CN214776526U - Foot rest and unmanned aerial vehicle - Google Patents

Foot rest and unmanned aerial vehicle Download PDF

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Publication number
CN214776526U
CN214776526U CN202022569249.8U CN202022569249U CN214776526U CN 214776526 U CN214776526 U CN 214776526U CN 202022569249 U CN202022569249 U CN 202022569249U CN 214776526 U CN214776526 U CN 214776526U
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China
Prior art keywords
landing
rod
foot rest
bar
unmanned aerial
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Expired - Fee Related
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CN202022569249.8U
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Chinese (zh)
Inventor
李博
黄稀荻
农贵升
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SZ DJI Technology Co Ltd
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SZ DJI Technology Co Ltd
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Priority to CN202022569249.8U priority Critical patent/CN214776526U/en
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Abstract

The application provides foot rest and unmanned aerial vehicle relates to unmanned air vehicle technical field, the foot rest specifically includes: the supporting rods are arranged in a plurality of numbers, the first ends of the supporting rods are fixedly connected with the unmanned aerial vehicle body, and the second ends of the supporting rods extend in the direction far away from the unmanned aerial vehicle body; the landing rod is arranged at the second end of the supporting rod and is in contact with the ground when the unmanned aerial vehicle lands; wherein the strength of the support bar is higher than the strength of the landing bar. In the embodiment of this application, the design of the weak point of intensity of foot rest is in landing pole department, and when unmanned aerial vehicle landed, hardly damaged unmanned aerial vehicle's fuselage, maintenance duration is short and cost of maintenance is lower. Moreover, the foot rest can realize effectively supporting the unmanned aerial vehicle fuselage, avoids influencing the life of the electrical apparatus on fuselage and the fuselage when unmanned aerial vehicle lands, improves unmanned aerial vehicle's safety in utilization.

Description

Foot rest and unmanned aerial vehicle
Technical Field
The application relates to the technical field of unmanned aerial vehicles, in particular to a foot rest and an unmanned aerial vehicle.
Background
The foot rest can be used for when unmanned aerial vehicle lands, supports unmanned aerial vehicle. Because unmanned aerial vehicle has great speed when landing, moreover, the weight of large-scale unmanned aerial vehicle's fuselage is great, consequently, unmanned aerial vehicle when landing, the impact that the foot rest received is great. In the process of long-term use, the impact can all cause the influence to the structure of foot rest and fuselage to and, the life to the electron device on the fuselage.
In the prior art, the most common application form is to use a carbon fiber composite material pipe (hereinafter referred to as a carbon pipe) to manufacture the foot rest, or use an aluminum pipe to manufacture the foot rest. However, because the strength of the carbon tube is relatively high, the foot stool made of the carbon tube can cause the strength weakness of the unmanned aerial vehicle to move upwards, so that when the unmanned aerial vehicle falls, the body of the unmanned aerial vehicle is easily damaged, and the maintenance cost of the unmanned aerial vehicle is increased. Because the intensity of aluminum pipe is lower, the foot rest of using the aluminum pipe to make is very easily damaged when unmanned aerial vehicle lands, and then, influences the life of the electron device on fuselage and the fuselage very easily to, the foot rest that adopts the aluminum pipe to support is heavier, is unfavorable for unmanned aerial vehicle's continuation of the journey.
SUMMERY OF THE UTILITY MODEL
In view of the above, the present application is proposed in order to provide a foot rest and a drone that overcome or at least partially solve the above mentioned problems.
In order to solve the above problem, the first aspect, this application discloses a foot rest is applied to unmanned aerial vehicle, the foot rest includes:
the supporting rods are arranged in a plurality of numbers, the first ends of the supporting rods are fixedly connected with the unmanned aerial vehicle body, and the second ends of the supporting rods extend in the direction far away from the unmanned aerial vehicle body; and
the landing rod is arranged at the second end of the supporting rod and is in contact with the ground when the unmanned aerial vehicle lands;
wherein the strength of the support bar is higher than the strength of the landing bar.
Optionally, the support bar is of a different material than the landing bar;
and/or the support rod is made of a carbon tube;
and/or the landing bar is made of aluminum pipe.
Optionally, the landing bar is connected to at least two of the support bars;
the landing lever includes: the landing lever comprises a landing lever body and connecting rods arranged at two ends of the landing lever body, wherein the connecting rods extend towards the direction close to the machine body; wherein each connecting rod is connected with the second end of one supporting rod respectively; the landing lever body is arranged on one side of the connecting rod far away from the machine body
Optionally, the landing lever body and the connecting rod are integrally formed, and the connecting rod is formed by bending a pipe;
and/or the landing lever body is matched with the two connecting rods to form a U-shaped structure.
Optionally, at least a portion of the support rod near the second end is embedded in the landing rod;
and/or a pipe expanding structure is arranged on one side, close to the supporting rod, of the landing rod, and the diameter of the pipe expanding structure is larger than that of other parts of the landing rod;
at least part of the support rod close to the second end is embedded in the pipe expanding structure.
Optionally, the foot rest further comprises: a first limit piece;
a first through hole is formed in the side wall of the part, embedded in the landing rod, of the support rod, and a second through hole is formed in the position, opposite to the first through hole, of the landing rod;
the first limiting piece sequentially penetrates through the second through hole and the first through hole so as to be connected with the landing rod and the supporting rod, and the first limiting piece can limit the part, embedded in the landing rod, of the supporting rod in the landing rod;
the first stopper includes: at least one of a pin, a dowel, a screw, a bolt, and a stud;
and/or the part of the supporting rod embedded in the landing rod is in interference fit with the landing rod.
Optionally, the foot rest further comprises: and the connecting piece is respectively connected with the landing rod and the second end of the supporting rod, and the connecting piece is used for connecting the landing rod to the supporting rod.
Optionally, the connecting piece is an insert, at least part of one end of the connecting piece is embedded in the landing bar, and at least part of the other end of the connecting piece is embedded in the second end of the supporting bar;
and/or from one end to the other end of the connecting piece, the connecting piece comprises a first embedding part, a convex limiting part and a second embedding part which are sequentially arranged; wherein the content of the first and second substances,
the first embedding part is embedded in the landing rod, and the second embedding part is embedded in the second end of the supporting rod;
the outer diameter of the limiting part is larger than the outer diameters of the first embedding part and the second embedding part, and the limiting part is clamped between the landing rod and the second end of the supporting rod;
and/or the limiting part is provided with a first surface facing the landing rod and a second surface facing the supporting rod, the first surface and the second surface are arranged oppositely, the landing rod is abutted against the first surface, and the supporting rod is abutted against the second surface;
and/or the first embedding part is in interference fit with the landing rod, and the second embedding part is in interference fit with the supporting rod;
and/or, the insert is made of a metal pipe, and the metal pipe comprises: at least one of a steel pipe and an aluminum pipe.
Optionally, the landing leg body comprises an equal-diameter pipe section and a pipe reduction section, wherein the diameter of the pipe reduction section is smaller than that of the equal-diameter pipe section;
the reducing pipe section is arranged between the two equal-diameter pipe sections, and one end of each equal-diameter pipe section, which is far away from the reducing pipe section, is connected with the connecting rod;
and/or, the landing lever body further comprises: the reducing pipe section is located between the equal-diameter pipe section and the reducing pipe section, and the diameter of the reducing pipe section is gradually reduced from the equal-diameter pipe section to the reducing pipe section.
Optionally, the foot rest further comprises: the buffer piece is connected to the landing rod and used for buffering the impact on the landing rod;
the buffer piece is sleeved outside the landing rod;
the material of bolster includes: at least one of foam and rubber.
Optionally, the foot rest further comprises: the bracket is positioned among the support rods and connected with the support rods;
the bracket is also provided with a radar mounting part for mounting a radar;
the radar is at least one of laser radar and millimeter wave radar.
Optionally, the stent comprises: the radar mounting device comprises at least one mounting rod, at least one supporting rod and at least one radar mounting part, wherein each mounting rod is connected to at least one supporting rod; the central axis of each mounting rod and the central axis of the supporting rod connected with the mounting rod are positioned on the same plane, and the center of the radar is positioned in the plane;
the bracket comprises at least two mounting rods, and the radar mounting part is positioned at the intersection point of the mounting rods;
and/or the bracket is of a central symmetrical structure, and the radar mounting part is positioned at the central position of the bracket;
and/or a plurality of the mounting rods are arranged in a crossed manner to form an X-shaped structure;
and/or one end of the mounting rod is connected with the supporting rod and the landing rod at the joint of the supporting rod and the landing rod; the other end of the mounting rod is connected to the radar mounting portion.
Optionally, the foot rest further comprises: the fixing piece, the fixing piece with the first end of bracing piece is connected, is used for with the foot rest is fixed in the fuselage.
In a second aspect, the present application further discloses an unmanned aerial vehicle, the unmanned aerial vehicle includes: a body and any of the above foot rests; wherein the content of the first and second substances,
the supporting rod of the foot rest is connected with the machine body.
The application includes the following advantages:
in this application embodiment, the foot rest can be formed by bracing piece and landing lever combination, the first end and the unmanned aerial vehicle of bracing piece are connected, the second end of bracing piece with the landing lever is connected. Because the intensity of bracing piece is higher than the intensity of landing pole, the design of the weak point of intensity of foot rest is in landing pole department, when unmanned aerial vehicle landed, only landing pole easily receives the impact damage, hardly damages unmanned aerial vehicle's fuselage, when maintaining unmanned aerial vehicle, only need change landing pole can, maintenance duration is short and cost of maintenance is lower. Moreover, because the intensity of bracing piece is higher than the landing pole, the bulk strength of foot rest is higher, the foot rest can realize effectively supporting the unmanned aerial vehicle fuselage, influences the life of the electrical apparatus on fuselage and the fuselage when avoiding unmanned aerial vehicle to land, improves unmanned aerial vehicle's safety in utilization.
Drawings
Fig. 1 schematically shows a structural schematic view of a foot rest according to an embodiment of the present application;
fig. 2 schematically shows an exploded view of the foot rest shown in fig. 1;
FIG. 3 is a schematic sectional view of the foot rest of FIG. 1 at position A;
FIG. 4 schematically illustrates a structural view of the foot rest position B shown in FIG. 3;
FIG. 5 schematically illustrates a connection diagram of a support pole and a landing pole according to an embodiment of the present application;
figure 6 schematically shows a structural view of a landing lever in the foot stand shown in figure 1;
FIG. 7 schematically illustrates a structural view of the landing lever C position shown in FIG. 6;
FIG. 8 is a schematic structural diagram of another foot rest according to an embodiment of the present application;
FIG. 9 is a schematic diagram of another embodiment of a foot rest of the present application;
fig. 10 schematically shows an exploded view of the foot rest shown in fig. 9;
fig. 11 schematically shows a cross-sectional structure view of the position of the foot rest D shown in fig. 9;
fig. 12 schematically shows a structural view of the position of the foot rest E shown in fig. 11;
FIG. 13 schematically illustrates a structural view of a connector according to an embodiment of the present application;
fig. 14 schematically shows a certain angle structure diagram of a foot rest according to another embodiment of the present application;
FIG. 15 schematically illustrates another angular configuration of the foot rest of FIG. 14;
figure 16 schematically illustrates a structural view of a landing lever body of the present application;
FIG. 17 is a schematic structural diagram of a foot rest according to an embodiment of the present application;
fig. 18 schematically shows an exploded view of the foot rest of fig. 17;
FIG. 19 schematically illustrates a structural view of another landing lever of the present application;
fig. 20 schematically illustrates a structural diagram of an unmanned aerial vehicle according to an embodiment of the present application;
description of reference numerals: 10-support rod, 11-landing rod, 111-landing rod body, 1111-equal diameter pipe section, 1112-reduction pipe section, 1113-reducing pipe section, 112-connecting rod, 113-pipe expanding structure, 114-landing part, 115-buffer part, 12-connecting piece, 121-first embedding part, 122-limiting part, 1221-first surface, 1222-second surface, 123-second embedding part, 13-buffer part, 14-radar mounting part, 15-longitudinal rod, 16-transverse rod, 17-first connecting piece, 18-mounting rod, 19-second connecting piece, 20-fixing piece, 100-foot rest and 200-fuselage.
Detailed Description
In order to make the aforementioned objects, features and advantages of the present application more comprehensible, the present application is described in further detail with reference to the accompanying drawings and the detailed description.
The embodiment of the application provides a foot rest, the foot rest can be used for unmanned aerial vehicle, unmanned aerial vehicle can be used in each field of production, life, especially uses in aspects such as agricultural plant protection, aerial photography, patrolling and examining, survey and drawing, investigation. The foot rest can connect in unmanned aerial vehicle's fuselage bottom supports the fuselage. Specifically, the foot rest may include, but is not limited to, any one of a fixed foot rest and a foldable foot rest, and the embodiment of the present application is described by taking the fixed foot rest as an example, and other types of foot rests may be implemented by reference.
Referring to fig. 1, a schematic structural diagram of a foot rest according to an embodiment of the present application is shown, referring to fig. 2, an exploded schematic structural diagram of the foot rest shown in fig. 1 is shown, referring to fig. 3, a schematic sectional structural diagram of a position a of the foot rest shown in fig. 1 is shown, and referring to fig. 4, a schematic structural diagram of a position B of the foot rest shown in fig. 3 is shown, where the foot rest specifically includes:
the supporting rods 10 are multiple, the first ends of the supporting rods 10 are fixedly connected with the unmanned aerial vehicle body, and the second ends of the supporting rods 10 extend in the direction far away from the unmanned aerial vehicle body; and
the landing rod 11 is arranged at the second end of the supporting rod 10, and when the unmanned aerial vehicle lands, the landing rod 11 is in contact with the ground;
wherein the strength of the support bar 10 is higher than that of the landing bar 11.
In the embodiment of this application, the foot rest can be formed by the combination of bracing piece 10 and landing pole 11, and the first end and the unmanned aerial vehicle of bracing piece 10 are connected, and the second end and the landing pole 11 of bracing piece 10 are connected. Since the strength of the support bar 10 is higher than that of the landing bar 11, the weak point of strength of the foot stand is designed at the landing bar 11. When unmanned aerial vehicle lands, only landing pole 11 easily receives the impact damage, hardly damages unmanned aerial vehicle's fuselage, consequently, when maintaining unmanned aerial vehicle, only need change landing pole 11 can, maintenance duration is short and cost of maintenance is lower. Moreover, because the intensity of bracing piece 10 is higher than landing pole 11, the bulk strength of foot rest is higher, the foot rest can realize the effective support to the unmanned aerial vehicle fuselage, influences the life of the electrical apparatus on fuselage and the fuselage when avoiding unmanned aerial vehicle to land, improves unmanned aerial vehicle's safety in utilization.
Specifically, the first end of bracing piece 10 can fixed connection in the bottom of fuselage, also can swing joint in the bottom of fuselage to realize the rotation or folding of foot rest, so that taking in of foot rest, this application embodiment to bracing piece 10 with the connected mode of fuselage does not specifically limit.
Alternatively, in order to make the strength of the support pole 10 higher than that of the landing pole 11, the material of the support pole 10 and the material of the landing pole 11 may be different. For example, the support pole 10 may be made of a relatively strong metal material, while the landing pole 11 may be made of a relatively weak metal material. Alternatively, the support pole 10 and the landing pole 11 may be different in structure. For example, the supporting bar 11 is made of a thick profile, while the landing bar 11 can be made of a thin profile; for another example, the support bar 10 may be designed as a solid structure, and the landing bar 11 may be designed as a hollow structure.
It should be noted that, in practical applications, a person skilled in the art may select any one of the embodiments including, but not limited to, the above examples to make the strength of the support bar 10 higher than that of the landing bar 11 according to practical needs, and the embodiments of the present application are not limited thereto.
In the embodiment of the present application, the support rod 10 may be made of a carbon tube. Because the intensity of carbon pipe is higher, the bracing piece 10 that adopts the carbon pipe to make correspondingly has higher intensity, like this, can make the bulk strength of foot rest is higher, in order to realize the foot rest is right the effective support of fuselage influences the life of the electrical apparatus on fuselage and the fuselage when avoiding unmanned aerial vehicle to land, improves unmanned aerial vehicle's safety in utilization.
Specifically, the landing lever 11 is made of an aluminum pipe. Because the quality of aluminum pipe is lighter, and intensity is moderate for the carbon pipe, consequently, adopt the aluminum pipe to make landing lever 11, not only can realize the lightweight design of foot rest, can also make unmanned aerial vehicle is when landing, landing lever 11's damage is less.
In practical applications, the support rods 10 may be made of carbon tubes and the landing rods 11 may be made of aluminum tubes, so that not only the overall strength of the foot rest may be increased, but also the weak points of the strength of the foot rest may be lowered to the landing rods 11. Moreover, the carbon tube is lighter than the aluminum tube, so that the design of the foot rest can be lighter.
Alternatively, the landing pole 11 may be connected with at least two support poles 10 to integrally connect the at least two support poles 10, thereby improving the overall strength of the foot rest.
It should be noted that fig. 1 and fig. 2 only show the case that the landing bar 11 connects two support bars 10, but in practical applications, the landing bar 11 can also connect 3, 4, or even 6 support bars 10, and the number of the support bars 10 connected to the landing bar 11 is not specifically limited in the present application.
Referring to fig. 5, a schematic diagram of the connection between a support bar and a landing bar according to the embodiment of the present application is shown, and as shown in fig. 5, a landing bar 11 may be connected to only one support bar 10. The number of the support bars 10 to which the landing bar 11 is connected is not particularly limited in the embodiment of the present application.
Referring to fig. 6 showing a structural view of the landing lever in the foot stool shown in fig. 1, and referring to fig. 7 showing a structural view of the position of the landing lever C shown in fig. 6, the landing lever 11 may include: a landing lever body 111 and a connecting rod 112 disposed at both ends of the landing lever body 111, the connecting rod 112 extending in a direction approaching the fuselage; wherein, each connecting rod 112 is connected with the second end of one supporting rod 10; the landing lever body 11 is disposed on the side of the connecting rod 112 remote from the fuselage.
Specifically, since the connecting rods 112 at the two ends of the landing rod body 111 extend in the direction of the body, the connecting rods 112 can be easily connected to the supporting rods 10, and the connection between the connecting rods 112 and the supporting rods 10 is reliable, so that the convenience and reliability of connection between the landing rods 11 and the supporting rods 10 can be improved.
In some optional embodiments of the present application, the landing bar body 111 and the connecting rod 112 may be integrally formed, the connecting rod 112 is formed by bending a pipe, the processing process is simple, and the connection strength between the landing bar body 111 and the connecting rod 112 may be high.
Referring to fig. 8, which shows a schematic structural diagram of another foot rest according to an embodiment of the present disclosure, as shown in fig. 8, the landing bar body 111 and the connecting bar 112 may also be separate structures, and the connecting bar 112 may be connected to two ends of the landing bar 111 by welding, clamping, or fastening.
In this embodiment, the landing bar body 111 and the two connecting rods 112 may cooperate to form a U-shaped structure, wherein the bottom of the U-shaped structure may be the landing bar body 111, and the two side wings of the U-shaped structure may be the two connecting rods 112. Through forming the U-shaped structure with landing pole body 111 and two connecting rods 112 cooperation, not only can make the structure of foot rest is comparatively stable, moreover, can also improve the outward appearance aesthetic property of foot rest.
In the foot stool shown in fig. 1 and 2, at least a portion of the support rod 10 near the second end is embedded in the landing rod 11 to connect the support rod 10 to the landing rod 11. Thus, it is possible to avoid the need for additional connecting members for connecting the support bar 10 and the landing bar 11, to reduce the number of parts of the foot stand, and to simplify the mounting process of the foot stand.
Specifically, one side of the landing bar 11 close to the support bar 10 is provided with a pipe expanding structure 113, and the diameter of the pipe expanding structure 113 is larger than that of the rest part of the landing bar 11; at least a portion of the support pole 10 near the second end is embedded within the expanding structure 113 to connect the support pole 10 to the landing pole 11.
In practical applications, a pipe expanding process may be adopted to process the side of the landing bar 11 close to the support bar 10 into the pipe expanding structure 113, and increase the inner diameter of the pipe expanding structure 113 to be the same as or substantially the same as the outer diameter of the support bar 11, so that at least a portion of the support bar 11 close to the second end may be embedded in the pipe expanding structure 113.
In this application embodiment, the foot rest can also include: a first limit piece; a first through hole is arranged on the side wall of the part of the support rod 10 embedded in the landing rod 11, and a second through hole is arranged on the landing rod 11 at the position opposite to the first through hole; the first limiting part sequentially penetrates through the second through hole and the first through hole to connect the landing rod 11 and the supporting rod 10, the first limiting part can limit the part of the supporting rod 10 embedded in the landing rod 11, and the supporting rod 10 is prevented from sliding or rotating in the landing rod 11, so that the connection reliability of the supporting rod 10 in the landing rod 11 is improved.
Specifically, the first limiting member may include, but is not limited to: at least one of a pin, a screw, a bolt, and a stud, the structure of the first limiting member is not specifically limited in the embodiment of the present application.
Alternatively, the portion of the support rod 10 embedded in the landing rod 11 and the landing rod 11 may be in interference fit to further improve the reliability of the connection between the support rod 10 and the landing rod 11.
Referring to fig. 9, a schematic structural view of another foot rest according to an embodiment of the present application is shown, referring to fig. 10, an exploded schematic structural view of the foot rest shown in fig. 9 is shown, referring to fig. 11, a schematic sectional structural view of a position of a foot rest D shown in fig. 9 is shown, and referring to fig. 12, a schematic structural view of a position of a foot rest E shown in fig. 11 is shown.
As shown in fig. 9 and 10, the foot rest may further include: a connecting member 12 connected to the second ends of the landing bar 11 and the support bar 10, respectively, the connecting member 12 may be used to connect the landing bar 11 to the support bar 10.
For example, the connection manner between the connecting member 12 and the landing bar 11 and the support bar 10 may include, but is not limited to, any one of clamping, screwing, fastening, and fitting, and the connection manner between the connecting member 12 and the landing bar 11 and the support bar 10 is not particularly limited in the embodiments of the present application.
In some alternative embodiments of the present application, the connecting member 12 may be an insert, one end of which is at least partially embedded in the landing bar 11 and the other end of which is at least partially embedded in the second end of the support bar 10 to connect the landing bar 11 to the support bar 10.
In practical application, under the condition that the connecting piece 12 is an embedded piece, in the assembling process of the foot rest, one end of the connecting piece 12 is embedded in the landing rod 11, and the other end of the connecting piece 12 is embedded in the supporting rod 10, so that the landing rod 11 and the supporting rod 10 can be connected, and the installation mode is simple. Moreover, the landing rod 11 and the supporting rod 11 can be prevented from being processed and reformed, and the installation process is relatively simple.
Referring to fig. 13, which shows a schematic structural diagram of a connecting element according to an embodiment of the present disclosure, as shown in fig. 13, from one end of the connecting element 12 to the other end, the connecting element 12 may include a first engaging portion 121, a convex limiting portion 122, and a second engaging portion 123, which are sequentially disposed; wherein, the first tabling portion 121 is inlaid in the landing pole 11, the second tabling portion 123 is inlaid in the second end of the supporting pole 10; the outer diameter of the limiting portion 122 is larger than the outer diameters of the first engaging portion 121 and the second engaging portion 123, and the limiting portion 122 is interposed between the landing bar 11 and the second end of the supporting bar 10 to prevent the landing bar 11 and the supporting bar 10 from directly abutting against each other. Furthermore, when can avoiding unmanned aerial vehicle to land, the impact that receives of landing pole 11 passes through connecting piece 12 and transmits to bracing piece 10, avoids the damage of bracing piece 10.
In the embodiment of the present invention, the position-limiting portion 122 has a first surface 1221 facing the landing bar 11 and a second surface 1222 facing the supporting bar 10, the first surface 1221 is disposed opposite to the second surface 1222, the landing bar 122 abuts against the first surface 1221, and the supporting bar 10 abuts against the second surface 1222, so as to avoid direct abutment between the landing bar 11 and the supporting bar 10.
Specifically, the foot rest may further include: the landing bar comprises a second limiting piece and a third limiting piece, wherein the first embedding part 121 is provided with a first limiting hole, the landing bar 11 is provided with a third through hole at a position opposite to the first limiting hole, the second limiting piece sequentially penetrates through the third through hole and the first limiting hole so as to connect the landing bar 11 and the first embedding part 121, the second limiting piece can limit the first embedding part 121 in the landing bar 11 so as to prevent the first embedding part 121 from generating axial movement and circumferential rotation in the landing bar 11, and the connection reliability between the connecting piece 12 and the landing bar 11 is improved.
Specifically, second gomphosis portion 123 is equipped with the spacing hole of second, the bracing piece 10 with the position that the spacing hole of second is relative is equipped with the fourth through-hole, the third locating part passes in proper order the fourth through-hole with the spacing hole of second to joint support pole 11 and second gomphosis portion 123, the third locating part can be spacing in bracing piece 11 with second gomphosis portion 123, in order to avoid second gomphosis portion 123 to take place axial cluster and axial rotation in bracing piece 10, improves the reliability of being connected between connecting piece 12 and the bracing piece 11.
Optionally, the second limiting member and the third limiting member may include, but are not limited to, at least one of a pin, a screw, a bolt, and a stud. In the embodiment of the present application, the structures of the second limiting part and the third limiting part are not specifically limited.
Alternatively, the first engaging portion 121 and the landing bar 11 may be in an interference fit, and the second engaging portion 123 and the support bar 10 may also be in an interference fit, so as to improve the connection reliability between the connecting member 12 and the landing bar 11 and the support bar 10.
For example, the inner insert can be made of a metal pipe, so that the inner insert can have both high strength and good processability. Specifically, the metal pipe may include: at least one of a steel pipe and an aluminum pipe, and the specific material of the insert in the embodiment of the present application may not be limited.
In other embodiments, the connecting member may be a tube body having a protruding structure facing the inside, one end of the landing bar 11 is embedded in one end of the connecting member, the second end of the supporting bar 10 is embedded in the other end of the connecting member, so as to achieve connection between the landing bar 11 and the supporting bar 10, and the landing bar 11 and the supporting bar 10 are respectively abutted to two surfaces opposite to the protruding structure.
Referring to fig. 14, which shows a schematic view of a certain angle of a foot rest according to another embodiment of the present disclosure, and referring to fig. 15, which shows a schematic view of another angle of the foot rest shown in fig. 14, as shown in fig. 14 and 15, the landing bar body 111 includes a constant diameter pipe section 1111 and a reducing pipe section 1112, and the diameter of the reducing pipe section 1112 is smaller than the diameter of the constant diameter pipe section 1111.
Specifically, the diameter of the constant diameter tube section 1111 may be the diameter of the tube material itself from which the landing rod body 111 is made, and the reducing tube section 1112 may be made by reducing the diameter of the tube material through a reducing tube process. In practical applications, the reducing pipe segment 1112 is disposed on the landing bar body 111, which is not only beneficial to enrich the shape of the landing bar 11, but also beneficial to reduce the weight of the landing bar 11.
Alternatively, the reducing pipe section 1112 may be disposed between two equal diameter pipe sections 1111, and one end of the equal diameter pipe section 1111 far from the reducing pipe section 1112 may be connected with the connecting rod 112, so as to improve the connection reliability between the landing rod body 111 and the connecting rod 112.
As shown in fig. 14 and 15, only one shortened section 1112 may be disposed between two equal-diameter pipe sections 1111, so as to reduce the number of pipe shrinkage and reduce the processing difficulty of the landing bar 11.
Referring to fig. 16, which shows a schematic structural diagram of a landing post body according to the present application, as shown in fig. 16, the landing post body 111 may include a plurality of equal-diameter pipe sections 1111 and a plurality of reducing pipe sections 1112, and the equal-diameter pipe sections 1111 and the reducing pipe sections 1112 may be alternately arranged to further enrich the shape of the landing post 11.
Optionally, the landing lever body 111 may further include: the reducing pipe segment 1113 is located between the equal-diameter pipe segment 1111 and the pipe reducing segment 1112, and the diameter of the reducing pipe segment 1113 is gradually reduced from the equal-diameter pipe segment 1111 to the pipe reducing segment 1112, so that smooth transition from the equal-diameter pipe segment 1111 to the pipe reducing segment 1112 is realized, stress concentration at the joint of the equal-diameter pipe segment 1111 and the pipe reducing segment 1112 is avoided, and the strength reliability of the landing rod body 111 is improved.
In some embodiments of the present application, the foot rest may further include: the support, the support can be located between a plurality of bracing pieces 10, and is connected with a plurality of bracing pieces 10, the support can be used for connecting a plurality of bracing pieces 10 into a whole, strengthens the bulk strength of foot rest, height the structural stability of foot rest.
In the embodiment of the application, still be provided with radar installation department 14 on the support for the installation radar. Specifically, the radar may be at least one of a laser radar and a millimeter wave radar, and the specific type of the radar may not be limited in the embodiment of the present application.
In some optional embodiments of the present application, the bracket comprises: a longitudinal bar 15 and two transverse bars 16; wherein, at the connection part of two different support bars 10 and landing bar 11, two ends of the cross bar 16 are respectively connected with one support bar 10 and landing bar 11 at the same time; both ends of the vertical rod 15 are connected with a cross rod 16 to form an I-shaped bracket, and the radar mounting part 14 is connected to the vertical rod 15.
In practical application, when the support is an i-shaped support composed of one longitudinal rod 15 and two transverse rods 16, not only the structural members of the support can be simple, but also the stability of the support can be good.
It should be noted that the cross bar 16 may also connect one of the support bar 10 and the landing bar 11, and the arrangement form of the cross bar 16 in the embodiment of the present application may not be particularly limited.
In this application embodiment, the foot rest can also include: the first conversion part 17 is arranged at the joint of the cross rod 16, the support rod 10 and the landing rod 11, and is used for connecting the cross rod 16 to the support rod 10 and the landing rod 11, so that the connection among the cross rod 16, the support rod 11 and the landing rod 11 is realized, and the structural stability of the foot rest is improved.
Specifically, the first joint 17 may include: the first transfer rod, the second transfer rod and the third transfer rod are arranged in the shell; one end of the first adapter rod, one end of the second adapter rod and one end of the third adapter rod are connected together respectively; the first adapter rod is sleeved outside the cross rod 16, the second adapter rod is sleeved outside the support rod 10, the third adapter rod is sleeved outside the landing rod 11, and therefore the cross rod 16 is connected to the support rod 10 and the landing rod 11.
In this application embodiment, the foot rest can also include: a fourth limiting member; wherein, the cross bar 16 is embedded in the part in the first adapter bar, the support bar 10 is embedded in the part in the second adapter bar and the landing bar 11 is embedded in the part in the third adapter bar are provided with the first connecting hole, the first adapter bar, the second adapter bar and the third adapter bar are provided with the fifth through hole at the position opposite to the first connecting hole, the fourth limiting piece sequentially passes through the fifth through hole and the first connecting hole to connect the first adapter bar to the cross bar 16, connect the second adapter bar to the support bar 10 and connect the third adapter bar to the landing bar 11, so as to avoid the axial crosstalk and circumferential rotation of the cross bar 16 in the first adapter bar, the support bar 10 in the second adapter bar and the landing bar 11 in the third adapter bar, and improve the first adapter 17 and the cross bar 16, The reliability of the connection between the support bar 10 and the landing bar 11.
Optionally, the fourth limiting member may include, but is not limited to: at least one of a pin, a dowel, a screw, a bolt, and a stud, and a specific structure of the fourth limiting member may not be limited in the embodiment of the present application.
Referring to fig. 17, a schematic structural diagram of a foot rest according to an embodiment of the present application is shown, and referring to fig. 18, an exploded schematic structural diagram of the foot rest 17 is shown, and as shown in fig. 17 and 18, the stand may include: at least one mounting bar 18, each mounting bar 18 being connected to at least one support bar 10, the radar mounting portion 14 being disposed on the mounting bar 18; the central axis of each mounting rod 18 and the central axis of the support rod 11 connected thereto are located on the same plane, and the center of the radar 141 is located in the plane.
In practical applications, the central axis of each mounting rod 18 in the bracket and the central axis of the support rod 11 connected thereto are located on the same plane, and the center of the radar is located in the plane. Therefore, the radar is under the condition of launching the electromagnetic wave, and installation pole 18 and bracing piece 11 can share and shelter from the region, and only form in the oblique side region of radar and shelter from the region, and all around of radar do not receive the sheltering from of foot rest, like this, can reduce the foot rest is to the sheltering from of radar, promotes the performance of radar for the radar is more comprehensive in detection all around, and detection distance is farther.
In the embodiment of the application, the support can include at least two installation pole 18, radar installation department 14 are located each intersection point department of installing pole 18, like this, on the one hand, can all can realize the support to radar installation department 14 for each installation pole 18, improve the radar and be in installation reliability on the foot rest, on the other hand can also make the distance between radar to each bracing piece 10 comparatively close, and then, can further reduce sheltering from the region of radar.
Alternatively, the bracket may have a central symmetrical structure, and the radar mounting portion 14 may be located at the central position of the bracket, so that the distance between the radar and each of the support rods 10 is relatively close, and further, the shielding area of the radar may be further reduced.
In the present embodiment, a plurality of mounting bars 18 may be arranged in a cross to form an X-shaped structure. The X-shaped structure enables the connection of the support pole 10 in a diagonal position. In practical application, under the condition of support X "type structure, not only can make the structure of support is comparatively stable, realizes the reliable support to the radar, moreover, can also be convenient for can set up the cross department of" X "type structure with radar installation department 14, be convenient for radar installation department 14 is in installation and location on the foot rest.
It should be noted that, in practical applications, the number of the mounting rods 18 is only one. In addition, when the number of the mounting bars 18 is plural, the plural mounting bars 18 may not be designed to intersect with each other, and the present application does not limit this.
Alternatively, at the junction of the support bar 10 and the landing bar 11, one end of the mounting bar 18 is connected to both the support bar 10 and the landing bar 11; the other end of installation pole 18 is connected in radar installation department 14, like this, not only can be in by convenient installation pole 18 installation and location on the foot rest to and radar installation department 14 are in installation and location on the support, moreover, can also connect into whole, improvement with bracing piece 10, landing pole 11 and radar installation department 14 through installation pole 18 the structural stability of foot rest.
In this application embodiment, the foot rest can also include: the second adaptor 19 and the second adaptor 19 may be used to connect the mounting rod 18 to the support rod 10 and the landing rod 11, so as to connect the mounting rod 18, the support rod 10 and the landing rod 11, thereby improving the structural stability of the foot rest.
In particular, the second adaptor 19 may comprise: a fourth transfer lever, a fifth transfer lever and a sixth transfer lever; one end of the fourth adapter rod, one end of the fifth adapter rod and one end of the sixth adapter rod are connected together respectively; the fourth adapter rod is sleeved outside the mounting rod 18, the fifth adapter rod is sleeved outside the support rod 10, and the sixth adapter rod is sleeved outside the landing rod 11, so that the mounting rod 18 is connected to the support rod 10 and the landing rod 11.
In this application embodiment, the foot rest can also include: a fifth limiting member; wherein, the installation pole 18 inlays to be located part in the fourth switching pole, bracing piece 10 inlay to be located part in the fifth switching pole and landing pole 11 inlay to be located part in the sixth switching pole all is provided with the second connecting hole, the fourth switching pole the fifth switching pole and the sixth switching pole with the position that the second connecting hole is relative is provided with the sixth through-hole, fifth locating part passes in proper order the sixth through-hole with the second connecting hole, in order to incite somebody to action the fourth switching pole is connected in installation pole 18, will the fifth switching pole is connected in bracing piece 10, and, incite somebody to action the sixth switching pole is connected in landing pole 11. So as to avoid the installation rod 18 in the fourth adapter rod, the support rod 10 in the fifth adapter rod and the landing rod 11 in the sixth adapter rod from generating axial crosstalk and circumferential rotation, and improve the reliability of connection between the second adapter piece 19 and the installation rod 18, the support rod 10 and the landing rod 11.
In an embodiment of the present application, the fifth limiting element may include, but is not limited to: at least one of a pin, a dowel, a screw, a bolt, and a stud, and a specific structure of the fifth limiting member may not be limited in the embodiment of the present application.
It should be noted that, in practical application, when the unmanned aerial vehicle is an agricultural plant protection unmanned aerial vehicle, the first adapter 17 and the second adapter 19 may also be used to carry a spraying module of the unmanned aerial vehicle.
In some embodiments of the present application, the foot rest may further include: and the buffer 13, the buffer 13 can be connected to the landing lever 11 for buffering the impact received by the landing lever 11.
In practical application, bolster 13 can be made by the material that possesses certain elasticity unmanned aerial vehicle lands or the in-process of transporting, bolster 13 can be prior to landing rod 11 and ground contact to the impact that buffering landing rod 11 received reduces landing rod 11's damage, and then, can improve the life of foot rest.
Optionally, the buffer 13 may be sleeved outside the landing rod 11 to buffer the impact on the landing rod 11 during the transferring or landing process. In practical application, the buffer 13 is sleeved outside the landing rod 11, so that the buffer 13 can be conveniently installed and positioned on the landing rod 11.
Specifically, in the case that the landing lever 11 includes the landing lever body 111, the buffer 13 may be sleeved outside the landing lever body 111 for buffering the impact received by the landing lever 11.
It should be noted that, in practical applications, a person skilled in the art may also set the buffer 13 at the bottom of the landing rod 11 according to practical needs, and the specific position of the buffer 13 may not be limited in the embodiment of the present application.
Optionally, the material of the buffer 13 may include: at least one of foam and rubber, and the specific material of the buffer 13 in the embodiment of the present application may not be limited.
Referring to fig. 19, which shows a schematic structural view of another landing lever of the present application, as shown in fig. 19, the landing lever 11 may include a land portion 114 and a buffer portion 115, the land portion 114 has a higher strength than the buffer portion 115, and the buffer portion 115 is interposed between the land portion 114 and the support lever 11. During landing of the drone, the landing part 114 may contact the ground, and the buffer part 115 may be used to absorb the impact energy transferred from the landing part 114 to the buffer part 115.
In practical applications, since the strength of the landing part 114 is higher than that of the buffer part 115, the landing part 114 is not easily damaged during the contact between the landing part 114 and the ground when the drone lands. When the land portion 114 transmits the impact force to the buffer portion 115, the buffer portion 115 has a low strength, and thus the buffer portion 115 has a good effect of buffering the impact force.
In a preferred embodiment of the present application, the landing part 114 may be made of a carbon tube, and the buffer part 115 may be made of an aluminum tube. So that the strength of the land portion 114 can be higher than that of the buffer portion 115.
In practical applications, the land portions 114 and the cushioning portions 115 may also be made different in structure. For example, the landing part 114 can be made of a thick profile, while the buffer part 115 can be made of a thin profile; for another example, the landing part 114 may be designed to have a solid structure, and the buffer part 115 may be designed to have a hollow structure, so that the strength of the landing part 114 may be higher than that of the buffer part 115.
In this application embodiment, the foot rest still includes: and the fixing part 20 is connected with the first end of the supporting rod 10 and is used for fixing the foot rest on the machine body.
Specifically, the first end of the supporting rod 10 may be connected to the fixing member 20 by a clamping, embedding or screwing connection, and the connection between the supporting rod 10 and the fixing member 20 is not particularly limited in the embodiment of the present application.
In summary, the foot rest according to the embodiment of the present application may include at least the following advantages:
in this application embodiment, the foot rest can be formed by bracing piece and landing lever combination, the first end and the unmanned aerial vehicle of bracing piece are connected, the second end of bracing piece with the landing lever is connected. Because the intensity of bracing piece is higher than the intensity of landing pole, the design of the weak point of intensity of foot rest is in landing pole department, when unmanned aerial vehicle landed, only landing pole easily receives the impact damage, hardly damages unmanned aerial vehicle's fuselage, when maintaining unmanned aerial vehicle, only need change landing pole can, maintenance duration is short and cost of maintenance is lower. Moreover, because the intensity of bracing piece is higher than the landing pole, the bulk strength of foot rest is higher, the foot rest can realize effectively supporting the unmanned aerial vehicle fuselage, influences the life of the electrical apparatus on fuselage and the fuselage when avoiding unmanned aerial vehicle to land, improves unmanned aerial vehicle's safety in utilization.
Referring to fig. 20, a schematic structural diagram of a drone according to an embodiment of the present application is shown, and as shown in fig. 20, the drone may include: a body 200 and a foot rest 100 according to any of the above embodiments; wherein, the support rods of the foot stool 100 are connected to the body 200.
In this embodiment, the structure of the stand 100 is the same as that of the stand in the previous embodiments, and the detailed description thereof is omitted.
In the embodiment of this application, because the intensity of the bracing piece of foot rest is higher than the intensity of landing pole, the design of the weak point of intensity of foot rest is in landing pole department, when unmanned aerial vehicle lands, only landing pole is more easily received the impact damage, hardly damages unmanned aerial vehicle's fuselage, when maintaining unmanned aerial vehicle, only needs to be changed landing pole can, maintenance duration is short and cost of maintenance is lower. Moreover, because the intensity of bracing piece is higher than the landing pole, the bulk strength of foot rest is higher, the foot rest can realize effectively supporting the unmanned aerial vehicle fuselage, avoids unmanned aerial vehicle to influence the life of the electrical apparatus on fuselage and the fuselage when touchhing down, improves unmanned aerial vehicle's safe in utilization
Finally, it should also be noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or terminal that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or terminal. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other like elements in a process, method, article, or terminal that comprises the element.
The foot rest and the unmanned aerial vehicle provided by the application are introduced in detail, specific examples are applied in the text to explain the principle and the implementation mode of the application, and the description of the above embodiments is only used for helping to understand the method and the core idea of the application; meanwhile, for a person skilled in the art, according to the idea of the present application, there may be variations in the specific embodiments and the application scope, and in summary, the content of the present specification should not be construed as a limitation to the present application.

Claims (14)

1. The utility model provides a foot rest, is applied to unmanned aerial vehicle, its characterized in that, the foot rest includes:
the supporting rods are arranged in a plurality of numbers, the first ends of the supporting rods are fixedly connected with the unmanned aerial vehicle body, and the second ends of the supporting rods extend in the direction far away from the unmanned aerial vehicle body; and
the landing rod is arranged at the second end of the supporting rod and is in contact with the ground when the unmanned aerial vehicle lands;
wherein the strength of the support bar is higher than the strength of the landing bar.
2. A foot rest according to claim 1, wherein the support bar is of a different material than the landing bar;
and/or the support rod is made of a carbon tube;
and/or the landing bar is made of aluminum pipe.
3. A foot rest according to claim 1, wherein the landing bar is connected to at least two of the support bars;
the landing lever includes: the landing lever comprises a landing lever body and connecting rods arranged at two ends of the landing lever body, wherein the connecting rods extend towards the direction close to the machine body; wherein each connecting rod is connected with the second end of one supporting rod respectively; the landing rod body is arranged on one side, far away from the machine body, of the connecting rod.
4. A foot rest according to claim 3, wherein the landing bar body is integrally formed with the connecting bar, the connecting bar being formed by bending a tube;
and/or the landing lever body is matched with the two connecting rods to form a U-shaped structure.
5. A foot rest according to claim 3, wherein at least part of the support bar near the second end is embedded in the landing bar;
and/or a pipe expanding structure is arranged on one side, close to the supporting rod, of the landing rod, and the diameter of the pipe expanding structure is larger than that of other parts of the landing rod;
at least part of the support rod close to the second end is embedded in the pipe expanding structure.
6. A foot rest according to claim 3, characterized in that the foot rest further comprises: a first limit piece;
a first through hole is formed in the side wall of the part, embedded in the landing rod, of the support rod, and a second through hole is formed in the position, opposite to the first through hole, of the landing rod;
the first limiting piece sequentially penetrates through the second through hole and the first through hole so as to be connected with the landing rod and the supporting rod, and the first limiting piece can limit the part, embedded in the landing rod, of the supporting rod in the landing rod;
the first stopper includes: at least one of a pin, a dowel, a screw, a bolt, and a stud;
and/or the part of the supporting rod embedded in the landing rod is in interference fit with the landing rod.
7. A foot rest according to claim 1, characterized in that the foot rest further comprises: and the connecting piece is respectively connected with the landing rod and the second end of the supporting rod, and the connecting piece is used for connecting the landing rod to the supporting rod.
8. A foot rest according to claim 7, wherein the connecting member is an inlay member, at least part of one end of the connecting member being embedded in the landing bar and at least part of the other end of the connecting member being embedded in the second end of the support bar;
the connecting piece comprises a first embedding part, a convex limiting part and a second embedding part which are sequentially arranged from one end to the other end of the connecting piece; wherein the content of the first and second substances,
the first embedding part is embedded in the landing rod, and the second embedding part is embedded in the second end of the supporting rod;
the outer diameter of the limiting part is larger than the outer diameters of the first embedding part and the second embedding part, and the limiting part is clamped between the landing rod and the second end of the supporting rod;
and/or the limiting part is provided with a first surface facing the landing rod and a second surface facing the supporting rod, the first surface and the second surface are arranged oppositely, the landing rod is abutted against the first surface, and the supporting rod is abutted against the second surface;
and/or the first embedding part is in interference fit with the landing rod, and the second embedding part is in interference fit with the supporting rod;
and/or, the insert is made of a metal pipe, and the metal pipe comprises: at least one of a steel pipe and an aluminum pipe.
9. A foot rest according to claim 3, wherein the landing bar body comprises a constant diameter pipe section and a reduced pipe section, the reduced pipe section having a diameter smaller than the constant diameter pipe section;
the reducing pipe section is arranged between the two equal-diameter pipe sections, and one end of each equal-diameter pipe section, which is far away from the reducing pipe section, is connected with the connecting rod;
and/or, the landing lever body further comprises: the reducing pipe section is located between the equal-diameter pipe section and the reducing pipe section, and the diameter of the reducing pipe section is gradually reduced from the equal-diameter pipe section to the reducing pipe section.
10. A foot rest according to claim 1, characterized in that the foot rest further comprises: the buffer piece is connected to the landing rod and used for buffering the impact on the landing rod;
the buffer piece is sleeved outside the landing rod;
the material of bolster includes: at least one of foam and rubber.
11. A foot rest according to claim 1, characterized in that the foot rest further comprises: the bracket is positioned among the support rods and connected with the support rods;
the bracket is also provided with a radar mounting part for mounting a radar;
the radar is at least one of laser radar and millimeter wave radar.
12. A foot rest according to claim 11, characterized in that the stand comprises: the radar mounting device comprises at least one mounting rod, at least one supporting rod and at least one radar mounting part, wherein each mounting rod is connected to at least one supporting rod; the central axis of each mounting rod and the central axis of the supporting rod connected with the mounting rod are positioned on the same plane, and the center of the radar is positioned in the plane;
the bracket comprises at least two mounting rods, and the radar mounting part is positioned at the intersection point of the mounting rods;
and/or the bracket is of a central symmetrical structure, and the radar mounting part is positioned at the central position of the bracket;
and/or a plurality of the mounting rods are arranged in a crossed manner to form an X-shaped structure;
and/or one end of the mounting rod is connected with the supporting rod and the landing rod at the joint of the supporting rod and the landing rod; the other end of the mounting rod is connected to the radar mounting portion.
13. A foot rest according to any of claims 1 to 12, further comprising: the fixing piece, the fixing piece with the first end of bracing piece is connected, is used for with the foot rest is fixed in the fuselage.
14. An unmanned aerial vehicle, comprising: a fuselage and a foot rest as claimed in any one of claims 1 to 13; wherein the content of the first and second substances,
the supporting rod of the foot rest is connected with the machine body.
CN202022569249.8U 2020-11-09 2020-11-09 Foot rest and unmanned aerial vehicle Expired - Fee Related CN214776526U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202022569249.8U CN214776526U (en) 2020-11-09 2020-11-09 Foot rest and unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202022569249.8U CN214776526U (en) 2020-11-09 2020-11-09 Foot rest and unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN214776526U true CN214776526U (en) 2021-11-19

Family

ID=78664196

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202022569249.8U Expired - Fee Related CN214776526U (en) 2020-11-09 2020-11-09 Foot rest and unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN214776526U (en)

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Granted publication date: 20211119