CN106394864B - Folding rack structure and unmanned plane - Google Patents
Folding rack structure and unmanned plane Download PDFInfo
- Publication number
- CN106394864B CN106394864B CN201611068395.4A CN201611068395A CN106394864B CN 106394864 B CN106394864 B CN 106394864B CN 201611068395 A CN201611068395 A CN 201611068395A CN 106394864 B CN106394864 B CN 106394864B
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- Prior art keywords
- pedestal
- bracket component
- folding rack
- rack structure
- unmanned plane
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Warehouses Or Storage Devices (AREA)
- Casings For Electric Apparatus (AREA)
Abstract
The present invention relates to unmanned plane fields；More particularly it relates to folding rack structure and unmanned plane.The folding rack structure includes：Pedestal；Bracket component, the one end for being used to support the pedestal and the bracket component are installed on the pedestal in a manner of it can dismantle；Foldable assembly, one end are installed on the bracket component, and the other end is rotatablely connected with the pedestal, can be rotated around the pedestal to drive the bracket component for being detached from installation with the pedestal to rotate；And lock assembly, it is used for foldable assembly described in locking.The present invention also provides a kind of unmanned planes using the folding rack structure.By using above-mentioned technical solution, the present invention provides a kind of folding rack structure and the unmanned plane using the folding rack structure so that the transportation of unmanned plane or packed and transported can more easily increase the stability and reliability of supporting structure simultaneously.
Description
Technical field
The present invention relates to unmanned plane fields；More particularly it relates to folding rack structure and including the folding rack
The unmanned plane of structure.
Background technology
With popularizing for unmanned plane, in the actual application of unmanned plane, user increasingly payes attention to unmanned plane block speed
The performance of dismounting and the performance of convenient transportation.Currently, the unmanned plane generally use fixed bracket of unmanned plane, especially rotor type
Structure.Using above-mentioned fixed bracket structure, cause the monnolithic case of unmanned plane bigger, the storage for being not easy to unmanned plane is taken
Band or packed and transported.Although it is good that effective Collapsible rack structure can give unmanned plane scene Quick Release fast-assembling, convenient transportation to provide
Solution, but existing Collapsible rack has much room for improvement in terms of the stationarity of support and reliability.
Invention content
In view of this, how the technical problem to be solved by the present invention is to make transportation or the packed and transported of unmanned plane
The stability and reliability of supporting structure are more easily improved simultaneously.
In order to solve the above-mentioned technical problem, of the invention to provide a kind of following folding rack structure, the folding branch
Frame structure includes：Pedestal；Bracket component, the bracket component be used to support one end of the pedestal and the bracket component with
The mode that can be dismantled is installed on the pedestal；One end of foldable assembly, the foldable assembly is installed on the bracket component, institute
The other end of foldable assembly is stated to be rotatablely connected with the pedestal, the foldable assembly can be rotated around the pedestal drive with
The pedestal is detached from the bracket component rotation of installation；And lock assembly, the lock assembly described in locking for folding
Component, the bracket component around the rotation of the pedestal can turn to the branch vertical with the pedestal with foldable assembly
Support state and the folded state parallel with the pedestal, the lock assembly is at least in the holding state and the rugosity
State limits rotation of the foldable assembly around the pedestal.
For above-mentioned folding rack structure, in one possible implementation, the foldable assembly include support element and
Rotating member, one end of the support element are sheathed on the bracket component and are existed with limiting the bracket component under the holding state
The other end of movement on the direction orthogonal with the length direction of the bracket component, the support element is pivotally attached to described turn
Moving part, and the rotating member is fixed on the pedestal.
For above-mentioned folding rack structure, in one possible implementation, the support element is relative to the holder
Component obliquely extends.
For above-mentioned folding rack structure, in one possible implementation, the rotating member is provided at least two
Locking hole, the lock assembly are set to the support element, and the lock assembly with the locking hole in a manner of it can be detached from
It is inserted into the locking hole, in the case where the lock assembly is inserted into the locking hole, the lock assembly limits the folding
Rotation of the component around the pedestal.
For above-mentioned folding rack structure, in one possible implementation, the support element has and the locking
The opposite sliding eye in hole, the lock assembly pass through the sliding eye to be inserted into the locking hole.
For above-mentioned folding rack structure, in one possible implementation, the folding rack structure further includes delaying
Stamping, the bolster are connect with the other end of the bracket component.
For above-mentioned folding rack structure, in one possible implementation, the pedestal has described for installing
The mounting groove of bracket component, the mounting groove are provided with internal thread, and one end of the bracket component is provided with external screw thread, the branch
Frame component can be threadedly coupled with the mounting groove.
In order to solve the above-mentioned technical problem, the present invention also provides a kind of unmanned plane, the unmanned plane includes above-mentioned technology
The folding rack structure of any one of scheme technical solution.
For above-mentioned unmanned plane, in one possible implementation, the pedestal of the folding rack structure is the nothing
Man-machine motor cabinet.
By using above-mentioned technical solution, the present invention provides a kind of folding rack structure and the folding rack knot is used
The unmanned plane of structure, this makes the transportation of unmanned plane or packed and transported more easily while can increase the stabilization of supporting structure
Property and reliability.
According to below with reference to the accompanying drawings becoming to detailed description of illustrative embodiments, other feature of the invention and aspect
It is clear.
Description of the drawings
Including in the description and the attached drawing of a part for constitution instruction and specification together illustrate the present invention's
Exemplary embodiment, and principle for explaining the present invention.
Fig. 1 shows the schematic diagram with the unmanned plane of folding rack structure according to an embodiment of the invention, wherein folding
Supporting structure is in holding state；
Fig. 2 shows the partial cutaway schematics of the unmanned plane in Fig. 1；
Fig. 3 shows another schematic diagram with the unmanned plane of folding rack structure according to an embodiment of the invention, wherein
Folding rack structure is in folded state.
Reference sign
10：Pedestal 20：Bracket component 30：Foldable assembly
301：Support element 302：Rotating member 40：Lock assembly
50：Bolster
Specific implementation mode
Below with reference to the attached drawing various exemplary embodiments that the present invention will be described in detail.Identical reference numeral table in attached drawing
Show functionally the same or similar element.Although the various aspects of embodiment are shown in the accompanying drawings, unless otherwise indicated, no
It must attached drawing drawn to scale.
Dedicated word " exemplary " means " being used as example, embodiment or illustrative " herein.Here as " exemplary "
Illustrated any embodiment should not necessarily be construed as preferred or advantageous over other embodiments.
In addition, in order to better illustrate the present invention, numerous details is given in specific implementation mode below.
It will be appreciated by those skilled in the art that without certain details, the present invention can equally be implemented.In some instances, for
Method well known to those skilled in the art, means are not described in detail, in order to highlight the purport of the present invention.
Fig. 1 shows the schematic diagram with the unmanned plane of folding rack structure according to an embodiment of the invention, wherein folding
Supporting structure is in holding state.As shown in Figure 1, the folding rack structure may include：Pedestal 10；Bracket component 20, holder
Component 20 is used to support pedestal 10 and one end of bracket component 20 is installed on pedestal 10 in a manner of it can dismantle；Foldable assembly
30, one end of foldable assembly 30 is installed on bracket component 20, and the other end and the pedestal 10 of foldable assembly 30 are rotatablely connected, folding group
Part 30 can rotate that the bracket component 20 for being detached from installation with pedestal 10 is driven to rotate together around pedestal 10；And lock assembly
40, lock assembly 40 is used for locking foldable assembly 30.
Wherein, bracket component 20 can be turned to pedestal 10 substantially with foldable assembly 30 around the rotation of pedestal 10
Vertical holding state and the folded state substantially parallel with pedestal 10, lock assembly 40 is at least in holding state and rugosity
State limits rotation of the foldable assembly 30 around pedestal 10.
The present embodiment does not limit the concrete type of pedestal 10.For example, pedestal 10 can be individually designed molding component, base
Seat 10 can also be a certain component installed included by carrier.It in actual application, can be according to folding rack structure
Installation environment selects suitable pedestal 10.
Further, it is for example round, oval, rectangular support that the bracket component 20 of the present embodiment, which can be section,
Bar is not restricted this.In addition, the present embodiment does not limit the making material of bracket component 20, such as can be aluminium alloy, carbon fiber
Dimension, titanium alloy etc..It in actual application, can be according to folding rack structure for toughness, elasticity, intensity and quality etc.
The related needs of parameter select different materials to make bracket component 20.
In one possible implementation, as shown in Fig. 2, pedestal 10 has the installation for mounting bracket assembly 20
Slot, mounting groove are provided with internal thread, and one end of bracket component 20 is provided with external screw thread, and bracket component 20 being capable of screw thread with mounting groove
Connection.
Specifically, during installation, bracket component 20 can be provided with to externally threaded one end alignment pedestal 10
Mounting groove realizes that bracket component 20 is installed on base then along the direction runing rest component 20 being threaded into tightening state
Seat 10.During folding, the direction runing rest that the bracket component 20 for being installed on pedestal 10 can be screwed out along screw thread
Component 20 is detached to mounting groove, realizes the separation of bracket component 20 and pedestal 10.Using the mounting means of above-mentioned threaded connection,
The installation and removal of bracket component 20 need not facilitate the installation and removal of folding rack structure by tool.
The present embodiment does not limit the specific mounting means between pedestal 10 and bracket component 20.Those skilled in the art answers
Pedestal 10 and bracket component 20 are used into the one kind being threadedly coupled in only numerous mounting means when being appreciated that.As this reality
An example of example is applied, for example, one end of bracket component 20 can be provided with elastic component and shackle member, the mounting groove of pedestal 10 can
To be provided with bayonet, the mode that clamping may be used in pedestal 10 and bracket component 20 is installed.
Further, the present embodiment does not limit the specific mounting means between bracket component 20 and foldable assembly 30, such as
Can be fixedly mounted, can also be movable installation.In actual application, between bracket component 20 and foldable assembly 30
Mounting means can be determined by the mounting means between pedestal 10 and bracket component 20.As an example of the present embodiment,
When pedestal 10 and bracket component 20 are using the mounting means being threadedly coupled, since bracket component 20 needs to revolve during the installation process
Enter the mounting groove of pedestal 10, therefore, movable installation may be used between bracket component 20 and foldable assembly 30.As this implementation
Another example of example, when pedestal 10 and bracket component 20 are using the mounting means being clamped, since bracket component 20 is being installed
Therefore fixation may be used between bracket component 20 and foldable assembly 30 in the mounting groove that pedestal 10 can be directly caught in the process
Installation or movable installation.
In one possible implementation, foldable assembly 30 includes support element 301 and rotating member 302, support element 301
One end is sheathed on bracket component 20 to limit bracket component 20 under holding state orthogonal with the length direction of bracket component 20
Direction on movement, the other end of support element 301 is pivotally attached to rotating member 302, and rotating member 302 is fixed on pedestal
10。
In one possible implementation, support element 301 obliquely extends relative to bracket component 20.
As shown in Figure 1, one end of support element 301 is the tablet with through-hole, bracket component 20 is passed through from through-hole, tablet
It is sheathed on the periphery of bracket component 20.The present embodiment does not limit the concrete shape of through-hole, such as can be round, rectangular etc..Into
One step, tablet can be full-closed structure.Using above-mentioned full-closed structure, under holding state if bracket component 20 by
To radial power, tablet can be with limit bracket component 20 in the fortune in all directions of 20 plane of bracket component (radial direction)
It is dynamic, have the function that stablize support.
As shown in Fig. 2, the other end of support element 301 is connect with rotating member 302.Wherein, rotating member 302 is fixed on pedestal
10.Rotating member 302 can be shaft, and support element 301 can be by the shaft of rotating member 302 around the certain angle of rotation of pedestal 10
Degree, such as 0~120 degree.
As an example of the present embodiment, bracket component 20 can be designed as the structure being tapered.For example, by holder
Component 20 is designed as the structure that either end starts to be tapered.Using the above-mentioned structure that is tapered so that bracket component 20 can
To be taken out from the through-hole of tablet.It can be convenient for changing in the case where bracket component 20 damages.
In one possible implementation, rotating member 302 is provided at least two locking holes, and lock assembly 40 is set to
Support element 301, lock assembly 40 are inserted into locking hole in a manner of it can be detached from locking hole；It is inserted into locking hole in lock assembly 40
In the case of, lock assembly 40 limits rotation of the foldable assembly 30 around pedestal 10.
In one possible implementation, there is support element 301 sliding eye opposite with locking hole, lock assembly 40 to wear
It crosses sliding eye and is inserted into locking hole.
There are two locking holes for the setting of rotating member 302 of the present embodiment.Wherein, a locking hole is used at bracket component 20
The locking support element 301 when holding state, another locking hole are used for the locking when bracket component 20 is in folded state and support
Part 301.Specifically, when lock assembly 40 is detached from locking hole, support element 301 can be rotated around rotating member 302.In locking group
When part 40 is inserted into locking hole, support element 302 keeps locking (cannot rotate).The concrete kind of the unlimited lock assembly 40 processed of the present embodiment
Type, such as can be knob plunger or other similar structures.
In the present embodiment, by locking hole and lock assembly 40, may be implemented folding rack structure holding state and
Folded state.It is in holding state for folding rack structure as shown in Figure 1, folding rack structure is illustrated in figure 3 and is in folding
State.Specifically, realizing that the process of folding or the installation of folding rack structure is as described below：
1, folding process：Since holding state (as shown in Figure 1), first by bracket component 20 out of, pedestal 10 mounting groove
It screws out.Then lock assembly 40 is pulled open, rotary support member 301, is further driven to bracket component 20 and lock assembly 40 turns to
Position as shown in Figure 3.Unclamp lock assembly 40 so that lock assembly 40 passes through sliding eye to be inserted into locking hole, is formed similar to such as
Fastening form shown in Fig. 2.After the front end of lock assembly 40 enters the locking hole (inclined hole) of shaft, support element 301 is locked
Only, reach folded state shown in Fig. 3, folding process is completed.
2, installation process：Since folded state (as shown in Figure 3), lock assembly 40 is first pulled open, rotary support member 301,
It is further driven to bracket component 20 and lock assembly 40 turns to position as shown in Figure 1.Then bracket component 20 is installed to
Pedestal 10 unclamps again lock assembly 40 so that lock assembly 40 passes through sliding eye to be inserted into locking hole, is formed as shown in Figure 2 tight
Solid formula.After the front end of lock assembly 40 enters the locking hole (inclined hole) of shaft, support element 301 is locked up, and reaches Fig. 1 institutes
The holding state shown, installation process are completed.
In one possible implementation, folding rack structure further includes bolster 50, bolster 50 and bracket component
20 other end connection.Bolster 50 can play the role of reducing to 20 impact endurance test shock of bracket component.
By using above-mentioned technical solution, the present embodiment provides a kind of folding rack structures.Wherein, folding rack structure
Installation and folding need not facilitate installation and folding, and save set-up time and cost by tool.In addition, above structure
The stability and reliability of folding rack structure can be increased.
The concrete structure and folding/installation process of folding rack structure according to the present invention have been carried out in detail above
Explanation.Unmanned plane according to the present invention is provided with above-mentioned folding rack structure.It is stored using the unmanned plane of the folding rack structure
Carrying or packed and transported can more easily increase the stability and reliability of unmanned plane simultaneously.Further, folding rack knot
The pedestal 10 of structure is the motor cabinet of unmanned plane.
By using above-mentioned technical solution, the present embodiment provides a kind of unmanned planes with folding rack structure.Wherein,
The installation and folding of folding rack structure need not facilitate installation and folding, and save set-up time and cost by tool.Folding
Folded supporting structure can reduce the occupied space of unmanned plane so that the transportation of unmanned plane or packed and transported are more convenient.In addition,
Above-mentioned folding rack structure can increase the stability and reliability of unmanned plane.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any
Those familiar with the art in the technical scope disclosed by the present invention, can easily think of the change or the replacement, and should all contain
Lid is within protection scope of the present invention.Therefore, protection scope of the present invention should be based on the protection scope of the described claims.
Claims (8)
1. a kind of folding rack structure, which is characterized in that the folding rack structure includes：
Pedestal；
Bracket component, the bracket component are used to support side of the one end of the pedestal and the bracket component can dismantle
Formula is installed on the pedestal；
Foldable assembly, one end of the foldable assembly are installed on the bracket component, the other end of the foldable assembly with it is described
Pedestal is rotatablely connected, and the foldable assembly can rotate to drive the branch for being detached from installation with the pedestal around the pedestal
Frame component rotates；And
Lock assembly, the lock assembly are used for foldable assembly described in locking,
The bracket component around the rotation of the pedestal can turn to the branch vertical with the pedestal with foldable assembly
Support state and the folded state parallel with the pedestal, the lock assembly is at least in the holding state and the rugosity
State limits rotation of the foldable assembly around the pedestal；Wherein, the foldable assembly includes support element and rotating member,
One end of the support element be sheathed on the bracket component with limited under the holding state bracket component with
Movement on the orthogonal direction of the length direction of the bracket component, the other end of the support element are pivotally attached to the rotation
Part,
And
The rotating member is fixed on the pedestal, and the rotating member is provided at least two locking holes, the lock assembly setting
In the support element, the lock assembly is inserted into the locking hole in a manner of it can be detached from the locking hole.
2. folding rack structure according to claim 1, which is characterized in that
The support element obliquely extends relative to the bracket component.
3. folding rack structure according to claim 1, which is characterized in that
In the case where the lock assembly is inserted into the locking hole, the lock assembly limits the foldable assembly around described
The rotation of pedestal.
4. folding rack structure according to claim 3, which is characterized in that
There is the support element sliding eye opposite with the locking hole, the lock assembly to pass through described in sliding eye insertion
Locking hole.
5. folding rack structure according to any one of claim 1 to 4, which is characterized in that the folding rack structure
Further include bolster, the bolster is connect with the other end of the bracket component.
6. folding rack structure according to any one of claim 1 to 4, which is characterized in that
There is the pedestal mounting groove for installing the bracket component, the mounting groove to be provided with internal thread, the holder
One end of component is provided with external screw thread, and the bracket component can be threadedly coupled with the mounting groove.
7. a kind of unmanned plane, which is characterized in that the unmanned plane includes folding rack according to any one of claims 1 to 6
Structure.
8. unmanned plane according to claim 7, which is characterized in that the pedestal of the folding rack structure is the unmanned plane
Motor cabinet.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610825738 | 2016-09-14 | ||
| CN2016108257380 | 2016-09-14 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106394864A CN106394864A (en) | 2017-02-15 |
| CN106394864B true CN106394864B (en) | 2018-10-26 |
Family
ID=58083305
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611068395.4A Active CN106394864B (en) | 2016-09-14 | 2016-11-29 | Folding rack structure and unmanned plane |
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| Country | Link |
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| CN (1) | CN106394864B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023272445A1 (en) * | 2021-06-28 | 2023-01-05 | 深圳市大疆创新科技有限公司 | Frame, stand, and unmanned aerial vehicle |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203047530U (en) * | 2012-08-21 | 2013-07-10 | 深圳市大疆创新科技有限公司 | Aircraft foot stand and aircraft with same |
| CN105197228A (en) * | 2015-10-30 | 2015-12-30 | 深圳市大疆创新科技有限公司 | Undercarriage and unmanned aerial vehicle |
| CN205293068U (en) * | 2016-01-08 | 2016-06-08 | 浙江天马行空创新科技有限公司 | Undercarriage device that can receive and release automatically |
| CN205311893U (en) * | 2015-10-27 | 2016-06-15 | 杭州海康威视数字技术股份有限公司 | Unmanned aerial vehicle and folding bracket mechanism |
| CN206202662U (en) * | 2016-09-14 | 2017-05-31 | 北京博瑞空间科技发展有限公司 | Folding rack structure and unmanned plane |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA3098531C (en) * | 2013-05-15 | 2022-11-15 | Autel Robotics Usa Llc | Compact unmanned rotary aircraft |
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2016
- 2016-11-29 CN CN201611068395.4A patent/CN106394864B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203047530U (en) * | 2012-08-21 | 2013-07-10 | 深圳市大疆创新科技有限公司 | Aircraft foot stand and aircraft with same |
| CN205311893U (en) * | 2015-10-27 | 2016-06-15 | 杭州海康威视数字技术股份有限公司 | Unmanned aerial vehicle and folding bracket mechanism |
| CN105197228A (en) * | 2015-10-30 | 2015-12-30 | 深圳市大疆创新科技有限公司 | Undercarriage and unmanned aerial vehicle |
| CN205293068U (en) * | 2016-01-08 | 2016-06-08 | 浙江天马行空创新科技有限公司 | Undercarriage device that can receive and release automatically |
| CN206202662U (en) * | 2016-09-14 | 2017-05-31 | 北京博瑞空间科技发展有限公司 | Folding rack structure and unmanned plane |
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| Publication number | Publication date |
|---|---|
| CN106394864A (en) | 2017-02-15 |
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