CN217533264U - Unmanned aerial vehicle fixing base and unmanned aerial vehicle - Google Patents

Abstract

The utility model provides an unmanned aerial vehicle fixing base and unmanned aerial vehicle, unmanned aerial vehicle fixing base: comprises a crossbeam, a first supporting side arm and a second supporting side arm; first support side arm and second support side arm fixed connection are at the crossbeam both ends to be the angle of setting for with the crossbeam, the size of angle corresponds to the contained angle of unmanned aerial vehicle fuselage and unmanned aerial vehicle supporting leg. Realize the dress of hanging of warning light through unmanned aerial vehicle, improved the efficiency of warning light dress of hanging, expanded unmanned aerial vehicle's function simultaneously, be applicable to any unmanned aerial vehicle that has the supporting leg, application scope is wide, can improve unmanned aerial vehicle's in-use rate of utilization.

Description

Unmanned aerial vehicle fixing base and unmanned aerial vehicle

The application is as follows: 11/19/2021, application No.: 202122859192X, name: unmanned aerial vehicle fixing base and the division of unmanned aerial vehicle application apply for.

Technical Field

The utility model relates to a transmission and distribution lines maintains the relevant technical field of device, specific theory relates to unmanned aerial vehicle fixing base and unmanned aerial vehicle.

Background

The statements in this section merely provide background information related to the present disclosure and may not necessarily constitute prior art.

The transmission and distribution line is bare wire at outdoor overhead line mostly, and electric power department hangs dress warning light on meeting the circuit for near have mechanical construction or pedestrian to remind, avoid the high voltage electric shock accident.

The existing method for hanging the warning lamp on the power transmission and distribution line generally adopts an insulated operating rod to hang the warning lamp on a shorter line; when the warning light is hung on a higher power transmission and distribution line, the warning light is hung in a live working mode, the risk is very high, the working process is very complicated, and the working efficiency is lower. Adopt unmanned aerial vehicle to hang dress electric line warning light, then can avoid this kind of operation risk to operating efficiency can improve greatly, no longer receives the influence of electric line height and topography. At present, the special unmanned aerial vehicle for hanging the warning lamp does not exist, the unmanned aerial vehicle of the common model can not directly fix the warning lamp, if the M200 series unmanned aerial vehicle in the Xinjiang province, the cradle head carrying function is only arranged below the fuselage, the function is single, the hanging of the warning lamp can not be realized, the use scene of the unmanned aerial vehicle is limited, the unmanned aerial vehicle is limited to be used for hanging the warning lamp, and the technical bottleneck of hanging the warning lamp in the power transmission and distribution line is formed.

SUMMERY OF THE UTILITY MODEL

The utility model discloses a solve above-mentioned problem, provided unmanned aerial vehicle fixing base and unmanned aerial vehicle, realized hanging of warning light through unmanned aerial vehicle, improved the efficiency that the warning light hung the dress, expanded unmanned aerial vehicle's function simultaneously, be applicable to any unmanned aerial vehicle who has the supporting leg, application scope is wide, can expand the application scene with unmanned aerial vehicle.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

one or more embodiments provide a drone mount comprising a cross beam, a first support side arm, and a second support side arm; first support side arm and second support side arm fixed connection are at the crossbeam both ends to be the angle of setting for with the crossbeam, the size of angle corresponds to the contained angle of unmanned aerial vehicle fuselage and unmanned aerial vehicle supporting leg.

One or more embodiments provide an unmanned aerial vehicle, set up foretell unmanned aerial vehicle fixing base on the unmanned aerial vehicle.

Compared with the prior art, the beneficial effects of the utility model are that:

(1) The utility model discloses a hang dress device and connect back warning light in unmanned aerial vehicle's top, can be convenient for the warning light to hang the dress on unsettled power transmission and distribution line, be applicable to the unmanned aerial vehicle that has the landing leg, like big M200 series unmanned aerial vehicle, the structure that corresponds unmanned aerial vehicle and warning light respectively sets up the dress structure of hanging that corresponds, has set up coupling assembling simultaneously and has improved the flexibility of hanging the dress device of this embodiment, improves the dress efficiency of hanging of warning light.

The utility model discloses a hang dress device selects for use unmanned aerial vehicle's landing leg as the stress component, and unmanned aerial vehicle's landing leg is in on the central horizontal line that unmanned aerial vehicle designed, and unmanned aerial vehicle fixing base crossbeam top just in time is outside unmanned aerial vehicle paddle working range, does benefit to the installation of unmanned aerial vehicle external equipment. In addition, unmanned aerial vehicle peripheral equipment installs on the crossbeam, and its gravity can exert a decurrent power for the device, and the two arms of the device design are the under shed, and the device receives the decurrent power, can make the fixed more firm of device.

Advantages of additional aspects of the invention will be set forth in part in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention.

Drawings

The accompanying drawings, which form a part of the specification, are provided to provide a further understanding of the invention, and are included to explain the illustrative embodiments and the description of the invention, and not to constitute a limitation of the invention.

Fig. 1 is a schematic structural view of a hanging device in embodiment 1 of the present invention;

fig. 2 is a schematic structural view of a warning lamp fixing base 1 according to embodiment 1 of the present invention;

fig. 3 is a schematic structural diagram of the connection assembly 2 according to embodiment 1 of the present invention

Fig. 4 is a schematic structural view of the warning lamp fixing base 1 and the connecting assembly 2 according to embodiment 1 of the present invention after assembly;

fig. 5 is a perspective view of the fixing base 3 of the unmanned aerial vehicle according to embodiment 1 of the present invention;

fig. 6 is a schematic structural view of the fixing base 3 of the unmanned aerial vehicle according to embodiment 1 of the present invention;

fig. 7 is a first structural schematic diagram of the spacer block of embodiment 1 of the present invention;

fig. 8 is a second schematic structural view of the spacer block according to embodiment 1 of the present invention;

wherein: 1. warning light fixing base, 2, coupling assembling, 3, unmanned aerial vehicle fixing base;

11. the locking device comprises a fixed arm framework, a locking arm framework 12, a tripping arm framework 13, an accommodating space 14, a connecting assembly fixing seat 15, a first inclined plane 16, a third inclined plane 17, a guide pin 18, a tripping groove 19 and a root part; 110. a first slot 111, a protrusion 141, a first connection hole;

21. the U-shaped side wall 22, the first through hole 23, the first mounting column 24 and the internal threaded hole;

31. the device comprises a first supporting side arm 32, a second supporting side arm 33, a first isolation block 34, a second isolation block 35, a cross beam 36 and a second mounting column;

41. a second clamping groove 42, a side arm mounting hole 43, a second through hole 44, a third through hole 45 and a threaded hole.

The specific implementation mode is as follows:

the present invention will be further explained with reference to the accompanying drawings and examples.

It should be noted that the following detailed description is exemplary and is intended to provide further explanation of the invention. Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs.

It is noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of exemplary embodiments according to the invention. As used herein, the singular forms "a", "an" and "the" are intended to include the plural forms as well, and it should be understood that when the terms "comprises" and/or "comprising" are used in this specification, they specify the presence of stated features, steps, operations, devices, components, and/or combinations thereof, unless the context clearly indicates otherwise. It should be noted that, in the present invention, the features of the embodiments and the examples may be combined with each other without conflict. The embodiments will be described in detail below with reference to the accompanying drawings.

The utility model discloses a combine unmanned aerial vehicle's structural feature and transmission and distribution lines warning light structure, researched and developed warning light and hung dress device. Be applicable to the warning light that has the spring landing leg, like patent number 2021207674068, the warning light in the patent of a power transmission and distribution lines warning light, the warning light has two closed spring stabilizer blades, and these two stabilizer blades are one long and one short, and wherein the short foot can pass from the long stabilizer blade, the utility model discloses a setting and fixed stabilizer blade matched with warning light fixing base realize the fixed of warning light. Simultaneously according to unmanned aerial vehicle's structural design and unmanned aerial vehicle matched with unmanned aerial vehicle fixing base, under the prerequisite that does not change unmanned aerial vehicle fuselage structure and do not influence unmanned aerial vehicle normal work, realized unmanned aerial vehicle and hung dress warning light, realized the high-efficient safe of warning light and hung the dress. The following examples are given for the purpose of illustration.

Example 1

In one or more embodiments, as shown in fig. 1 to 8, an unmanned aerial vehicle-based power transmission and distribution line warning lamp hanging device includes: warning light fixing base 1, unmanned aerial vehicle fixing base 3 and coupling assembling 2, warning light fixing base 1 includes the fixed arm of the dress landing leg of adaptation in the warning light, unmanned aerial vehicle fixing base 3 including with the supporting arm of unmanned aerial vehicle landing leg phase-match fixation, warning light fixing base 1 can be dismantled through coupling assembling 2 with unmanned aerial vehicle fixing base 3 and be connected.

In this embodiment, the device is connected the back warning light and is in unmanned aerial vehicle's top, can be convenient for the warning light to hang and adorn on unsettled power transmission and distribution line, is applicable to the unmanned aerial vehicle that has the landing leg, like big jiangjiang M200 series unmanned aerial vehicle, the structure that corresponds unmanned aerial vehicle and warning light respectively sets up the structure of hanging that corresponds, has set up coupling assembling simultaneously and has improved the flexibility of hanging the dress device of this embodiment, improves the efficiency of hanging the dress of warning light.

The warning lamp fixing base 1 can be a hanging rack structure, and can be a structure as shown in fig. 2. The warning lamp fixing seat 1 comprises a fixing arm, a trip arm and a supporting seat, wherein the fixing arm and the trip arm are arranged on the supporting seat according to a set included angle, and the set included angle is matched with the included angle of the supporting leg of the warning lamp.

In some embodiments, the fixing arm includes a fixing arm frame 11, a first leg fixing portion disposed inside the fixing arm frame 11; the first supporting leg fixing part comprises a guiding leg 17, the root of the guiding leg 17 is connected with the fixed arm framework 11 to form a clamping space, and a first clamping groove 110 is further formed in the bottom of the clamping space.

Specifically, the first engaging groove 110 is arc-shaped, and the center of the first engaging groove 110 is located near the guiding leg 17. The central position may be located within the guide foot 17 or at a short distance from the guide foot.

When the warning lamp is used, the support legs of the warning lamp are elastic parts, and the short support legs of the warning lamp slide into the first clamping grooves 110 through the guide legs 17. First stabilizer blade fixed part is used for one stabilizer blade of fixed warning light like short stabilizer blade, and guide foot 17 is used for realizing the roll-in or the roll-off of warning light stabilizer blade, and first draw-in groove 110 is used for realizing all fixing the back at two stabilizer blades of warning light, and is fixed to the block of one of them stabilizer blade, improves fixed stability.

Another stabilizer blade accident when the warning light drops, when playing on the fixed arm, the warning light receives the elasticity of spring and the influence of the impact force of beating on the fixed arm, and the short foot of warning light is deviate from the groove very easily, and the warning light probably breaks away from special dress base of hanging like this, can lead to the fact the safety threat to control personnel or unmanned aerial vehicle of below, and the freedom of warning light can be avoided to first draw-in groove 110 and drop.

According to a further technical scheme, the first clamping groove 110 is flared from the bottom to the top, and the opening is gradually enlarged.

When hanging, another stabilizer blade of warning light is that long stabilizer blade drops, and the joint is hung on the electric line together with the long stabilizer blade to short stabilizer blade, and unmanned aerial vehicle moves down, and under the pulling force effect of electric line wire, the short stabilizer blade is deviate from first draw-in groove 110. The horn-shaped first clamping groove 110 can enable the short support leg of the warning lamp to be smoothly separated from the special hanging base when the warning lamp is normally hung.

Further, the end of the fixing arm frame 11 is provided with a first inclined surface 15, and the end of the guide foot 17 is provided with a second inclined surface, and the angle of the second inclined surface is larger than that of the first inclined surface 15.

The first inclined surface 15 is a sliding-in guide surface when the lead enters, and is arranged to facilitate the sliding-in of the lead.

Optionally, in order to facilitate the smooth sliding of the wire and avoid friction with the wire, the surface of the root portion 19 of the fixing arm frame 11 may be a smooth surface, specifically, an arc shape.

In some embodiments, the support base may be configured in a Y-shape, and includes a connecting assembly fixing base 14, and side walls that are opened and extended at a predetermined angle on the connecting assembly fixing base 14, and form a receiving space 13 therebetween.

Optionally, the curved radian of the side wall is set, so that the accommodating space is matched with the appearance of the lampshade of the warning lamp, and the interval is set. Such as a "U" shape.

In this embodiment, form accommodation space 13 between the lateral wall and have the effect of the range that the restriction warning light rocked, after two stabilizer blades of warning light are fixed, the warning light casing of below is in 13 and is unsettled state.

The gap between the accommodating space and the warning lamp can be set to be 4-8mm.

The interval clearance that this embodiment set up can improve the success rate of hanging the dress, accommodation space and the spaced clearance of warning light are too little, when the warning light was tripped, the warning light can use wherein the landing leg fixed point department that the warning light did not trip (be first draw-in groove 110 in the picture) to do circular arc motion for centre of circle syncline below, if the clearance is too little or do not have the space, will lead to the unable removal of warning light casing, and then unable completion tripping operation, if the clearance is too big, accommodation space 13 just can not play the effect of restriction warning light seesaw.

Optionally, the connecting assembly fixing base 14 includes a connecting assembly fixing base body, and a first connecting hole 141 is provided on the connecting assembly fixing base body, for being fixedly connected with the connecting assembly 2.

The effect of trip arm can fix a stabilizer blade of warning light, can loosen the stabilizer blade naturally after the atress for the warning light breaks away from the trip arm. The specific structure can be as shown in fig. 1.

In some embodiments, the trip arm comprises a trip arm frame 12, a trip slot 18 disposed on the trip arm frame 12, a protrusion 111 disposed on an edge of the trip slot 18, and an opening of the trip slot 18 facing vertically downward.

The release groove 18 is used for fixing the long leg of the warning lamp, and the protrusion 111 prevents the leg of the warning lamp from freely falling out.

During the use, the long stabilizer blade that sets up the warning light in the tripping groove 18, because tripping groove 18 down, when reacing the dress position of hanging, the power transmission and distribution lines wire gives a decurrent power of warning light, makes the long stabilizer blade of warning light deviate from tripping groove 18, and is closed under the effect of elasticity with the short stabilizer blade of warning light, unmanned aerial vehicle downstream for the short stabilizer blade deviates from in the first draw-in groove 110 of guide foot 17 root, realizes the dress of hanging.

The design of arch 111 is very important, mainly for can be before not hanging the dress action, reliably fix the stabilizer blade of the warning light of putting into, if do not have this design, the stabilizer blade of warning light is probably unexpected to be come off, the warning light receives the elasticity of spring and hits the influence of the impact force on the fixed arm, the warning light is deviate from special dress base of hanging very easily, can cause the security threat to control personnel or unmanned aerial vehicle of below. The protrusion 111 cannot be too large, so that the spring support leg can be smoothly separated during hanging, and the operation of hanging the warning light is completed.

The end of the trip arm framework 12 is provided with a third inclined surface 16, so that the lead can smoothly slide in. The third inclined plane 16 and the tripping groove are arranged at a spaced distance, so that the situation that the wire is mistakenly touched on the top end of the long support leg of the warning lamp when the wire enters, and the hanging operation fails can be prevented.

Optionally, the third inclined surface 16 forms a first included angle with the trip arm frame 12, the first inclined surface 15 forms a second included angle with the fixed arm frame 11, and the first included angle and the second included angle are equal.

Optionally, a hollowed-out structure is disposed below the third inclined plane 16, so that the weight of the tripping arm side can be reduced, and the weights of the two support arms are close to each other as much as possible, so that the device is in a balanced state.

Similarly, the surface of the root portion 19 of the trip arm skeleton 12 may be a smooth surface, and specifically, may be a circular arc shape.

In this embodiment, coupling assembling 2's structure is exactly in order to realize being connected to dismantling of warning light fixing base 1 and unmanned aerial vehicle fixing base 3, can set up to multiple structure, and the structure of this embodiment can be as shown in fig. 3.

Optionally, the connecting assembly 2 includes a U-shaped sidewall 21 and a first mounting post 23, and the U-shaped sidewall 21 is provided with a first through hole 22.

The U-shaped side wall 21 is used for fixedly connecting a supporting seat of the warning lamp fixing seat 1; first erection column 23 is used for fixed connection unmanned aerial vehicle fixing base 3.

Specifically, first erection column 23 and unmanned aerial vehicle fixing base 3 can set up to threaded connection, and first erection column 23 sets up internal thread hole 24.

In some embodiments, the drone fixing base 3 may be a bracket, a binding band, or the like, and in this embodiment, is configured as a bracket structure, as shown in fig. 5 to 7.

The unmanned aerial vehicle fixing seat 3 comprises a cross beam 35, a first supporting side arm 31 and a second supporting side arm 32; first support side arm 31 and second support side arm 32 fixed connection are at crossbeam 35 both ends to be the angle A of setting for with crossbeam 35, angle A's size corresponds to the contained angle of unmanned aerial vehicle fuselage and unmanned aerial vehicle supporting leg.

The length of the first support side arm 31 and the second support side arm 32 corresponds to the length of the unmanned aerial vehicle support leg.

Specifically, the cross beam 35, the first support side arm 31 and the second support side arm 32 may be circular tubes, and specifically, carbon fiber tubes, such as carbon fiber tubes with an outer diameter of 18mm and a wall thickness of 1mm, may be used. The side arm can be a carbon fiber tube with the outer diameter of 10mm and the wall thickness of 1 mm.

Optionally, the fixing manner of the cross beam 35, the first support side arm 31 and the second support side arm 32 may be welding, specifically, a circular hole is formed in the cross beam 35, and the first support side arm 31 and the second support side arm 32 penetrate through the circular hole and are fixedly connected.

Optionally, the fixed mode of first support side arm 31 and second support side arm 32 and unmanned aerial vehicle's landing leg can adopt the flexible coupling, if adopt accessories such as auto-lock ribbon, magic tape to ligate.

Unmanned aerial vehicle peripheral equipment can install on this crossbeam 35, and the unmanned aerial vehicle peripheral hardware can be fixed on this crossbeam 35 through modes such as punching, ligature.

Optionally, a second mounting post 36 may be further disposed on the cross beam 35, and the second mounting post 36 is connected to the first mounting post 23 of the connecting assembly 2.

Furtherly, for the distance between extension warning light fixing base 1 and the unmanned aerial vehicle fixing base 3 and the quick assembly disassembly of being convenient for, still include the quick detach subassembly, the first erection column 23 on second erection column 36 and the coupling assembling 2 is connected through the quick detach subassembly, the quick detach subassembly is including the extension bar and the rotatory buckle 2.1 that are connected.

This embodiment has set up two sections extension bars, and two sections extension bars are connected with two matching pieces of rotatory buckle 2.1 respectively, and two sections extension bars are connected to second erection column 36 and the first erection column 23 on the coupling assembling 2 respectively.

The second mounting post 36 may be a circular tube with an outer diameter of 10mm, an inner diameter of 8mm and a length of 50mm, and is embedded in the central position of the cross beam 35.

Further, according to the technical scheme, the first supporting side arm 31 and the second supporting side arm 32 can be further provided with a spacer block in a connecting mode. In this embodiment, two side walls of the isolation block are respectively provided with a first isolation block 33 and a second isolation block 34.

The spacing block is used for adjusting the matching angle of the side arm (comprising the first supporting side arm 31 and the second supporting side arm 32) and the unmanned aerial vehicle support leg, and the stability of fixing. The number of the spacer blocks is not limited, and the present embodiment will be described by providing one spacer block each.

Optionally, spare parts such as auto-lock ribbon, magic tape ribbon can be adopted in spacing block department and the ligature of unmanned aerial vehicle landing leg is carried out. Adopt the connected mode of flexible coupling, do not punch the operation such as to unmanned aerial vehicle, adaptability, maneuverability are high.

In some embodiments, the spacer may be configured as shown in fig. 7-8, and includes a spacer base, a side arm mounting hole 42 disposed on the spacer base, and a second slot 41 disposed on the spacer base and aligned with the side arm mounting hole 42, wherein an inner surface of the second slot 41 is engaged with an outer surface of the leg of the drone.

In order to connect the spacer block with the first support side arm 31 and the second support side arm 32, a threaded hole 45 is formed in the side wall of the side arm mounting hole 42, and the first support side arm 31 and the second support side arm 32 are respectively fixed by matching a fixing screw with the threaded hole 45.

Furthermore, the isolation block base further comprises binding fixing holes which can be arranged on two sides of the second clamping groove 41 and can also be arranged at other positions on the isolation block base.

To improve the flexibility of the flexible connection, in some embodiments, the lashing attachment holes may optionally include a second through hole 43 and a third through hole 44 extending through the spacer block base and extending through both sides of the spacer block base to which the second slot 41 is attached.

The sizes of the holes of the second through hole 43 penetrating through the two sections of the isolation block base are different, namely the sizes of the two ends of the second through hole 43 are different; or/and the third through hole 44 has the same size penetrating through the two cross sections of the isolation block base.

When the magic adhesive with the knot at the tail end penetrates through the second through hole 43 and penetrates through the end with the large hole, the knot at the tail end of the magic adhesive tape is clamped in the middle of the second through hole 43, so that the magic adhesive tape and the isolation block can be quickly installed and fixed.

Alternatively, the second through hole 43 and the third through hole 44 may be provided as long holes, circular holes, or polygonal cross sections, or the like. In this embodiment, the fixing through-hole is rectangular in cross section.

Set up two through-holes on the spacing block, including second through-hole 43 and third through-hole 44, can improve fixed flexibility, specific use is as follows: if the magic tape is a right buckle, the magic tape is fixed behind the second through hole 43, bypasses the second clamping groove 41 and bypasses the side arm mounting hole 42, and the effect of connecting the two rods is achieved. If the magic tape is reversely buckled, the magic tape is fixed at the second through hole 43, bypasses the second clamping groove 41, passes through the third through hole 44 and bypasses the side arm mounting hole 42 to complete the function of connecting the two rods. The third through hole 44 is designed as a long hole, so that the problem of the magic tape positive and negative buckle application is solved.

In another implementation, the second through hole 43 penetrates through one side surface of the second card slot 41, and the third through hole 44 penetrates through two side surfaces of the spacer block base connected to the second card slot 41.

The structure of unmanned aerial vehicle fixing base 3 can make fixed more firm, and unmanned aerial vehicle's atress part or position have a lot of, and the device chooses for use unmanned aerial vehicle's landing leg as the atress part, and unmanned aerial vehicle's landing leg is in on the central horizontal line that unmanned aerial vehicle designed, and crossbeam 35 top just in time is outside being located unmanned aerial vehicle paddle working range, does benefit to the installation of unmanned aerial vehicle external equipment. In addition, the unmanned aerial vehicle peripheral equipment is installed on crossbeam 35, and its gravity can exert a downward force for the device, and the two arms of the device design are the downwardly opening, and the device receives downward force, can make the device fixed more firm.

Example 2

Based on embodiment 1, the present embodiment provides an unmanned aerial vehicle, wherein the unmanned aerial vehicle is provided with the warning lamp hanging device described in embodiment 1; or the unmanned aerial vehicle is provided with the unmanned aerial vehicle fixing seat 3 of the embodiment 1.

The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Although the present invention has been described with reference to the accompanying drawings, it is not intended to limit the scope of the present invention, and those skilled in the art should understand that various modifications or variations that can be made by those skilled in the art without inventive work are still within the scope of the present invention.

Claims (8)

1. Unmanned aerial vehicle fixing base, characterized by: comprises a crossbeam, a first supporting side arm and a second supporting side arm; first support side arm and second support side arm fixed connection are at the crossbeam both ends to be the angle of setting for with the crossbeam, the size of angle corresponds to the contained angle of unmanned aerial vehicle fuselage and unmanned aerial vehicle supporting leg.

2. The unmanned aerial vehicle fixing base of claim 1, characterized by: the crossbeam is provided with a second mounting column.

3. The unmanned aerial vehicle fixing base of claim 2, characterized by: the unmanned aerial vehicle fixing base still includes the quick detach subassembly, and the quick detach subassembly is used for connecting the second erection column, the quick detach subassembly is including extension bar and the rotatory buckle that is connected.

4. The unmanned aerial vehicle fixing base of claim 1, characterized by: the first supporting side arm and the second supporting side arm are also provided with an isolation block in a connecting way.

5. The unmanned aerial vehicle fixing base of claim 4, characterized by: and the isolation blocks are subjected to binding of the support legs of the unmanned aerial vehicle by adopting flexible connection.

6. The unmanned aerial vehicle fixing base of claim 4, characterized by: the spacing block includes the spacing block base, sets up the side arm mounting hole on the spacing block base, set up on the spacing block base and with the second draw-in groove of side arm mounting hole syntropy, the internal surface of second draw-in groove cooperatees with the surface of unmanned aerial vehicle landing leg.

7. The unmanned aerial vehicle fixing base of claim 6, characterized by: still be provided with the ligature fixed orifices on the spacing block base, including running through second through-hole and third through-hole on the spacing block base to two sides on the spacing block base of through connection second draw-in groove.

8. An unmanned aerial vehicle, characterized by: the unmanned aerial vehicle is provided with the unmanned aerial vehicle fixing seat of any one of claims 1 to 7.

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