CN214524369U - Transportation unmanned aerial vehicle high strength skeleton - Google Patents
Transportation unmanned aerial vehicle high strength skeleton Download PDFInfo
- Publication number
- CN214524369U CN214524369U CN202023209298.7U CN202023209298U CN214524369U CN 214524369 U CN214524369 U CN 214524369U CN 202023209298 U CN202023209298 U CN 202023209298U CN 214524369 U CN214524369 U CN 214524369U
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- Prior art keywords
- connecting pieces
- connecting piece
- unmanned aerial
- reinforcing
- aerial vehicle
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- Expired - Fee Related
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- 230000003014 reinforcing effect Effects 0.000 claims description 29
- 239000000463 material Substances 0.000 claims description 6
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 239000010935 stainless steel Substances 0.000 claims description 3
- 229910001220 stainless steel Inorganic materials 0.000 claims description 3
- 238000003466 welding Methods 0.000 claims description 3
- 230000002787 reinforcement Effects 0.000 abstract 1
- 238000011161 development Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000012827 research and development Methods 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
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Abstract
The utility model discloses a transportation unmanned aerial vehicle high strength skeleton, including four stands (2), at least four reinforcement gasket (3), four rotor base (4), at least six stiffening ribs (5), four connecting piece two (6) and four connecting piece one (8), connecting piece two (6) are semicircular in shape, connecting piece one (8) are the rectangle, connecting piece one (8) are equipped with stiffening beam (7), connecting piece one (8) with stiffening beam (7) integrated into one piece; the utility model has the advantages of structural strength is high, consequently the utility model discloses but wide application and unmanned aerial vehicle field.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field specifically indicates a transportation unmanned aerial vehicle high strength skeleton.
Background
Along with unmanned aerial vehicle's vigorous development, adopt unmanned aerial vehicle transportation goods to have become the development trend of modern science and technology, the use of photographic or other non-transportation tasks of current small unmanned aerial vehicle mainly used shoots, then mainly rely on large-scale unmanned aerial vehicle in to the transportation of goods, but its volume of large-scale unmanned aerial vehicle is great in nevertheless, and have certain requirement to the take off and land area, and the heavy object is hardly carried to its own structure of the small unmanned aerial vehicle that the flexibility ratio is higher, consequently, the less transportation unmanned aerial vehicle high strength skeleton of a research and development size has important realistic meaning.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model discloses a high-strength framework for transporting unmanned aerial vehicles, which comprises four stand columns, at least four reinforcing gaskets, a four-rotor base, at least six reinforcing ribs, four connecting pieces two and four connecting pieces one, wherein the connecting pieces two are semicircular, the connecting pieces one are rectangular, the connecting pieces one are provided with reinforcing beams, the connecting pieces one and the reinforcing beams are integrally formed, four end parts of the four-rotor base are provided with blade hoisting holes, the four stand columns are arranged at equal intervals, the four connecting pieces one are sequentially arranged between two adjacent stand columns, and the connecting piece one is connected with two stand columns close to the four stand columns through bolts;
openings of the four second connecting pieces are all arranged downwards, any two of the four second connecting pieces are arranged at the lower parts of the first connecting pieces symmetrically in a group, the reinforcing ribs are arranged at the joints of the upright posts, the first connecting pieces and the second connecting pieces or at the joints of the first connecting pieces and the two second connecting pieces, and the upright posts, the reinforcing ribs, the first connecting pieces and the second connecting pieces are connected through bolts or the first connecting pieces, the reinforcing ribs and the second connecting pieces are connected through bolts;
the four-rotor base is arranged at the upper part of the first connecting piece and is connected with the first connecting piece through bolts, four arms of the four-rotor base are connected with the upper end of the upright post in an interference fit mode, a reinforcing gasket is sleeved at the upper end of the upright post, and the upper end of the upright post, the reinforcing gasket and the four-rotor base are sequentially connected in a welding mode;
furthermore, hollow holes are formed in the first connecting piece and the second connecting piece;
further, the reinforcing beam is X-shaped;
furthermore, the four upright posts are made of stainless steel;
further, the material of the four first connecting pieces and the material of the four second connecting pieces all comprise aluminum alloy.
Technical scheme more than adopting, the utility model has the technical effect that structural strength is high, the utility model discloses four link one-tenth overall frame that set up, four rotor bases that set up are used for consolidating the upper portion of four connecting pieces one, and four connecting pieces two that set up are responded to pressure and are kept away from, very big reinforcing connecting piece two's load-carrying capacity, the holistic intensity of further increase of the stiffening rib of setting finally reaches to have the high effect of structural strength.
Drawings
Fig. 1 is a front view of an embodiment of the present invention;
fig. 2 is a first perspective view of the embodiment of the present invention;
fig. 3 is a perspective view of a second embodiment of the present invention;
FIG. 4 is a perspective view of a first embodiment of the present invention with the quad-rotor base and reinforcing spacers removed;
as shown in the figure:
1-blade hoisting hole, 2-upright post, 3-reinforcing gasket, 4-four rotor base, 5-reinforcing rib, 6-connecting piece II, 7-reinforcing beam and 8-connecting piece I.
Detailed Description
For better explaining the present invention, the present invention will be further explained with reference to the following embodiments, and it should be noted that the following contents are only for better explaining the present invention and do not limit the scope of the claims of the present invention;
example one
As shown in fig. 1 to 4, a high-strength framework for transporting an unmanned aerial vehicle comprises four upright posts 2, at least four reinforcing gaskets 3, a four-rotor base 4, at least six reinforcing ribs 5, four connecting pieces two 6 and four connecting pieces one 8;
the second connecting piece 6 is semicircular, the first connecting piece 8 is rectangular, the first connecting piece 8 is provided with a reinforcing beam 7, and the first connecting piece 8 and the reinforcing beam 7 are integrally formed;
four ends of the four rotor wing bases 4 are provided with blade hoisting holes 1;
the four upright posts 2 are arranged at equal intervals, the four connecting pieces I8 are sequentially arranged between two adjacent upright posts 2, and the connecting pieces I8 are connected with the two adjacent upright posts 2 through bolts;
openings of the four second connecting pieces 6 are all arranged downwards, and any two of the four second connecting pieces 6 are symmetrically arranged at the lower parts of the first connecting pieces 8 in a group;
the reinforcing rib 5 is arranged at the joint of the upright post 2, the first connecting piece 8 and the second connecting piece 6 or at the joint of the first connecting piece 8 and the two second connecting pieces 6;
the upright post 2, the reinforcing rib 5, the first connecting piece 8 and the second connecting piece 6 are connected through a bolt or the first connecting piece 8, the reinforcing rib 5 and the second connecting piece 6 are connected through a bolt;
the four-rotor base 4 is arranged at the upper part of the first connecting piece 8, and the four-rotor base 4 is connected with the first connecting piece 8 through bolts;
four arms of the four-rotor base 4 are connected with the upper end of the upright post 2 in an interference fit manner;
the upper end of the upright post 2 is sleeved with a reinforcing gasket 3, and the upper end of the upright post 2, the reinforcing gasket 3 and the four-rotor base 4 are sequentially connected in a welding manner;
hollow holes are formed in the first connecting piece 8 and the second connecting piece 6;
the stiffening beam 7 is X-shaped;
the four upright posts 2 are made of stainless steel;
the material of the four first connecting pieces 8 and the material of the four second connecting pieces 6 all comprise aluminum alloy.
In using the utility model discloses the time, the region that four connecting pieces 8 enclose, essential power electronic equipment is placed to mainly used, and the staff can be according to the in-service use condition, the position of two 6 of adjusting connection spare, and two 6 reply names of connecting piece set up in principle, the utility model discloses when needing hoist and mount heavy object, only need set up extra stores pylon on two 6 of connecting piece, perhaps lug connection is at two 6 of connecting piece, and what need notice, connecting piece two 6 should consider the balance problem of heavy object when the carry heavy object, can not only hang on two 6 of connecting piece on one side.
The embodiments of the present invention are described above, and the present invention is not limited to the embodiments described above, and all of the embodiments are within the scope of the claims.
Claims (5)
1. A high-strength framework for transporting an unmanned aerial vehicle is characterized by comprising four upright posts (2), at least four reinforcing gaskets (3), a four-rotor base (4), at least six reinforcing ribs (5), four connecting pieces II (6) and four connecting pieces I (8), the second connecting piece (6) is semicircular, the first connecting piece (8) is rectangular, the first connecting piece (8) is provided with a reinforcing beam (7), the first connecting piece (8) and the reinforcing beam (7) are integrally formed, four ends of the four rotor wing bases (4) are respectively provided with a blade hoisting hole (1), the four upright posts (2) are arranged at equal intervals, the four first connecting pieces (8) are sequentially arranged between two adjacent upright posts (2), the first connecting piece (8) is connected with the two adjacent upright posts (2) through bolts;
openings of the four second connecting pieces (6) are all arranged downwards, any two of the four second connecting pieces (6) are symmetrically arranged at the lower parts of the first connecting pieces (8) in a group, the reinforcing ribs (5) are arranged at the joints of the upright columns (2), the first connecting pieces (8) and the second connecting pieces (6) or at the joints of the first connecting pieces (8) and the two second connecting pieces (6), and the upright columns (2), the reinforcing ribs (5), the first connecting pieces (8) and the second connecting pieces (6) are connected through bolts or the first connecting pieces (8), the reinforcing ribs (5) and the second connecting pieces (6) are connected through bolts;
four rotor bases (4) set up the upper portion of connecting piece (8), four rotor bases (4) through the bolt with connecting piece (8) are connected, four arms of four rotor bases (4) all through the interference fit mode with the upper end of stand (2) is connected, the pot head of stand (2) is equipped with strengthens gasket (3), the upper end of stand (2) strengthen gasket (3) with four rotor bases (4) loop through the welding mode and connect.
2. The high-strength framework for the transportation of unmanned aerial vehicles as claimed in claim 1, wherein the first connecting member (8) and the second connecting member (6) are both provided with hollowed holes.
3. A high-strength skeleton for transport unmanned aerial vehicles according to claim 1, wherein the reinforcing beam (7) is X-shaped.
4. A high-strength framework for a transport drone according to claim 1, characterised in that the four uprights (2) are made of stainless steel.
5. The high-strength framework for the transportation unmanned aerial vehicle as claimed in claim 1, wherein the material of the first four connecting members (8) and the material of the second four connecting members (6) comprise aluminum alloy.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023209298.7U CN214524369U (en) | 2020-12-28 | 2020-12-28 | Transportation unmanned aerial vehicle high strength skeleton |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023209298.7U CN214524369U (en) | 2020-12-28 | 2020-12-28 | Transportation unmanned aerial vehicle high strength skeleton |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214524369U true CN214524369U (en) | 2021-10-29 |
Family
ID=78297792
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023209298.7U Expired - Fee Related CN214524369U (en) | 2020-12-28 | 2020-12-28 | Transportation unmanned aerial vehicle high strength skeleton |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214524369U (en) |
-
2020
- 2020-12-28 CN CN202023209298.7U patent/CN214524369U/en not_active Expired - Fee Related
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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 |
Granted publication date: 20211029 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |