CN209290669U - Self-balancing type multi-rotor unmanned aerial vehicle foot prop - Google Patents
Self-balancing type multi-rotor unmanned aerial vehicle foot prop Download PDFInfo
- Publication number
- CN209290669U CN209290669U CN201821847696.1U CN201821847696U CN209290669U CN 209290669 U CN209290669 U CN 209290669U CN 201821847696 U CN201821847696 U CN 201821847696U CN 209290669 U CN209290669 U CN 209290669U
- Authority
- CN
- China
- Prior art keywords
- foot prop
- arm
- aerial vehicle
- unmanned aerial
- connecting plate
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Vibration Dampers (AREA)
Abstract
The utility model discloses a kind of self-balancing type multi-rotor unmanned aerial vehicle foot props, including foot prop arm, the top of foot prop arm is provided with barrel coupler, damping ball component is provided between the inner bottom of barrel coupler and the top of foot prop arm, the outer tip end of barrel coupler is connect with multi-rotor unmanned aerial vehicle rack；The top two sidewalls of foot prop arm are fixed with foot prop connector by nut, and foot prop connector is fixedly connected with the bottom end of damping ball component, barrel coupler respectively by nut；The top two sidewalls of foot prop arm are located at barrel coupler two sides bottom end and are additionally provided with damping spring component, and damping spring component is fixedly connected with barrel coupler and foot prop connector respectively by nut；The bottom end setting balance ball component of foot prop arm.The utility model in multi-rotor unmanned aerial vehicle after completing flight operation, even if in the terrain environment of out-of-flatness, also can safety and stability completion landing, which can be substantially improved the efficiency of flight operation, reduce equipment because of accident caused by landing.
Description
Technical field
The utility model belongs to unmanned plane field, more specifically to a kind of self-balancing type multi-rotor unmanned aerial vehicle foot prop.
Background technique
Multi-rotor unmanned aerial vehicle refines routine inspection mode as a kind of novel electric power line pole tower, due to its high efficiency, just
The advantages such as victory and ease for operation carry out application in fields such as China's electric power, forestry and agriculturals, especially in mountain area on a large scale
Flight operation is carried out, the advantages such as efficient, portable, simple considerably reduce the labor intensity of manual work.However by landform
The influence of landforms, multi-rotor unmanned aerial vehicle must land after the completion of operation on very smooth ground, otherwise easily cause nobody
Machine landing shakiness causes rack to damage.
The a part of foot prop as unmanned plane structure platform, structure type directly affect the reliability of unmanned plane landing,
At present with the foot prop of line data-logging multi-rotor unmanned aerial vehicle mostly with " I " fonts and " four fulcrums " type, the foot prop of two kinds of patterns is not pacified
Damping device is filled, foot prop ground terminal also do not install self-adaptive component, when multi-rotor unmanned aerial vehicle is when out-of-flatness shaped area is landed,
Foot prop cannot achieve adjust automatically body balance, even if two ways high level operation person is landed, however it remains front/rear to incline
Or rollover situation.
Summary of the invention
In order to overcome the defect of existing multi-rotor unmanned aerial vehicle stability difference in the landing of out-of-flatness landforms, the utility model
A kind of self-balancing type multi-rotor unmanned aerial vehicle foot prop is provided, which can assist features of terrain of the unmanned plane according to landing when, from
It is dynamic to alleviate landing impulse force and keep organism balance.
The technical scheme adopted by the utility model to solve the technical problem is as follows:
A kind of self-balancing type multi-rotor unmanned aerial vehicle foot prop, including foot prop arm are designed, the top setting of the foot prop arm is organic
Frame connector is provided with damping ball component, the rack between the inner bottom of the barrel coupler and the top of foot prop arm
The outer tip end of connector is connect with multi-rotor unmanned aerial vehicle rack；The top two sidewalls of the foot prop arm are fixed with foot by nut
Frame connector, the foot prop connector are fixedly connected with the bottom end of damping ball component, barrel coupler respectively by nut；It is described
The top two sidewalls of foot prop arm are located at barrel coupler two sides bottom end and are additionally provided with damping spring component, and the damping spring component passes through
Nut is fixedly connected with barrel coupler and foot prop connector respectively；The bottom end setting balance ball component of the foot prop arm.
In the above scheme, the damping ball component includes two pieces of upper junction plates and lower connecting plate disposed in parallel, in institute
It states and opens up multiple connection holes on upper junction plate and lower connecting plate, the connection hole being overlapped on the upper junction plate and lower connecting plate
Between be fixed with shock-absorbing ball, the lower connecting plate is fixedly connected by nut with foot prop connector.
In the above scheme, the damping spring component includes T-shaped framework connecting plate, the top of the framework connecting plate
It is fixedly connected by nut with barrel coupler side bottom end, the framework connecting plate bottom periphery is cased with damping spring, described
The bottom end of framework connecting plate is rabbeted in the buffering hole on foot prop arm connecting plate, the foot prop arm connecting plate by nut respectively with
Foot prop arm, foot prop connector are fixedly connected.
In the above scheme, the balance ball component includes the balanced ball of foot prop arm bottom end, and the balanced ball is located at ground connection
In 3/4 circular trough that foot prop opens up.
The utility model is by barrel coupler, damping ball component, foot prop connector, damping spring component, foot prop arm, balance group
Part composition, damping ball component have used for reference holder damping device principle and have cooperated damping spring component, drop jointly for multi-rotor unmanned aerial vehicle
Cushion effect is provided when falling；Maximum Contact face can be kept according to landform adjust automatically ground engaging end and ground by balancing ball component, be guaranteed
Stationarity when multi-rotor unmanned aerial vehicle is landed, keeps rack to balance jointly in combination with damping device.
The utility model compared with prior art, has the advantages that
The utility model in multi-rotor unmanned aerial vehicle after completing flight operation, even if also can in the terrain environment of out-of-flatness
The completion landing of safety and stability, the device can be substantially improved the efficiency of flight operation, reduce equipment because of accident caused by landing.
Detailed description of the invention
Below in conjunction with accompanying drawings and embodiments, the utility model is described in further detail, in attached drawing:
Fig. 1 is the structural schematic diagram of self-balancing type multi-rotor unmanned aerial vehicle foot prop；
Fig. 2 is the structural schematic diagram of damping spring component in Fig. 1；
Fig. 3 is the side view of shock-absorbing ball modular construction in Fig. 1；
Fig. 4 is the top view of shock-absorbing ball modular construction in Fig. 1；
Fig. 5 is the structural schematic diagram of barrel coupler in Fig. 1；
Fig. 6 is the structural schematic diagram of foot prop connector in Fig. 1.
In figure: foot prop arm 1, barrel coupler 2, damping ball component 3 (wherein: upper junction plate 3.1, lower connecting plate 3.2, even
Connect hole 3.3, shock-absorbing ball 3.4), foot prop connector 4, damping spring component 5 (wherein: framework connecting plate 5.1, damping spring 5.2,
Foot prop arm connecting plate 5.3 buffers hole 5.4), (wherein: balanced ball 6.1 is grounded 6.2,3/4 circular trough of foot prop to balance ball component 6
6.3)。
Specific embodiment
For a clearer understanding of the technical features, objectives and effects of the utility model, now control attached drawing is detailed
Illustrate specific embodiment of the present utility model.
As shown in Figure 1, the utility model provides a kind of self-balancing type multi-rotor unmanned aerial vehicle foot prop, including foot prop arm 1, foot prop
The top of arm 1 is provided with barrel coupler 2.As shown in figure 5, barrel coupler 2 is in handstand U shape, barrel coupler 2
Inner bottom offers nut bore, for connecting damping ball component 3.The inner bottom of barrel coupler 2 and the top of foot prop arm 1
Between be provided with damping ball component 3, the outer tip end of barrel coupler 2 is connect with multi-rotor unmanned aerial vehicle rack.The top of foot prop arm 1
Two sidewalls are held to be fixed with foot prop connector 4 by nut, as shown in fig. 6, foot prop connector 4 is opened in handstand U shape and two sides
Equipped with nut bore, it to be used for connecting pin boom 1.Foot prop connector 4 by nut respectively with the bottom end of damping ball component 3, rack
Connector 2 is fixedly connected.Wherein, as shown in Figure 3 and Figure 4, damping ball component 3 includes two pieces of upper junction plates 3.1 disposed in parallel
With lower connecting plate 3.2, multiple connection holes 3.3 are opened up on upper junction plate 3.1 and lower connecting plate 3.2, upper junction plate 3.1 is under
Shock-absorbing ball 3.4 is fixed between the connection hole 3.3 being overlapped on connecting plate 3.2, lower connecting plate 3.2 is connect by nut with foot prop
Part 4 is fixedly connected.
The top two sidewalls of foot prop arm 1 are located at 2 two sides bottom end of barrel coupler and are additionally provided with damping spring component 5, damping spring
Component 5 is fixedly connected with barrel coupler 2 and foot prop connector 4 respectively by nut.Wherein, as shown in Fig. 2, damping spring component
5 include T-shaped framework connecting plate 5.1, and the top of framework connecting plate 5.1 is solid by nut and 2 side bottom end of barrel coupler
Fixed connection, 5.1 bottom periphery of framework connecting plate are cased with damping spring 5.2, and the bottom end interlocking of framework connecting plate 5.1 connects in foot prop arm
In buffering hole 5.4 on fishplate bar 5.3, foot prop arm connecting plate 5.3 is fixed with foot prop arm 1, foot prop connector 4 respectively by nut
Connection.
The bottom end setting balance ball component 6 of foot prop arm 1, balance ball component 6 includes the balanced ball 6.1 of 1 bottom end of foot prop arm, is put down
Weighing apparatus ball 6.1 is located in 3/4 circular trough 6.3 that ground connection foot prop 6.2 opens up.
The embodiments of the present invention are described above in conjunction with attached drawing, but the utility model is not limited to
The specific embodiment stated, the above mentioned embodiment is only schematical, rather than restrictive, this field it is common
Technical staff is not departing from the utility model aims and scope of the claimed protection situation under the enlightenment of the utility model
Under, many forms can be also made, these are belonged within the protection of the utility model.
Claims (4)
1. the top setting of a kind of self-balancing type multi-rotor unmanned aerial vehicle foot prop, including foot prop arm (1), the foot prop arm (1) is organic
Frame connector (2) is provided with damping ball component between the inner bottom of the barrel coupler (2) and the top of foot prop arm (1)
(3), the outer tip end of the barrel coupler (2) is connect with multi-rotor unmanned aerial vehicle rack；The top two sides of the foot prop arm (1)
Wall is fixed with foot prop connector (4) by nut, the foot prop connector (4) by nut respectively with damping ball component (3)
Bottom end, barrel coupler (2) are fixedly connected；The top two sidewalls of the foot prop arm (1) are located at barrel coupler (2) two sides bottom end
It is additionally provided with damping spring component (5), the damping spring component (5) is connect with barrel coupler (2) and foot prop respectively by nut
Part (4) is fixedly connected；Bottom end setting balance ball component (6) of the foot prop arm (1).
2. self-balancing type multi-rotor unmanned aerial vehicle foot prop according to claim 1, which is characterized in that the damping ball component
It (3) include two pieces of upper junction plates (3.1) disposed in parallel and lower connecting plate (3.2), in the upper junction plate (3.1) and lower connection
Multiple connection holes (3.3), the connecting hole being overlapped on the upper junction plate (3.1) and lower connecting plate (3.2) are opened up on plate (3.2)
It is fixed between hole (3.3) shock-absorbing ball (3.4), the lower connecting plate (3.2) connects by the way that nut and foot prop connector (4) are fixed
It connects.
3. self-balancing type multi-rotor unmanned aerial vehicle foot prop according to claim 1, which is characterized in that the damping spring component
It (5) include T-shaped framework connecting plate (5.1), the top of the framework connecting plate (5.1) passes through nut and barrel coupler
(2) side bottom end is fixedly connected, and framework connecting plate (5.1) bottom periphery is cased with damping spring (5.2), the rack connection
The bottom end of plate (5.1) is rabbeted in the buffering hole (5.4) on foot prop arm connecting plate (5.3), the foot prop arm connecting plate (5.3)
It is fixedly connected respectively with foot prop arm (1), foot prop connector (4) by nut.
4. self-balancing type multi-rotor unmanned aerial vehicle foot prop according to claim 1, which is characterized in that the balance ball component
(6) include foot prop arm (1) bottom end balanced ball (6.1), the balanced ball (6.1) be located at ground connection foot prop (6.2) open up 3/4 circle
In shape slot (6.3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821847696.1U CN209290669U (en) | 2018-11-10 | 2018-11-10 | Self-balancing type multi-rotor unmanned aerial vehicle foot prop |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821847696.1U CN209290669U (en) | 2018-11-10 | 2018-11-10 | Self-balancing type multi-rotor unmanned aerial vehicle foot prop |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209290669U true CN209290669U (en) | 2019-08-23 |
Family
ID=67647956
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821847696.1U Active CN209290669U (en) | 2018-11-10 | 2018-11-10 | Self-balancing type multi-rotor unmanned aerial vehicle foot prop |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209290669U (en) |
-
2018
- 2018-11-10 CN CN201821847696.1U patent/CN209290669U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103817507B (en) | Replacement method for pitching hinged point bearing of reclaimer | |
| CN209290669U (en) | Self-balancing type multi-rotor unmanned aerial vehicle foot prop | |
| CN205346360U (en) | Container unloader for bulk cargo | |
| CN207727954U (en) | Compound operating platform | |
| CN108104452A (en) | A kind of new steel structure builds platform device for high-altitude operation | |
| CN104832197B (en) | Cantilever support quick despatch lifting apparatus | |
| CN104847283B (en) | Cluster well drilling module drilling rod ramp, ocean | |
| CN207015575U (en) | Take photo by plane unmanned plane | |
| CN202745895U (en) | Filling device for anchoring agent | |
| CN204152219U (en) | Side fascia stone tongs | |
| CN208122257U (en) | A kind of new steel structure building platform device for high-altitude operation | |
| CN205602093U (en) | Unmanned plant protection machine undercarriage | |
| CN103669823B (en) | The rear support of angle rotatable | |
| CN105222975A (en) | Spent fuel storage rack fall-down test stand | |
| CN208122242U (en) | A kind of shrinkable steel building platform device for high-altitude operation | |
| CN211468765U (en) | Four-axis plant protection unmanned aerial vehicle's antidetonation frame | |
| CN104044743B (en) | Tail gas balance system of unmanned helicopter | |
| CN203716196U (en) | Rollover prevention excavator | |
| CN207293959U (en) | Special lifting platform is installed in the lifting of assembly concrete building element | |
| CN209586262U (en) | A kind of drilling machine | |
| CN205770125U (en) | A kind of interchangeable dispersion stress undercarriage | |
| CN205709520U (en) | A kind of bridge crane diving platform structure | |
| CN208882104U (en) | High-intensitive polling transmission line multi-rotor unmanned aerial vehicle foot prop | |
| CN205895157U (en) | Roof -bolter fixed bolster | |
| CN207892220U (en) | A kind of working at height Hanging Basket |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |