CN214986158U - Unmanned aerial vehicle fuselage device of upset - Google Patents
Unmanned aerial vehicle fuselage device of upset Download PDFInfo
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- CN214986158U CN214986158U CN202120859806.1U CN202120859806U CN214986158U CN 214986158 U CN214986158 U CN 214986158U CN 202120859806 U CN202120859806 U CN 202120859806U CN 214986158 U CN214986158 U CN 214986158U
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Abstract
The utility model discloses a device of unmanned aerial vehicle fuselage upset, including the base, install a pair of supporting seat on the base, be provided with the riding wheel group on the supporting seat, all be equipped with rotatable supporting disk on two riding wheel groups, link to each other through the pull rod between the supporting disk, the supporting disk inboard is equipped with the lug, through using the utility model discloses make the rotation of unmanned aerial vehicle fuselage convenient and reliable more, can be used to in the unmanned aerial vehicle manufacturing.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle produces technical field, in particular to unmanned aerial vehicle fuselage production auxiliary fixtures.
Background
The airframe structure of the unmanned aerial vehicle can be divided into a plurality of parts, namely an airframe, a wing, an empennage and an undercarriage, wherein the airframe section is a force bearing center of the unmanned aerial vehicle, an oil storage tank, a fuel system, a control center device and a weapon load are also arranged on the force bearing center, and the wing, the empennage and the undercarriage are also arranged on the airframe structure. Therefore, the structure of the body part of the unmanned aerial vehicle body is complex, the system is complex, the requirements are numerous, the space is narrow, the assembly operation content is also many, the unmanned aerial vehicle body assembly operation comprises the whole fuel tank sealing riveting, and fuel oil transportation, control system installation and partial structure riveting assembly. Can only operate through oil tank upper portion maintenance flap during the fuselage assembly, because the fuselage structure of unmanned aerial vehicle organism is complicated, operating space is narrow and small, the personnel can't creep into the inside operation that carries out of fuselage, can only bore into the fuselage and from last down carry out the operation, workman intensity of labour is big, and frock efficiency is on the low side, also has the hidden danger to quality stability.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a device of unmanned aerial vehicle fuselage upset for the fuselage upset is more convenient.
The purpose of the utility model is realized like this: the utility model provides a device of unmanned aerial vehicle fuselage upset, includes the base, install a pair of supporting seat on the base, be provided with the riding wheel group on the supporting seat, all be equipped with rotatable supporting disk on two riding wheel groups, link to each other through the pull rod between the supporting disk, the supporting disk inboard is equipped with the lug.
The utility model discloses during the use, with unmanned aerial vehicle fuselage hoist and mount back, with nodical frame auricle and lug fixed connection on the unmanned aerial vehicle fuselage, this moment the utility model discloses can with the electrodeless rotation of fuselage. Compared with the prior art, the beneficial effects of the utility model reside in that: through using the utility model discloses make the rotation of unmanned aerial vehicle fuselage convenient and reliable more.
As a further improvement, the supporting disk includes first dish and second dish of pegging graft together, first dish all is equipped with the engaging lug seat with second dish both ends both sides quotation, links to each other through the connecting plate between the engaging lug seat of first dish and second dish homonymy, links to each other through the connecting pin between the both ends of connecting plate and the engaging lug seat. So design makes after the unmanned aerial vehicle fuselage hoist and mount be connected more conveniently with the lug on the supporting disk, during the use, detaches first dish earlier, with hanging into second dish from the top between the unmanned aerial vehicle fuselage, with first dish and second dish assembly.
As a further improvement, the supporting seat is provided with a positioning seat below the supporting plate, the positioning seat is connected with a movable bolt, and the supporting plate is provided with a positioning hole matched with the movable bolt. The design of positioning seat and activity bolt makes when adding man-hour to the fuselage part, avoids its rotation, and convenient to use is nimble.
As a further improvement of the utility model, the bottom of the base is provided with a pulley. The design of pulley makes the utility model discloses it is more convenient to remove.
As a further improvement of the utility model, the bottom of the base is provided with an adjustable supporting rod. The design of adjusting the bracing piece makes the utility model discloses the location after the removal is more convenient.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the provided drawings without creative efforts.
Fig. 1 is a schematic view of the three-dimensional structure of the present invention.
Fig. 2 is an enlarged view of a portion a in fig. 1.
The device comprises a base 1, pulleys 2, an adjustable supporting rod 3, a supporting seat 4, a supporting wheel group 5, a supporting disk 6, an upper half disk 6a, a lower half disk 6b, a pull rod 7, a lifting lug 8, a connecting lug seat 9, a connecting plate 10, a connecting pin 11, a positioning seat 12 and a movable bolt 13.
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.
As shown in fig. 1-2, an unmanned aerial vehicle body turning device comprises a base 1, pulleys 2 are arranged at the bottom of the base 1, adjustable support rods 3 are arranged at the bottom of the base 1, a pair of support seats 4 are arranged on the base 1, the support seats 4 are provided with carrier roller sets 5, the two carrier roller sets 5 are both provided with rotatable support plates 6, the support plates 6 are connected through pull rods 7, lifting lugs 8 are arranged at the inner sides of the support plates 6, the support plates 6 comprise an upper half plate 6a and a lower half plate 6b which are spliced together, both side plate surfaces at both ends of the upper half plate 6a and the lower half plate 6b are both provided with connecting lug seats 9, the connecting lug seats 9 at the same side of the upper half plate 6a and the lower half plate 6b are connected through a connecting plate 10, both ends of the connecting plate 10 are connected with the connecting lug seats 9 through connecting pins 11, a positioning seat 12 arranged on the support seat 4 and positioned below the support plate 6, a movable bolt 13 is connected on the positioning seat 12, the supporting disk 6 is provided with a positioning hole matched with the movable bolt 13.
The utility model discloses during the use, earlier with first 6a of separating second 6b of twining, with the unmanned aerial vehicle fuselage hoist and mount back, put into from second 6b of twining's top, with nodical frame auricle and 8 fixed connection of lug on the unmanned aerial vehicle fuselage, first 6a of twining on the dress uses connecting pin 11 cooperation connecting plate 10 to accomplish assembly between them, this moment the utility model discloses can with the electrodeless rotation of fuselage.
The above description of the embodiments is only intended to help understand the method of the present invention and its core ideas. It should be noted that, for those skilled in the art, without departing from the principle of the present invention, the present invention can be further modified and modified, and such modifications and modifications also fall within the protection scope of the appended claims.
Claims (5)
1. The utility model provides a device of unmanned aerial vehicle fuselage upset, its characterized in that, includes base (1), install a pair of supporting seat (4) on base (1), be provided with riding wheel group (5) on supporting seat (4), all be equipped with rotatable supporting disk (6) on two riding wheel group (5), link to each other through pull rod (7) between supporting disk (6), supporting disk (6) inboard is equipped with lug (8).
2. The unmanned aerial vehicle fuselage of claim 1 device of overturning, characterized in that, the supporting disk (6) includes half first dish (6a) and half second dish (6b) of pegging graft together, half first dish (6a) and half second dish (6b) both ends both sides quotation all are equipped with connecting ear seat (9), link to each other through connecting plate (10) between connecting ear seat (9) of half first dish (6a) and half second dish (6b) homonymy, link to each other through connecting pin (11) between both ends of connecting plate (10) and connecting ear seat (9).
3. The unmanned aerial vehicle fuselage of claim 1 or 2, characterized in that, a positioning seat (12) is provided below the supporting plate (6) on the supporting seat (4), a movable plug (13) is connected to the positioning seat (12), and a positioning hole matched with the movable plug (13) is provided on the supporting plate (6).
4. The unmanned aerial vehicle fuselage of claim 1 or 2 is turned over the device, characterized in that, the bottom of base (1) is equipped with pulley (2).
5. The unmanned aerial vehicle fuselage of claim 4 is turned over the device, characterized in that, the bottom of base (1) is equipped with adjustable support rod (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120859806.1U CN214986158U (en) | 2021-04-25 | 2021-04-25 | Unmanned aerial vehicle fuselage device of upset |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120859806.1U CN214986158U (en) | 2021-04-25 | 2021-04-25 | Unmanned aerial vehicle fuselage device of upset |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214986158U true CN214986158U (en) | 2021-12-03 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120859806.1U Active CN214986158U (en) | 2021-04-25 | 2021-04-25 | Unmanned aerial vehicle fuselage device of upset |
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| CN (1) | CN214986158U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117226789A (en) * | 2023-11-13 | 2023-12-15 | 哈尔滨安宇迪航空工业股份有限公司 | Unmanned aerial vehicle lightweight organism frock |
-
2021
- 2021-04-25 CN CN202120859806.1U patent/CN214986158U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117226789A (en) * | 2023-11-13 | 2023-12-15 | 哈尔滨安宇迪航空工业股份有限公司 | Unmanned aerial vehicle lightweight organism frock |
| CN117226789B (en) * | 2023-11-13 | 2024-01-26 | 哈尔滨安宇迪航空工业股份有限公司 | Unmanned aerial vehicle lightweight organism frock |
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