CN209382257U - A kind of weatherability unmanned plane paddle components - Google Patents
A kind of weatherability unmanned plane paddle components Download PDFInfo
- Publication number
- CN209382257U CN209382257U CN201822248393.4U CN201822248393U CN209382257U CN 209382257 U CN209382257 U CN 209382257U CN 201822248393 U CN201822248393 U CN 201822248393U CN 209382257 U CN209382257 U CN 209382257U
- Authority
- CN
- China
- Prior art keywords
- saddle
- blade
- rotor
- unmanned plane
- weatherability
- 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.)
- Expired - Fee Related
Links
Landscapes
- Wind Motors (AREA)
Abstract
The utility model provides a kind of weatherability unmanned plane paddle components, comprising: mounting bracket, rotor, mounting rod；The upside of mounting bracket is arranged in rotor, and rotor is bolted with mounting bracket and is connected；Mounting rod is located at the middle part of rotor；The upside of rotor is arranged in saddle, and saddle is connected with mounting rod by fitting mode；Fixing axle is located at the middle part of saddle, and fixing axle is an integral structure with saddle；The top of saddle is arranged in blade, and blade is connected with saddle by the way that fixing axle is chimeric；The top of saddle is arranged in fixing piece, and fixing piece is connected with saddle by inserting mode；The upper end of rotor is arranged in nut, and nut is connected with mounting rod by threaded engagement；The improvement to existing apparatus is crossed, which has blade convenient for disassembly and assembly, is able to carry out the replacement of single blade, and maintenance cost is low, and the advantages of can prevent erosion by wind and rain, thus the problem of effective solution existing apparatus and deficiency.
Description
Technical field
The utility model relates to unmanned plane blade technical fields, more specifically, more particularly to a kind of weatherability unmanned plane
Paddle components.
Background technique
For unmanned plane as a kind of novel remote sensing monitoring platform, flight operation intelligence degree is high, can be autonomous by prebriefed pattern
Other operations are flown, imaged or carried out, the fields such as surveying and drawing, taking photo by plane using extremely wide, but existing unmanned plane blade has
There is following deficiency:
Existing unmanned plane blade is mostly one-piece construction, includes there are two blade or three blades, when wherein one more
When a blade damages, then needs entirety to be replaced, cause maintenance cost higher, and the replacement process of blade is cumbersome, it is time-consuming to take
Power.
In view of this, being studied improvement for existing problem, a kind of weatherability unmanned plane paddle components are provided, it is intended to
By the technology, achievees the purpose that solve the problems, such as and improve practical value.
Utility model content
The purpose of this utility model is to provide a kind of weatherability unmanned plane paddle components, to solve in above-mentioned background technique
The existing unmanned plane blade proposed is mostly one-piece construction, includes that there are two blade or three blades, when one of them more
When blade damages, then needs entirety to be replaced, cause maintenance cost higher, and the replacement process of blade is cumbersome, it is time-consuming and laborious
The problem of and deficiency.
To achieve the above object, the utility model provides a kind of weatherability unmanned plane paddle components, by skill in detail below
Art means are reached:
A kind of weatherability unmanned plane paddle components, comprising: mounting bracket, rotor, mounting rod, saddle, fixing axle, blade,
Fixing piece, nut；The upside of mounting bracket is arranged in the rotor, and rotor is bolted with mounting bracket and is connected；
The mounting rod is located at the middle part of rotor；The upside of rotor is arranged in the saddle, and saddle and mounting rod pass through fitting mode
It is connected；The fixing axle is located at the middle part of saddle, and fixing axle is an integral structure with saddle；The blade is arranged in saddle
Top, and blade and saddle are connected by the way that fixing axle is chimeric；The fixing piece is arranged in the top of saddle, and fixing piece with
Saddle is connected by inserting mode；The upper end of rotor is arranged in the nut, and nut passes through threaded engagement phase with mounting rod
Connection.
As advanced optimizing for the technical program, saddle described in a kind of weatherability unmanned plane paddle components of the utility model
Cylindrical structure, the top of saddle is provided with semi-circular recesses at three, and is provided with fixing axle in the groove on saddle top.
It is fixed described in a kind of weatherability unmanned plane paddle components of the utility model as advanced optimizing for the technical program
Axis semicircular in shape column structure, and circular hole is provided in the middle part of fixing axle.
Root is advanced optimized as the technical program, paddle described in a kind of weatherability unmanned plane paddle components of the utility model
The inner end of leaf is round connecting column, and is provided with semi-circular through hole in the middle part of the round connecting column of blade.
As advanced optimizing for the technical program, blade described in a kind of weatherability unmanned plane paddle components of the utility model
It is provided with three altogether, and blade and saddle and fixing axle spray corrosion-resistant finishes.
It is fixed described in a kind of weatherability unmanned plane paddle components of the utility model as advanced optimizing for the technical program
Part structure in the form of a circular plate, and cylinder at three is provided on the downside of fixing piece.
As advanced optimizing for the technical program, installed described in a kind of weatherability unmanned plane paddle components of the utility model
The lower partial cross section of bar is in long ellipticity, and the top of the oblong groove mounting rod of corresponding mounting rod is provided in the middle part of saddle
End is provided with screw thread.
Due to the application of the above technical scheme, the utility model has the advantage that compared with prior art
1, a kind of weatherability unmanned plane paddle components of the utility model are by setting separate type at three for unmanned plane blade
Blade, and this at three blade the top of rotor is mounted on by saddle, and be locked by fixing piece and nut, should
Blade has convenient for disassembly and assembly, and the advantages of being able to carry out the replacement of single blade when blade damages, and safeguards time saving and energy saving and cost
It is low.
2, a kind of weatherability unmanned plane paddle components of the utility model on the surface of blade and saddle and fixing axle by spraying
Weather proof coating is applied, it can prevent wind and rain steam from impacting to paddle components using pure phenolic resin coating, effectively prolong
The paddle components service life is grown.
3, the utility model has blade convenient for disassembly and assembly, is able to carry out single blade by the improvement to existing apparatus
Replacement, maintenance cost is low, and the advantages of can prevent erosion by wind and rain, so that effective solution the utility model is in background technique
The problem of being proposed in one and deficiency.
Detailed description of the invention
The attached drawing constituted part of this application is used to provide a further understanding of the present invention, the utility model
Illustrative embodiments and their description are not constituteed improper limits to the present invention for explaining the utility model.In attached drawing
In:
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the configuration schematic diagram of the utility model；
Fig. 3 is the blade and saddle attachment structure schematic diagram of the utility model.
In figure: mounting bracket 1, rotor 2, mounting rod 3, saddle 4, fixing axle 5, blade 6, fixing piece 7, nut 8.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.
It should be noted that in the description of the present invention, unless otherwise indicated, the meaning of " plurality " is two or two
More than a；The instructions such as term " on ", "lower", "left", "right", "inner", "outside", " front end ", " rear end ", " head ", " tail portion "
Orientation or positional relationship is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of description the utility model and simplification
Description, rather than the device or element of indication or suggestion meaning must have a particular orientation, constructed and grasped with specific orientation
Make, therefore should not be understood as limiting the present invention.
In addition, term " first ", " second ", " third " etc. are used for description purposes only, it is not understood to indicate or imply
Relative importance.
Meanwhile in the description of the present invention, unless otherwise clearly defined and limited, term " connected ", " connection "
It 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 be mechanical connect
It connects, is also possible to be electrically connected；It can be directly connected, it can also be indirectly connected through an intermediary.For the general of this field
For logical technical staff, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
Referring to Figure 1 to Fig. 3, the utility model provides a kind of particular technique embodiment party of weatherability unmanned plane paddle components
Case:
A kind of weatherability unmanned plane paddle components, comprising: mounting bracket 1, rotor 2, mounting rod 3, saddle 4, fixing axle 5,
Blade 6, fixing piece 7, nut 8；The upside of mounting bracket 1 is arranged in rotor 2, and rotor 2 is bolted with mounting bracket 1
It is connected；Mounting rod 3 is located at the middle part of rotor 2；The upside of rotor 2 is arranged in saddle 4, and saddle 4 and mounting rod 3 pass through fitting
Mode is connected；Fixing axle 5 is located at the middle part of saddle 4, and fixing axle 5 is an integral structure with saddle 4；The setting of blade 6 is being held in the palm
The top of platform 4, and blade 6 is connected with saddle 4 by the way that fixing axle 5 is chimeric；The top of saddle 4 is arranged in fixing piece 7, and fixed
Part 7 is connected with saddle 4 by inserting mode；The upper end of rotor 2 is arranged in nut 8, and nut 8 and mounting rod 3 pass through screw thread
It screws and is connected.
Specifically, the cylindrical structure of saddle 4, the top of saddle 4 is provided with semi-circular recesses at three, and 4 top of saddle
Groove in be provided with fixing axle 5, for connecting blade.
Specifically, 5 semicircular in shape column structure of fixing axle, and the middle part of fixing axle 5 is provided with circular hole, for being connected and fixed
Part.
Specifically, the inner end of blade 6 is round connecting column, and semicircle is provided in the middle part of the round connecting column of blade 6
Through-hole, for being connected and fixed axis and being limited.
Specifically, the blade 6 is provided with three altogether, and blade 6 and saddle 4 and fixing axle 5 spray corrosion-resistant finishes,
Pure phenolic resin coating prolongs the service life for preventing erosion by wind and rain paddle components.
Specifically, the structure in the form of a circular plate of fixing piece 7, and the downside of fixing piece 7 is provided with cylinder at three, it is solid for connecting
Dead axle limits blade.
Specifically, the lower partial cross section of mounting rod 3 is in long ellipticity, and the middle part of saddle 4 is provided with corresponding mounting rod 3
Oblong groove, the installation for saddle 4 limit, and the top of mounting rod 3 is provided with screw thread, is used for coupling nut 8.
Specific implementation step:
When using the device, rotor 2 is bolted to mounting bracket 1, mounting bracket 1 connects unmanned plane main body,
Later in 3 sets of the mounting rod upper saddles 4 on 2 top of rotor, then blade 6 is fixed by the semicircle of inner end connecting column and saddle 4
Axis 5 is fitting to connection, and then the cylinder of 7 lower end of fixing piece is inserted at three in the circular hole of fixing axle 5, finally by nut 8 and installation
The connection of bar 3 is fixed part 7, and when the blade needs repairing or replaces, nut 8 is screwed off, removes fixing piece 7, later
It can carry out the fast quick-detach of blade 6；The device has convenient for disassembly and assembly, the low advantage of paddle components maintenance cost.
In summary: a kind of weatherability unmanned plane paddle components, by setting separate type at three for unmanned plane blade
Blade, and this at three blade the top of rotor is mounted on by saddle, and be locked by fixed plate and nut, should
Blade has convenient for disassembly and assembly, and the advantages of being able to carry out the replacement of single blade when blade damages, and safeguards time saving and energy saving and cost
It is low；By spraying weather proof coating on the surface of blade, saddle and fixing axle, it can prevent wind and rain steam from making to paddle components
At influence, the paddle components service life is effectively extended, solving existing unmanned plane blade is mostly one-piece construction, includes more
There are two blade or three blades, when the damage of one of blade, then needs it is whole replaced, cause maintenance cost compared with
Height, and the replacement process of blade is cumbersome, time-consuming and laborious problem.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (7)
1. a kind of weatherability unmanned plane paddle components, comprising: mounting bracket (1), mounting rod (3), saddle (4), is consolidated rotor (2)
Dead axle (5), blade (6), fixing piece (7), nut (8)；It is characterized by: the rotor (2) is arranged in the upper of mounting bracket (1)
Side, and rotor (2) is bolted with mounting bracket (1) and is connected；The mounting rod (3) is located at the middle part of rotor (2)；Institute
It states saddle (4) to be arranged in the upside of rotor (2), and saddle (4) is connected with mounting rod (3) by fitting mode；The fixation
Axis (5) is located at the middle part of saddle (4), and fixing axle (5) is an integral structure with saddle (4)；The blade (6) is arranged in saddle
(4) top, and blade (6) is connected with saddle (4) by the way that fixing axle (5) are chimeric；The fixing piece (7) is arranged in saddle
(4) top, and fixing piece (7) is connected with saddle (4) by inserting mode；The nut (8) is arranged in the upper of rotor (2)
End, and nut (8) is connected with mounting rod (3) by threaded engagement.
2. a kind of weatherability unmanned plane paddle components according to claim 1, it is characterised in that: the saddle (4) is in circle
Column structure, the top of saddle (4) is provided with semi-circular recesses at three, and is provided with fixation in the groove on saddle (4) top
Axis (5).
3. a kind of weatherability unmanned plane paddle components according to claim 1, it is characterised in that: the fixing axle (5) is in
Semicircle column structure, and circular hole is provided in the middle part of fixing axle (5).
4. a kind of weatherability unmanned plane paddle components according to claim 1, it is characterised in that: the blade (6) it is interior
End is round connecting column, and is provided with semi-circular through hole in the middle part of the round connecting column of blade (6).
5. a kind of weatherability unmanned plane paddle components according to claim 1, it is characterised in that: the blade (6) sets altogether
Three are equipped with, and blade (6) and saddle (4) and fixing axle (5) spray corrosion-resistant finishes.
6. a kind of weatherability unmanned plane paddle components according to claim 1, it is characterised in that: the fixing piece (7) is in
Circular plate structure, and cylinder at three is provided on the downside of fixing piece (7).
7. a kind of weatherability unmanned plane paddle components according to claim 1, it is characterised in that: the mounting rod (3)
Lower partial cross section is in long ellipticity, and the oblong groove of corresponding mounting rod (3), mounting rod are provided in the middle part of saddle (4)
(3) top is provided with screw thread.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822248393.4U CN209382257U (en) | 2018-12-29 | 2018-12-29 | A kind of weatherability unmanned plane paddle components |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822248393.4U CN209382257U (en) | 2018-12-29 | 2018-12-29 | A kind of weatherability unmanned plane paddle components |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209382257U true CN209382257U (en) | 2019-09-13 |
Family
ID=67862807
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822248393.4U Expired - Fee Related CN209382257U (en) | 2018-12-29 | 2018-12-29 | A kind of weatherability unmanned plane paddle components |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209382257U (en) |
-
2018
- 2018-12-29 CN CN201822248393.4U patent/CN209382257U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209382257U (en) | A kind of weatherability unmanned plane paddle components | |
| CN203233099U (en) | Tool for mounting bird scarer on live-line | |
| CN207962524U (en) | A kind of lampshade mounting device of passenger plane wing navigation lights | |
| CN208053454U (en) | A kind of front wheel housing assembly | |
| CN106368978A (en) | Centrifugal pump impeller positioning and rapid bearing replacing mechanism, impeller positioning method and bearing replacing method | |
| CN209526191U (en) | A kind of medium resonant rod support construction | |
| CN209080026U (en) | The scalable integrated stand of new-energy automobile All-in-One equipment and automobile | |
| CN208925041U (en) | A kind of anticollision plant protection drone spray head convenient for adjusting height and water spray size | |
| CN202903267U (en) | Flowmeter with rotatable meter head | |
| CN207914724U (en) | A kind of bolt thread prosthetic device | |
| CN207490090U (en) | Light weight radar antenna | |
| CN211160230U (en) | Novel combined anode tube bundle device | |
| CN205175683U (en) | Piston spouts target device that beats of hook | |
| CN205127867U (en) | Leaf structure is changed to agitator | |
| CN208795031U (en) | A kind of novel coal gas air cooling tower | |
| CN219417129U (en) | Insulator hydrophobicity testing arrangement based on unmanned aerial vehicle control | |
| CN217554468U (en) | SAW corrodes basket | |
| CN208381493U (en) | A kind of general-purpose aircraft support of pipelines | |
| CN214034530U (en) | Novel corrosion-resistant fluorine carbon aluminium veneer system | |
| CN211167423U (en) | A remote control unmanned aerial vehicle for high altitude liquid medicine sprays | |
| CN219552184U (en) | Insulator hydrophobicity test system based on unmanned aerial vehicle control | |
| CN208417989U (en) | A kind of oblique angle positioning pin | |
| CN208278320U (en) | A kind of detachable unmanned plane propeller arrangement | |
| CN211724725U (en) | Condensing equipment that single-effect evaporator used | |
| CN209293565U (en) | A kind of metal hand rail for facilitating maintenance to replace |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190913 Termination date: 20201229 |