of the telescopic rod (3) penetrates through the inside of the sleeve shell (2) and extends to the outside of the sleeve shell (2), a mounting plate (4) is fixedly connected to one end of the telescopic rod (3) positioned outside the sleeve shell (2), a sliding groove is formed in the bottom of the mounting plate (4), one end, far away from the sleeve shell (2), of the side supporting rod (5) is slidably sleeved inside the sliding groove, a guide rod (6) is fixedly connected to the center of the top of the mounting plate (4), a spring (7) is arranged above the guide rod (6), and a guide rod (6) and a ring top plate (8) are fixedly connected to the, annular (9) have been seted up to the side of ring roof (8), the inside joint of annular (9) has branch roof (15), divide the middle part of roof (15) below to rotate and be connected with cradling piece (11), the one end rotation connection at mounting panel (4) that the roof (15) was kept away from in cradling piece (11).
2. The supporting device for aviation component maintenance according to claim 1, wherein: the support rod (11) comprises a first support rod (1101), a second support rod (1102) and a limiting plate (1103), the two ends of the first support rod (1101) are respectively rotatably connected with the outer wall of the top separating plate (15) and the second support rod (1102), one end, far away from the first support rod (1101), of the second support rod (1102) is rotatably connected above the mounting plate (4), the limiting plate (1103) is fixedly connected to the lower portion of the second support rod (1102), and the limiting plate (1103) extends to the lower portion of the first support rod (1101).
3. The supporting device for aviation component maintenance according to claim 1, wherein: divide the quantity of roof (15) to be four and be located the side of ring roof (8) respectively, the top fixed mounting of mounting panel (4) has branch pole (14) that are located the cradling piece (11) outside, the top and the cradling piece (11) of branch pole (14) are rotated and are connected.
4. The supporting device for aviation component maintenance according to claim 1, wherein: the sub-top plate (15) is triangular, two mutually vertical side faces of the sub-top plate (15) are respectively provided with a clamping plate (12) and a clamping groove (10), and the clamping grooves (10) and the clamping plates (12) arranged on the same side of the two adjacent sub-top plates (15) are mutually clamped.
5. The supporting device for aviation component maintenance according to claim 1, wherein: the bottom of the sub-top plate (15) is connected with a guide rail (13) in a sliding mode, and one end, far away from the sub-top plate (15), of the guide rail (13) is sleeved on the side face of the annular top plate (8) in a sliding mode.
6. The supporting device for aviation component maintenance according to claim 1, wherein: the lower part of the base (1) is provided with a walking wheel, and the deformation length of the spring (7) is the height value between the top of the ring top plate (8) and the top of the sub top plate (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922381624.3U CN212096244U (en) | 2019-12-26 | 2019-12-26 | Strutting arrangement is used in maintenance of aviation spare part |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922381624.3U CN212096244U (en) | 2019-12-26 | 2019-12-26 | Strutting arrangement is used in maintenance of aviation spare part |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212096244U true CN212096244U (en) | 2020-12-08 |
Family
ID=73625277
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922381624.3U Expired - Fee Related CN212096244U (en) | 2019-12-26 | 2019-12-26 | Strutting arrangement is used in maintenance of aviation spare part |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212096244U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113119046A (en) * | 2021-03-08 | 2021-07-16 | 全汉强 | Supporting device convenient to adjust and used for maintaining aviation parts |
-
2019
- 2019-12-26 CN CN201922381624.3U patent/CN212096244U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113119046A (en) * | 2021-03-08 | 2021-07-16 | 全汉强 | Supporting device convenient to adjust and used for maintaining aviation parts |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| 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: 20201208 Termination date: 20211226 |