CN220616219U - Low-sensitivity type fixed wing unmanned aerial vehicle with high production speed - Google Patents
Low-sensitivity type fixed wing unmanned aerial vehicle with high production speed Download PDFInfo
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- CN220616219U CN220616219U CN202322273463.2U CN202322273463U CN220616219U CN 220616219 U CN220616219 U CN 220616219U CN 202322273463 U CN202322273463 U CN 202322273463U CN 220616219 U CN220616219 U CN 220616219U
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- unmanned aerial
- aerial vehicle
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- wing unmanned
- fixed wing
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- 238000004519 manufacturing process Methods 0.000 title claims abstract description 15
- 239000007788 liquid Substances 0.000 claims abstract description 11
- 239000000463 material Substances 0.000 claims abstract description 5
- 239000002184 metal Substances 0.000 claims abstract description 5
- 239000000835 fiber Substances 0.000 claims abstract description 4
- 210000001503 joint Anatomy 0.000 claims description 18
- 230000035945 sensitivity Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract description 4
- 238000001914 filtration Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model belongs to the technical field of fixed wing unmanned aerial vehicles, and particularly relates to a low-sensitivity fixed wing unmanned aerial vehicle with high production speed, which comprises a fixed wing unmanned aerial vehicle and a low-sensitivity mechanism, wherein the fixed wing unmanned aerial vehicle comprises a shell and two wings; the low-sensitivity mechanism comprises a liquid pump and two counterweight cavities; the two wings are respectively connected to the front side and the rear side of the shell, the two weight cavities are respectively and fixedly arranged on the outer sides of the two wings, and the liquid pump is fixedly arranged in the shell and connected with the two weight cavity pipelines; the shell is made of metal fiber filtering materials, and connecting plates are fixed at the inner ends of the two wings; the front side and the rear side of the shell are provided with notches, the connecting plates are inserted into the notches, and a hollow cavity is fixedly arranged in the shell; the device has solved the problem of guarantee fixed wing unmanned aerial vehicle flight stability when current fixed wing unmanned aerial vehicle can't realize quick installation improvement production efficiency.
Description
Technical Field
The utility model belongs to the technical field of fixed wing unmanned aerial vehicles, and particularly relates to a low-sensitivity fixed wing unmanned aerial vehicle with high production speed.
Background
The unmanned aerial vehicle with fixed wing has the sweepback angle of the outer end of the wing capable of being regulated automatically or manually with speed. Because of excellent functions and modularized integration, the method is widely applied to the professions such as mapping, geology, petroleum, agriculture and forestry and the like, and has wide market application prospect.
The existing fixed wing unmanned aerial vehicle is when production, unmanned aerial vehicle shell and wing can't the quick connect to joint strength is low, has reduced production efficiency on the one hand, and on the other hand unmanned aerial vehicle's stability reduces, and the wing drops easily in the flight, leads to unmanned aerial vehicle to drop the damage. This phenomenon is a problem to be solved by those skilled in the art.
Disclosure of Invention
The utility model aims to provide a low-sensitivity fixed wing unmanned aerial vehicle with high production speed, so as to solve the problems in the background technology.
In order to solve the technical problems, the utility model provides the following technical scheme: the low-sensitivity type fixed wing unmanned aerial vehicle with the high production speed comprises a fixed wing unmanned aerial vehicle and a low-sensitivity mechanism, wherein the fixed wing unmanned aerial vehicle comprises a shell and two wings;
the low-sensitivity mechanism comprises a liquid pump and two counterweight cavities;
the two wings are respectively connected to the front side and the rear side of the shell, the two weight cavities are respectively and fixedly arranged on the outer sides of the two wings, and the liquid pump is fixedly arranged in the shell and connected with the two weight cavity pipelines;
the shell is made of metal fiber filter materials.
The utility model further describes that the inner ends of the two wings are fixed with connecting plates;
the front side and the rear side of the shell are provided with notches, the connecting plates are inserted into the notches, and a hollow cavity is fixedly arranged in the shell;
the sliding grooves are formed in the front side and the rear side of the hollow cavity, the connecting plate is inserted into the sliding grooves, the tapered rod is fixed on the left side of the connecting plate, the butt joint block is fixed on the left side of the inner wall of the hollow cavity, and two butt joint holes are formed in the right side of the butt joint block and aligned with the tapered rod;
the conical rod is inserted into the butt joint hole.
According to the utility model, the magnetic blocks are fixed on the right side of the connecting plate, and the magnetic poles of the two magnetic blocks are opposite.
Compared with the prior art, the utility model has the following beneficial effects: according to the fixed wing unmanned aerial vehicle, an operator inserts the wing into the shell through the connecting plate, the connecting plate is respectively connected with the notch and the inner wall of the sliding groove in a sliding mode, then the wing is pushed to move leftwards, so that the conical rod at the left side of the connecting plate is inserted into the butt joint hole, the conical rod is tightly connected with the butt joint hole due to the conical degree of the connecting plate, the wing is fixed, the wing is tightly connected with the shell, the installation efficiency of the fixed wing unmanned aerial vehicle can be relatively improved, the production speed is improved, the stability of the fixed wing unmanned aerial vehicle after installation is ensured, when the fixed wing unmanned aerial vehicle needs to be disassembled, the wing is reversely pulled, the wing is convenient to disassemble quickly, the disassembly efficiency of the fixed wing unmanned aerial vehicle is high, the magnetic blocks at the right ends of the two connecting plates generate magnetic attraction force which is mutually attracted, the two wings are tightly connected, the connection strength between the wing and the shell is further improved, the phenomenon that the wing is separated in the flight process is fully avoided, and the protection of the fixed wing unmanned aerial vehicle is enhanced.
Drawings
The accompanying drawings are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate the utility model and together with the embodiments of the utility model, serve to explain the utility model. In the drawings:
FIG. 1 is a schematic view of the overall structure of the present utility model;
FIG. 2 is a top view of the present utility model;
FIG. 3 is a schematic plan view of a hollow cavity of the present utility model;
in the figure: 1. a housing; 2. a wing; 3. a liquid pump; 4. a weight cavity; 5. a connecting plate; 6. a notch; 7. a hollow cavity; 8. a chute; 9. a tapered rod; 10. a butt joint block; 11. a butt joint hole; 12. a magnetic block.
Detailed Description
The technical scheme of the present utility model is further described in non-limiting detail below with reference to the preferred embodiments and the accompanying drawings. It will be apparent that the described embodiments are only some, but not all, embodiments of the utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-3, the present utility model provides the following technical solutions: the low-sensitivity type fixed wing unmanned aerial vehicle with high production speed comprises a fixed wing unmanned aerial vehicle and a low-sensitivity mechanism, wherein the fixed wing unmanned aerial vehicle comprises a shell 1 and two wings 2;
the low-sensitivity mechanism comprises a liquid pump 3 and two counterweight cavities 4;
the two wings 2 are respectively connected to the front side and the rear side of the shell 1, the two weight cavities 4 are respectively and fixedly arranged on the outer sides of the two wings 2, and the liquid pump 3 is fixedly arranged in the shell 1 and is connected with the two weight cavities 4 in a pipeline manner;
the shell 1 is made of metal fiber filter materials;
the shell 1 of the fixed wing unmanned aerial vehicle made of metal fiber materials is superior to ceramic filter materials in high pressure drop, purification capacity and stability, when the fixed wing unmanned aerial vehicle is produced, the produced wing 2 is installed on the front side and the rear side of the shell 1, when the fixed wing unmanned aerial vehicle flies, liquid is injected into the two counterweight cavities 4 through the liquid pump 3, so that the weight of the outer end of the wing 2 changes, the sensitivity of the fixed wing unmanned aerial vehicle during the flying can be reduced, the fixed wing unmanned aerial vehicle is prevented from being capable of emergency avoiding due to high sensitivity when the flying speed is too fast, and the effect of protecting the fixed wing unmanned aerial vehicle is achieved.
The inner ends of the two wings 2 are fixed with connecting plates 5;
the front side and the rear side of the shell 1 are provided with notches 6, a connecting plate 5 is inserted into the notches 6, and a hollow cavity 7 is fixedly arranged in the shell 1;
the sliding grooves 8 are formed in the front side and the rear side of the hollow cavity 7, the connecting plate 5 is inserted into the sliding grooves 8, the conical rod 9 is fixed on the left side of the connecting plate 5, the butt joint block 10 is fixed on the left side of the inner wall of the hollow cavity 7, and two butt joint holes 11 are formed in the right side of the butt joint block 10 and aligned with the conical rod 10;
the conical rod 9 is inserted into the butt joint hole 11;
the operating personnel inserts wing 2 in casing 1 through connecting plate 5, at this moment connecting plate 5 respectively with notch 6 and spout 8 inner wall sliding connection, later promote wing 2 left side removal, make the conical rod 9 of connecting plate 5 left side insert in butt joint hole 11, because its tapering, make conical rod 7 and butt joint hole 11 zonulae occludens, thereby fix wing 2, make wing 2 and casing 1 zonulae occludens, can improve fixed wing unmanned aerial vehicle's installation effectiveness relatively, the production speed is improved, and ensure the stability after the fixed wing unmanned aerial vehicle installs, when dismantling, then reverse pulling wing 2, be convenient for dismantle wing 2 fast, fixed wing unmanned aerial vehicle's dismouting efficiency is high.
The right side of the connecting plate 5 is fixedly provided with magnetic blocks 12, and the magnetic poles of the two magnetic blocks 12 are opposite;
the magnetic blocks 12 at the right ends of the two connecting plates 5 generate magnetic attraction force which is mutually attracted and are tightly connected, so that the two wings 2 are tightly connected, the connection strength between the wings 2 and the shell 1 is further improved, the phenomenon that the wings 2 are separated in the flying process is fully avoided, and the protection of the fixed wing unmanned aerial vehicle is enhanced.
In the description of the present utility model, it should be understood that the directions or positional relationships indicated by the terms "upper", "lower", "front", "rear", "left", "right", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of describing the present utility model, and do not indicate or imply that the apparatus or elements referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present utility model.
Finally, it should be pointed out that: the above embodiments are only for illustrating the technical solution of the present utility model, and are not limiting. Although the utility model has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may be modified or some technical features may be equivalently replaced, and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the embodiments of the present utility model.
Claims (3)
1. The utility model provides a fast low sensitivity type fixed wing unmanned aerial vehicle of production, includes fixed wing unmanned aerial vehicle and low sensitive mechanism, its characterized in that: the fixed wing unmanned aerial vehicle comprises a shell (1) and two wings (2);
the low-sensitivity mechanism comprises a liquid pump (3) and two counterweight cavities (4);
the two wings (2) are respectively connected to the front side and the rear side of the shell (1), the two weight balancing cavities (4) are respectively and fixedly arranged on the outer sides of the two wings (2), and the liquid pump (3) is fixedly arranged in the shell (1) and is connected with the two weight balancing cavities (4) through pipelines;
the shell (1) is made of metal fiber filter materials.
2. The low-sensitivity fixed wing unmanned aerial vehicle with high production speed according to claim 1, wherein: the inner ends of the two wings (2) are fixed with connecting plates (5);
the front side and the rear side of the shell (1) are provided with notches (6), the connecting plate (5) is inserted into the notches (6), and a hollow cavity (7) is fixedly arranged in the shell (1);
the sliding chute (8) is formed in the front side and the rear side of the hollow cavity (7), the connecting plate (5) is inserted into the sliding chute (8), a conical rod (9) is fixed on the left side of the connecting plate (5), a butt joint block (10) is fixed on the left side of the inner wall of the hollow cavity (7), and two butt joint holes (11) are formed in the right side of the butt joint block (10) and are aligned with the conical rod (9);
the conical rod (9) is inserted into the butt joint hole (11).
3. The low-sensitivity fixed wing unmanned aerial vehicle with high production speed according to claim 2, wherein: the right side of the connecting plate (5) is fixedly provided with magnetic blocks (12), and the magnetic poles of the two magnetic blocks (12) are opposite.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322273463.2U CN220616219U (en) | 2023-08-23 | 2023-08-23 | Low-sensitivity type fixed wing unmanned aerial vehicle with high production speed |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322273463.2U CN220616219U (en) | 2023-08-23 | 2023-08-23 | Low-sensitivity type fixed wing unmanned aerial vehicle with high production speed |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220616219U true CN220616219U (en) | 2024-03-19 |
Family
ID=90224174
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322273463.2U Active CN220616219U (en) | 2023-08-23 | 2023-08-23 | Low-sensitivity type fixed wing unmanned aerial vehicle with high production speed |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220616219U (en) |
-
2023
- 2023-08-23 CN CN202322273463.2U patent/CN220616219U/en active Active
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