CN115230976A - Unmanned aerial vehicle load quick assembly disassembly device - Google Patents
Unmanned aerial vehicle load quick assembly disassembly device Download PDFInfo
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- CN115230976A CN115230976A CN202210784032.XA CN202210784032A CN115230976A CN 115230976 A CN115230976 A CN 115230976A CN 202210784032 A CN202210784032 A CN 202210784032A CN 115230976 A CN115230976 A CN 115230976A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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Abstract
The invention relates to a rapid load dismounting device for an unmanned aerial vehicle. The method comprises the following steps: load mounting panel, a plurality of load support arm offer the load mounting hole that is used for installing a plurality of load modules on the load mounting panel, a plurality of load support arm one end can be dismantled and connect on the load mounting panel, and the load support arm other end is connected with and presss from both sides the cover mechanism, presss from both sides the cover mechanism and is used for being connected with the unmanned aerial vehicle horn. According to the invention, the load mounting plate is provided with the load mounting holes for mounting the plurality of load modules, so that the load modules with the suitable types and the suitable number can be selected according to the use requirements, the requirements for carrying different types and different numbers of load modules can be met, a multi-task mode is realized, and the operation efficiency is improved; by arranging the plurality of load support arms, the load support arms with the appropriate number can be selected according to different types of unmanned aerial vehicles; through setting up the cover mechanism that presss from both sides, press from both sides the cover mechanism and can fixed connection on the unmanned aerial vehicle horn, can realize quick assembly disassembly, improve change efficiency, the flexibility is higher.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a device for quickly disassembling and assembling a load of an unmanned aerial vehicle.
Background
In recent years, high-rise buildings are developed along with the development of cities, but the overhaul of the high-rise buildings still depends on manual monitoring at present, is limited by high-rise structures, and has great potential safety hazards. The unmanned aerial vehicle is fast in development and widely applied to the field of aerial photography, such as aerial photography, traffic management, fire early warning and the like, on the basis, the expansion with the unmanned aerial vehicle as a carrier can be applied to the field of inspection of high-rise buildings, and the unmanned aerial vehicle can obtain high-definition orthographic images by matching with a visible light camera so as to monitor the surface quality condition of the outside of the high-rise buildings.
In unmanned aerial vehicle aerial photography and remote sensing system, unmanned aerial vehicle load system carrying device contains cloud platform camera or other load module and fixed cloud platform camera or other load module's supporting equipment, cloud platform camera is through self-stabilization, can guarantee that the sensor visual axis is stable, make aerial photography or data collection undistorted, and unmanned aerial vehicle load system carrying device stabilizes cloud platform camera or other load module on unmanned aerial vehicle, the security of unmanned aerial vehicle operation process has been guaranteed, simultaneously can also reduce substantially because unmanned aerial vehicle vibration, the disturbance that unstable factors such as fuselage slope caused aerial photography camera, keep the stability of camera visual angle, make the picture of shooing more clear, thereby improve the aerial photography quality, therefore unmanned aerial vehicle load carries and seems to be especially important.
In recent years, with the rapid development of the unmanned aerial vehicle industry, various forms of unmanned aerial vehicles are continuously brought into the market, and the unmanned aerial vehicle has wide application in the industries such as police, city management, agriculture, address, weather, electric power, emergency rescue and disaster relief, aerial photography and the like. Meanwhile, application equipment with various functions is continuously emerged, and convenience is brought to different industries. The common carrying platform is a single-mode single-load module carrying platform, and mainly shows that the unmanned aerial vehicle carries a single load (a photoelectric pod, a Mini SAR, a laser radar, an oblique camera, an aerial camera and the like) through the carrying platform to realize task requirements. Most unmanned aerial vehicles in the market can carry only one load module, and because the unmanned aerial vehicle needs to be modified to carry the load module,
the current unmanned aerial vehicle carries on load module has the shortcoming of following shortcoming mode to be:
1. the existing unmanned aerial vehicle carrying load module is single in type and lacks variability.
When the unmanned aerial vehicle performs different tasks, different load modules are generally required to be carried. The existing unmanned aerial vehicle can only carry one load module generally, and the requirements of different tasks can not be met.
2. The existing carrying platform can not realize the combined carrying of various load modules, and has a single operation mode.
The existing unmanned aerial vehicle only considers a certain task requirement and technical requirement of a single type in design, and only can meet a single-platform single-task mode. Such a mounting platform is not only economically inefficient, but also cannot be mounted in combination with a plurality of types of load modules.
3. The existing carrying platform is lack of flexibility and rapidity in dismounting.
When the supporting equipment of the load module or the fixed holder camera or other load modules needs to be replaced according to conditions such as weather, landform, operation requirements and the like, the supporting equipment of the load module or the fixed holder camera or other load modules needs to be replaced together, the replacement time is long, the operation is complex, the flexibility is lacked, and the emergency tasks such as urgent surveying and mapping and disaster observation are extremely unfavorable.
Disclosure of Invention
Based on this, it can be according to the user demand to be necessary one kind, selects the load module that suits type and quantity, can satisfy the demand of carrying on the load module of different grade type and different quantity, can realize the multitask mode, improves the operating efficiency, and can realize quick assembly disassembly, improves and changes efficiency, the higher unmanned aerial vehicle load quick assembly disassembly device of flexibility.
The utility model provides an unmanned aerial vehicle load quick assembly disassembly device which characterized in that includes:
the load mounting plate is provided with a load mounting hole for mounting a load module;
the first ends of the load support arms are arranged along the circumferential direction of the load mounting plate at intervals, detachably connected to the load mounting plate, the second ends of the load support arms are connected with a clamping mechanism, and the clamping mechanism is used for being connected with an unmanned aerial vehicle arm.
By arranging the load mounting plate, the load mounting plate is provided with the load mounting holes for mounting the plurality of load modules, the load modules with the adaptive types and the number can be selected according to the use requirements, the requirements for carrying different types and different numbers of load modules can be met, the operation modes are diversified, the multi-task mode is realized, the design cost is reduced, and the operation efficiency is improved; by arranging the plurality of load support arms, the load support arms with the appropriate number can be selected according to different types of unmanned aerial vehicles; through setting up the cover mechanism that presss from both sides, press from both sides the cover mechanism and can fixed connection on the unmanned aerial vehicle horn, can realize quick assembly disassembly, improve change efficiency, the flexibility is higher.
In one embodiment, the second end of the load arm is hingedly or gimbaled to the collet mechanism.
Through with load support arm and the articulated or universal swivelling joint of clamp cover mechanism for clamp cover mechanism relative load support arm is rotatable, can adapt to and install on the unmanned aerial vehicle horn of different grade type, and adaptability is stronger.
In one embodiment, the load support arms are detachably connected to the load mounting plate by quick connect assemblies.
The load support arm can be dismantled with the load mounting panel through quick connect assembly and be connected, can realize the quick assembly disassembly of load support arm and load mounting panel, improves and changes efficiency.
In one embodiment, the quick connection assembly comprises a positioning hole arranged on the load mounting plate, a threaded hole arranged on the load support arm and a connecting bolt, the positioning hole and the threaded hole are arranged correspondingly, and the connecting bolt penetrates through the positioning hole of the load mounting plate and is in threaded connection with the threaded hole of the load support arm.
In one embodiment, the load mounting plate is provided with a connecting hole for mounting a damping table.
Through setting up the connecting hole, can install the shock attenuation platform to the load mounting panel on to install the load module to the shock attenuation platform, can guarantee to reduce the impact damage to the load module at the executive task in-process.
In one embodiment, the load arm includes a connecting portion connected to the load mounting plate, the connecting portion being parallel to the load mounting plate, and an inclined portion disposed obliquely to the connecting portion.
Through setting up the relative connecting portion slope of slope portion and setting up, can make the level of load mounting panel be higher than unmanned aerial vehicle's level to can not hinder unmanned aerial vehicle's motion.
In one embodiment, the load arm tapers in width from proximate the first end of the load mount plate to distal the second end of the load mount plate.
In one embodiment, the clamping mechanism comprises a clamp body and a fastening component, the fastening component comprises a first pin shaft seat fixedly connected to a first end of the clamp body, a second pin shaft seat fixedly connected to a second end of the clamp body, and a locking pin, and pin holes matched with the locking pin are arranged on the first pin shaft seat and the second pin shaft seat.
In one embodiment, the load receiving holes include circular holes and kidney holes.
In one embodiment, the load mounting plate is a carbon fiber plate.
In the scheme, the load mounting plate is provided with the load mounting holes for mounting the plurality of load modules, so that the load modules of the corresponding types and the number can be selected according to the use requirements, the requirements for carrying different types and the different numbers of load modules can be met, the operation modes are diversified, a multi-task mode is realized, the design cost is reduced, and the operation efficiency is improved; by arranging the plurality of load support arms, the load support arms with the appropriate number can be selected according to different types of unmanned aerial vehicles; through setting up the cover mechanism that presss from both sides, press from both sides the cover mechanism and can fixed connection on the unmanned aerial vehicle horn, can realize quick assembly disassembly, improve change efficiency, the flexibility is higher.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this application, illustrate embodiments of the invention and, together with the description, serve to explain the invention and not to limit the invention.
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.
Fig. 1 is a schematic structural view of a rapid dismounting device for a load of an unmanned aerial vehicle according to an embodiment of the present invention;
fig. 2 is a schematic view of an installation structure of a rapid load dismounting device, a load module, a damping table and an unmanned aerial vehicle arm of an unmanned aerial vehicle according to an embodiment of the present invention;
fig. 3 is a schematic structural diagram of a part of the rapid dismounting device for load of an unmanned aerial vehicle according to an embodiment of the present invention, and the structure of the load mounting plate is not shown in the figure;
fig. 4 is an enlarged schematic view of a portion a in fig. 1.
Description of the reference numerals
10. An unmanned aerial vehicle load rapid dismounting device; 100. a load mounting plate; 110. a load mounting hole; 111. a circular hole; 112. a waist-shaped hole; 120. positioning holes; 130. connecting holes; 200. a load support arm; 210. a connecting portion; 220. an inclined portion; 230. a threaded hole; 300. a load module; 400. a jacket mechanism; 410. a clamp body; 411. a first clamp; 412. a second clamp; 420. a fastening assembly; 421. a first pin shaft seat; 422. a second pin shaft seat; 423. a locking pin; 424. a pin hole; 425. a second groove portion; 426. a pull ring; 500. an unmanned aerial vehicle arm; 600. shock attenuation platform.
Detailed Description
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in detail below. In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein.
In the description of the present invention, it is to be understood that the terms "central," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," "counterclockwise," "axial," "radial," "circumferential," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the invention and to simplify the description, and are not intended to indicate or imply that the referenced device or element must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting of the invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless explicitly specified otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
In the present invention, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may be directly contacting the second feature or the first and second features may be indirectly contacting each other through intervening media. Also, a first feature "on," "over," and "above" a second feature may be directly or diagonally above the second feature, or may simply indicate that the first feature is at a higher level than the second feature. A first feature "under," "beneath," and "under" a second feature may be directly under or obliquely under the second feature, or may simply mean that the first feature is at a lesser elevation than the second feature.
It will be understood that when an element is referred to as being "secured to" or "disposed on" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. As used herein, the terms "vertical," "horizontal," "upper," "lower," "left," "right," and the like are for purposes of illustration only and do not denote a single embodiment.
Referring to fig. 1 and 2, an embodiment of the present application relates to an unmanned aerial vehicle load quick dismounting device 10, which includes a load mounting plate 100 and a plurality of load support arms 200. Load mount plate 100 is used in conjunction with load module 300. First ends of a plurality of load arms 200 are attached to load mount plate 100. A collet mechanism 400 is attached to the second end of the plurality of load arms 200. The collet mechanism 400 is used to connect with the drone arm 500.
Referring to fig. 1 and 2, the load mounting plate 100 is provided with a load mounting hole 110 for mounting the load module 300. The load modules 300 with the suitable types and the suitable number can be selected according to the use requirements, and the requirements for carrying the load modules 300 with different types and different numbers are met, so that a multi-task mode is realized, the design cost is reduced, and the operation efficiency is improved. It is to be understood that the load module 300 may be a pan-tilt camera, other third party fixed camera, a multiline lidar, or the like.
The load mounting holes 110 include a plurality of circular holes 111 and a plurality of kidney holes 112, which are suitable for mounting and fixing different types of load modules 300. It should be understood that when the load module 300 is mounted on the load mounting plate 100, a screw nut assembly is required to be provided to match the load mounting hole 110, so as to enable the load module 300 to be quickly disassembled. In the present embodiment, the load mounting plate 100 is a carbon fiber plate. The carbon fiber plate has good performances such as high tensile strength, corrosion resistance, shock resistance and impact resistance.
Referring to fig. 1 and 2, first ends of a plurality of load arms 200 are removably coupled to load mount plate 100 at spaced intervals along the circumference of load mount plate 100. The load support arms 200 with the suitable number can be selected according to the unmanned aerial vehicles of different types and the use requirements, and the application range is wide. For example, the drone has four drone arms 500, and four load arms 200 may be selected. The unmanned aerial vehicle horn 500 is six, and four load arms 200 or six load arms 200 can be selected. Similarly, the number of unmanned aerial vehicle booms 500 is eight, and four load support arms 200, six load support arms 200, or eight load support arms 200 can be selected. The load arm 200 is made of nylon material, and has excellent mechanical strength, high strength, wear resistance and better corrosion resistance.
A plurality of load arms 200 are removably coupled to load mount plate 100 via quick connect assemblies. Referring to fig. 3, the quick-connect assembly includes a positioning hole 120 formed on the load mounting plate 100, a threaded hole 230 formed on the load arm 200, and a connecting bolt. The positioning hole 120 is disposed corresponding to the threaded hole 230. The connecting bolt is threaded through the positioning hole 120 of the load mounting plate 100 and is in threaded connection with the threaded hole 230 of the load arm 200. In this embodiment, each load arm 200 is detachably connected to the load mounting plate 100 by at least two sets of quick connect assemblies, which prevent the load arm 200 from rotating relative to the load mounting plate 100. During assembly or disassembly, the load mounting plate 100 and the load support arm 200 can be quickly disassembled and assembled only by adjusting the connecting bolts.
Referring to fig. 1 and 2, the second end of the load arm 200 is hingedly or gimbaled to a collet mechanism 400. Jacket mechanism 400 can be demountable installation on unmanned aerial vehicle horn 500 to can realize dismantling fast, improve and change efficiency. The jacket mechanism 400 is made of nylon material, and has excellent mechanical strength, high strength, wear resistance and better corrosion resistance.
In this embodiment, the second end of the load arm 200 is articulated to the collet mechanism 400 by an articulation assembly. Specifically, the end of the second end of the load arm 200 is formed with a first groove portion. A projecting portion is formed on the collet mechanism 400, and the projecting portion of the collet mechanism 400 is fitted into the first groove portion of the load arm 200. The hinge assembly comprises a first rotating shaft which is convexly formed at two sides of the protruding portion and a first shaft hole which is formed at the inner walls of two sides of the first groove portion and matched with the first rotating shaft.
In other embodiments, the second end of the load arm 200 is gimbaled for rotation with the collet mechanism 400 by a rotation assembly. Specifically, the rotating component includes a rotating ball protruding from the clamping mechanism 400 and a connecting sleeve disposed at the second end of the load support arm 200, and is coupled to the rotating ball in a universal rotation manner and relatively non-detachable manner. In other embodiments, the second end of the load arm 200 is fixedly attached to the collet mechanism 400.
Referring to fig. 1, 2 and 4, the collet mechanism 400 includes a clip body 410 and a fastening assembly 420. The fastening assembly 420 includes a first pin shaft seat 421 fixedly connected to the first end of the clamp body 410, a second pin shaft seat 422 fixedly connected to the second end of the clamp body 410, and a locking pin 423, wherein the first pin shaft seat 421 and the second pin shaft seat 422 are provided with a pin hole 424 matched with the locking pin 423. Specifically, the first pin shaft seat 421 includes two. A second groove 425 capable of accommodating the second pin shaft seat 422 is formed between the two first pin shaft seats 421. The second pin shaft seat 422 is embedded in the second groove portion 425, and can be matched with the pin holes 424 of the first pin shaft seat 421 and the second pin shaft seat 422 through the locking pin 423, so that the first end of the clamp body 410 can be locked with the second end of the clamp body 410.
The locking pin 423 is provided with a pulling ring 426 for facilitating the pulling out or inserting of the locking pin 423. In this embodiment, locking pin 423 adopts steel ball spring pin, locates unmanned aerial vehicle horn 500 with clamp body 410 cover on to hold the locking through locking pin 423 with the first end of clamp body 410 and the second of clamp body 410, can make clamp body 410 be difficult for breaking away from unmanned aerial vehicle horn 500, in order to guarantee the security of using. When needing to dismantle, only need pull out fitting pin 423, alright demolish clamp body 410 from unmanned aerial vehicle horn 500. The band body 410 includes a first band 411 and a second band 412, and a first end of the first band 411 is hinged to a first end of the second band 412. The second end of load arm 200 is fixedly attached to first yoke 411. In other embodiments, the clip body 410 is a unitary structure, such as a resilient clip sheet.
Referring to fig. 1, 2 and 3, the load arm 200 includes a connection portion 210 and an inclined portion 220. The connection portion 210 is connected to the load mounting plate 100. The connection portion 210 is parallel to the load mounting plate 100, and the inclined portion 220 is obliquely disposed with respect to the connection portion 210. The load arm 200 tapers in width from the first end of the proximal load mount plate 100 to the second end of the distal load mount plate 100. Specifically, the inclined portion 220 of the load arm 200 tapers in width from the proximal connecting portion 210 to the distal connecting portion 210.
It will be appreciated that when the collet mechanism 400 attached to the second ends of the plurality of load arms 200 is secured to the drone arm 500, the angled portion 220 enables the level of the load mount plate 100 to be higher than the level of the drone so as not to impede the movement of the drone.
Referring to fig. 1 and 2, the load mounting plate 100 is provided with a coupling hole 130 for mounting the damping table 600. When the damping table 600 is installed, a screw and nut assembly matched with the connection hole 130 is used to install the damping table 600 on the load installation plate 100 and install the load module 300 on the damping table 600, so that it can be ensured that impact damage to the load module 300 is reduced in the process of executing a task.
When the rapid unmanned aerial vehicle load dismounting device 10 is used, the load support arms 200 with the appropriate number are selected according to different types of unmanned aerial vehicles.
A number of load arms 200 are mounted to the load mount plate 100. Each load support arm 200 is detachably connected to the load mounting plate 100 through at least two sets of quick connection assemblies, so that the load support arm 200 can be prevented from rotating relative to the load mounting plate 100. Specifically, the connecting bolt is threaded through the positioning hole 120 of the load mounting plate 100 and is in threaded connection with the threaded hole 230 of the load arm 200. It should be understood that the quick assembly and disassembly of the load mounting plate 100 and the load arm 200 can be accomplished by adjusting the connecting bolts during assembly or disassembly.
Selecting a suitable load module 300 according to the use requirement, and mounting the load module 300 on the load mounting plate 100. Wherein, when the load module 300 is installed, a screw nut assembly engaged with the load installation hole 110 is used to install the load module 300 to the load installation plate 100. The requirements of carrying different types and different numbers of load modules 300 can be met, so that a multi-task mode is realized, the design cost is reduced, and the working efficiency is improved.
Whether the damping table 600 is used or not is selected according to use requirements. When the damping table 600 is required to be used, the screw and nut assemblies matched with the connecting holes 130 are required to be used so as to mount the damping table 600 on the load mounting plate 100 and mount the load module 300 on the damping table 600, and thus, the reduction of impact damage to the load module 300 in the process of executing tasks can be ensured.
wherein, locking pin 423 adopts steel ball spring pin, can make clamp body 410 be difficult for breaking away from unmanned aerial vehicle horn 500 to guarantee the security of using. When needing to dismantle, only need extract locking pin 423, alright demolish clamp body 410 from unmanned aerial vehicle horn 500.
The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.
The above-mentioned embodiments only express several embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the invention. It should be noted that various changes and modifications can be made by those skilled in the art without departing from the spirit of the invention, and these changes and modifications are all within the scope of the invention. Therefore, the protection scope of the present patent shall be subject to the appended claims.
Claims (10)
1. The utility model provides an unmanned aerial vehicle load quick assembly disassembly device which characterized in that includes:
the load mounting plate is provided with a load mounting hole for mounting a load module;
the first ends of the load support arms are arranged along the circumferential direction of the load mounting plate at intervals, detachably connected to the load mounting plate, the second ends of the load support arms are connected with a clamping mechanism, and the clamping mechanism is used for being connected with an unmanned aerial vehicle arm.
2. An unmanned aerial vehicle load quick assembly disassembly device of claim 1, wherein the second end of load arm with press from both sides jacket mechanism articulated or universal swivelling joint.
3. An unmanned aerial vehicle load quick assembly disassembly device of claim 1, wherein a plurality of the load support arm can be detachably connected with the load mounting plate through a quick-connect assembly.
4. The rapid unmanned aerial vehicle load disassembly and assembly device of claim 3, wherein the rapid connection assembly comprises a positioning hole arranged on the load mounting plate, a threaded hole arranged on the load support arm, and a connection bolt, the positioning hole is arranged corresponding to the threaded hole, and the connection bolt is arranged through the positioning hole of the load mounting plate and is in threaded connection with the threaded hole of the load support arm.
5. The unmanned aerial vehicle load quick assembly disassembly device of claim 1, wherein be provided with the connecting hole that is used for installing the shock attenuation platform on the load mounting panel.
6. The unmanned aerial vehicle load quick assembly disassembly device of claim 1, wherein the load support arm includes a connecting portion and an inclined portion, the connecting portion is connected with the load mounting plate, the connecting portion is parallel to the load mounting plate, and the inclined portion is disposed in an inclined manner relative to the connecting portion.
7. The unmanned aerial vehicle load quick disconnect device of claim 1, wherein the load arm tapers in width from proximate the first end of the load mounting plate to distal the second end of the load mounting plate.
8. The rapid unmanned aerial vehicle load dismounting device according to claim 1 or 2, wherein the clamping mechanism comprises a clamp body and a fastening component, the fastening component comprises a first pin shaft seat fixedly connected to a first end of the clamp body, a second pin shaft seat fixedly connected to a second end of the clamp body, and a locking pin, and pin holes matched with the locking pin are arranged on the first pin shaft seat and the second pin shaft seat.
9. An unmanned aerial vehicle load quick assembly disassembly device of claim 1, wherein the load mounting hole includes a plurality of circular holes and a plurality of kidney holes.
10. The unmanned aerial vehicle load quick assembly disassembly device of claim 1, wherein the load mounting panel adopts carbon fiber board.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202210784032.XA CN115230976A (en) | 2022-07-05 | 2022-07-05 | Unmanned aerial vehicle load quick assembly disassembly device |
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| CN202210784032.XA CN115230976A (en) | 2022-07-05 | 2022-07-05 | Unmanned aerial vehicle load quick assembly disassembly device |
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| CN113700793A (en) * | 2017-08-28 | 2021-11-26 | 深圳市大疆创新科技有限公司 | Unmanned plane |
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