CN218055674U - Base for aircraft wallboard inspection tool - Google Patents
Base for aircraft wallboard inspection tool Download PDFInfo
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- CN218055674U CN218055674U CN202220983347.2U CN202220983347U CN218055674U CN 218055674 U CN218055674 U CN 218055674U CN 202220983347 U CN202220983347 U CN 202220983347U CN 218055674 U CN218055674 U CN 218055674U
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- supporting leg
- base
- base body
- plate
- screw rod
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Abstract
The utility model discloses a base for an aircraft panel inspection tool, which comprises a base body and supporting leg components arranged at four corners of the bottom of the base body and used for adjusting the installation height of the base body; positioning holes and connecting holes are formed in the four corners of the bottom of the base body; the supporting leg assembly comprises a supporting leg disc, a supporting leg screw rod, a nut, a supporting leg plate and at least one connecting piece, one end of the supporting leg screw rod is connected with the supporting leg disc, the other end of the supporting leg screw rod extends into the positioning hole, the nut is in threaded connection with the supporting leg screw rod, the supporting leg plate is arranged on the supporting leg screw rod in a sliding sleeve mode, the supporting leg plate is located on the nut, and the supporting leg plate is connected with the base body through the connecting piece and the connecting hole. The utility model discloses a set up the stabilizer blade subassembly and can adjust base body's mounting height, and stabilizer blade subassembly passes through bolted connection with base body, and stability is good during the use, the condition of base body and stabilizer blade subassembly dislocation can not appear.
Description
Technical Field
The utility model relates to an aircraft spare part processingequipment technical field, in particular to base for aircraft wallboard inspection frock.
Background
The aircraft wall plate parts are generally thin-wall parts with irregular curved surfaces. And product inspection is required after the part processing is finished.
The aircraft wallboard inspection tool is used for fixing and assisting in inspection of parts during inspection. The base of the existing aircraft wallboard inspection tool is of a size (height) fixed integrated structure, the height of the existing aircraft wallboard inspection tool cannot be adjusted according to actual requirements during installation, the height of the existing aircraft wallboard inspection tool can be adjusted only in a mode of increasing a base plate or a cushion block at the bottom, and the existing aircraft wallboard inspection tool is poor in stability of the existing aircraft wallboard inspection tool, easy to shake and misplace during use and directly influences the inspection precision of parts.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to overcome prior art's is not enough, provides an aircraft wallboard inspection base for frock, can adjust base body's mounting height through setting up the stabilizer blade subassembly, and stabilizer blade subassembly passes through bolted connection with base body, and stability is good during the use, the condition of base body and stabilizer blade subassembly dislocation can not appear.
The purpose of the utility model is realized through the following technical scheme:
a base for an aircraft panel inspection tool comprises a base body and support leg assemblies, wherein the support leg assemblies are arranged at four corners of the bottom of the base body and are used for adjusting the mounting height of the base body;
positioning holes and connecting holes are formed in the four corners of the bottom of the base body;
the supporting leg assembly comprises a supporting leg disc, a supporting leg screw rod, a nut, a supporting leg plate and at least one connecting piece, one end of the supporting leg screw rod is connected with the supporting leg disc, the other end of the supporting leg screw rod extends into the positioning hole, the nut is in threaded connection with the supporting leg screw rod, the supporting leg plate is slidably sleeved on the supporting leg screw rod, the supporting leg plate is located on the nut, and the supporting leg plate is connected with the base body through the connecting piece and the connecting hole.
Furthermore, the connecting piece is a screw, the connecting hole is a threaded hole, and the foot supporting plate is in threaded connection with the base body through the connecting piece and the connecting hole.
Furthermore, the supporting foot plate is a square plate.
Furthermore, the connecting pieces are four in number and distributed at four corners of the supporting leg plate.
Furthermore, the supporting leg disc is of a circular plate structure, and the supporting leg screw rod and the supporting leg disc are coaxially arranged.
Furthermore, the positioning hole is a threaded hole, and one end of the support leg screw rod, which is far away from the support leg disc, is in threaded connection with the positioning hole.
Furthermore, a conical groove is formed in the top surface of the supporting leg disc, and the end portion of the supporting leg screw rod is of a conical structure matched with the conical groove.
Further, the base body comprises a supporting frame and a supporting plate, and the supporting plate is detachably connected with the supporting frame through a bolt.
Furthermore, the side of the support frame is provided with a reinforcing plate.
Further, the reinforcing plate is provided with an arched shackle.
The beneficial effects of the utility model are that:
the utility model discloses a set up the stabilizer blade subassembly and can adjust base body's mounting height, and the stabilizer blade subassembly passes through bolted connection with base body, and stability is good during the use, the condition of base body and stabilizer blade subassembly dislocation can not appear.
Drawings
Fig. 1 is a first perspective view of a base for an aircraft panel inspection tool according to an embodiment of the present invention;
fig. 2 is a second perspective view of the base for the aircraft panel inspection tool in the embodiment of the present invention;
FIG. 3 is a schematic structural view of the leg assembly;
FIG. 4 is a top view of the foot assembly;
FIG. 5 is a cross-sectional view of the headboard;
FIG. 6 is a schematic view of the structure of the leg screw;
in the figure, 1, a base body; 2. a leg assembly; 3. positioning holes; 4. a supporting leg disc; 5. a leg screw; 6. a nut; 7. a foot support plate; 8. a connecting member; 9. a tapered groove; 10. a support frame; 11. a support plate; 12. a reinforcing plate; 13. and (4) bow shackle.
Detailed Description
The technical solutions of the present invention will be described clearly and completely below with reference to embodiments, and it should be understood that the described embodiments are only some embodiments of the present invention, but not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by those skilled in the art without creative efforts belong to the protection scope of the present invention.
Referring to fig. 1 to 6, the present invention provides a technical solution:
the embodiment is as follows:
as shown in fig. 1 to 6, a base for an aircraft panel inspection tool comprises a base body 1 and leg assemblies 2 arranged at four corners of the bottom of the base body 1 and used for adjusting the mounting height of the base body 1;
the four corners of the bottom of the base body 1 are provided with positioning holes 3 and connecting holes;
the stabilizer blade subassembly 2 includes a stabilizer blade dish 4, stabilizer blade screw rod 5, nut 6, stabilizer blade board 7 and at least one connecting piece 8, the one end of stabilizer blade screw rod 5 with a stabilizer blade dish 4 is connected, and the other end of stabilizer blade screw rod 5 stretches into locating hole 3, nut 6 and 5 threaded connection of stabilizer blade screw rod, 7 slip covers of stabilizer blade board are established on the stabilizer blade screw rod 5, a stabilizer blade board 7 is located on the nut 6, a stabilizer blade board 7 through connecting piece 8, connecting hole with base body 1 is connected.
The working principle is as follows: the height of the supporting leg component 2 is adjusted according to actual needs during installation, and then the height of the base is adjusted. The height adjustment process of the leg assembly 2 is as follows: when the height needs to be adjusted, the amount of the connecting screw rod stretching into the positioning hole 3 is increased, and when the stretching amount of the adjusting screw rod is adjusted, the position of the corresponding adjusting nut 6 gives way for the support leg plate 7. When the adjusting is in place, the top surface of the supporting foot plate 7 is in contact with the ground of the base body 1, and the supporting foot plate 7 is fixed with the base body 1 through the connecting piece 8 and the connecting hole. And the ground of the supporting foot plate 7 is contacted with the top surface of the adjusting nut 6, and the whole base is supported by the nut 6 and the right-angle screw rod at the moment.
When the height needs to be adjusted, the amount of the connecting screw rod extending into the positioning hole 3 is reduced. The conditioning process was as described previously.
The utility model discloses a set up stabilizer blade subassembly 2 and can adjust base body 1's mounting height, and stabilizer blade subassembly 2 passes through bolted connection with base body 1, and stability is good during the use, the condition of base body 1 with stabilizer blade subassembly 2 dislocation can not appear.
Furthermore, the connecting piece 8 is a screw, the connecting hole is a threaded hole, and the supporting plate 7 is in threaded connection with the base body 1 through the connecting piece 8 and the connecting hole. So set up, connection structure is simple, connects stably.
Further, as shown in fig. 4, the leg supporting plate 7 is a square plate, the number of the connecting members 8 is four, and the four connecting members 8 are distributed at four corners of the leg supporting plate 7. The arrangement is convenient for the arrangement of the screws, and the screws are arranged at the four corners of the foot supporting plate 7.
Further, as shown in fig. 4, the leg plate 4 is a circular plate structure, and the leg screw 5 is coaxially disposed with the leg plate 4.
The circular plate structure has a large contact area with the ground, and can improve the stability of the leg plate 4.
Furthermore, the positioning hole 3 is a threaded hole, and one end of the support leg screw, which is far away from the support leg disc 4, is in threaded connection with the positioning hole 3. So set up stability that can improve between connecting screw and the base body 1.
Further, as shown in fig. 5 and 6, a tapered groove 9 is formed in the top surface of the leg plate 4, and the end of the leg screw 5 is in a conical structure adapted to the tapered groove 9. The leg screw 5 and the leg plate 4 may be fixed by welding, but not limited thereto. The conical groove 9 is arranged, so that the positioning effect is achieved when the support leg screw rod 5 and the support leg disc 4 are installed, and meanwhile, the contact area between the support leg screw rod 5 and the support leg disc 4 can be increased.
Further, as shown in fig. 1 and 2, the base body 1 includes a support frame 10 and a support plate 11, and the support plate 11 is detachably connected to the support frame 10 by bolts. So set up, during the use, the mould child subassembly of inspection frock is directly connected with backup pad 11, the supporting area of multiplicable mould child subassembly and the tie point with base body 1.
Further, as shown in fig. 1, a reinforcing plate 12 is provided on a side surface of the supporting frame 10. The reinforcing plate 12 ensures the strength of the support frame 10 and improves the bearing capacity thereof.
Further, as shown in fig. 1, the reinforcing plate 12 is provided with a bow shackle 13. The bow shackles can be used for hoisting the base body.
The foregoing is illustrative of the preferred embodiments of the present invention, and it is to be understood that the invention is not limited to the precise forms disclosed herein and that the invention is not to be considered as limited to the disclosed embodiments, but is capable of use in various other combinations, modifications, and environments and is capable of changes within the scope of the inventive concept as expressed herein, commensurate with the above teachings, or the skill or knowledge of the relevant art. But that modifications and variations may be effected by those skilled in the art without departing from the spirit and scope of the invention, which is to be limited only by the claims appended hereto.
Claims (10)
1. The utility model provides an aircraft wallboard inspection base for frock which characterized in that: the base comprises a base body and supporting leg assemblies arranged at four corners of the bottom of the base body and used for adjusting the mounting height of the base body;
positioning holes and connecting holes are formed in the four corners of the bottom of the base body;
the supporting leg assembly comprises a supporting leg disc, a supporting leg screw rod, a nut, a supporting leg plate and at least one connecting piece, one end of the supporting leg screw rod is connected with the supporting leg disc, the other end of the supporting leg screw rod extends into the positioning hole, the nut is in threaded connection with the supporting leg screw rod, the supporting leg plate is slidably sleeved on the supporting leg screw rod, the supporting leg plate is located on the nut, and the supporting leg plate is connected with the base body through the connecting piece and the connecting hole.
2. The base for the aircraft panel inspection tool of claim 1, wherein: the connecting piece is a screw, the connecting hole is a threaded hole, and the supporting foot plate is in threaded connection with the base body through the connecting piece and the connecting hole.
3. The base for the aircraft panel inspection tool of claim 2, wherein: the supporting foot plate is a square plate.
4. The base for the aircraft panel inspection tool of claim 3, wherein: the connecting piece has four, and four connecting pieces distribute in stabilizer blade four corners department.
5. The base for the aircraft panel inspection tool of claim 1, wherein: the supporting leg disc is of a circular plate structure, and the supporting leg screw rod and the supporting leg disc are coaxially arranged.
6. The base for the aircraft panel inspection tool of claim 5, wherein: the positioning hole is a threaded hole, and one end, far away from the supporting foot disc, of the supporting foot screw is in threaded connection with the positioning hole.
7. The base for the aircraft panel inspection tool of claim 5, wherein: the top surface of the supporting leg disc is provided with a conical groove, and the end part of the supporting leg screw rod is of a conical structure matched with the conical groove.
8. The base for the aircraft panel inspection tool of claim 1, wherein: the base body comprises a support frame and a support plate, and the support plate is detachably connected with the support frame through a bolt.
9. The base for the aircraft panel inspection tool of claim 8, wherein: and a reinforcing plate is arranged on the side surface of the supporting frame.
10. The base for the aircraft panel inspection tool of claim 9, wherein: the reinforcing plate is provided with an arch shackle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220983347.2U CN218055674U (en) | 2022-04-26 | 2022-04-26 | Base for aircraft wallboard inspection tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220983347.2U CN218055674U (en) | 2022-04-26 | 2022-04-26 | Base for aircraft wallboard inspection tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218055674U true CN218055674U (en) | 2022-12-16 |
Family
ID=84429380
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220983347.2U Active CN218055674U (en) | 2022-04-26 | 2022-04-26 | Base for aircraft wallboard inspection tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218055674U (en) |
-
2022
- 2022-04-26 CN CN202220983347.2U patent/CN218055674U/en active Active
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