CN208602713U - A kind of protection mechanism of unmanned plane wing - Google Patents
A kind of protection mechanism of unmanned plane wing Download PDFInfo
- Publication number
- CN208602713U CN208602713U CN201821240852.8U CN201821240852U CN208602713U CN 208602713 U CN208602713 U CN 208602713U CN 201821240852 U CN201821240852 U CN 201821240852U CN 208602713 U CN208602713 U CN 208602713U
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- CN
- China
- Prior art keywords
- ring
- support plate
- protection mechanism
- support sleeve
- unmanned plane
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Abstract
The utility model provides a kind of protection mechanism of unmanned plane wing, including bending support plate, horizontal positioning plate, and flat thread set slides locating rod, spring, apical ring and plum blossom threaded rod；The head end position support of the flight support plate is equipped with rotor driving motor at one, and the left and right sides symmetric support of its front position has locating slot at two；The sliding locating rod extends through the inside that vertical support sleeve at three is inserted under semicircle top sheet and protrusion by vertical support sleeve at three at three, and the end that locating rod is slided at three is provided with a prescription shape baffle, this three prescriptions shape baffle can be pressed against on intermediate buffering ring in vertical support sleeve downslide at three, the setting of buffering stand at the utility model six, when intermediate buffering ring is by the impact for sliding locating rod at three, impact force can be transferred to buffering stand at six by it, U-bend batten can carry out snubber to impact force with elastic bending deflection about buffering stand at six at this time.
Description
Technical field
The utility model belongs to the mating protective device technical field of unmanned plane, more specifically, in particular to it is a kind of nobody
The protection mechanism of machine wing.
Background technique
Unmanned plane will receive the shadow of the sundries such as aerial fallen leaves, branch, the paper to fly up and food bag in flight course
It rings, once these sundries are involved in the rotor of unmanned plane, just winds rotor, gently then unmanned plane slowly falls, heavy then unmanned plane is straight
Connect it is stuck fall, cause destructive damage；Meanwhile unmanned plane manipulator is easy to appear various controls during manipulation and asks
Topic, for example unmanned plane blade is hurted sb.'s feelings, unmanned plane blade collides building or trees or aerial cable etc., so inventing a kind of protection
Device is particularly important to guarantee its flight safety just.
It is found in conjunction with prior art people, although existing equipment is able to carry out conventional use, but it is in reality
Exist in the application of border, buffer structure design is not reasonable, is mostly merely able to carry out the buffer protection of single, mechanism body is caused to exist
Easily occur broken when by very big impact force, rotor damage probability is caused to increase, in addition the charge and discharge operations of mechanism body are not more
Just the problem of.
Then, in view of this, being studied improvement for existing structure and missing, a kind of guarantor of unmanned plane wing is provided
Mechanism is protected, to achieve the purpose that with more more practical value.
Summary of the invention
In order to solve the above-mentioned technical problem, the utility model provides a kind of protection mechanism of unmanned plane wing, existing to solve
There is the design of wing protection mechanism buffer structure not reasonable, is mostly merely able to carry out the buffer protection of single, causes mechanism body
Easily occur when by very big impact force broken, rotor damage probability is caused to increase, in addition the charge and discharge operations of mechanism body are more
Inconvenient problem.
The purpose and effect of the protection mechanism of the utility model unmanned plane wing, are reached by technological means in detail below:
A kind of protection mechanism of unmanned plane wing, including flight support plate, locating slot, rotor driving motor, base ring delay
Rush bracket, curved support plate, intermediate buffering ring, vertical support sleeve, bending support plate, horizontal positioning plate, flat thread set, sliding
Locating rod, spring, apical ring and plum blossom threaded rod；The head end position support of the flight support plate is equipped with rotor driving electricity at one
Machine, and the left and right sides symmetric support of its front position has locating slot at two；The vertical support sleeve is in rectangle two at three
Head semicircle is excessively arranged, and circular array support sleeve is set on intermediate buffering ring and base ring, and vertical support sleeve and bottom at three
Ring is fixed together；The sliding locating rod is extended through through the semicircle top sheet of vertical support sleeve at three and convex at three
It is inserted in the inside of vertical support sleeve at three down out, and the end that locating rod is slided at three is provided with a prescription shape baffle, this
Three prescription shape baffles can be pressed against on intermediate buffering ring in vertical support sleeve downslide at three；The horizontal positioning plate and two prescriptions
Shape thread bush just corresponding front and rear sides for being inserted against locating slot at two in this, and plum blossom threaded rod sequentially passes through horizontal positioning at two
On plate two at jack, locating slot and lock onto the inside of two prescription shape thread bush at two, and then protection mechanism ontology is locked
Tight card support is positioned on flight support plate.
Further, annular array support is provided with buffering stand at six, and this between the intermediate buffering ring and base ring
Buffering stand U-bend batten connection combination about is formed at six.
Further, circular array is provided with the curved support plate supported downwards at three on the apical ring, and this is at three
The tail end of curved support plate links together with base ring screw locking.
Further, the top screw locking of the sliding locating rod is supported by apical ring at one at three, and slided at three it is fixed
As soon as spring at being arranged on the bar of position, this at three spring be folded at apical ring and three between vertical support sleeve by compression.
Further, hanging brace has bending at one to support on the inner side end of the vertical support sleeve lower half portion at three
Plate, wherein the tail end injection molded of front side bending support plate is provided with horizontal positioning plate at one, the left and right two of this horizontal positioning plate
End position symmetrically offers two and goes out jack, and the end of bending support plate shapes and is provided with a prescription shape at the two of the left and right sides
Thread bush.
Compared with prior art, the utility model has the following beneficial effects:
The utility model passes through spring at three, curved support plate cooperation support use can at buffering stand and three at six
Buffering dilution three times is carried out to the vertical direction toward impact power acted on apical ring, and then impact failure dynamics is made greatly to drop bottom, is reduced
The probability for causing rotor to damage because protective cover is broken, and pass through horizontal positioning plate and two prescription shape thread bush, protection mechanism sheet
Body, which can be realized, facilitates sliding plug disassembly assembly.
Detailed description of the invention
Fig. 1 is the utility model installation site relation schematic diagram.
Fig. 2 is the utility model installation site relationship three dimensional structure diagram.
Fig. 3 is the utility model structure diagram.
Fig. 4 is the utility model three dimensional structure diagram.
In figure, the corresponding relationship of component names and accompanying drawing number are as follows:
1- flight support plate, 101- locating slot, 2- rotor driving motor, 3- base ring, 301- buffering stand, 4- arc branch
Fagging, 5- intermediate buffering ring, the vertical support sleeve of 6-, 601- bending support plate, the horizontal positioning plate of 6011-, 6012- flat thread
Set, 7- slide locating rod, 701- spring, 8- apical ring, 9- plum blossom threaded rod.
Specific embodiment
The embodiments of the present invention is described in further detail with reference to the accompanying drawings and examples.Following embodiment
For illustrating the utility model, but cannot be used to limit the scope of the utility model.
In the description of the present invention, unless otherwise indicated, the meaning of " plurality " is two or more；Term
The orientation of the instructions such as "upper", "lower", "left", "right", "inner", "outside", " front end ", " rear end ", " head ", " tail portion " or position are closed
System is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of describing the present invention and simplifying the description, rather than
The device or element of indication or suggestion meaning must have a particular orientation, be constructed and operated in a specific orientation, therefore cannot
It is construed as a limitation of the present invention.In addition, term " first ", " second ", " third " etc. are used for description purposes only, and cannot
It is interpreted as indication or suggestion relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
To be mechanical connection, it is also possible to be electrically connected；It can be directly connected, it can also be indirectly connected through an intermediary.For this
For the those of ordinary skill in field, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
Embodiment:
As shown in attached drawing 1 to attached drawing 4:
The utility model provides a kind of protection mechanism of unmanned plane wing, including flight support plate 1, locating slot 101, rotation
Wing driving motor 2, base ring 3, buffering stand 301, curved support plate 4, intermediate buffering ring 5, vertical support sleeve 6, bending support plate
601, horizontal positioning plate 6011, flat thread set 6012 slides locating rod 7, spring 701, apical ring 8 and plum blossom threaded rod 9；It is described
The head end position support of flight support plate 1 is equipped with rotor driving motor 2 at one, and the left and right sides of its front position is symmetrically propped up
Support has locating slot 101 at two；The vertical support sleeve 6 is excessively arranged in rectangle both ends semicircle at three, circular array
Support sleeve is set on intermediate buffering ring 5 and base ring 3, and vertical support sleeve 6 is fixed together with base ring 3 at three；Three places
It states sliding locating rod 7 and extends through to be inserted at three under semicircle top sheet and protrusion by vertical support sleeve 6 at three and prop up vertically
The inside of support set 6, and the end that locating rod 7 is slided at three is provided with a prescription shape baffle, this three prescriptions shape baffle can edge
The vertical downslide of support sleeve 6 is pressed against on intermediate buffering ring 5 at three；The horizontal positioning plate 6011 and two prescription shape thread bush 6012
With regard to the corresponding front and rear sides for being inserted against locating slot 101 at two in this, and plum blossom threaded rod 9 sequentially passes through horizontal positioning plate at two
On 6011 two at jack, locating slot 101 and lock onto the inside of two prescription shape thread bush 6012 at two, and then protection mechanism
Ontology be locked card support be positioned on flight support plate 1.
Wherein, annular array support is provided with buffering stand 301 at six, and this between the intermediate buffering ring 5 and base ring 3
At six buffering stand 301 about U-bend batten connection combination formed, when intermediate buffering ring 5 by come from and three
When the impact of place's sliding locating rod 7, impact force can be transferred to buffering stand 301 at six, at this time buffering stand 301 at six
About U-bend batten can with elastic bending deflection to impact force carry out snubber.
Wherein, circular array is provided with the curved support plate 4 supported downwards at three on the apical ring 8, and this arc at three
The tail end of shape support plate 4 links together with 3 screw locking of base ring, and curved support plate 4 can bear side impact, to rotation
The wing carries out lateral support protection.
Wherein, the top screw locking of the sliding locating rod 7 is supported by apical ring 8 at one at three, and positioning is slided at three
As soon as spring 701 at being arranged on bar 7, this at three spring 701 by compression be folded at apical ring 8 and three vertical support sleeve 6 it
Between, when unmanned plane rollover lands, apical ring 8 is hit first contiguously plays support protective action in face of rotor, in the process
Apical ring 8 will drive slide the downslide of spring 701 at the compression of locating rod 7 three at three under the influence of the impact force, and then spring 701 at three
Can elastic rebound the first snubber is carried out to impact force, and arc at buffering stand 301 and three at spring 701, six at three
The cooperation support of shape support plate 4, which uses to the vertical direction toward impact power acted on apical ring 8 buffer three times, to be diluted, and is reduced and is impacted
Power reduces the broken probability of apical ring 8 to collsion damage caused by apical ring 8, so make apical ring 8 can with it is more efficiently to rotor into
Row support protection.
Wherein, hanging brace has bending support plate at one on the inner side end of vertical 6 lower half portion of support sleeve at three
601, wherein the tail end injection molded of front side bending support plate 601 is provided with horizontal positioning plate 6011 at one, this horizontal positioning plate
6011 left and right ends positional symmetry offer two go out jack, and at the two of the left and right sides bending support plate 601 end at
Shape is provided with a prescription shape thread bush 6012, and by horizontal positioning plate 6011 and two prescription shape thread bush 6012, protection mechanism can
Realization facilitates sliding plug disassembly assembly, only by the insertion of plum blossom threaded rod 9 locking at two or need to unclamp to take out and can be completed to guarantor
The disassembling operations for protecting mechanism, this greatly simplifies protection mechanism ontologies to load and unload process, improves the using flexible of protection mechanism
Property.
The specifically used mode and effect of the present embodiment:
Horizontal positioning plate 6011 and two prescription shape thread bush 6012 are inserted against with regard to correspondence in this by the utility model assemble flow
The front and rear sides of locating slot 101 at two then sequentially pass through plum blossom threaded rod 9 at two at two on horizontal positioning plate 6011
Jack locating slot 101 and lock onto the inside of two prescription shape thread bush 6012 at two, and protection mechanism ontology can be made to be locked
Card support is positioned on flight support plate 1.
The embodiments of the present invention are given for the purpose of illustration and description, and are not exhaustively or to incite somebody to action
The utility model is limited to disclosed form.Many modifications and variations are aobvious and easy for the ordinary skill in the art
See.Embodiment was chosen and described in order to better illustrate the principle and practical application of the utility model, and makes this field
Those of ordinary skill it will be appreciated that the utility model to designing various embodiments suitable for specific applications with various modifications.
Claims (5)
1. a kind of protection mechanism of unmanned plane wing, it is characterised in that: the protection mechanism of the unmanned plane wing includes flight support
Plate (1), locating slot (101), rotor driving motor (2), base ring (3), buffering stand (301), curved support plate (4) are intermediate
Buffering ring (5), vertical support sleeve (6), bending support plate (601), horizontal positioning plate (6011), flat thread set (6012) are sliding
Dynamic locating rod (7), spring (701), apical ring (8) and plum blossom threaded rod (9)；The head end position of the flight support plate (1) supports
Rotor driving motor (2) at one are installed, and the left and right sides symmetric support of its front position there are locating slot at two (101)；
The vertical support sleeve (6) is excessively arranged in rectangle both ends semicircle at three, and circular array support sleeve is set to intermediate buffering
On ring (5) and base ring (3), and vertical support sleeve (6) is fixed together with base ring (3) at three；The sliding positioning at three
Bar (7) extends through and is inserted in vertical support sleeve (6) at three under semicircle top sheet and protrusion by vertical support sleeve (6) at three
Inside, and at three slide locating rod (7) end be provided with a prescription shape baffle, this three prescriptions shape baffle can be at three
Vertical support sleeve (6) downslide is pressed against on intermediate buffering ring (5)；The horizontal positioning plate (6011) and two prescription shape thread bush
(6012) with regard to the corresponding front and rear sides for being inserted against locating slot (101) at two in this, and plum blossom threaded rod (9) sequentially passes through cross at two
It sets jack at two on positioning plate (6011), locating slot (101) and lock onto the interior of two prescription shape thread bush (6012) at two
Portion, so protection mechanism ontology be locked card support be positioned on flight support plate (1).
2. the protection mechanism of unmanned plane wing as described in claim 1, it is characterised in that: the intermediate buffering ring (5) and base ring
(3) annular array support is provided with buffering stand at six (301) between, and this buffering stand (301) U about at six
Type is bent batten connection combination and is formed.
3. the protection mechanism of unmanned plane wing as described in claim 1, it is characterised in that: circular array on the apical ring (8)
Be provided with the curved support plate (4) supported downwards at three, and the tail end of this curved support plate (4) at three with base ring (3) screw
Locking links together.
4. the protection mechanism of unmanned plane wing as described in claim 1, it is characterised in that: sliding locating rod (7) at three
Top screw locking is supported by apical ring at one (8), and is slided on locating rod (7) at three and be arranged with spring at one (701), this three
Place spring (701) is just folded at apical ring (8) and three between vertical support sleeve (6) by compression.
5. the protection mechanism of unmanned plane wing as described in claim 1, it is characterised in that: at three under the vertical support sleeve (6)
Equal hanging brace has bending support plate (601) at one on the inner side end of half part, wherein the tail end note of front side bending support plate (601)
It is moulded into shape and is provided with horizontal positioning plate (6011) at one, the left and right ends positional symmetry of this horizontal positioning plate (6011) offers two
Jack out, and the end of bending support plate (601) shapes and is provided with a prescription shape thread bush (6012) at the two of the left and right sides.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821240852.8U CN208602713U (en) | 2018-08-02 | 2018-08-02 | A kind of protection mechanism of unmanned plane wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821240852.8U CN208602713U (en) | 2018-08-02 | 2018-08-02 | A kind of protection mechanism of unmanned plane wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208602713U true CN208602713U (en) | 2019-03-15 |
Family
ID=65670340
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821240852.8U Expired - Fee Related CN208602713U (en) | 2018-08-02 | 2018-08-02 | A kind of protection mechanism of unmanned plane wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208602713U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108910029A (en) * | 2018-08-02 | 2018-11-30 | 滨州学院 | A kind of protection mechanism of unmanned plane wing |
-
2018
- 2018-08-02 CN CN201821240852.8U patent/CN208602713U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108910029A (en) * | 2018-08-02 | 2018-11-30 | 滨州学院 | A kind of protection mechanism of unmanned plane wing |
| CN108910029B (en) * | 2018-08-02 | 2021-06-04 | 滨州学院 | Protection mechanism of unmanned aerial vehicle wing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190315 Termination date: 20190802 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |