CN206569265U - A kind of safe fast-demounting blade protective cover and unmanned plane - Google Patents
A kind of safe fast-demounting blade protective cover and unmanned plane Download PDFInfo
- Publication number
- CN206569265U CN206569265U CN201720264034.0U CN201720264034U CN206569265U CN 206569265 U CN206569265 U CN 206569265U CN 201720264034 U CN201720264034 U CN 201720264034U CN 206569265 U CN206569265 U CN 206569265U
- Authority
- CN
- China
- Prior art keywords
- protective cover
- demounting
- blade
- elastic
- main body
- 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
- Blinds (AREA)
Abstract
The utility model provides a kind of safe fast-demounting blade protective cover, including protective cover main body and elastic arm lock, and the protective cover main body is the open hollow cover body structure of a side, and the elastic arm lock is arranged on the opening surface of the protective cover main body；The protective cover main body is latched by the elastic arm and is detachably connected with the notch of the fuselage side wall of unmanned plane, wraps up unmanned plane horn and blade and its Power Component.The utility model is simple in construction; omnibearing protection is carried out to unmanned plane; and the unmanned plane with the safe fast-demounting blade protective cover can realize landing of taking off on hand; the protection comprehensive to user; and ensure that the enough flying powers of unmanned plane; and protective cover can also be removed in the state of safety is not considered, lifting blade power ensures the flight time of aircraft.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, and in particular to a kind of safe fast-demounting blade protective cover and unmanned plane.
Background technology
The power of multi-rotor unmanned aerial vehicle in the market is all to drive propeller blade to produce by motor, and propeller is in height
The power of strength is produced when speed is rotated, while the blade of high-speed rotation can bring very big potential safety hazard to user.In order to
Protecting user to obtain unmanned plane on the market at present all can be with an easy blade anticollision cover, but this blade anticollision cover rises not
To comprehensive protecting effect.
The content of the invention
The purpose of this utility model is to provide a kind of safe fast-demounting blade protective cover, simple in construction, 360 degrees omnidirection pair
Unmanned plane and user are protected, and the unmanned plane with the safe fast-demounting blade protective cover can realize drop of taking off on hand
Fall, the protection comprehensive to user, and protective cover can also be removed in the state of safety is not considered, lift blade power
Ensure the flight time of aircraft.
In order to solve the above-mentioned technical problem, the utility model provides a kind of safe fast-demounting blade protective cover, including protective cover
Main body and elastic arm lock, the protective cover main body are the open hollow cover body structure of a side, and the elastic arm lock is set
In on the opening surface of the protective cover main body；
The protective cover main body is latched detachable with the notch of the fuselage side wall of unmanned plane by the elastic arm
Connection, parcel unmanned plane horn and blade and its Power Component.
It is preferred that, the non-opening surface region of the protective cover main body is the netted hollow out being interconnected to constitute by multiple ribs
Structure.
Using the beneficial effect of above-mentioned preferred scheme：By said structure design, make unmanned plane horn and blade and its dynamic
Power component is isolated by the protective cover main body with human body and foreign object, and directly safe oar can be grabbed by hand in blade rotary work process
Leaf protective cover, not only increases the security of unmanned plane operation, is also that unmanned plane horn and blade and its Power Component are provided
Protection, simultaneously because the protective cover agent structure is frivolous, it is ensured that the enough flying power spaces of unmanned plane.
It is preferred that, the protective cover body interior centre position is horizontally arranged with support transverse slat, and the support transverse slat is by institute
State protective cover main body and be separated into one horn of parcel and blade and its Power Component in two hollow cavities, each hollow cavity.
Using the beneficial effect of above-mentioned preferred scheme：Support transverse slat to support the formation of protective cover main body, prevent in the guarantor that takes
During shield, the top and bottom of protective cover main body can be moved by extruding touches blade and its Power Component, each middle cavity
The horn and blade and its Power Component of a unmanned plane are can be inserted into body.
It is preferred that, the notch includes open slot and two through holes being symmetricly set at the top of the open slot.
It is preferred that, the elastic arm lock includes support frame and lock, and support frame as described above is arranged on the protective cover main body
Opening surface, and its top and bottom be fixedly connected respectively with the top and bottom of the protective cover main body, lateral surface is provided with
The lock；The lock insertion open slot is simultaneously detachably connected with two through holes.
Using the beneficial effect of above-mentioned preferred scheme：Realize being detachably connected for protective cover and fuselage.
It is preferred that, the lock includes elastic pressing piece, two fixed plates and two connecting plates, two fixed plates
Level is fixedly installed on the both sides of support frame as described above lateral surface respectively for one end, and opened with support frame as described above one one side of formation
The area pressed of mouth, the side of the other end is fixedly connected by two connecting plates with the elastic pressing piece respectively, the elasticity
Pressing piece is arranged in the area pressed, and detachable with two through holes by being moved up and down in the area pressed
Connection.
Using the beneficial effect of above-mentioned preferred scheme：Realize being detachably connected for protective cover and fuselage.
It is preferred that, the elastic pressing piece includes elastic press section and two elastic transverse slats, two elastic transverse slats
Two outer end side surfaces are fixedly connected by two connecting plates with two fixed plates respectively, above two medial extremitys straight up
It is provided with the top of the press section that can be pressed down on, two elastic transverse slats and is symmetrically arranged with what is be adapted with two through holes
Two buckles；Two fixed plates, two elastic transverse slats and two connecting plates insert the open slot together
In, two buckles are linked together with two necks by way of buckle, press the elastic press section, two
The buckle is taken apart with two necks.
Using the beneficial effect of above-mentioned preferred scheme：Realize being detachably connected for protective cover and fuselage.
It is preferred that, two track structures corresponding with two connecting plates, two are provided with the open slot internal symmetry
Individual adjacent fixed plate and elastic transverse slat slip into institute by connecting plate therebetween on corresponding track structure respectively
State in open slot.
Using the beneficial effect of above-mentioned preferred scheme：Two adjacent fixed plates and elastic transverse slat slidably pass in and out described open
Mouth groove, dismounting more facilitates.
It is preferred that, each track structure includes being correspondingly arranged at two tracks at the top and bottom of open slot.
Using the beneficial effect of above-mentioned preferred scheme：Two adjacent fixed plates and elastic transverse slat is facilitated to slide turnover described
It is more smooth when open slot.
It is preferred that, the open slot may be configured as two, and be respectively connected together by two connecting plates two are adjacent
Fixed plate and elastic transverse slat are inserted in two corresponding open slots respectively.
Using the beneficial effect of above-mentioned preferred scheme：According to the structure sum of the concrete condition designed openings groove of unmanned plane
Amount, makes structure more firm.
It is preferred that, two elastic transverse slats or two fixed plates or two connecting plates are just to open slot
End surface symmetric be fixedly installed two spring structures, during inserting the open slot with the lock, the opening
The inwall of groove constantly two spring structures of extruding.
Using the beneficial effect of above-mentioned preferred scheme：After the lock with neck unblock, the elastic force meeting of the spring
The protective cover is gently flicked, two buckles can leave the lower section of two necks, without worrying two cards
Button can and two necks be connected together again, can now without artificially pressing the elastic press section always with hand
The side or top of directly crawl guard take off the protective cover along the direction of horn, convenient operation.
It is preferred that, the bottom of the elastic pressing piece, which is provided with, only stops structure, presses the elastic press section, described only to stop
Elastic pressing piece is stated in Structural lock residence, and the elastic press section is pressed again, and the structure of only stopping unclamps the elastic pressing piece.
Using the beneficial effect of above-mentioned preferred scheme：By compression elasticity press section, elastic pressing piece is only stopped structure pinning, nothing
Method is resetted, you can easily capture protective cover side or top, and protective cover is taken out along horn direction.After taking-up, bullet is pressed
Property press section unblock, elastic pressing piece can be resetted, when assembling protective cover again, and horizontal sliding protective cover main body 1 is matched somebody with somebody with fuselage neck
Conjunction is blocked, you can complete assembling, safe ready.
Connected respectively on a kind of unmanned plane, including fuselage and two pairs of horns for being arranged at fuselage left and right side, each horn
Have in blade and its Power Component, in addition to two safe fast-demounting blade protective covers, two safe fast-demounting blade protective covers
Chamber wraps up two pairs of horns and blade and its Power Component respectively, and is detachably connected with fuselage.
After such scheme, the unmanned plane with the safe fast-demounting blade protective cover passes through above-mentioned in the utility model
Structure design, its operationally, the safe fast-demounting blade protective cover can 360 degrees omnidirection unmanned plane is protected, have
The unmanned plane of the safe fast-demounting blade protective cover can realize landing of taking off on hand, the protection comprehensive to user, to making
User provides very safe use environment, can meet the demand for security of crawl aircraft manually.In addition, the protective cover is netted
Hollow out design ensure that the enough flying power spaces of unmanned plane, and protective cover can also take in the state of safety is not considered
Under, lifting blade power ensures the flight time of aircraft.Protective cover is attached and separated by elastic arm lock with fuselage, is adopted
No screw designs are taken, the Quick Release of protective cover is realized, with stronger practicality.
Brief description of the drawings
Fig. 1 is the disassembled state dimensional structure diagram of the utility model unmanned plane and safe fast-demounting blade protective cover；
Fig. 2 is the assembling dimensional structure diagram of the utility model unmanned plane and a safe fast-demounting blade protective cover；
Fig. 3 is the assembling dimensional structure diagram of the utility model unmanned plane and two safe fast-demounting blade protective covers；
Fig. 4 is the dimensional structure diagram of the utility model safe fast-demounting blade protective cover；
Fig. 5 is the decomposition texture schematic diagram of the utility model safe fast-demounting blade protective cover；
The dimensional structure diagram that Fig. 6 latches for the elastic arm in the utility model safe fast-demounting blade protective cover；
Fig. 7 is the slot mechanism structural representation that the utility model is arranged on fuselage；
Fig. 8 is that the decomposition texture of the utility model unmanned plane and the elastic arm lock in safe fast-demounting blade protective cover is illustrated
Figure；
Fig. 9 is the safe fast-demounting blade protective cover dimensional structure diagram that the utility model has spring structure；
Figure 10 is the decomposition texture schematic diagram for the safe fast-demounting blade protective cover that the utility model has spring structure.
Embodiment
The utility model is illustrated below according to accompanying drawing illustrated embodiment.This time disclosed embodiment can consider in institute
It is to illustrate to have aspect, without limitation.Scope of the present utility model is not limited by the explanation of implementation below, only by right
Shown in the scope of claim, and including having all changes in the same meaning and right with right
Shape.
As shown in Figure 1 to Figure 3, the installation of the safe fast-demounting blade protective cover and unmanned plane of the utility model embodiment one is whole
Body structural representation, including protective cover main body 1 and elastic arm lock 2, the protective cover main body 1 is the open hollow cover of a side
Body structure, the elastic arm lock 2 is arranged on the opening surface of the protective cover main body 1；The protective cover main body 1 is by described
Elastic arm lock 2 is detachably connected with the notch 3 of the fuselage side wall of unmanned plane, wrap up unmanned plane horn and blade and its
Power Component.
Protective cover main body described in the present embodiment 1 can be ellipse or square, or other shapes.
Wherein, the protective cover main body 1 includes the center of upper lid, lower cover and a side opening, the upper lid and lower cover point
The top and bottom of the center are not arranged on, form the hollow cavity of a side opening.
The non-opening surface region of the protective cover main body 1 is the netted engraved structure being interconnected to constitute by multiple ribs,
The line space design for the rib that the non-opening surface region of protective cover main body 1 is set meets ergonomics, and energy within 12mm
Ensure that unmanned plane there are enough flying powers.By said structure design, make unmanned plane horn and blade and its Power Component logical
Cross the protective cover main body with human body and foreign object to isolate, both effectively meet the power power effect demand of unmanned plane in itself, while
User provides very safe use environment, can meet the demand for security of crawl aircraft manually, be also unmanned plane horn and oar
Leaf and its Power Component provide protection, simultaneously because the protective cover agent structure is frivolous, it is ensured that unmanned plane flying enough
Action edge space.
In the course of the work, it is necessary to which when assembling the safe fast-demounting blade protective cover, protective cover main body 1 described in horizontal sliding is led to
The notch 3 for crossing elastic arm lock 2 and fuselage side wall is connected, can by a pair of the horns and blade of unmanned plane side and its
Power Component is positioned in a protective cover main body 1 together, and unmanned plane can be in takeoff and landing on hand；Needing to remove described
During safe fast-demounting blade protective cover, it will can be unlocked between elastic arm lock 2 and the notch 3 of fuselage side wall, so
The safe fast-demounting blade protective cover is taken off along the direction of horn afterwards.
In addition, the bosom position of protective cover main body 1 can be horizontally arranged with support transverse slat 14, the support transverse slat 14
The protective cover main body 1 is separated into two hollow cavities, each hollow cavity and wraps up a horn and blade and its power
Component.Support transverse slat to support the formation of protective cover main body, prevent when taking protective cover, the top and bottom of protective cover main body meet with
It can be moved to extruding and touch blade and its Power Component, the horn and oar of a unmanned plane are can be inserted into each hollow cavity
Leaf and its Power Component.
With reference to shown in Fig. 4 to Fig. 7, the dimensional decomposition structure diagram of implementation two of the present utility model.Specific such as Fig. 7 is simultaneously tied
Close shown in Fig. 8, the notch 3 includes open slot 31 and is symmetricly set on two through holes at the top of open slot 31
32。
Specifically as shown in Figures 4 to 7, the elastic arm lock 2 includes support frame 21 and lock 22, and support frame as described above 21 is set
The opening surface in the protective cover main body 1 is put, and top and bottom of its top and bottom respectively with the protective cover main body 1 are consolidated
Fixed connection, lateral surface is provided with the lock 22；The insertion of lock 22 open slot 31 simultaneously can with two through holes 32
Dismounting connection.
The lock 22 includes elastic pressing piece 221, two fixed plates 222 and two connecting plates 226, and two described solid
Level is fixedly installed on the both sides of the lateral surface of support frame as described above 21 respectively for one end of fixed board 222, and is formed with support frame as described above 21
The open area pressed 227 of one one side, the side of the other end passes through two connecting plates 226 and the elastic pressing piece respectively
221 are fixedly connected, and the elastic pressing piece 221 is arranged in the area pressed 227, and by the area pressed 227
Interior up and down motion is detachably connected with two through holes 32.
The elastic pressing piece 221 includes elastic press section 223 and two elastic transverse slats 224, two elastic transverse slats
224 two outer end side surfaces are fixedly connected by two connecting plates 226 with two fixed plates 222 respectively, two medial extremitys
It is provided with the press section 223 that can be pressed down on straight up above, two elastic tops of transverse slat 224 are symmetrically arranged with and two
Two buckles 225 that the individual through hole 32 is adapted.
In the course of the work, a pair of horns and blade and its Power Component by unmanned plane side are being needed to be positioned over together
When in one safe fast-demounting blade protective cover, protective cover main body 1 described in horizontal sliding, by two fixed plates 222, two bullets
Property transverse slat 224 and two connecting plates 226 are inserted in the open slot 31 together, two buckles 225 and two institutes
State neck 32 to link together by way of buckle, unmanned plane can be in takeoff and landing on hand；Needing to remove the peace
During full Quick Release blade protective cover, the elastic press section 223 is pressed, two buckles 225 are taken apart with two necks 32,
Then the elastic press section 223 is pressed always and takes off the safe fast-demounting blade protective cover along the direction of horn.
Embodiment of the present utility model three as shown in Figure 8, is provided with and two companies in the internal symmetry of open slot 31
Two corresponding track structures 33 of fishplate bar 226, two adjacent fixed plates 222 and elastic transverse slat 224 respectively by the two it
Between connecting plate 226 slipped on corresponding track structure 33 in the open slot 31, wherein, each track structure includes
The adjacent fixed plate 222 of 34 two, two tracks and elastic transverse slat 224 for being correspondingly arranged at the top and bottom of open slot 31 are slided
The open slot 31 is passed in and out, dismounting more facilitates.
In addition, the open slot 31 may be configured as two, two be respectively connected together by two connecting plates 226 are adjacent
Fixed plate 222 and elastic transverse slat 224 insert respectively in two corresponding open slots 31.Specifically can be according to the specific feelings of unmanned plane
Condition designed openings groove, structure is more firm.
Example IV of the present utility model as shown in Figure 9 and Figure 10, in two elastic transverse slats 224 or two institutes
State fixed plate 222 or two connecting plates 226 and two spring structures just are fixedly installed to the end surface symmetric of open slot 31
227, during the insertion of lock 22 open slot 31, described in the inwall constantly extruding two of the open slot 31
Spring structure 227, after two buckles 225 and two necks 32 are taken apart, the elastic force of the spring is by the protection
Cover main body is flicked.
In the course of the work, a pair of horns and blade and its Power Component by unmanned plane side are being needed to be positioned over together
When in one safe fast-demounting blade protective cover, protective cover main body 1 described in horizontal sliding, by two fixed plates 222, two institutes
State elastic transverse slat 224 and two connecting plates 226 are inserted in the open slot 31 together, two buckles 225 and two
The individual neck 32 is linked together by way of buckle, while the spring in the fixed column can be with two fixations
The movement of plate 222, two the elastic transverse slats 224 and two connecting plates 226, constantly extrudes the interior of the open slot 31
Wall, unmanned plane can be in takeoff and landing on hand；When needing to remove the safe fast-demounting blade protective cover, the elasticity is pressed
Press section 223, two buckles 225 are taken apart with two necks 32, and then the elastic force of the spring can be by the protection
Cover main body 1 is gently flicked, and described two buckles 225 can leave the lower section of two necks 32, now without pressing always
The elastic press section 223 is pressed to prevent two buckles 225 to be connected together again with two necks 32, directly will
The safe fast-demounting blade protective cover is taken off along the direction of horn, convenient operation.
Embodiment five, structure is only stopped alternatively, it is also possible to be provided with the bottom of the elastic pressing piece 221（Do not show in figure
Go out）, the elastic press section 223 is pressed, described only stopping Structural lock residence states elastic pressing piece 221, and the elasticity is pressed again
Press section 223, the structure of only stopping unclamps the elastic pressing piece 221.Only prior art can be used by stopping structure described in specific
In common ball pen or mechanical pencil only stop structure, realize and press compression elasticity press section 223, the elastic quilt of pressing piece 221
Pin, it is impossible to reset, again by compression elasticity press section 223, the elastic pressing piece 221 resets.
In the course of the work, a pair of horns and blade and its Power Component by unmanned plane side are being needed to be positioned over together
When in one safe fast-demounting blade protective cover, protective cover main body 1 described in horizontal sliding, by two fixed plates 222, two bullets
Property transverse slat 224 and two connecting plates 226 are inserted in the open slot 31 together, two buckles 225 and two institutes
State neck 32 to link together by way of buckle, unmanned plane can be in takeoff and landing on hand；Needing to remove the peace
During full Quick Release blade protective cover, the elastic press section 223 is pressed, described only stopping Structural lock residence states elastic pressing piece 221, institute
Stating elastic pressing piece 221 can not reset, and now can easily capture protective cover side or top, prolong horn direction and take out guarantor
Shield, without pressing the elastic press section 223 always to prevent two buckles 225 and two necks 32 secondary card again
It is connected together.Take out after the safe fast-demounting blade protective cover, unlocked again by compression elasticity press section 223, now the bullet
Property pressing piece 221 can reset.When assembling safe fast-demounting blade protective cover again, protective cover main body 1 described in horizontal sliding and fuselage card
Groove, which coordinates, can complete assembling, safe ready.
Embodiment six, with reference to Fig. 1 to Figure 10, a kind of unmanned plane, including fuselage 4 and two couple for being arranged at fuselage left and right side
Blade and its Power Component 6, in addition to the safe fast-demounting blade protective cover, two are connected on horn 5, each horn
Two pairs of horns 5 and blade and its Power Component 6 are wrapped up in individual safe fast-demounting blade protective cover inner chamber respectively, and removable with fuselage
Connection is unloaded, two pairs of horns 5 and blade and its Power Component 6 are detachably arranged in two safe fast-demounting blade protective covers
Horn 5 and a pair of blades and its Power Component 6 described in a pair are wrapped up in chamber, each safe fast-demounting blade protective cover inner chamber.
In the course of the work, it is necessary to when assembling the safe fast-demounting blade protective cover, protective cover main body 1 described in horizontal sliding, institute
Assembling can be completed by stating elastic arm lock and coordinating with the neck on fuselage, by the two pairs of horns and blade of unmanned plane both sides and its dynamic
Power component is respectively placed in two protective cover cavitys together, and unmanned plane can be in takeoff and landing on hand；Needing to remove institute
When stating safe fast-demounting blade protective cover, it will can be unlocked between elastic arm lock 2 and the notch 3 of fuselage side wall,
Then the safe fast-demounting blade protective cover is taken off along the direction of horn.The safe fast-demounting blade protective cover can 360
Degree is comprehensive to be protected to unmanned plane, and provides the use environment of safety to user, can be met and be captured aircraft manually
Demand for security.In addition, the netted hollow out design of the protective cover main body 1 ensure that the enough flying power spaces of unmanned plane, and
And protective cover can also be removed in the state of safety is not considered, lifting blade power ensures the flight time of aircraft.
Those skilled in the art will readily occur to its of the present invention after considering specification and putting into practice invention disclosed herein
Its embodiment.The application be intended to the present invention any modification, purposes or adaptations, these modifications, purposes or
Person's adaptations follow the general principle of the present invention and including undocumented common knowledge or usual in the art
Technological means.Description and embodiments be considered only as it is exemplary, true scope and spirit of the invention by following right will
Ask and point out.
It should be appreciated that the invention is not limited in the precision architecture for being described above and being shown in the drawings, and
And various modifications and changes can be being carried out without departing from the scope.The scope of the present invention is only limited by appended claim.
Claims (13)
1. a kind of safe fast-demounting blade protective cover, it is characterised in that latched including protective cover main body and elastic arm, the protective cover
Main body is the open hollow cover body structure of a side, and the elastic arm lock is arranged on the opening surface of the protective cover main body；
The protective cover main body is latched by the elastic arm and is detachably connected with the notch of the fuselage side wall of unmanned plane,
Wrap up unmanned plane horn and blade and its Power Component.
2. a kind of safe fast-demounting blade protective cover as claimed in claim 1, it is characterised in that the non-of protective cover main body opens
Mouth face region is the netted engraved structure being interconnected to constitute by multiple ribs.
3. a kind of safe fast-demounting blade protective cover as claimed in claim 1, it is characterised in that in the protective cover body interior
Between position be horizontally arranged with support transverse slat, the protective cover main body is separated into two hollow cavities by the support transverse slat, each
A horn and blade and its Power Component are wrapped up in hollow cavity.
4. a kind of safe fast-demounting blade protective cover as claimed in claim 1, it is characterised in that the notch includes opening
Groove and two through holes being symmetricly set at the top of the open slot.
5. a kind of safe fast-demounting blade protective cover as claimed in claim 4, it is characterised in that the elastic arm lock includes branch
Support and lock, support frame as described above are arranged on the opening surface of the protective cover main body, and its top and bottom is protected with described respectively
It is fixedly connected at the top and bottom of boot main body, lateral surface is provided with the lock；The lock insertion open slot and with
Two through holes are detachably connected.
6. a kind of safe fast-demounting blade protective cover as claimed in claim 5, it is characterised in that the lock includes elasticity and pressed
Part, two fixed plates and two connecting plates, level is fixedly installed on support frame as described above respectively for one end of two fixed plates
The both sides of lateral surface, and the area pressed open with support frame as described above one one side of formation, the side of the other end passes through respectively
Two connecting plates are fixedly connected with the elastic pressing piece, and the elastic pressing piece is arranged in the area pressed, and is passed through
Move up and down and be detachably connected with two through holes in the area pressed.
7. a kind of safe fast-demounting blade protective cover as claimed in claim 6, it is characterised in that the elastic pressing piece includes bullet
Property press section and two elastic transverse slats, two outer end side surfaces of two elastic transverse slats pass through two connecting plates and two respectively
The fixed plate is fixedly connected, and is provided with the press section that can be pressed down on, two bullets above two medial extremitys straight up
Property transverse slat at the top of be symmetrically arranged with two buckles being adapted with two through holes；Two fixed plates, two bullets
Property transverse slat and two connecting plates are inserted in the open slot together, and two buckles and two necks pass through card
The mode of button links together, and presses the elastic press section, and two buckles are taken apart with two necks.
8. a kind of safe fast-demounting blade protective cover as claimed in claim 7, it is characterised in that in the open slot internal symmetry
Two track structures corresponding with two connecting plates are provided with, two adjacent fixed plates and elastic transverse slat are respectively by the two
Between connecting plate slipped on corresponding track structure in the open slot.
9. a kind of safe fast-demounting blade protective cover as claimed in claim 8, it is characterised in that each track structure includes correspondence
It is arranged on two tracks at the top and bottom of open slot.
10. a kind of safe fast-demounting blade protective cover as claimed in claim 7, it is characterised in that the open slot may be configured as
Two, two adjacent fixed plates being respectively connected together by two connecting plates and elastic transverse slat insert respectively two it is corresponding
In open slot.
11. a kind of safe fast-demounting blade protective cover as claimed in claim 7, it is characterised in that two elastic transverse slats or
Two fixed plates of person or two connecting plates are just fixedly installed two spring structures to the end surface symmetric of open slot,
During the open slot being inserted with the lock, inwall constantly two spring structures of extruding of the open slot.
12. a kind of safe fast-demounting blade protective cover as claimed in claim 7, it is characterised in that the bottom of the elastic pressing piece
Portion, which is provided with, only stops structure, presses the elastic press section, described only stopping Structural lock residence states elastic pressing piece, and institute is pressed again
Elastic press section is stated, the structure of only stopping unclamps the elastic pressing piece.
13. connected respectively on a kind of unmanned plane, including fuselage and two pairs of horns for being arranged at fuselage left and right side, each horn
There are blade and its Power Component, it is characterised in that the also safe fast-demounting oar including two as described in any one of claim 1 to 12
Two pairs of horns and blade and its Power Component are wrapped up in leaf protective cover, two safe fast-demounting blade protective cover inner chambers respectively, and
It is detachably connected with fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720264034.0U CN206569265U (en) | 2017-03-17 | 2017-03-17 | A kind of safe fast-demounting blade protective cover and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720264034.0U CN206569265U (en) | 2017-03-17 | 2017-03-17 | A kind of safe fast-demounting blade protective cover and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206569265U true CN206569265U (en) | 2017-10-20 |
Family
ID=60054798
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720264034.0U Active CN206569265U (en) | 2017-03-17 | 2017-03-17 | A kind of safe fast-demounting blade protective cover and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206569265U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108033003A (en) * | 2018-01-11 | 2018-05-15 | 深圳市中联讯科技有限公司 | A kind of aircraft protective cover and aircraft |
| CN108058823A (en) * | 2018-01-26 | 2018-05-22 | 湖州职业技术学院 | A kind of unmanned plane rotor protective device |
| CN108974337A (en) * | 2018-07-23 | 2018-12-11 | 深圳市中联讯科技有限公司 | A kind of aircraft protective cover |
| CN110667834A (en) * | 2019-11-18 | 2020-01-10 | 湖南捷飞科技有限公司 | Wing protective structure for unmanned aerial vehicle |
| WO2020038356A1 (en) * | 2018-08-24 | 2020-02-27 | Hangzhou Zero Zero Technology Co., Ltd. | Detachable protection structure for unmanned aerial systems |
| CN111874244A (en) * | 2020-07-28 | 2020-11-03 | 东南大学 | Novel unmanned aerial vehicle paddle safety cover |
| WO2021077252A1 (en) * | 2019-10-21 | 2021-04-29 | 深圳市大疆创新科技有限公司 | Blade protection device and aircraft |
| CN115158681A (en) * | 2022-08-30 | 2022-10-11 | 南京开天眼无人机科技有限公司 | Protective mesh enclosure for flight rotor wing, application and forming process thereof |
-
2017
- 2017-03-17 CN CN201720264034.0U patent/CN206569265U/en active Active
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108033003A (en) * | 2018-01-11 | 2018-05-15 | 深圳市中联讯科技有限公司 | A kind of aircraft protective cover and aircraft |
| CN108058823A (en) * | 2018-01-26 | 2018-05-22 | 湖州职业技术学院 | A kind of unmanned plane rotor protective device |
| CN108058823B (en) * | 2018-01-26 | 2024-05-10 | 湖州职业技术学院 | Unmanned aerial vehicle rotor wing protection device |
| CN108974337A (en) * | 2018-07-23 | 2018-12-11 | 深圳市中联讯科技有限公司 | A kind of aircraft protective cover |
| WO2020038356A1 (en) * | 2018-08-24 | 2020-02-27 | Hangzhou Zero Zero Technology Co., Ltd. | Detachable protection structure for unmanned aerial systems |
| US11530038B2 (en) | 2018-08-24 | 2022-12-20 | Hangzhou Zero Zero Technology Co., Ltd | Detachable protection structure for unmanned aerial systems |
| WO2021077252A1 (en) * | 2019-10-21 | 2021-04-29 | 深圳市大疆创新科技有限公司 | Blade protection device and aircraft |
| CN110667834A (en) * | 2019-11-18 | 2020-01-10 | 湖南捷飞科技有限公司 | Wing protective structure for unmanned aerial vehicle |
| CN111874244A (en) * | 2020-07-28 | 2020-11-03 | 东南大学 | Novel unmanned aerial vehicle paddle safety cover |
| CN115158681A (en) * | 2022-08-30 | 2022-10-11 | 南京开天眼无人机科技有限公司 | Protective mesh enclosure for flight rotor wing, application and forming process thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206569265U (en) | A kind of safe fast-demounting blade protective cover and unmanned plane | |
| CN106184711B (en) | The wingfold mechanism of variant aircraft | |
| CN108945478A (en) | The parachute opener of unmanned plane | |
| CN106672205B (en) | A kind of large-scale change sweepback supersonic aircraft layout | |
| CN103523223B (en) | Transverse course control system and transverse course control method for flying wing configuration | |
| CN205837216U (en) | A kind of light-duty stealthy electromagnetism unlocks drag parachute housing structure | |
| CN108583842A (en) | A kind of composite material light lid mechanism for film covering | |
| CN206456545U (en) | It is a kind of can fast folding multi-rotor unmanned aerial vehicle | |
| CN103600844A (en) | Combined flight vehicle generating greater lift force | |
| DE102014218041A1 (en) | Protective helmet, in particular motorcycle helmet, with pivoting and removable chin part | |
| CN205753153U (en) | A kind of pressure relief device of switch cabinet | |
| CN208201707U (en) | A kind of gate passage beating door | |
| CN215270836U (en) | Helmet | |
| CN205607009U (en) | 80 degrees refrigerator door baffle plate structures of burden | |
| CN209617447U (en) | A kind of twin vertical fin medium transport aircraft | |
| CN206801707U (en) | Rectification shade assembly, nacelle and fanjet | |
| CN105756444B (en) | Front cover for vehicle lockset | |
| CN108313303A (en) | A kind of unmanned plane umbrella and its de- umbrella device | |
| CN206926808U (en) | Unmanned plane undercarriage | |
| CN202227837U (en) | Quick-release lock | |
| CN105667788B (en) | A kind of unmanned plane | |
| CN206163564U (en) | Battery quick assembly disassembly positioning locking device | |
| CN204527612U (en) | A kind of jet mechanism that can realize aircraft roll | |
| CN201197786Y (en) | Hyperbaric oxygen chamber with top door | |
| CN109292078A (en) | A kind of airplane landing gear assemblies of the anti-low energy damage of new energy |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |