CN214776582U - Unmanned aerial vehicle carrier - Google Patents
Unmanned aerial vehicle carrier Download PDFInfo
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- CN214776582U CN214776582U CN202121325278.8U CN202121325278U CN214776582U CN 214776582 U CN214776582 U CN 214776582U CN 202121325278 U CN202121325278 U CN 202121325278U CN 214776582 U CN214776582 U CN 214776582U
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- cargo hold
- carrier
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- aerial vehicle
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Abstract
The utility model discloses an unmanned aerial vehicle carrier. The carrier comprises a cargo hold part for loading cargo, and the cargo hold part can be loaded and unloaded with a hanging rack arranged on the lower abdominal bottom side of the unmanned aerial vehicle; a buffer part connected to a front end of the cargo hold part, the buffer part contacting the cargo unloading area when the carrier and the hanger are unloaded and lowered to the cargo unloading area; and the speed reduction part is connected with the rear end of the cargo hold part, and is used for controlling the falling speed and direction of the carrier when the carrier falls. The utility model provides an unmanned aerial vehicle carrier can load and uninstall with the stores pylon of installing in unmanned aerial vehicle lower abdomen bottom side, and the carrier has the cushioning effect, can avoid loading in the goods damage of cargo hold portion, and can control the carrier and descend to the descending direction and the descending speed when the goods uninstallation zone time after the hanging machine uninstallation, guarantees the stability and the accuracy nature of carrier descending.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle carrier.
Background
The unmanned aerial vehicle carrier is used for loading goods to load and uninstall with the stores pylon of installing in unmanned aerial vehicle lower abdomen bottom side, in order to realize the transportation to the goods. At present, no carrier for externally hanging a fixed wing unmanned aerial vehicle exists.
SUMMERY OF THE UTILITY MODEL
The utility model provides an unmanned aerial vehicle carrier can load and uninstall with the stores pylon of installing in the lower abdomen bottom side of unmanned aerial vehicle. The carrier can be conveniently loaded and unloaded by manual work when unmanned aerial vehicle parks the state, also can carry out the air-drop with unmanned aerial vehicle's stores pylon uninstallation when flying in the air. The carrier anterior segment has the cushioning effect, can avoid loading in the goods damage of cargo hold portion, and descending direction and descending speed when the rear segment can control the carrier air-drop guarantee the descending stability and the accuracy nature of carrier.
The above purpose is realized by the following technical scheme:
an unmanned aerial vehicle carrier comprising:
the cargo hold part is used for loading cargoes and can be loaded and unloaded with a hanging rack arranged on the lower abdominal bottom side of the unmanned aerial vehicle;
a buffer part connected to a front end of the cargo hold part, the buffer part contacting the cargo unloading area when the carrier and the hanger are unloaded and lowered to the cargo unloading area;
and the speed reduction part is connected with the rear end of the cargo hold part, and is used for controlling the falling speed and direction of the carrier when the carrier falls.
Optionally, the vehicle further comprises a locking hook mounted on the cargo compartment portion for hooking with a hook provided on the hanger.
Optionally, the cargo compartment comprises:
a cargo compartment skeleton;
the cargo compartment door is detachably mounted on the cargo compartment framework and encloses with the cargo compartment framework to form a cargo compartment, and the cargo is arranged in the cargo compartment.
Optionally, the cargo compartment portion further comprises a locking structure by which the cargo door is detachably connected to the cargo compartment skeleton.
Optionally, both the upper end and the lower end of the cargo door are detachably connected to the cargo compartment skeleton via the locking structure.
Optionally, the cargo door is provided with more than two.
Optionally, the locking structure comprises:
a first latch mounted on the cargo door;
the second lock catch is arranged on the cargo compartment framework;
and a lock pin capable of switching between two states of being inserted into the first locker and the second locker to lock the first locker and the second locker and being withdrawn from the first locker and the second locker to unlock the first locker and the second locker.
Optionally, two cargo hold doors are provided, two cargo hold frameworks are provided, one cargo hold door is provided at one side of the two cargo hold frameworks, one end of the cargo hold door is detachably connected with one cargo hold framework through the locking structure, and the other end of the cargo hold door is detachably connected with the other cargo hold framework through the locking structure; the other cargo hold door is arranged on the other side of the two cargo hold frameworks, one end of the cargo hold door is detachably connected with one cargo hold framework through the locking structure, the other end of the cargo hold door is detachably connected with the other cargo hold framework through the locking structure, and the two second lock catches arranged on the same cargo hold framework are integrally formed.
Alternatively, the buffer portion gradually increases in diameter from the front to the rear to be the same as the diameter of the cargo compartment portion.
Optionally, the buffering part comprises a plurality of layers of buffering parts, the plurality of layers of buffering parts are formed by bending from the rear part to the front part of the buffering part, and the plurality of layers of buffering parts are stacked from inside to outside and are arranged at intervals.
Compared with the prior art, the utility model discloses an at least including following beneficial effect:
the utility model provides an unmanned aerial vehicle carrier includes cargo hold portion, buffering portion and speed reduction portion. The cargo hold part is used for loading cargoes, and the cargo hold part can be loaded and unloaded with the stores pylon of installing in the lower abdomen bottom side of unmanned aerial vehicle. The buffer part is connected with the front end of the cargo hold part, and when the carrier is unloaded and descends to the cargo unloading area, the buffer part is contacted with the cargo unloading area so as to buffer the carrier and avoid the damage of the cargo loaded on the cargo hold part. The speed reduction portion is connected with the rear end of cargo hold portion, and when the carrier descends, the speed reduction portion is used for controlling the descending speed and the direction of carrier to can descend towards predetermined position and with predetermined speed when descending to the goods uninstallation district after carrier and stores pylon uninstallation, and then make the carrier can steadily descend in the goods uninstallation district, guarantee the stability and the accuracy nature that the carrier descends.
Drawings
Fig. 1 is a three-dimensional structure diagram of an unmanned aerial vehicle carrier according to an embodiment of the present invention;
FIG. 2 is an enlarged view at A in FIG. 1;
fig. 3 is a right side view of an unmanned aerial vehicle carrier according to an embodiment of the present invention;
fig. 4 is a front view of an unmanned aerial vehicle carrier according to an embodiment of the present invention;
fig. 5 is a right side view of a buffering portion of an unmanned aerial vehicle carrier according to an embodiment of the present invention;
fig. 6 is a sectional view at B in fig. 5.
In the figure:
1. a cargo compartment portion; 11. a cargo compartment skeleton;
2. a buffer section; 21. a buffer member;
3. a deceleration section;
4. a cargo compartment door; 41. a seal member;
5. a locking structure; 51. a first lock catch; 52. a second lock catch; 531. a pin body; 532. a handle;
6. a latch hook.
Detailed Description
The present invention is illustrated by the following examples, but the present invention is not limited to these examples. To the embodiment of the present invention, modify or replace some technical features, without departing from the spirit of the present invention, it should be covered in the technical solution scope of the present invention.
Referring to fig. 1-4, the present invention provides an unmanned aerial vehicle carrier, which includes a cargo compartment portion 1, a buffering portion 2 and a decelerating portion 3. The cargo hold part 1 is used for loading cargo, and the cargo hold part 1 can be loaded and unloaded with a hanger installed on the lower ventral bottom side of the unmanned aerial vehicle. The buffer part 2 is connected with the front end of the cargo hold part 1, and when the carrier is unloaded and descends to the cargo unloading area, the buffer part 2 is in contact with the cargo unloading area to buffer the carrier and avoid the damage of the cargo loaded on the cargo hold part 1. The speed reduction part 3 is connected with the rear end of the cargo hold part 1, and when the carrier descends, the speed reduction part 3 is used for controlling the descending speed and the descending direction of the carrier, so that the carrier can descend towards a preset direction and at a preset speed when descending to a cargo unloading area after unloading the carrier and the hanging rack, and further the carrier can stably descend in the cargo unloading area.
Optionally, the vehicle further comprises a latch hook 6, the latch hook 6 being mounted on the cargo compartment 1 for hooking with a hook provided on the pylon. Through set up latch hook 6 on cargo hold portion 1, be convenient for articulate with the couple that sets up on the stores pylon, and then be convenient for load and uninstallation between carrier and the stores pylon to the efficiency of loading and unloading goods has been improved.
Optionally, the cargo compartment 1 comprises a cargo compartment skeleton 11 and a cargo door 4. The cargo hold door 4 is detachably mounted on the cargo hold framework 11 and encloses with the cargo hold framework 11 to form a cargo hold, and cargoes are placed in the cargo hold. The cargo can be placed in the cargo hold or the cargo in the cargo hold can be taken out only by detaching one end of the cargo hold door 4 from the cargo hold framework 11, and the cargo hold is simple in structure and easy to operate.
Optionally, the cargo compartment 1 further comprises a locking structure 5, and the cargo door 4 is detachably connected to the cargo compartment skeleton 11 via the locking structure 5.
Optionally, the upper end and the lower end of the cargo door 4 are detachably connected to the cargo compartment frame 11 through the locking structure 5, so that a user can detach one end of the cargo door 4 from the cargo compartment frame 11 from different directions, thereby improving cargo loading and unloading efficiency.
Alternatively, more than two cargo hold doors 4 are provided, and a user can place the cargo in the cargo hold or take out the cargo in the cargo hold by detaching one end of one cargo hold door 4 from the cargo hold frame 11 nearby, so that the cargo handling efficiency is higher.
Optionally, the locking structure 5 comprises a first catch 51, a second catch 52 and a locking pin. A first catch 51 is mounted on the cargo door 4. And the second lock catch 52 is arranged on the cargo compartment framework 11. The lock pin can be switched between two states of being inserted into the first locker 51 and the second locker 52 to lock the first locker 51 and the second locker 52 and being withdrawn from the first locker 51 and the second locker 52 to unlock the first locker 51 and the second locker 52. When the lock pin is inserted into the first lock catch 51 and the second lock catch 52 to lock the first lock catch 51 and the second lock catch 52, the cargo door 4 is locked with the cargo compartment skeleton 11; when the lock pin is withdrawn from the first and second latches 51 and 52 to unlock the first and second latches 51 and 52, the cargo door 4 is unlocked from the cargo compartment frame 11.
Optionally, the lock pin includes a pin body 531 and a handle 532 disposed at one end of the pin body 531, a user can hold the handle 532 to insert the pin body 531 into the first lock catch 51 and the second lock catch 52, and can also hold the handle 532 to withdraw the pin body 531 from the first lock catch 51 and the second lock catch 52, and the handle 532 is disposed to facilitate the user's operation.
Optionally, two cargo hold doors 4 are provided, two cargo hold frameworks 11 are provided, one cargo hold door 4 is provided at one side of the two cargo hold frameworks 11, and one end of the cargo hold door 4 is detachably connected with one cargo hold framework 11 through a locking structure 5, and the other end of the cargo hold door 4 is detachably connected with the other cargo hold framework 11 through the locking structure 5; another cargo hold door 4 is arranged at the other side of the two cargo hold frameworks 11, one end of the cargo hold door 4 is detachably connected with one cargo hold framework 11 through the locking structure 5, the other end of the cargo hold door 4 is detachably connected with the other cargo hold framework 11 through the locking structure 5, and the two second lock catches 52 in the two groups of locking structures 5 arranged on the same cargo hold framework 11 are integrally formed, so that the structure of the locking structure 5 is simple, and the production and preparation of the locking structure 5 are facilitated.
Optionally, two cargo hold frameworks 11 are arranged in a mirror symmetry manner, two cargo hold doors 4 are also arranged in a mirror symmetry manner, and after the two cargo hold doors 4 are connected with the two cargo hold frameworks 11, the cargo hold part 1 is formed into a square or rectangular shape, so that no matter the carrier drops onto a cargo unloading area after being unloaded from the hanger, any surface faces downwards and is tightly attached to the cargo unloading area, and at least one part of the two cargo hold doors 4, which is connected with the cargo hold frameworks 11 through the locking structure 5, is always not located on one side tightly attached to the cargo unloading area, so that a user can conveniently open the cargo hold doors 4 and unload cargos in the cargo hold doors 4.
Optionally, the two second lock catches 52 in the two sets of locking structures 5 disposed on the same cargo compartment frame 11 may also be integrally formed with the lock hooks 6, so as to further simplify the structure of the carrier, and facilitate the production and preparation of the carrier.
Optionally, all be provided with sealing member 41 between cargo hold door 4 and cargo hold skeleton 11, speed reduction portion 3 and the buffer portion 2 to the clearance between sealed cargo hold door 4 and cargo hold skeleton 11, speed reduction portion 3 and the buffer portion 2 guarantees that the atmospheric pressure in the cargo hold is stable, and then has guaranteed the stability of unmanned aerial vehicle flight.
Optionally, the deceleration section is provided with a deceleration parachute, the deceleration parachute is opened when the carrier descends, and the descending direction of the carrier can be controlled by adjusting the length of part of the parachute cords of the deceleration parachute. Specifically, the drogue will shift towards the direction in which the relatively short parachute line is located, thereby achieving control over the direction in which the vehicle is dropped.
Referring to fig. 1, 5 and 6, optionally, the diameter of the buffer part 2 gradually increases from the front to the rear to be the same as that of the cargo hold part 1, and when the unmanned aerial vehicle flies, the buffer part 2 of the structure reduces the friction force with the air, so that the flying speed of the unmanned aerial vehicle is increased, and the energy consumption of the unmanned aerial vehicle is reduced.
Alternatively, the buffering part 2 includes a plurality of layers of buffering members 21, the plurality of layers of buffering members 21 are bent from the rear to the front of the buffering part 2, and the plurality of layers of buffering members 21 are stacked and spaced from each other from the inside to the outside, thereby obtaining a good buffering effect.
What has been described above are only some embodiments of the invention. For those skilled in the art, without departing from the inventive concept, several modifications and improvements can be made, which are within the scope of the invention.
Claims (10)
1. An unmanned aerial vehicle carrier, comprising:
the cargo hold part (1) is used for loading cargoes, and the cargo hold part (1) can be loaded and unloaded with a hanging rack installed on the lower abdominal bottom side of the unmanned aerial vehicle;
a buffer part (2) connected with the front end of the cargo hold part (1), wherein when the carrier and the hanging rack are unloaded and fall to a cargo unloading area, the buffer part (2) is in contact with the cargo unloading area;
and the speed reduction part (3) is connected with the rear end of the cargo hold part (1), and when the carrier descends, the speed reduction part (3) is used for controlling the descending speed and the descending direction of the carrier.
2. An unmanned vehicle according to claim 1, further comprising a latch hook (6), the latch hook (6) being mounted on the cargo compartment portion (1) for hooking with a hook provided on the pylon.
3. An unmanned aerial vehicle carrier as claimed in claim 1, wherein the cargo compartment portion (1) comprises:
a cargo compartment skeleton (11);
the cargo hold door (4) is detachably mounted on the cargo hold framework (11) and is enclosed with the cargo hold framework (11) to form a cargo hold, and the cargo is placed in the cargo hold.
4. An unmanned aerial vehicle carrier as claimed in claim 3, wherein the cargo compartment portion (1) further comprises a locking structure (5), the cargo compartment door (4) being detachably connected to the cargo compartment skeleton (11) by the locking structure (5).
5. An unmanned aerial vehicle carrier according to claim 4, wherein the cargo door (4) is detachably connected at both its upper and lower ends to the cargo compartment skeleton (11) by the locking structure (5).
6. An unmanned aerial vehicle carrier according to claim 5, wherein the cargo door (4) is provided with more than two.
7. The unmanned aerial vehicle carrier of claim 6, wherein the locking structure (5) comprises:
a first catch (51) mounted on the cargo door (4);
the second lock catch (52) is arranged on the cargo compartment framework (11);
a lock pin switchable between two states of being inserted into the first locker (51) and the second locker (52) to lock the first locker (51) and the second locker (52) and being withdrawn from the first locker (51) and the second locker (52) to unlock the first locker (51) and the second locker (52).
8. An unmanned aerial vehicle carrier as claimed in claim 7, wherein the cargo door (4) is provided with two flaps, the cargo compartment frames (11) are provided with two flaps, one cargo door (4) is provided at one side of the two cargo compartment frames (11), and one end of the cargo door (4) is detachably connected with one cargo compartment frame (11) through the locking structure (5) and the other end is detachably connected with the other cargo compartment frame (11) through the locking structure (5); another cargo hold door (4) is arranged on the other side of the two cargo hold frameworks (11), one end of the cargo hold door (4) is detachably connected with one cargo hold framework (11) through the locking structure (5), the other end of the cargo hold door is detachably connected with the other cargo hold framework (11) through the locking structure (5), and the two groups of second lock catches (52) arranged on the same cargo hold framework (11) in the locking structure (5) are integrally formed.
9. An unmanned aerial vehicle carrier according to any of claims 1-8, wherein the diameter of the bumper portion (2) gradually increases from front to rear to be the same as the diameter of the cargo compartment portion (1).
10. The unmanned aerial vehicle carrier of any one of claims 1-8, wherein the buffering portion (2) comprises a plurality of layers of buffering members (21), the plurality of layers of buffering members (21) are bent from the rear portion to the front portion of the buffering portion (2), and the plurality of layers of buffering members (21) are stacked and spaced from the inside to the outside.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121325278.8U CN214776582U (en) | 2021-06-15 | 2021-06-15 | Unmanned aerial vehicle carrier |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121325278.8U CN214776582U (en) | 2021-06-15 | 2021-06-15 | Unmanned aerial vehicle carrier |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214776582U true CN214776582U (en) | 2021-11-19 |
Family
ID=78712614
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121325278.8U Active CN214776582U (en) | 2021-06-15 | 2021-06-15 | Unmanned aerial vehicle carrier |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214776582U (en) |
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2021
- 2021-06-15 CN CN202121325278.8U patent/CN214776582U/en active Active
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