CN109774924A - A kind of dedicated damping type undercarriage of unmanned plane - Google Patents
A kind of dedicated damping type undercarriage of unmanned plane Download PDFInfo
- Publication number
- CN109774924A CN109774924A CN201711103456.0A CN201711103456A CN109774924A CN 109774924 A CN109774924 A CN 109774924A CN 201711103456 A CN201711103456 A CN 201711103456A CN 109774924 A CN109774924 A CN 109774924A
- Authority
- CN
- China
- Prior art keywords
- undercarriage
- flight
- vacuum
- unmanned plane
- bracket
- 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.)
- Withdrawn
Links
Abstract
The invention discloses a kind of dedicated damping type undercarriages of unmanned plane, its structure includes reflective mirror, flight host, heat release hole, art designing's lines, propeller, live spindle, flight bracket, undercarriage, camera bracket, camera, undercarriage is set altogether is installed on flight host bottom four corners there are four and by embedded mode, and flight stent ends are equipped with the groove of activity installing live spindle.This is practical the utility model has the advantages that the undercarriage being equipped with opens negative pressure of vacuum by inner vacuum controller, and then Vacuum container is made to generate suction function, vacuum chuck is set to adsorb on landing plate in landing, it effectively avoids unmanned plane from occurring in landing unstable, prevents unmanned plane inclination from damaging.
Description
Technical field
The present invention is a kind of dedicated damping type undercarriage of unmanned plane, belongs to unmanned plane undercarriage field.
Background technique
Unmanned plane is a kind of Miniature Vehicle device by remotely controlling, and compared with manned aircraft, unmanned plane is often
It is more suitable for the task of those too " slow-witted, dirty or dangerous ".Unmanned plane press application field, can be divided into it is military with it is civilian.Military side
Face, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+industrial application are that unmanned plane has really just needed；Exist at present
It takes photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, Xin Wen Bao
The application in road, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded the use of unmanned plane itself
On the way, developed country also in actively extension industrial application and develops unmanned air vehicle technique.
Prior art discloses application No. is a kind of 201720088432.1 unmanned plane dedicated damping type undercarriage,
Including unmanned plane undercarriage bottom plate, rubber damping rubber mat, the unmanned plane are provided with below the unmanned plane undercarriage bottom plate
The top both ends of undercarriage bottom plate are provided with undercarriage telescopic rod, separate unmanned plane undercarriage bottom on the undercarriage telescopic rod
One end of plate is provided with anti-falling limit block, and undercarriage telescopic rod outer cylinder is provided on the outside of the undercarriage telescopic rod, described
One end on undercarriage telescopic rod outer cylinder close to undercarriage telescopic rod is provided with undercarriage telescopic rod fixed ring, and the undercarriage is stretched
Undercarriage shock-absorbing spring is internally provided with close to undercarriage telescopic rod outer cylinder on contracting bar；Shock-absorbing spring is convenient in UAV Landing
When reduce unmanned plane undercarriage to the impact force of unmanned plane body, and then convenient for protection unmanned plane body, while being also convenient for preventing
Unmanned plane run-off the straight or the problem of topple over when landing.
Existing technology can not carry out vacuum suction while damping and fix, it is possible to cause unmanned plane landing uneven
Surely, appearance is inclined happens, and unmanned plane is caused to be damaged.
Summary of the invention
In view of the deficienciess of the prior art, it is an object of the present invention to provide a kind of dedicated damping type undercarriage of unmanned plane,
Vacuum suction can not be carried out while damping to solve existing technology to fix, it is possible to cause unmanned plane landing unstable,
Occur it is inclined happen, cause unmanned plane impaired problem occur.
To achieve the goals above, the present invention is to realize by the following technical solutions: a kind of unmanned plane is dedicated subtracts
Vibration shape undercarriage, structure include reflective mirror, flight host, heat release hole, art designing's lines, propeller, live spindle, flight branch
Frame, undercarriage, camera bracket, camera, the undercarriage is set altogether is installed on flight master there are four and by embedded mode
Motor spindle quadrangle, the flight stent ends are equipped with the groove of activity installing live spindle, and the live spindle upper end is logical
It crosses manner to be connected with propeller bottom, the heat release hole sets there are four altogether and is respectively set to flight back-end support and as one
Forming structure, the flight mid-stent are respectively provided with art designing's lines, and the undercarriage includes vacuum controller, true
It is spaced apart pass, actuator push rod, return spring, undercarriage frame body, Vacuum container, vacuum chuck, the vacuum chuck is circle
Structure and middle part is connected by manner with undercarriage frame body bottom, the undercarriage frame body upper end passes through embedded mode
In the middle part of the vacuum controller lower end, the vacuum controller inner upper end sets that there are two vacuum switch, the undercarriages
Frame body upper end sets there are two actuator push rod and is mutually perpendicular to vacuum switch, the negative pressure of vacuum bottom of the tube and vacuum chuck phase
Connection, the Vacuum container upper end are connected through undercarriage frame body with vacuum controller, the actuator push rod with time
Power spring phase fitting and it is connected by middle section inside return spring and vacuum controller.
Further, there are four the propeller is set altogether and overhead height is parallel to each other.
Further, the flight host lower end is set there are two the groove of activity installing camera bracket, and described takes the photograph
As head bracket bottom is connected at the top of camera by fitting mode.
Further, the flight bracket sets there are four altogether and is distributed in flight host quadrangle and the knot that is integrally formed
Structure.
Further, the flight host surface is coated with one layer of aluminium foil layer.
Further, flight host, heat release hole and the camera are waterproof material, effectively prevent internal infiltration
Cause damage parts.
Further, the undercarriage frame body is stainless steel material, effectively improves service life.
Beneficial effect
A kind of dedicated damping type undercarriage of unmanned plane of the present invention, the invention has the benefit that this practical undercarriage being equipped with
Negative pressure of vacuum is opened by inner vacuum controller, and then Vacuum container is made to generate suction function, vacuum chuck is made to land
When can landing plate on adsorb, effectively avoid unmanned plane landing when occur it is unstable, prevent unmanned plane inclination damage.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention,
Objects and advantages will become more apparent upon:
Fig. 1 is a kind of structural schematic diagram of the dedicated damping type undercarriage of unmanned plane of the present invention.
Fig. 2 is undercarriage schematic diagram of internal structure of the invention.
Fig. 3 is another morphosis schematic diagram of undercarriage of the invention.
In figure: reflective mirror -1, flight host -2, heat release hole -3, art designing's lines -4, propeller -5, live spindle -6, flight
Bracket -7, undercarriage -8, camera bracket -9, camera -10, vacuum controller -801, vacuum switch -802, actuator push rod -
803, return spring -804, undercarriage frame body -805, Vacuum container -806, vacuum chuck -807.
Specific embodiment
To be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, below with reference to
Specific embodiment, the present invention is further explained.
Fig. 1, Fig. 2 and Fig. 3 are please referred to, the present invention provides a kind of dedicated damping type undercarriage technical solution of unmanned plane: its
Structure includes reflective mirror 1, flight host 2, heat release hole 3, art designing's lines 4, propeller 5, live spindle 6, flight bracket 7, rises and falls
Frame 8, camera bracket 9, camera 10, the undercarriage 8 set there are four altogether and are installed on flight host 2 by embedded mode
Bottom four corners, 7 end of flight bracket are equipped with the groove of activity installing live spindle 6, and 6 upper end of live spindle is logical
It crosses manner to be connected with 5 bottom of propeller, the heat release hole 3 sets there are four altogether and is respectively set to 7 rear end of flight bracket simultaneously
It is an integral molding structure, art designing's lines 4 is respectively provided in the middle part of the flight bracket 7, the undercarriage 8 includes vacuum control
Device 801 processed, vacuum switch 802, actuator push rod 803, return spring 804, undercarriage frame body 805, Vacuum container 806, vacuum
Sucker 807, the vacuum chuck 807 is circular configuration and middle part is connected by manner with 805 bottom of undercarriage frame body
It connects, 805 upper end of undercarriage frame body is set in the middle part of 801 lower end of vacuum controller by embedded mode, the vacuum control
801 inner upper end of device processed is set there are two vacuum switch 802, and 805 upper end of undercarriage frame body sets that there are two actuator push rods 803
And be mutually perpendicular to vacuum switch 802,806 bottom of Vacuum container is connected with vacuum chuck 807, the vacuum
806 upper end of negative tube is connected through undercarriage frame body 805 with vacuum controller 801, the actuator push rod 803 and time power bullet
804 phase fitting of spring and it is connected by return spring 804 with 801 inside middle section of vacuum controller, the propeller 5 is equipped with altogether
Four and overhead height are parallel to each other, and 2 lower end of flight host is set there are two the groove of activity installing camera bracket 9,
9 bottom of camera bracket is connected with 10 top of camera by fitting mode, and the flight bracket 7 is equipped with four altogether
A and be distributed in 2 four jiaos of flight host and be an integral molding structure, 2 surface of flight host is coated with one layer of aluminium foil layer, institute
Flight host 2, heat release hole 3 and the camera 10 stated are waterproof material, effectively prevent internal infiltration to cause damage parts, institute
The undercarriage frame body 805 stated is stainless steel material, effectively improves service life.
Return spring 804 described in this is practical is a kind of machine components for utilizing elasticity come work.It is made of elastic material
Part deformation occurs under external force, remove external force after again restore to the original state.
When user need to this it is practical carry out using when, so that it may carried out by reflective mirror 1 it is reflective, and then improve
Unmanned plane identification is then to provide heat dissipation inside flight host 2 by heat release hole 3, and the flight host 2 being equipped with is for operating control
Live spindle 6 processed is rotated, and then is controlled propeller 5 and carried out rotation flight, and the undercarriage 8 being equipped with is used to land in unmanned plane
When provide support fix, the undercarriage frame body 805 being equipped with contact landing plate pushed when, pass through top actuator push rod 803
It pushes vacuum switch 802 and then starts vacuum controller 801, the vacuum controller 801 being equipped with controls Vacuum container 806 and opens
Negative pressure of vacuum is adsorbed on vacuum chuck 807 on landing plate, and then fixed unmanned plane.
Problems solved by the invention is that existing technology can not carry out vacuum suction while damping and fix, it is possible to be led
Cause unmanned plane landing unstable, appearance is inclined to be happened, and unmanned plane is caused to be damaged, and the present invention passes through above-mentioned component
It is combined with each other, effectively avoids unmanned plane from occurring in landing unstable, prevent unmanned plane inclination from damaging.
The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention, for this field skill
For art personnel, it is clear that invention is not limited to the details of the above exemplary embodiments, and without departing substantially from spirit of the invention or
In the case where essential characteristic, the present invention can be realized in other specific forms.Therefore, in all respects, should all incite somebody to action
Embodiment regards exemplary as, and is non-limiting, the scope of the present invention by appended claims rather than on state
Bright restriction, it is intended that including all changes that fall within the meaning and scope of the equivalent elements of the claims in the present invention
It is interior.Any reference signs in the claims should not be construed as limiting the involved claims.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (5)
1. a kind of dedicated damping type undercarriage of unmanned plane, structure include reflective mirror (1), flight host (2), heat release hole (3),
Art designing's lines (4), propeller (5), live spindle (6), flight bracket (7), undercarriage (8), camera bracket (9), camera
(10), it is characterised in that:
The undercarriage (8) is set altogether is installed on flight host (2) bottom four corners there are four and by embedded mode, and described flies
Row bracket (7) end is equipped with the groove of activity installing live spindle (6), and the live spindle (6) upper end passes through manner
It is connected with propeller (5) bottom, the heat release hole (3) sets there are four altogether and is respectively set to flight bracket (7) rear end and as one
Forming structure, flight bracket (7) middle part are respectively provided with art designing's lines (4)；
The undercarriage (8) includes vacuum controller (801), vacuum switch (802), actuator push rod (803), return spring
(804), undercarriage frame body (805), Vacuum container (806), vacuum chuck (807), the vacuum chuck (807) are circle
Structure and middle part is connected by manner with undercarriage frame body (805) bottom, undercarriage frame body (805) upper end are logical
Embedded mode is crossed in the middle part of vacuum controller (801) lower end, the vacuum controller (801) inner upper end sets that there are two true
Be spaced apart pass (802), described undercarriage frame body (805) upper end set there are two actuator push rod (803) and with vacuum switch (802) phase
Mutually vertical, Vacuum container (806) bottom is connected with vacuum chuck (807), on the Vacuum container (806)
End is connected through undercarriage frame body (805) with vacuum controller (801), the actuator push rod (803) and return spring
(804) phase fitting and it is connected by the internal middle section of return spring (804) and vacuum controller (801).
2. the dedicated damping type undercarriage of a kind of unmanned plane according to claim 1, it is characterised in that: the propeller
(5) there are four setting altogether and overhead height is parallel to each other.
3. the dedicated damping type undercarriage of a kind of unmanned plane according to claim 1, it is characterised in that: the flight master
Machine (2) lower end sets that there are two the groove of activity installing camera bracket (9), the camera bracket (9) bottom and cameras
(10) top is connected by fitting mode.
4. the dedicated damping type undercarriage of a kind of unmanned plane according to claim 1, it is characterised in that: the reflective mirror
(1) it sets altogether there are two and flight host (2) front end is installed on by manner, there are four the flight bracket (7) is set altogether
And it is distributed in flight host (2) quadrangle and is an integral molding structure.
5. the dedicated damping type undercarriage of a kind of unmanned plane according to claim 1, it is characterised in that: the flight master
Machine (2) surface is coated with one layer of aluminium foil layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711103456.0A CN109774924A (en) | 2017-11-10 | 2017-11-10 | A kind of dedicated damping type undercarriage of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711103456.0A CN109774924A (en) | 2017-11-10 | 2017-11-10 | A kind of dedicated damping type undercarriage of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109774924A true CN109774924A (en) | 2019-05-21 |
Family
ID=66484402
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711103456.0A Withdrawn CN109774924A (en) | 2017-11-10 | 2017-11-10 | A kind of dedicated damping type undercarriage of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109774924A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110460296A (en) * | 2019-06-28 | 2019-11-15 | 常州中信博新能源科技有限公司 | Photovoltaic bracket wind resistance damping device |
| CN112171692A (en) * | 2020-10-15 | 2021-01-05 | 吉林大学 | Intelligent detection device and method for bridge deflection |
-
2017
- 2017-11-10 CN CN201711103456.0A patent/CN109774924A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110460296A (en) * | 2019-06-28 | 2019-11-15 | 常州中信博新能源科技有限公司 | Photovoltaic bracket wind resistance damping device |
| CN112171692A (en) * | 2020-10-15 | 2021-01-05 | 吉林大学 | Intelligent detection device and method for bridge deflection |
| CN112171692B (en) * | 2020-10-15 | 2023-12-12 | 吉林大学 | Intelligent bridge deflection detection device and method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207595246U (en) | A kind of dedicated damping type undercarriage of unmanned plane | |
| CN207257974U (en) | A kind of unmanned plane landing buffer frame | |
| CN109774924A (en) | A kind of dedicated damping type undercarriage of unmanned plane | |
| CN208264584U (en) | One kind, which is taken photo by plane, surveys and draws unmanned plane | |
| CN205589460U (en) | Be used for air -borne early warning unmanned aerial vehicle | |
| CN205045003U (en) | Novel unmanned aerial vehicle camera installing support device | |
| CN207670657U (en) | A kind of plain type quadrotor drone | |
| CN213229120U (en) | Remote sensing surveying and mapping unmanned aerial vehicle with accurate positioning | |
| CN108569391A (en) | A kind of adjustable uav bottom supporting rack | |
| CN204942969U (en) | A kind of novel camera mounting support of taking photo by plane | |
| CN214084743U (en) | Unmanned aerial vehicle intelligence defense device | |
| CN207089641U (en) | A kind of unmanned plane shock mount | |
| CN107826240A (en) | One kind, which is taken photo by plane, uses unmanned plane | |
| CN210503909U (en) | Convenient portable unmanned aerial vehicle anticollision shock attenuation transport case | |
| CN209051589U (en) | One kind making an inspection tour multi-rotor unmanned aerial vehicle for electric wire | |
| CN213677201U (en) | Unmanned aerial vehicle takes photo by plane of camera protective structure | |
| CN213892881U (en) | Take-off and landing bracket for amphibious unmanned aerial vehicle | |
| CN108891582A (en) | A kind of unmanned plane undercarriage with pooling feature | |
| CN208233352U (en) | One kind using buffer unit based on unmanned plane landing | |
| CN209560388U (en) | Ground control box is used in a kind of operation of unmanned plane | |
| CN214216171U (en) | Unmanned aerial vehicle frame supporting device for life cycle test of unmanned aerial vehicle | |
| CN207670682U (en) | A kind of unmanned plane support construction of stability when can improve ejection | |
| CN209480003U (en) | A kind of unmanned plane flight collision avoidance device | |
| CN209410320U (en) | A kind of hollow vertical touching lever fold mechanism | |
| CN210761293U (en) | Many unmanned aerial vehicle event support auxiliary device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190521 |