CN221214663U - Unmanned aerial vehicle stops storehouse cabin cover structure - Google Patents
Unmanned aerial vehicle stops storehouse cabin cover structure Download PDFInfo
- Publication number
- CN221214663U CN221214663U CN202323241744.6U CN202323241744U CN221214663U CN 221214663 U CN221214663 U CN 221214663U CN 202323241744 U CN202323241744 U CN 202323241744U CN 221214663 U CN221214663 U CN 221214663U
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- cabin cover
- unmanned aerial
- aerial vehicle
- strengthening
- cover structure
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- 238000005728 strengthening Methods 0.000 claims abstract description 41
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 28
- 230000001681 protective effect Effects 0.000 claims description 14
- 230000002146 bilateral effect Effects 0.000 claims 1
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000000694 effects Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle shutdown cabin cover structure which comprises a cabin cover main body, wherein a protecting shell is fixedly arranged above the cabin cover main body, reinforcing ribs are fixedly connected below the protecting shell, reinforcing strips are symmetrically and fixedly connected on two sides below the protecting shell, an auxiliary rotating mechanism is arranged in the protecting shell and is used for being connected with an external driving piece, and the protecting shell and the cabin cover main body are assisted to rotate. The beneficial effects of the utility model are as follows: through the strengthening rib that sets up, the strengthening rib is provided with a plurality ofly simultaneously, and a plurality of strengthening ribs alternately set up in the below of protecting crust for a plurality of strengthening ribs are latticed, and the diameter of strengthening rib is less, and then the weight of a plurality of strengthening ribs is less, has greatly increased the structural strength of protecting crust when increasing less quality to the protecting crust, also through the strengthening bar that sets up, and two strengthening bars have all seted up the weight-reducing cavity in one side in opposite directions, then reduced the weight of strengthening bar.
Description
Technical Field
The utility model relates to a hatch cover structure, in particular to an unmanned aerial vehicle shutdown hatch cover structure, and belongs to the technical field of unmanned aerial vehicle shutdown cabins.
Background
The unmanned plane is called as unmanned plane for short, and is a unmanned plane operated by radio remote control equipment and a self-contained program control device. Unmanned aerial vehicles are in fact a collective term for unmanned aerial vehicles, which from a technical point of view can be defined as: unmanned helicopter, unmanned fixed wing aircraft, unmanned multi-rotor aircraft, unmanned airship and unmanned parachute wing aircraft.
The unmanned aerial vehicle shut down the storehouse and is used for storing unmanned aerial vehicle's storehouse body, and in order to protect unmanned aerial vehicle to the inside unmanned aerial vehicle in unmanned aerial vehicle shut down storehouse, can be provided with the cabin cover that is used for protecting at the top in unmanned aerial vehicle shut down storehouse generally, the cabin cover is in the in-process of using, receives the collision easily, and the cabin cover opens and closes for convenient driving piece, its structural quality is less, then mechanism strength is lower, damages easily, consequently we propose an unmanned aerial vehicle shut down cabin cover structure.
Disclosure of utility model
The utility model aims to solve the problems and provide the unmanned aerial vehicle shutdown cabin cover structure, through the arranged reinforcing ribs, a plurality of reinforcing ribs are arranged at the same time, the reinforcing ribs are arranged below the protective shell in a crossing way, so that the reinforcing ribs are in a grid shape, the diameters of the reinforcing ribs are smaller, the weight of the reinforcing ribs is smaller, the structural strength of the protective shell is greatly increased while the weight of the protective shell is increased, and the weight-reducing cavities are formed in the opposite sides of the two reinforcing ribs through the arranged reinforcing ribs, so that the weight of the reinforcing ribs is reduced, and the reinforcing ribs have an effective structural reinforcing effect on the protective shell.
The utility model realizes the aim through the following technical scheme, and the unmanned aerial vehicle shutdown cabin cover structure comprises a cabin cover main body, wherein a protective shell is fixedly arranged above the cabin cover main body, reinforcing ribs are fixedly connected below the protective shell, reinforcing ribs are symmetrically and fixedly connected on two sides below the protective shell, an auxiliary rotating mechanism is arranged in the protective shell and is used for being connected with an external driving piece, and the protective shell and the cabin cover main body are assisted to rotate.
Preferably, the reinforcing ribs are arranged in a plurality, and the reinforcing ribs are arranged below the protective shell in a crossing manner.
Preferably, the two opposite sides of the reinforcing strips are provided with weight-reducing cavities.
Preferably, the auxiliary rotating mechanism comprises two rotating rods, the two rotating rods are symmetrically and fixedly connected to the inner wall of the hatch main body, and two first rotating holes which are communicated inside and outside are formed in the outer wall of the hatch main body.
Preferably, a through second rotating hole is formed in the end portion of the rotating rod.
Preferably, the axle center axes of the first rotating hole and the second rotating hole are coincident, and the first rotating hole and the second rotating hole are used for being inserted into a driving shaft of an external driving piece.
The beneficial effects of the utility model are as follows: through the strengthening rib that sets up, the strengthening rib is provided with a plurality ofly simultaneously, a plurality of strengthening ribs alternately set up in the below of protecting crust for a plurality of strengthening ribs are latticed, and the diameter of strengthening rib is less, and then the weight of a plurality of strengthening ribs is less, greatly increased the structural strength of protecting crust when increasing less quality to the protecting crust, equally through the strengthening bar that sets up, and two strengthening bars have all seted up and have subtracted heavy cavity in one side in opposite directions, then reduced the weight of strengthening bar, and the strengthening bar plays effectual structure reinforced effect to the protecting crust.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic structural view of a protective shell according to the present utility model;
Fig. 3 is an enlarged schematic view of portion a of fig. 2 in accordance with the present utility model.
In the figure: 1. a hatch cover main body; 2. a protective shell; 201. reinforcing ribs; 202. reinforcing strips; 203. a rotating lever; 204. a first rotation hole; 205. and a second rotation hole.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. 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.
The embodiment of the utility model discloses a cabin cover structure for an unmanned aerial vehicle parking cabin.
According to the drawings 1-3, the protection cover comprises a cover main body 1, wherein a protection cover 2 is fixedly arranged above the cover main body 1, reinforcing ribs 201 are fixedly connected below the protection cover 2, reinforcing ribs 202 are symmetrically and fixedly connected on two sides below the protection cover 2, an auxiliary rotating mechanism is arranged inside the protection cover 2 and is used for being connected with an external driving piece, and the protection cover 2 and the cover main body 1 are assisted to rotate.
Through the strengthening rib 201 that sets up, the strengthening rib 201 is provided with a plurality ofly simultaneously, a plurality of strengthening ribs 201 alternately set up in the below of protecting crust 2 for a plurality of strengthening ribs 201 are latticed, and the diameter of strengthening rib 201 is less, then the weight of a plurality of strengthening ribs 201 is less, greatly increased the structural strength of protecting crust 2 when increasing less quality to protecting crust 2, equally through the strengthening rib 202 of setting up, and two strengthening ribs 202 all have seted up the weight-reducing cavity in one side in opposite directions, then reduced the weight of strengthening rib 202, and the strengthening rib 202 plays effectual structural reinforcement's effect to protecting crust 2.
Preferably, a plurality of reinforcing ribs 201 are provided, and a plurality of reinforcing ribs 201 are disposed below the protective case 2 in a crossing manner.
Preferably, the opposite sides of the two reinforcing strips 202 are each provided with a weight-reducing cavity.
Preferably, the auxiliary rotating mechanism comprises two rotating rods 203, the two rotating rods 203 are symmetrically and fixedly connected to the inner wall of the hatch main body 1, and two first rotating holes 204 which are communicated with the inside and the outside are formed in the outer wall of the hatch main body 1.
Preferably, the end of the rotation lever 203 is provided with a second rotation hole 205 therethrough.
Preferably, the central axes of the first rotation hole 204 and the second rotation hole 205 coincide, and the first rotation hole 204 and the second rotation hole 205 are used for plugging a driving shaft of an external driving member.
In the process of installation, the driving shaft of the external driving piece passes through the first rotating hole 204 on the outer wall of the hatch main body 1 and is inserted into the second rotating hole 205 formed at the end part of the rotating rod 203, so that the driving shaft of the driving piece can drive the hatch main body 1 and the rotating rod 203 to rotate simultaneously when the driving piece works, and the hatch main body 1 rotates more stably.
Through the strengthening rib 201 that sets up, the strengthening rib 201 is provided with a plurality ofly simultaneously, a plurality of strengthening ribs 201 alternately set up in the below of protecting crust 2 for a plurality of strengthening ribs 201 are latticed, and the diameter of strengthening rib 201 is less, then the weight of a plurality of strengthening ribs 201 is less, greatly increased the structural strength of protecting crust 2 when increasing less quality to protecting crust 2, equally through the strengthening rib 202 of setting up, and two strengthening ribs 202 all have seted up the weight-reducing cavity in one side in opposite directions, then reduced the weight of strengthening rib 202, and the strengthening rib 202 plays effectual structural reinforcement's effect to protecting crust 2.
Furthermore, it should be understood that although the present disclosure describes embodiments, not every embodiment is provided with a separate embodiment, and that this description is provided for clarity only, and that the disclosure is not limited to the embodiments described in detail below, and that the embodiments described in the examples may be combined as appropriate to form other embodiments that will be apparent to those skilled in the art.
Claims (6)
1. The utility model provides an unmanned aerial vehicle parks storehouse cabin cover structure, includes cabin cover main part (1), its characterized in that, the top fixed mounting protection shell (2) of cabin cover main part (1), the below fixedly connected with strengthening rib (201) of protection shell (2), and the bilateral symmetry fixedly connected with strengthening strip (202) of protection shell (2) below, and the inside of protection shell (2) is provided with supplementary rotary mechanism, supplementary rotary mechanism is used for being connected with external driving piece, supplementary protection shell (2) and cabin cover main part (1) rotate.
2. The unmanned aerial vehicle shutdown cabin cover structure according to claim 1, wherein a plurality of reinforcing ribs (201) are provided, and a plurality of reinforcing ribs (201) are arranged below the protective shell (2) in a crossing manner.
3. The unmanned aerial vehicle shutdown cabin cover structure according to claim 1, wherein the two reinforcing strips (202) are provided with weight-reducing cavities on opposite sides.
4. The unmanned aerial vehicle shutdown cabin cover structure according to claim 1, wherein the auxiliary rotating mechanism comprises two rotating rods (203), the two rotating rods (203) are symmetrically and fixedly connected to the inner wall of the cabin cover main body (1), and two first rotating holes (204) which are communicated with the inside and the outside are formed in the outer wall of the cabin cover main body (1).
5. The unmanned aerial vehicle shutdown cabin cover structure according to claim 4, wherein the end of the rotating rod (203) is provided with a second through rotating hole (205).
6. The unmanned aerial vehicle shutdown cabin cover structure according to claim 5, wherein the central axes of the first rotation hole (204) and the second rotation hole (205) are coincident, and the first rotation hole (204) and the second rotation hole (205) are used for plugging a driving shaft of an external driving member.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323241744.6U CN221214663U (en) | 2023-11-29 | 2023-11-29 | Unmanned aerial vehicle stops storehouse cabin cover structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323241744.6U CN221214663U (en) | 2023-11-29 | 2023-11-29 | Unmanned aerial vehicle stops storehouse cabin cover structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221214663U true CN221214663U (en) | 2024-06-25 |
Family
ID=91580362
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323241744.6U Active CN221214663U (en) | 2023-11-29 | 2023-11-29 | Unmanned aerial vehicle stops storehouse cabin cover structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221214663U (en) |
-
2023
- 2023-11-29 CN CN202323241744.6U patent/CN221214663U/en active Active
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