CN211996182U - Novel unmanned aerial vehicle load module and unmanned aerial vehicle - Google Patents
Novel unmanned aerial vehicle load module and unmanned aerial vehicle Download PDFInfo
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- CN211996182U CN211996182U CN202020026320.5U CN202020026320U CN211996182U CN 211996182 U CN211996182 U CN 211996182U CN 202020026320 U CN202020026320 U CN 202020026320U CN 211996182 U CN211996182 U CN 211996182U
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Abstract
The embodiment of the utility model discloses novel unmanned aerial vehicle load module and unmanned aerial vehicle is applied to unmanned air vehicle technique field, include: positioner, locking device and unlocking device, this positioner and this unmanned aerial vehicle fuselage positioner phase-match, the two combines together and to fix a position this novel unmanned aerial vehicle load module's loading position, this locking device stretches out this novel unmanned aerial vehicle load module's surface, fuselage locking device who corresponds on with this unmanned aerial vehicle combines together, this novel unmanned aerial vehicle load module of locking and this unmanned aerial vehicle, this novel unmanned aerial vehicle load module locks as an organic wholely with this unmanned aerial vehicle after the locking, this novel unmanned aerial vehicle load module need not to set up the load cabin alone on unmanned aerial vehicle's the aircraft back, also reduced the weight cost when improving complete machine intensity, and, this novel unmanned aerial vehicle load module's appearance and unmanned aerial vehicle's fuselage combine together, flight air resistance has been reduced, and pneumatic efficiency is improved.
Description
Technical Field
The utility model belongs to the technical field of machinery, especially, relate to novel unmanned aerial vehicle load module and unmanned aerial vehicle.
Background
Unmanned aerial vehicle is as a emerging high-tech product, and is high-efficient reliable during the operation, is favored by the user deeply, and load module is its indispensable equipment of operation. Therefore, how to reasonably install the load module becomes a great subject of unmanned aerial vehicle design.
At present most unmanned aerial vehicle producers adopt be the design form of seting up the load cabin on the back of the plane, place the load module in the fuselage inside, but this technique is great to the destruction of fuselage intensity, and both need strengthen the load cabin alone, need add load cabin cover again, and weight cost loss is great.
SUMMERY OF THE UTILITY MODEL
The utility model provides a novel unmanned aerial vehicle load module and unmanned aerial vehicle, through with load module, load cabin cover, load cabin locking mechanism is integrated integrative, and it is great to the destruction of fuselage intensity to have solved current load module, and both need strengthen the load cabin alone, need add load cabin cover again, the great problem of weight cost loss.
The embodiment of the utility model provides a novel unmanned aerial vehicle load module, include: the locking device is arranged on the unlocking device; the positioning device is matched with a body positioning device on the unmanned aerial vehicle body, and the positioning device is combined with the body positioning device to position the position of the novel unmanned aerial vehicle load module, which is installed on the unmanned aerial vehicle; locking device stretches out novel unmanned aerial vehicle load module's surface, with the last fuselage locking device that corresponds of unmanned aerial vehicle combines together, locks novel unmanned aerial vehicle load module with unmanned aerial vehicle, the locking back novel unmanned aerial vehicle load module with unmanned aerial vehicle locking is as an organic whole, just, novel unmanned aerial vehicle load module's surface does unmanned aerial vehicle's surface.
Optionally, the positioning device is a positioning column or a positioning hole, and is arranged at the front end of the novel unmanned aerial vehicle load module.
Optionally, the number of the positioning columns or the positioning holes is four.
Optionally, the positioning column is made of a soft material.
Optionally, the locking device is two lock tongues that set up respectively novel unmanned aerial vehicle load module both sides.
Optionally, the unlocking device comprises two unlocking buttons which are respectively arranged on two sides of the novel unmanned aerial vehicle load module and close to the lower surface of the novel unmanned aerial vehicle load module.
The embodiment of the utility model provides an unmanned aerial vehicle for load as above novel unmanned aerial vehicle load module, its characterized in that, unmanned aerial vehicle includes: a machine body positioning device and a machine body locking device; the body positioning device is arranged in a load cabin of the unmanned aerial vehicle and is matched with the positioning device of the novel unmanned aerial vehicle load module, and the body positioning device is combined with the positioning device to position the position of the novel unmanned aerial vehicle load module, which is installed on the unmanned aerial vehicle; fuselage locking device sets up the internal surface in load cabin, the locking device of novel unmanned aerial vehicle load module stretches out the surface of novel unmanned aerial vehicle load module, with the fuselage locking device that corresponds on the unmanned aerial vehicle combines together, locks novel unmanned aerial vehicle load module with unmanned aerial vehicle, after the locking novel unmanned aerial vehicle load module with unmanned aerial vehicle locking is as an organic whole, just, the surface of novel unmanned aerial vehicle load module does unmanned aerial vehicle's surface.
Optionally, the positioning device of the machine body comprises a positioning column or a positioning hole.
Optionally, the load compartment set up in unmanned aerial vehicle's ventral, and the opening in the ventral, the opening size in load compartment novel unmanned aerial vehicle load module phase-match is used for holding novel unmanned aerial vehicle load module.
As can be seen from the above embodiment of the utility model, the novel unmanned aerial vehicle load module comprises a positioning device, a locking device and an unlocking device, the positioning device is combined with the body positioning device to position the position of the novel unmanned aerial vehicle load module installed on the unmanned aerial vehicle, the locking device extends out of the outer surface of the novel unmanned aerial vehicle load module to lift the novel unmanned aerial vehicle load module to rotate upwards around the positioning device at the front end, the body locking device corresponding to the unmanned aerial vehicle locks to realize the locking of the novel unmanned aerial vehicle load module and the unmanned aerial vehicle, the locked novel unmanned aerial vehicle load module and the unmanned aerial vehicle are locked into a whole, and the outer surface of the novel unmanned aerial vehicle load module is a part of the outer surface of the unmanned aerial vehicle, a load cabin does not need to be separately arranged on the back of the unmanned aerial vehicle, and further does not need to add a load cabin cover and a locking mechanism of the load cabin, and, this novel unmanned aerial vehicle load module's appearance and unmanned aerial vehicle's fuselage combine together, have avoided the flight air resistance that this novel unmanned aerial vehicle load module brought, have improved pneumatic efficiency.
Drawings
In order to illustrate the embodiments of the present invention or the technical solutions in the prior art more clearly, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention.
Fig. 1 is a schematic view of a load assembly form of a novel unmanned aerial vehicle load module on an unmanned aerial vehicle according to an embodiment of the present invention;
fig. 2 is a schematic view of a load unloading form of a novel unmanned aerial vehicle load module provided by an embodiment of the present invention;
fig. 3 is the embodiment of the utility model provides a novel unmanned aerial vehicle load module's structure schematic diagram.
Detailed Description
To make the objects, features and advantages of the present invention more obvious and understandable, the embodiments of the present invention are clearly and completely described with reference to the accompanying drawings in the embodiments of the present invention, and obviously, the described embodiments are only some embodiments, not all embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by the skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1 to 3, fig. 1 is a schematic view of a load assembly form of a novel unmanned aerial vehicle load module on an unmanned aerial vehicle, provided by an embodiment of the present invention; fig. 2 is a schematic view of a load unloading form of a novel unmanned aerial vehicle load module provided by an embodiment of the present invention; fig. 3 is the embodiment of the utility model provides a novel unmanned aerial vehicle load module's structure schematic diagram.
The novel unmanned aerial vehicle load module in this embodiment for load with unmanned aerial vehicle's fuselage. For convenience of illustration, this embodiment takes the loading form of the novel unmanned aerial vehicle load module ventral as an example, novel unmanned aerial vehicle load module 200 can also be loaded at any position of the unmanned aerial vehicle fuselage, the load cabin of the unmanned aerial vehicle fuselage is correspondingly provided with the volume of novel unmanned aerial vehicle load module 200, the loading position of the shape is matched, after novel unmanned aerial vehicle load module 200 is loaded onto the unmanned aerial vehicle, novel unmanned aerial vehicle load module 200 and unmanned aerial vehicle close into a complete fuselage, that is, become a part of unmanned aerial vehicle after novel unmanned aerial vehicle load module 200 is loaded, the outer surface of novel unmanned aerial vehicle load module 200 is a part of the outer surface of unmanned aerial vehicle, and is concrete, when novel unmanned aerial vehicle load module 200 is the loading form of the ventral, the lower surface of novel unmanned aerial vehicle load module 200 is a part. Need not to establish the load cabin that inside held novel unmanned aerial vehicle load module 200 in addition on unmanned aerial vehicle's surface, and then need not to set up corresponding load cabin cover. Be provided with the electronic plug on novel unmanned aerial vehicle load module 200, with the socket switch-on back of unmanned aerial vehicle's loading position, accomplish the connection of circuit.
The novel unmanned aerial vehicle load module in this embodiment is used for loading on unmanned aerial vehicle 100, and novel unmanned aerial vehicle load module 200 includes: the positioning device 10, the locking device 20 and the unlocking device 30;
the positioning device 10 matches with a fuselage positioning device (not marked in the figure) on the fuselage of the unmanned aerial vehicle 100, and the positioning device 10 is combined with the fuselage positioning device to position the position of the novel unmanned aerial vehicle load module 200 installed on the unmanned aerial vehicle 100.
Wherein, linkage in locking device 20 and the unlocking device 30, but locking device 20 and the locking device 30 closure to lock novel unmanned aerial vehicle load module 200 and unmanned aerial vehicle 100. In the locked state, the unlocking device 30 is pressed to unlock the locking device 20, so that the locking device 20 is unlocked and separated from the fuselage locking device.
Further, the positioning device 10 is a positioning column or a positioning hole, preferably, the number of the positioning column or the positioning hole is four, and the positioning column or the positioning hole is disposed at the front end of the novel unmanned aerial vehicle load module 200, and of course, the positioning column or the positioning hole can also be disposed at the tail end or other surfaces of the novel unmanned aerial vehicle load module 200. In this embodiment, the positioning device 10 is taken as an example of a positioning column, and the body positioning device corresponding to the positioning device 10 in the unmanned aerial vehicle 100 is a body positioning hole matched with the positioning column in position and size.
Further, the locking device 20 is two lock tongues respectively arranged at two sides of the novel unmanned aerial vehicle load module 200, one of the lock tongues 20 is shown in fig. 3, and the other lock tongue 20 is arranged at the other side of the novel unmanned aerial vehicle load module 200.
Unlocking device 30 includes two release button, sets up respectively in novel unmanned aerial vehicle load module 200 both sides, and for novel unmanned aerial vehicle load module 200's upper surface, release button 30 more is close to the position of novel unmanned aerial vehicle load module 200 lower surface. One of the unlock buttons 30 is shown in fig. 3, with the other unlock button 30 on the other side of the new drone load module 200. The user presses two unlock buttons 30 simultaneously, two spring bolts 20 retractions for novel unmanned aerial vehicle load module 200 unlocks from unmanned aerial vehicle 100 fast, improves the uninstallation speed of dismantling novel unmanned aerial vehicle load module 200.
Further, the material of reference column can be hard material, when loading novel unmanned aerial vehicle load module 200 onto unmanned aerial vehicle 100, supports the reference column in four corresponding fuselage locating holes in unmanned aerial vehicle 100's load cabin, can fix a position novel unmanned aerial vehicle load module 200 in unmanned aerial vehicle 100's load cabin.
It should be noted that, in this embodiment, during assembly, the positioning column first enters the positioning hole of the fuselage, and then the novel unmanned aerial vehicle load module 200 needs to be lifted upwards, so that the novel unmanned aerial vehicle load module 200 rotates clockwise in the vertical plane around the positioning column at the front end thereof (the arrow in the figure indicates the direction for installation), and the locking tongue 20 is locked with the fuselage locking device, thereby completing the loading of the novel unmanned aerial vehicle load module 200. Like this, the material of reference column can be soft material, has certain toughness, avoids novel unmanned aerial vehicle load module 200 and unmanned aerial vehicle 100's hard collision at the loading in-process, avoids the damage of spare part.
Further, still be provided with electronic plug 40 on novel unmanned aerial vehicle load module 200, when novel unmanned aerial vehicle load module 200 loaded onto unmanned aerial vehicle 100, need put through electronic plug 40 and the last electronic socket (not marked in the figure) that matches of unmanned aerial vehicle 100, realize communicating with each other with unmanned aerial vehicle 100 circuit.
The embodiment of the utility model provides a novel unmanned aerial vehicle load module, including positioner, locking device and unlocking device, positioner combines together with fuselage positioner, position the position that this novel unmanned aerial vehicle load module installs on this unmanned aerial vehicle, locking device stretches out novel unmanned aerial vehicle load module's surface, lift this novel unmanned aerial vehicle load module and upwards rotate around the positioner of front end, with the locking of the fuselage locking device that corresponds on the unmanned aerial vehicle, realize this novel unmanned aerial vehicle load module and this unmanned aerial vehicle's locking, novel unmanned aerial vehicle load module after the locking locks as an organic whole with unmanned aerial vehicle, and, novel unmanned aerial vehicle load module's surface is a part of unmanned aerial vehicle's surface, load module, unmanned aerial vehicle load cabin cover and load cabin locking mechanism integration among the prior art to need not to set up the load cabin alone on unmanned aerial vehicle's the back of the aircraft, furthermore, a load cabin cover and a locking mechanism of the load cabin are not required to be additionally arranged, so that the weight cost is reduced while the strength of the whole machine is improved, and the optimization of the design is realized; meanwhile, the appearance of the novel unmanned aerial vehicle load module is integrated with the body of the unmanned aerial vehicle, the flying air resistance caused by the novel unmanned aerial vehicle load module is avoided, and the pneumatic efficiency is improved.
The embodiment of the utility model provides a still provide an unmanned aerial vehicle 100, have as above novel unmanned aerial vehicle load module 200, unmanned aerial vehicle 100 includes: a body positioning device and a body locking device (not shown).
The fuselage positioning device is arranged in a load cabin of the unmanned aerial vehicle 100 and is matched with a positioning device of the novel unmanned aerial vehicle load module 200, and the fuselage positioning device is combined with the positioning device to position the position of the novel unmanned aerial vehicle load module 200, which is arranged on the unmanned aerial vehicle;
the fuselage locking device is arranged on the inner surface of the load cabin, the locking device of the novel unmanned aerial vehicle load module 200 extends out of the outer surface of the novel unmanned aerial vehicle load module 200 and is combined with the corresponding fuselage locking device on the unmanned aerial vehicle to lock the novel unmanned aerial vehicle load module 200 and the unmanned aerial vehicle, the novel unmanned aerial vehicle load module 200 and the unmanned aerial vehicle are locked into a whole after being locked, and the outer surface of the novel unmanned aerial vehicle load module 200 is the outer surface of the unmanned aerial vehicle;
further, this fuselage positioner includes reference column or locating hole, and this fuselage positioner and the last positioner 10 phase-matches of novel unmanned aerial vehicle load module 200, if positioner 10 is the reference column, then this fuselage positioner is the locating hole, if positioner 10 is the locating hole, then this fuselage positioner is the reference column for the assembled position of novel unmanned aerial vehicle load module 200 in unmanned aerial vehicle 100's load cabin of interactive positioning.
Further, as shown in fig. 2 and fig. 3, the load compartment is disposed on the belly of the drone and has an opening in the belly, and the opening of the load compartment is smaller than the load module 200 of the novel drone, so as to accommodate the load module 200 of the novel drone.
The unmanned aerial vehicle provided by the embodiment of the utility model has a novel unmanned aerial vehicle load module, after the locking device of the novel unmanned aerial vehicle load module is locked with the corresponding body locking device on the unmanned aerial vehicle, thereby realizing the locking of the novel unmanned aerial vehicle load module and the unmanned aerial vehicle, the novel unmanned aerial vehicle load module after being locked is locked with the unmanned aerial vehicle into a whole, and the outer surface of the novel unmanned aerial vehicle load module, namely the outer surface of the unmanned aerial vehicle, does not need to separately set a load cabin on the back of the unmanned aerial vehicle, and further does not need to add a load cabin cover and a locking mechanism of the load cabin, so that the weight cost is reduced while the strength of the whole machine is improved, and the optimization of the design; meanwhile, the appearance of the novel unmanned aerial vehicle load module is integrated with the body of the unmanned aerial vehicle, the flying air resistance caused by the novel unmanned aerial vehicle load module is avoided, and the pneumatic efficiency is improved.
It is right above the utility model provides a novel unmanned aerial vehicle load module and unmanned aerial vehicle's description, to the technical personnel in this field, the foundation the utility model discloses the thought of embodiment all has the change part on concrete implementation and application scope, to sum up, this description content should not be understood as right the utility model discloses a restriction.
Claims (10)
1. The utility model provides a novel unmanned aerial vehicle load module, its characterized in that, novel unmanned aerial vehicle load module includes:
the locking device is arranged on the unlocking device;
the positioning device is matched with a body positioning device on the unmanned aerial vehicle body, and the positioning device is combined with the body positioning device to position the position of the novel unmanned aerial vehicle load module, which is installed on the unmanned aerial vehicle;
locking device stretches out novel unmanned aerial vehicle load module's surface, with the last fuselage locking device that corresponds of unmanned aerial vehicle combines together, locks novel unmanned aerial vehicle load module with unmanned aerial vehicle, the locking back novel unmanned aerial vehicle load module with unmanned aerial vehicle locking is as an organic whole, just, novel unmanned aerial vehicle load module's surface does unmanned aerial vehicle's surface.
2. The novel unmanned aerial vehicle load module of claim 1, wherein the positioning device is a positioning post or a positioning hole disposed at a front end of the novel unmanned aerial vehicle load module.
3. The novel unmanned aerial vehicle load module of claim 2, wherein the number of positioning posts or positioning holes is four.
4. The novel unmanned aerial vehicle load module of claim 3, wherein the positioning posts are made of soft materials.
5. A novel unmanned aerial vehicle load module according to any one of claims 1-4, wherein the locking device is two lock tongues respectively arranged on two sides of the novel unmanned aerial vehicle load module.
6. The novel unmanned aerial vehicle load module of claim 5, wherein the unlocking device comprises two unlocking buttons, and the two unlocking buttons are respectively arranged at two sides of the novel unmanned aerial vehicle load module and are close to the lower surface of the novel unmanned aerial vehicle load module.
7. The novel unmanned aerial vehicle load module of claim 6, wherein the locking device is linked with the unlocking device, and the unlocking device is pressed to unlock the locking device, so that the locking device is unlocked and separated from the fuselage locking device.
8. An unmanned aerial vehicle for carrying a novel unmanned aerial vehicle load module as claimed in claims 1-7, the unmanned aerial vehicle comprising:
a machine body positioning device and a machine body locking device;
the body positioning device is arranged in a load cabin of the unmanned aerial vehicle and is matched with the positioning device of the novel unmanned aerial vehicle load module, and the body positioning device is combined with the positioning device to position the position of the novel unmanned aerial vehicle load module, which is installed on the unmanned aerial vehicle;
fuselage locking device sets up the internal surface in load cabin, the locking device of novel unmanned aerial vehicle load module stretches out the surface of novel unmanned aerial vehicle load module, with the fuselage locking device that corresponds on the unmanned aerial vehicle combines together, locks novel unmanned aerial vehicle load module with unmanned aerial vehicle, after the locking novel unmanned aerial vehicle load module with unmanned aerial vehicle locking is as an organic whole, just, the surface of novel unmanned aerial vehicle load module does unmanned aerial vehicle's surface.
9. The drone of claim 8, wherein the fuselage positioning device comprises positioning posts or holes.
10. The drone of claim 8 or 9, wherein the load compartment is disposed in a belly of the drone and opens to the belly, the opening of the load compartment being sized to match the new drone load module for receiving the new drone load module.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020026320.5U CN211996182U (en) | 2020-01-07 | 2020-01-07 | Novel unmanned aerial vehicle load module and unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020026320.5U CN211996182U (en) | 2020-01-07 | 2020-01-07 | Novel unmanned aerial vehicle load module and unmanned aerial vehicle |
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| CN211996182U true CN211996182U (en) | 2020-11-24 |
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| CN202020026320.5U Active CN211996182U (en) | 2020-01-07 | 2020-01-07 | Novel unmanned aerial vehicle load module and unmanned aerial vehicle |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114379803A (en) * | 2021-12-28 | 2022-04-22 | 中电科芜湖通用航空产业技术研究院有限公司 | Unmanned aerial vehicle load quick detach mechanism |
| CN117465712A (en) * | 2023-12-26 | 2024-01-30 | 成都金支点科技有限公司 | Locking structure with tongue-shaped elastic sheet for unmanned aerial vehicle, load cabin and unmanned aerial vehicle |
-
2020
- 2020-01-07 CN CN202020026320.5U patent/CN211996182U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114379803A (en) * | 2021-12-28 | 2022-04-22 | 中电科芜湖通用航空产业技术研究院有限公司 | Unmanned aerial vehicle load quick detach mechanism |
| CN117465712A (en) * | 2023-12-26 | 2024-01-30 | 成都金支点科技有限公司 | Locking structure with tongue-shaped elastic sheet for unmanned aerial vehicle, load cabin and unmanned aerial vehicle |
| CN117465712B (en) * | 2023-12-26 | 2024-03-15 | 成都金支点科技有限公司 | Locking structure with tongue-shaped elastic sheet for unmanned aerial vehicle, load cabin and unmanned aerial vehicle |
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Address after: 518000, 1st Floor, 16th Building, Zhiheng Industrial Park, Nantou Street, Nanshan District, Shenzhen City, Guangdong Province Patentee after: Shenzhen Pegasus Robotics Co.,Ltd. Country or region after: China Address before: 518000, 1st Floor, 16th Building, Zhiheng Industrial Park, Nantou Street, Nanshan District, Shenzhen City, Guangdong Province Patentee before: SHENZHEN FEIMA ROBOTICS Co.,Ltd. Country or region before: China |
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Address after: 518000, 13th Floor, Building A4, Nanshan Zhiyuan, No. 1001 Xueyuan Avenue, Changyuan Community, Taoyuan Street, Nanshan District, Shenzhen, Guangdong Province Patentee after: Shenzhen Pegasus Robotics Co.,Ltd. Country or region after: China Address before: 518000, 1st Floor, 16th Building, Zhiheng Industrial Park, Nantou Street, Nanshan District, Shenzhen City, Guangdong Province Patentee before: Shenzhen Pegasus Robotics Co.,Ltd. Country or region before: China |
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