CN204916163U - Foot rest and unmanned aerial vehicle - Google Patents
Foot rest and unmanned aerial vehicle Download PDFInfo
- Publication number
- CN204916163U CN204916163U CN201520430546.0U CN201520430546U CN204916163U CN 204916163 U CN204916163 U CN 204916163U CN 201520430546 U CN201520430546 U CN 201520430546U CN 204916163 U CN204916163 U CN 204916163U
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- Prior art keywords
- foot rest
- strut member
- abutting part
- rotating junction
- unmanned plane
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Abstract
The utility model discloses a foot rest and unmanned aerial vehicle. The foot rest is installed be used for supporting the unmanned aerial vehicle fuselage on unmanned aerial vehicle, the foot rest includes a support piece, the 2nd support piece and locating part, a support piece's one end with unmanned aerial vehicle's fuselage is connected, a support piece's the other end with the 2nd support piece rotates the connection, the foot rest has extension state and fold condition, the locating part include with a support piece butt so that the foot rest is in the first butt portion of extension state, and connect in first butt portion and through pressing so that first butt portion with a support piece removes the elasticity of butt state and presses the splenium. Unmanned aerial vehicle is including above -mentioned foot rest. The utility model discloses a foot rest is connected with the 2nd support piece's rotation through a support piece, makes this foot rest have a foot rest that extends with folding two types, greatly reduced be provided with unmanned aerial vehicle shared spaces that have when the packing of this foot rest, reduced package cost, it is more convenient that the messenger transports.
Description
Technical field
The utility model relates to unmanned plane field, particularly a kind of foot rest and unmanned plane.
Background technology
Unmanned plane with its action flexibly, landing environmental requirement is lower, and has good operating characteristic etc., be widely used in take photo by plane, monitor, investigate, the numerous areas such as search and rescue.This unmanned plane generally all has foot rest, so that unmanned plane is when landing, and can by its foot rest to unmanned plane standing support.
The foot rest of existing unmanned plane is fixed type, and foot rest entirety is fixedly connected with fuselage, and being assemblied in of unmanned plane entirety completes before dispatching from the factory.But when packing, in order to support whole body, the space that usual foot rest takies is 1 to 2 times of body, considerably increases packing cost and traffic cost.
Utility model content
Main purpose of the present utility model is to provide a kind of foot rest and unmanned plane, is intended to solve existing unmanned plane and takies larger space when packing, thus causes packing cost and the high problem of traffic cost.
Realize above-mentioned purpose, the utility model provides a kind of foot rest, be arranged on unmanned plane in order to support unmanned aerial vehicle body, described foot rest comprises the first strut member, second strut member and locating part, one end of described first strut member is connected with the fuselage of described unmanned plane, the other end and described second strut member of described first strut member are rotationally connected, described foot rest has extended configuration and folded state, described locating part comprises and abuts to make described foot rest be in the first abutting part of extended configuration with described first strut member, and be connected to described first abutting part, and by pressing to make the first abutting part remove the elasticity press section of the state that abuts with described first strut member.
Preferably, described first strut member comprises and extends the first rotating junction towards described second strut member; Described second strut member comprises and is oppositely arranged two second side plates, described two the second side plates extend the second rotating junction of described first rotating junction clamping towards described first strut member, and described second rotating junction and described first rotating junction are rotationally connected.
Preferably, described elasticity press section is arranged between described two the second side plates, and all offers slot between described elasticity press section and described two the second side plates.
Preferably, the arc that described first strut member is provided with described first direction, rotating junction projection is dorsad stepped down plate, described first abutting part from top, described elasticity press section, along described in plate of stepping down extend to the first strut member.
Preferably, described in the step down side of plate be provided with first protruding, described first abutting part tail end is provided with second of described first protruding interference fit protruding, to be fixed in a folded configuration by foot rest.
Preferably, described in plate of stepping down be provided with second baffle near described second bracing frame one end, when described foot rest is in extended configuration, described first abutting part abuts with described second baffle.
Preferably, the side that described first abutting part deviates from described first rotating junction is provided with one for the antenna clip of fixed antenna.
Preferably, described second strut member comprise for earth surface to support the ground terminal of described unmanned plane, described ground terminal is provided with an elastic portion for abutting with ground.
Preferably, described first both sides, rotating junction are equipped with the second abutting part, described two the second side plates are connected to described second abutting part near the end of described first strut member, to prevent described second strut member from continuing to inner rotary, make described foot rest keep extended configuration.
For achieving the above object, the utility model also provides a kind of unmanned plane, and described unmanned plane comprises the foot rest described in above-mentioned any one.
Foot rest of the present utility model is rotationally connected by the first strut member and the second strut member, this foot rest is made to have the foot rest of stretching, extension and folding two states, greatly reducing the space that the unmanned plane that is provided with this foot rest occupies when packing, reducing packing cost, making transport more convenient.
Accompanying drawing explanation
Fig. 1 is the mounting structure schematic diagram of foot rest one embodiment of the present utility model and unmanned aerial vehicle body, and wherein this foot rest is in extended configuration;
Fig. 2 is the mounting structure schematic diagram of foot rest one embodiment of the present utility model and unmanned aerial vehicle body, and wherein this foot rest is in folded state;
Fig. 3 is the structural representation at a visual angle of foot rest in Fig. 1;
Fig. 4 is the structural representation at another visual angle of foot rest in Fig. 1; Wherein, the first strut member and the second strut member in the state before assembled;
Fig. 5 is the birds-eye view of the utility model foot rest in Fig. 1; Wherein this foot rest is in extended configuration;
Fig. 6 is the cutaway view of the foot rest in Fig. 5 along A-A line;
Fig. 7 is the birds-eye view of the utility model foot rest in Fig. 1; Wherein this foot rest is in folded state;
Fig. 8 is the cutaway view of the foot rest in Fig. 7 along B-B line;
Fig. 9 is C portion structure for amplifying schematic diagram in Fig. 4;
Figure 10 is D portion structure for amplifying schematic diagram in Fig. 4.
The realization of the utility model object, functional characteristics and advantage will in conjunction with the embodiments, are described further with reference to accompanying drawing.
Detailed description of the invention
Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
Referring to figs. 1 through Fig. 4, the utility model provides a kind of foot rest 10, be arranged on unmanned plane in order to support unmanned aerial vehicle body, described foot rest 10 comprises the first strut member 11, second strut member 12 and locating part, one end of described first strut member 11 is connected with the fuselage of described unmanned plane, the other end and described second strut member 12 of described first strut member 11 are rotationally connected, described foot rest 10 has extended configuration and folded state, described locating part comprises and abuts to make described foot rest 10 be in the first abutting part 123 of extended configuration with described first strut member 11, and be connected to described first abutting part 123, and by pressing to make the first abutting part 123 remove the elasticity press section 124 of the state of abutting with described first strut member 11.
When described foot rest 10 is in extended configuration, described first abutting part 123 abuts with described first strut member 11, in case described second strut member 12 inwardly rotates relative to the first strut member 11, the lower end of described first strut member 11 side outwardly abuts with the upper end of described second strut member 12 side outwardly, in case described second strut member 12 outwards rotates relative to the first strut member 11, thus described foot rest 10 is made to keep extended configuration.Pressing described press section 124 to be convenient to user further in addition, described press section 124 can also be arranged salient point or raised line 1240.
Described first strut member 11 can be direct coupled with unmanned aerial vehicle body 20, also can abut with ground; Equally, described second strut member 12 also can connect with unmanned plane straight 20 in succession, also can abut with ground, and among the two, any one is directly connected with unmanned aerial vehicle body 20 and is all fine.Concrete, be followingly directly connected with unmanned aerial vehicle body 20 with the first strut member 11, the second strut member 12 abuts as example is described with ground.
The upper end of described first abutting part 123 and the second strut member side is outwardly arranged at the inside and outside both sides being rotationally connected place between described first strut member 11 and the second strut member 12, and described first abutting part 123 is connected with described second strut member 12; Described first abutting part 123 is for when described foot rest 10 is in extended configuration, abut with described first strut member 11, in case described second strut member 12 inwardly rotates along the described place of being rotationally connected, described first abutting part 123 is for when this first abutting part 123 abuts with described first strut member 11, prevent described second strut member 12 from inwardly rotating along the described place of being rotationally connected, thus make described foot rest 10 keep extended configuration; Described first abutting part 123 is connected with described second strut member 12 elasticity, and in order to be separated with described first strut member 11 when deformation in compression, and make, described second strut member 12 can inwardly turn to described folded state.
When mounted, the described one end in the first strut member portion 11 is fixedly connected with the fuselage 20 of unmanned plane or removably connects, the other end of described first strut member 11 and one end of described second strut member 12 are rotationally connected, and the other end of described second strut member 12 abuts with ground.First strut member 11 and the second strut member 12 are rotationally connected and the second strut member 12 can be made to rotate centered by the described place of being rotationally connected (rotate counterclockwise, rotate clockwise), when the second strut member 12 is in extended configuration, on the one hand under the first abutting part 123 acts on, described second strut member 12 can not inwardly rotate, when the first strut member 11 side outwardly lower end with described second strut member 12 side outwardly upper end abut, described second strut member 12 can not outwards rotate, thus the first strut member 11 and the second strut member 12 mutually spacing, to support unmanned aerial vehicle body 20.
When packing, first needing described foot rest 10 to fold, making this foot rest 10 be in folded state, be then seated in packing box, to reduce the packaging space occupied by unmanned plane entirety.In addition, if this foot rest 10 removably connects with the fuselage 20 of unmanned plane, when packing, foot rest 10 and unmanned aerial vehicle body 20 split can be placed, and described foot rest 10 is folded, thus saving packaging space further.
Foot rest 10 of the present utility model is rotationally connected by the first strut member 11 and the second strut member 12, this foot rest 10 is made to have stretching, extension and folding two states, greatly reducing the space that the unmanned plane that is provided with this foot rest 10 occupies when packing, reducing packing cost, making transport more convenient.
Further, with reference to Fig. 3 and 4, described first strut member 11 comprises first rotating junction 113 of extending towards described second strut member 12; Described second strut member 12 comprises and is oppositely arranged two second side plates 122, two described second side plates 122 extend the second rotating junction 1221 clamped described first rotating junction 113 towards described first strut member 11, described second rotating junction 1221 is rotationally connected with described first rotating junction 113.
Concrete, described first strut member 11 comprises the first panel 111, be arranged at the first side plate 112 of the relative dual-side of described first panel 111, connect the base plate 115 of described first panel 111 and two the first side plates 112, two described first side plates 112 are all arranged at the medial surface of described first panel 111, described base plate 115 extends first rotating junction 113 for being rotationally connected with described second strut member 12 towards described second strut member 12, described first rotating junction 113 is extended by the direction of described base plate 115 towards the second strut member 12, described second rotating junction 1221 is parts that two described second side plates 122 extend towards the first strut member 11, described first rotating junction 113 and the second rotating junction 1221 all offer pin-and-hole 114, first rotating junction 113 clamps by described second rotating junction 1221, and be inserted in described pin-and-hole 114 by a rotating shaft 1140, so that described first rotating junction 113 and the second rotating junction 1221 are fixed, thus, described second rotating junction 113 can be rotated centered by described rotating shaft 1140.
Further, described elasticity press section 124 is arranged between described two the second side plates 122, and all offers slot between described elasticity press section 124 and described two the second side plates 122.
The arc that described first strut member 11 is provided with described first rotating junction 113 direction projection is dorsad stepped down plate 152, described first abutting part 123 from top, described elasticity press section 124, along described in plate 152 of stepping down extend to the first strut member 11.
Particularly, continue with reference to Fig. 4, the setting of described slot is convenient to described elasticity press section 124, when being pressed, elastic deformation is occurred, so that described first abutting part 123 can abut or remove abutting state with the first strut member 11 very smoothly.Described second strut member 12 comprises the second panel 121, and described second panel 121 extends described first abutting part 123 from described medial surface towards the direction deviating from this medial surface, and described elasticity press section 124 is arranged at described second panel 121.Described base plate 115 comprises arc and to step down plate 1152, described in plate 1152 of stepping down be arranged between described first baffle plate 1151 and described second baffle 1153; The described plate 1152 of stepping down is arranged in arc cambered outwards towards the side deviating from described first rotating junction 113, described in step down plate 1152 for stepping down to the rotation of described second rotating junction 1121.
Further, described in the step down side of plate 1152 be provided with the first projection 116, described first abutting part 123 tail end is provided with the second projection 128 with described first protruding 116 interference fit, to be fixed in a folded configuration by foot rest 10.
Even if described foot rest 10 is in folded state, can save more space when packing, but this folded state of foot rest 10 is also unstable, when user opens packaging, described foot rest 10 may be scattered everywhere.In the present embodiment, by the setting of the described first protruding 116 and second projection 128, effectively can avoid the generation of this situation.
Further, described in plate 1152 of stepping down be provided with second baffle 1153 near described second bracing frame 12 one end, when described foot rest 10 is in extended configuration, described first abutting part 123 abuts with described second baffle 1153.
Described base plate 115 comprises the first baffle plate 1151, the second baffle 1153 for abutting with described first abutting part 123 that abut with the upper end of described second strut member 12 side outwardly, described in plate 1152 of stepping down be arranged between described first baffle plate 1151 and described second baffle 1153.
When described foot rest 10 is in extended configuration, the upper end of described second strut member 12 side outwardly abuts with described first baffle plate 1151, described second rotating junction 1121 comprises towards the first bearing surface of described first baffle plate 1151 and the first cambered surface 1221b towards described plate 1152 evagination of stepping down, described first bearing surface abuts with described first baffle plate 1151, described first abutting part 123 abuts with described second baffle 1153, so, described second strut member 12 inwardly can not rotate and can not outwards rotate, and described foot rest 10 remains on extended configuration.
When described foot rest 10 folds by needs, press described elasticity press section 124, make described first abutting part 123 towards the offset inboard of this second strut member 12, to make described first abutting part 123 remove with described second baffle 1153 state of abutting, then described second strut member 12 is inwardly rotated centered by described rotating shaft 1140.Now, described first cambered surface 1221b is under the directional tagging of plate 1152 of stepping down, and described second strut member 12 can smooth rotation, and the most described foot rest 10 folds.It should be noted that, it is preferred implementation that described first cambered surface 1221b has identical curvature with plate 1152 of stepping down on rotation path.
Further, with reference to Fig. 5, Fig. 6, Fig. 7, Fig. 8 and Figure 10, the side that described first abutting part 123 deviates from described first rotating junction 113 is provided with one for the antenna clip 125 of fixed antenna.
Concrete, described antenna clip 125 is provided with antenna hold down groove, and antenna passes described antenna hold down groove, to realize the fixing of antenna.Because this foot rest 10 is folding, so described antenna also should adopt bent antenna.
Further, with reference to Fig. 4, Fig. 6 and Fig. 8, described second strut member 12 comprise for earth surface to support the ground terminal 126 of described unmanned plane, described ground terminal 126 is provided with an elastic portion 127 for abutting with ground.
When described elastic portion 127 is in order to lower unmanned plane landing and the vibrations that produce of earth surface, to increase the balanced capacity of unmanned plane.The material of this elastic portion can be sponge, silica gel or rubber etc.
Further, described first both sides, rotating junction 113 are equipped with the second abutting part, described two the second side plates are connected to described second abutting part near the end of described first strut member, to prevent described second strut member 12 from continuing to inner rotary, make described foot rest 10 keep extended configuration.
Further, described first abutting part 123 is arranged in arc cambered outwards towards the side deviating from described first rotating junction 113.
In the present embodiment, the curved setting of described first abutting part 123 can increase elasticity, so that the self-locking between the first strut member 11 and the second strut member 12.
Concrete, when the foot rest 10 being in folded state extends by needs, just need manually described second strut member 12 to be broken towards anticlockwise direction, and the second strut member 12 in a folded configuration time, described first abutting part 123 is in elastic deformation state, when the second strut member 12 stretches gradually, described second strut member 12 recovers elastic deformation gradually, when this foot rest 10 full extension, described first abutting part 123 recovers elastic deformation, described first baffle plate 1153 abuts with the one side of described second strut member 123 towards the first baffle plate 1153, so just achieve the self-locking between the first strut member 11 and the second strut member 12, be convenient to user operation.
The utility model also provides a kind of unmanned plane, and described unmanned plane comprises the foot rest 10 described in above-mentioned any embodiment.
Concrete, owing to this unmanned plane being provided with the foot rest 10 described in above-mentioned any one, therefore, all these unmanned planes of usefulness of this foot rest 10 also should one should to have, and do not repeat one by one at this.
The foregoing is only preferred embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every utilize the utility model specification sheets and accompanying drawing content to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present utility model.
Claims (10)
1. a foot rest, be arranged on unmanned plane in order to support unmanned aerial vehicle body, it is characterized in that, described foot rest comprises the first strut member, second strut member and locating part, one end of described first strut member is connected with the fuselage of described unmanned plane, the other end and described second strut member of described first strut member are rotationally connected, described foot rest has extended configuration and folded state, described locating part comprises and abuts to make described foot rest be in the first abutting part of extended configuration with described first strut member, and be connected to described first abutting part, and by pressing to make the first abutting part remove the elasticity press section of the state that abuts with described first strut member.
2. foot rest as claimed in claim 1, is characterized in that, described first strut member comprises and extends the first rotating junction towards described second strut member; Described second strut member comprises and is oppositely arranged two second side plates, described two the second side plates extend the second rotating junction of described first rotating junction clamping towards described first strut member, and described second rotating junction and described first rotating junction are rotationally connected.
3. foot rest as claimed in claim 2, it is characterized in that, described elasticity press section is arranged between described two the second side plates, and all offers slot between described elasticity press section and described two the second side plates.
4. foot rest as claimed in claim 3, it is characterized in that, the arc that described first strut member is provided with described first direction, rotating junction projection is dorsad stepped down plate, described first abutting part from top, described elasticity press section, along described in plate of stepping down extend to the first strut member.
5. foot rest as claimed in claim 4, is characterized in that, described in the step down side of plate be provided with first protruding, described first abutting part tail end is provided with second of described first protruding interference fit protruding, to be fixed in a folded configuration by foot rest.
6. foot rest as claimed in claim 3, is characterized in that, described in plate of stepping down be provided with second baffle near described second bracing frame one end, when described foot rest is in extended configuration, described first abutting part abuts with described second baffle.
7. the foot rest as described in any one of claim 1 to 6, is characterized in that, the side that described first abutting part deviates from described first rotating junction is provided with one for the antenna clip of fixed antenna.
8. the foot rest as described in any one of claim 1 to 6, is characterized in that, described second strut member comprise for earth surface to support the ground terminal of described unmanned plane, described ground terminal is provided with an elastic portion for abutting with ground.
9. the foot rest as described in any one of claim 2 to 6, it is characterized in that, described first both sides, rotating junction are equipped with the second abutting part, and described two the second side plates are connected to described second abutting part near the end of described first strut member, make described foot rest keep extended configuration.
10. a unmanned plane, is characterized in that, described unmanned plane comprises the foot rest as described in any one of claim 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520430546.0U CN204916163U (en) | 2015-06-19 | 2015-06-19 | Foot rest and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520430546.0U CN204916163U (en) | 2015-06-19 | 2015-06-19 | Foot rest and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204916163U true CN204916163U (en) | 2015-12-30 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520430546.0U Expired - Fee Related CN204916163U (en) | 2015-06-19 | 2015-06-19 | Foot rest and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204916163U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105905280A (en) * | 2016-05-25 | 2016-08-31 | 北京小米移动软件有限公司 | Aircraft and foot stool structure thereof |
| CN107521671A (en) * | 2016-06-22 | 2017-12-29 | 北京臻迪机器人有限公司 | Turbine worm holder device |
| CN107521676A (en) * | 2016-06-22 | 2017-12-29 | 北京臻迪机器人有限公司 | A kind of locking device of foot stool |
| CN108216588A (en) * | 2016-05-19 | 2018-06-29 | 泉州泉港璟冠信息科技有限公司 | A kind of unmanned plane |
| EP3453615A4 (en) * | 2017-07-10 | 2019-03-20 | Autel Robotics Co., Ltd. | Antenna and unmanned aerial vehicle |
| WO2019140661A1 (en) * | 2018-01-19 | 2019-07-25 | 深圳市大疆创新科技有限公司 | Landing gear and unmanned aerial vehicle |
| US10707572B2 (en) | 2017-07-10 | 2020-07-07 | Autel Robotics Co., Ltd. | Antenna and unmanned aerial vehicle |
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2015
- 2015-06-19 CN CN201520430546.0U patent/CN204916163U/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108216588A (en) * | 2016-05-19 | 2018-06-29 | 泉州泉港璟冠信息科技有限公司 | A kind of unmanned plane |
| CN108216588B (en) * | 2016-05-19 | 2021-05-25 | 南通寓无疆科技有限公司 | Unmanned aerial vehicle |
| CN105905280A (en) * | 2016-05-25 | 2016-08-31 | 北京小米移动软件有限公司 | Aircraft and foot stool structure thereof |
| CN107521671A (en) * | 2016-06-22 | 2017-12-29 | 北京臻迪机器人有限公司 | Turbine worm holder device |
| CN107521676A (en) * | 2016-06-22 | 2017-12-29 | 北京臻迪机器人有限公司 | A kind of locking device of foot stool |
| CN107521671B (en) * | 2016-06-22 | 2021-08-10 | 北京臻迪机器人有限公司 | Turbine scroll bar support device |
| CN107521676B (en) * | 2016-06-22 | 2021-11-30 | 北京臻迪机器人有限公司 | Locking device of foot rest |
| EP3453615A4 (en) * | 2017-07-10 | 2019-03-20 | Autel Robotics Co., Ltd. | Antenna and unmanned aerial vehicle |
| US10707572B2 (en) | 2017-07-10 | 2020-07-07 | Autel Robotics Co., Ltd. | Antenna and unmanned aerial vehicle |
| WO2019140661A1 (en) * | 2018-01-19 | 2019-07-25 | 深圳市大疆创新科技有限公司 | Landing gear and unmanned aerial vehicle |
| CN110300703A (en) * | 2018-01-19 | 2019-10-01 | 深圳市大疆创新科技有限公司 | Foot prop and unmanned vehicle |
| CN110300703B (en) * | 2018-01-19 | 2022-06-03 | 深圳市大疆创新科技有限公司 | Foot rest and unmanned vehicles |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160216 Address after: Baoan District Shiyan street Shenzhen city Guangdong province 518108 Songbai road Tangtou junctions electric science and Technology Park Patentee after: Shenzhen Aee Technology Co., Ltd. Address before: Baoan District Shiyan street Shenzhen city Guangdong province 518108 Songbai road Tangtou junctions electric science and Technology Park Patentee before: Shenzhen Aee Technology Co., Ltd. Patentee before: Shenzhen Aee Technology Co., Ltd. |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151230 Termination date: 20180619 |