CN208102333U - The double-deck rotor wings frame in a kind of unmanned plane - Google Patents
The double-deck rotor wings frame in a kind of unmanned plane Download PDFInfo
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- CN208102333U CN208102333U CN201820649416.XU CN201820649416U CN208102333U CN 208102333 U CN208102333 U CN 208102333U CN 201820649416 U CN201820649416 U CN 201820649416U CN 208102333 U CN208102333 U CN 208102333U
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- loading plate
- carrier
- rotor
- double
- unmanned plane
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Abstract
The utility model discloses rotor wings frames double-deck in a kind of unmanned plane；After the utility model is by improving, which can realize the double-deck rotor setting, and from structure composition, which has multibilayer rotor fixed cell, upper carrier, lower carrier；Every group of bilayer rotor fixed cell is separately fixed between carrier and lower carrier, then the rotor wings frame self structure is simple, is found by test, and protection obtained and carrying dynamics are higher after rotor wings frame molding；And the cooperation of bolts and nuts can be used between rotor wings frame each section to assemble, so that easy to be quick when disassembly is with assembling.
Description
Technical field
The utility model relates to rotors in unmanned plane to protect field, be especially the double-deck rotor wings frame in a kind of unmanned plane.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Unmanned plane can be divided into a variety of classification such as fixed-wing, rotor, the umbrella wing, flapping wing according to flying method.With nothing
The development and maturation of line technology, control technology and mechanical part, unmanned plane can carry a variety of loads and complete various complicated
Business, such as air observation and shooting, the delivery etc. of package and cargo.As most simple and intuitive stability contorting structure quadrotor disappears
Expense grade unmanned plane gradually shows one's promises in electronic consumer markets.However, unmanned plane can inevitably be touched in flight course it is various
Building, branch or other articles, thus will cause the damage of unmanned plane rotor, the operation of subsequent unmanned plane is impacted；Institute
It is carried with needing corresponding flight support frame in unmanned plane.
It is found by retrieval, the utility model of patent No. CN201420838024.X discloses a kind of quadrotor drone machine
Frame and quadrotor drone.Wherein, quadrotor drone rack includes fuselage and four horns, and whole is in I-shaped, the machine
A horn is each side stretched out in body rear and front end to it.Quadrotor drone includes the quadrotor drone rack.
The utility model is by using I-shaped rack construction, so that posture of the quadrotor drone in flight course is more steady
It is fixed, solve the problems, such as existing quadrotor drone because the unreasonable cause flight of rack construction is unstable, to reduce quadrotor
Unmanned plane the application error in fields such as surveys and draws, takes photo by plane in remote sensing, improves the service precision in surveying and drawing, taking photo by plane and expands
The application field of quadrotor drone.
The utility model of patent No. CN201520550192.3 discloses a kind of unmanned plane rotor fender bracket and unmanned plane, with
Solve the problems, such as that current rotor fender bracket causes unmanned plane volume to increase and dismount trouble.The unmanned plane of the utility model revolves
Wing fender bracket includes fender bracket ontology, is removably disposed in one end end on unmanned plane horn far from drone body, end
Portion is provided with propeller, and perpendicular to the surface of fender bracket ontology, fender bracket ontology can avoid completely for the rotation axis of propeller
Unmanned plane propeller contacts in flight course with any of human body, it is ensured that personal safety；Meanwhile, it is capable to suffer unmanned plane
When meeting different directions shock, bears simultaneously to absorb certain energy by flexible deformation, reduce impact damage, further increase peace
Full performance is high.
The utility model of patent No. CN201420608060.7 discloses a kind of more rotor plant protection drones of novel double-layer, institute
Stating unmanned plane includes：Fuselage main body, motor, rotor, support plate, battery, automatic flight instrument, function pod, undercarriage.Its feature exists
In：The fuselage main body structure is that oval (including circle) or rectangle (including square), every group of motor are mountable in fuselage
Also mountable the same side in fuselage main body, rotor are mounted on motor for the two sides up and down of main body, and motor is symmetrically mounted in fuselage master
On body, in fuselage main body, battery is placed on support plate support plate device, and automatic flight instrument is mounted in support plate, function pod peace
Mounted in the lower section of fuselage main body, undercarriage is fixed in fuselage main body, is mounted on the lower section of fuselage main body.
The analysis found that most of rotor wing unmanned aerial vehicles belong to single layer rotor, double-deck more rotor forms are less, except this it
Outside, for the rotor wings frame of existing unmanned plane, some rotor wings frame self structures are too simple, after installation it is obtained protection and
Carrying dynamics is limited；Some rotor wings frame self structures are again excessively complicated, and disassembly seems when assembling to be more troublesome；So for ability
For the personnel of domain, it is desirable to possess a kind of double-deck rotor wings frame that can be quickly disassembled and can get preferably carrying dynamics.
Utility model content
Therefore, in order to solve above-mentioned deficiency, the utility model provides the double-deck rotor wings frame in a kind of unmanned plane herein；This is practical
It is novel by improving after, which can realize the setting of double-deck rotor, and from structure composition, which has
Multibilayer rotor fixed cell, upper carrier, lower carrier；Every group of bilayer rotor fixed cell is separately fixed at carrier
It between lower carrier, then the rotor wings frame self structure is simple, is found by test, guarantor obtained after rotor wings frame molding
Shield and carrying dynamics are higher；And the cooperation of bolts and nuts can be used between rotor wings frame each section to assemble, so that disassembly
It is easy to be quick when with assembling.
The utility model is realized in this way constructing the double-deck rotor wings frame in a kind of unmanned plane, it is characterised in that：Bilayer rotation
Wing frame has multibilayer rotor fixed cell, upper carrier, lower carrier；Every group of bilayer rotor fixed cell is separately fixed at
Between upper carrier and lower carrier；
Every group of bilayer rotor fixed cell is respectively provided with loading plate, lower loading plate and fixing axle, and upper loading plate is held under
Support plate is integrally in triangular shape, and internal both ends Jiao Chu is respectively provided with connection through-hole, and loading plate thereon and lower loading plate is made to pass through company
It connects hole to be set in fixing axle, while fixing axle upper sleeve through has three groups of spacers, so that upper carrier, upper loading plate, lower carrying
It is separated respectively by different spacers between plate, lower carrier；The end up and down of fixing axle by nut and upper carrier and under hold
Carrier connection.The utility model provides the double-deck rotor wings frame in a kind of unmanned plane by improving herein, firstly, the rotor wings frame can be realized
The double-deck rotor setting, from structure composition, which has multibilayer rotor fixed cell 1, upper carrier
2, lower carrier；Every group of bilayer rotor fixed cell is separately fixed between carrier and lower carrier, then the rotor wings frame
Self structure is simple, by test find, the rotor wings frame molding after it is obtained protection and carrying dynamics it is higher；And rotor wings frame
The cooperation of bolts and nuts can be used between each section to assemble, so that easy to be quick when disassembly is with assembling.
As an improvement of the above technical solution, the double-deck rotor wings frame in a kind of unmanned plane, it is characterised in that：Upper carrying
Plate, lower loading plate outer end have for rotor blade component installation opening；When installing rotor blade component, rotor is filled
Paddle components can be caught in from opening and fix again.
As an improvement of the above technical solution, the double-deck rotor wings frame in a kind of unmanned plane, it is characterised in that：It goes up on described
The multiple groups bolt hole A fixed for rotor blade component is provided with around the opening of loading plate and lower loading plate, so that working as rotor
After leaf component is caught in opening, then corresponding fastening bolt is mixed at bolt hole A, further fix rotor blade component；
Meanwhile two groups of bolt hole B also are provided in the side of bolt hole A, the bolt hole B between upper loading plate and lower loading plate outer end
Place's setting carrying cushion block；Since upper loading plate and lower loading plate are parallel to each other, then in upper loading plate and lower loading plate outer end
Between the benefit of setting carrying cushion block be bearing capacity of both enhancings at outer end；Help to promote the whole strong of rotor wings frame
Degree.
As an improvement of the above technical solution, the double-deck rotor wings frame in a kind of unmanned plane, it is characterised in that：In upper carrying
The upper end of frame is provided with instrument mounting rack by fixing axle and spacer；Can be set at instrument mounting rack solar panel or
Instrument is maked an inspection tour in other flights of person.
As an improvement of the above technical solution, the double-deck rotor wings frame in a kind of unmanned plane, it is characterised in that：Upper carrying
Frame, upper loading plate, lower loading plate, lower carrier are respectively that alloy material is made；Light and intensity is higher.
As an improvement of the above technical solution, the double-deck rotor wings frame in a kind of unmanned plane, it is characterised in that：Bilayer rotation
Wing frame has four groups of bilayer rotor fixed cells；It is connected to the surrounding of carrier and lower carrier.
The utility model has the following advantages that：The utility model provides the double-deck rotor in a kind of unmanned plane by improving herein
Frame, as Figure 1-Figure 5, have the advantages that as follows improve and；
Advantage 1：The bilayer rotor wings frame has multibilayer rotor fixed cell, upper carrier, lower carrier；Every group double-deck
Rotor fixed cell is separately fixed between carrier and lower carrier；Every group of bilayer rotor fixed cell is respectively provided with and holds
Support plate, lower loading plate and fixing axle, upper loading plate and lower loading plate are integrally in triangular shape, and internal both ends Jiao Chu is respectively provided with company
Hole is connected, is set on loading plate thereon and lower loading plate in fixing axle by connecting through-hole, while fixing axle（Or screw rod）
Upper sleeve through has three groups of spacers, so that respectively by different spacers between upper carrier, upper loading plate, lower loading plate, lower carrier
It separates；The end up and down of fixing axle is connect by nut with upper carrier and lower carrier.The utility model is by improving herein
The double-deck rotor wings frame in a kind of unmanned plane is provided, firstly, the rotor wings frame can realize the double-deck rotor setting, from structure composition,
The bilayer rotor wings frame has multibilayer rotor fixed cell, upper carrier, lower carrier；Every group of bilayer rotor fixed cell point
It is not fixed between carrier and lower carrier, then the rotor wings frame self structure is simple, is found by test, the rotor wings frame
After molding it is obtained protection and carrying dynamics it is higher；And the cooperation of bolts and nuts can be used between rotor wings frame each section
Assemble so that when disassembly is with assembling it is easy quickly.
Advantage 2：The double-deck rotor wings frame, the outer end of upper loading plate, lower loading plate in a kind of unmanned plane described in the utility model
With the opening installed for rotor blade component；When installing rotor blade component, dress rotor blade component can be from opening
It is caught in and fixes again.
Advantage 3：The double-deck rotor wings frame in a kind of unmanned plane described in the utility model, the upper loading plate and lower loading plate are opened
The multiple groups bolt hole A fixed for rotor blade component is provided with around mouthful, so that after rotor blade component is caught in opening, then
Corresponding fastening bolt is mixed at bolt hole A, further fixes rotor blade component；Meanwhile also in the side of bolt hole A
Two groups of bolt hole B are provided with, setting carrying cushion block at the bolt hole B between upper loading plate and lower loading plate outer end；Due to upper
Loading plate and lower loading plate are parallel to each other, then setting carries the benefit of cushion block between upper loading plate and lower loading plate outer end
It is the bearing capacity at both enhancings outer end；Facilitate the integral strength of promotion rotor wings frame.
Advantage 4：The double-deck rotor wings frame, passes through fixing axle in the upper end of upper carrier in a kind of unmanned plane described in the utility model
Spacer is provided with instrument mounting rack；Solar panel or other flights or inspection instrument can be set at instrument mounting rack
Device.
Advantage 5：The double-deck rotor wings frame, upper carrier, upper loading plate, lower carrying in a kind of unmanned plane described in the utility model
Plate, lower carrier may respectively be alloy material and be made；Light and intensity is higher.
Detailed description of the invention
Fig. 1 is the implementation diagram of the double-deck rotor wings frame in unmanned plane described in the utility model；
Fig. 2 is the schematic top plan view of the double-deck rotor wings frame in unmanned plane described in the utility model；
Fig. 3 is upper loading plate and the corresponding schematic diagram of lower loading plate in the utility model；
Fig. 4-Fig. 5 is a kind of unmanned plane schematic diagram of application bilayer rotor wings frame.
Wherein：The double-deck rotor fixed cell 1, upper carrier 2, lower carrier 3, upper loading plate 4, lower loading plate 5, fixing axle
6, connect through-hole 7, spacer 8, opening 9, bolt hole A10, bolt hole B11, instrument mounting rack 13.
Specific embodiment
The utility model is described in detail below in conjunction with attached drawing 1- Fig. 5, to the skill in the utility model embodiment
Art scheme is clearly and completely described, it is clear that and the described embodiments are only a part of the embodiments of the utility model, and
The embodiment being not all of.Based on the embodiments of the present invention, those of ordinary skill in the art are not making creativeness
Every other embodiment obtained, fall within the protection scope of the utility model under the premise of labour.
The utility model provides the double-deck rotor wings frame in a kind of unmanned plane by improving herein, as Figure 1-Figure 5, can be by
It is practiced according to such as under type；The bilayer rotor wings frame has multibilayer rotor fixed cell 1, upper carrier 2, lower carrier 3；
Every group of bilayer rotor fixed cell 1 is separately fixed between carrier 2 and lower carrier 3；Every group of bilayer rotor fixed cell 1
It is respectively provided with loading plate 4, lower loading plate 5 and fixing axle 6, upper loading plate 4 and 5 entirety of lower loading plate are in triangular shape, inside
Both ends Jiao Chu is respectively provided with connection through-hole 7, and loading plate 4 thereon and lower loading plate 5 is made to be set on fixing axle 6 by connecting through-hole 7
On, while fixing axle 6（Or screw rod）Upper sleeve through has three groups of spacers 8 so that upper carrier 2, upper loading plate 4, lower loading plate 5,
It is separated respectively by different spacers 8 between lower carrier 3；The end up and down of fixing axle 6 by nut and upper carrier 2 and under hold
Carrier 3 connects.
The utility model provides the double-deck rotor wings frame in a kind of unmanned plane by improving herein, firstly, the rotor wings frame can be realized
The double-deck rotor setting, from structure composition, which has multibilayer rotor fixed cell 1, upper carrier
2, lower carrier 3；Every group of bilayer rotor fixed cell 1 is separately fixed between carrier 2 and lower carrier 3, then the rotation
Wing frame self structure is simple, by test find, the rotor wings frame molding after it is obtained protection and carrying dynamics it is higher；And it revolves
The cooperation of bolts and nuts can be used to assemble between wing frame each section, so that easy to be quick when disassembly is with assembling.
On the other hand, the double-deck rotor wings frame in a kind of unmanned plane described in the utility model, upper loading plate 4, lower loading plate 5 it is outer
End has the opening 9 for the installation of rotor blade component；When installing rotor blade component, dress rotor blade component can be from opening
It is caught at mouth 9 and fixes again.
On the other hand, the double-deck rotor wings frame, the upper loading plate 4 and lower loading plate in a kind of unmanned plane described in the utility model
The multiple groups bolt hole A10 fixed for rotor blade component is provided with around 5 opening 9, so that when rotor blade component is caught in out
After at mouth 9, then corresponding fastening bolt is mixed at bolt hole A10, further fix rotor blade component；Meanwhile also existing
The side of bolt hole A10 is provided with two groups of bolt hole B11, the bolt hole B11 between upper loading plate 4 and lower 5 outer end of loading plate
Place's setting carrying cushion block 12；Since upper loading plate 4 and lower loading plate 5 are parallel to each other, then in upper loading plate 4 and lower loading plate 5
The benefit of setting carrying cushion block 12 is the bearing capacity at both enhancings outer end between outer end；Help to promote rotor wings frame
Integral strength.
On the other hand, the double-deck rotor wings frame in a kind of unmanned plane described in the utility model, passes through solid in the upper end of upper carrier 2
Dead axle and spacer are provided with instrument mounting rack 13；Solar panel or other flights can be set at instrument mounting rack 13
Or make an inspection tour instrument.
On the other hand, the double-deck rotor wings frame in a kind of unmanned plane described in the utility model, upper carrier 2, upper loading plate 4, under
Loading plate 5, lower carrier 3 may respectively be alloy material and be made；Light and intensity is higher.
The foregoing description of the disclosed embodiments can be realized professional and technical personnel in the field or using originally practical new
Type.Various modifications to these embodiments will be readily apparent to those skilled in the art, and determine herein
The General Principle of justice can be realized in other embodiments without departing from the spirit or scope of the present utility model.Cause
This, the present invention will not be limited to the embodiments shown herein, and is to fit to and principles disclosed herein
The widest scope consistent with features of novelty.
Claims (6)
1. the double-deck rotor wings frame in a kind of unmanned plane, it is characterised in that：The bilayer rotor wings frame has multibilayer rotor fixed cell
（1）, upper carrier（2）, lower carrier（3）；Every group of bilayer rotor fixed cell（1）It is separately fixed at carrier（2）With under
Carrier（3）Between；
Every group of bilayer rotor fixed cell（1）It is respectively provided with loading plate（4）, lower loading plate（5）And fixing axle（6）, upper carrying
Plate（4）With lower loading plate（5）Whole is in triangular shape, and internal both ends Jiao Chu is respectively provided with connection through-hole（7）, make loading plate thereon
（4）With lower loading plate（5）By connecting through-hole（7）It is set on fixing axle（6）On, while fixing axle（6）Upper sleeve through have three groups every
Set（8）, so that upper carrier（2）, upper loading plate（4）, lower loading plate（5）, lower carrier（3）Between respectively by different spacers
（8）It separates；Fixing axle（6）End up and down pass through nut and upper carrier（2）With lower carrier（3）Connection.
2. the double-deck rotor wings frame in a kind of unmanned plane according to claim 1, it is characterised in that：Upper loading plate（4）, lower loading plate
（5）Outer end have for rotor blade component installation opening（9）.
3. the double-deck rotor wings frame in a kind of unmanned plane according to claim 1, it is characterised in that：Upper loading plate（4）With lower carrying
Plate（5）Opening（9）Surrounding is provided with the multiple groups bolt hole A fixed for rotor blade component（10）, in bolt hole A（10）Side
Face is provided with two groups of bolt hole B（11）, in upper loading plate（4）With lower loading plate（5）Bolt hole B between outer end（11）Place's setting
Carry cushion block（12）.
4. the double-deck rotor wings frame in a kind of unmanned plane according to claim 1, it is characterised in that：In upper carrier（2）Upper end
Fixing axle and spacer are provided with instrument mounting rack（13）.
5. the double-deck rotor wings frame in a kind of unmanned plane according to claim 1, it is characterised in that：Upper carrier（2）, upper loading plate
（4）, lower loading plate（5）, lower carrier（3）Respectively alloy material is made.
6. the double-deck rotor wings frame in a kind of unmanned plane according to claim 1, it is characterised in that：The bilayer rotor wings frame has four groups
The double-deck rotor fixed cell（1）；It is connected to carrier（2）With lower carrier（3）Surrounding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820649416.XU CN208102333U (en) | 2018-05-03 | 2018-05-03 | The double-deck rotor wings frame in a kind of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820649416.XU CN208102333U (en) | 2018-05-03 | 2018-05-03 | The double-deck rotor wings frame in a kind of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208102333U true CN208102333U (en) | 2018-11-16 |
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ID=64115326
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820649416.XU Expired - Fee Related CN208102333U (en) | 2018-05-03 | 2018-05-03 | The double-deck rotor wings frame in a kind of unmanned plane |
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| Country | Link |
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| CN (1) | CN208102333U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI716218B (en) * | 2019-12-09 | 2021-01-11 | 英屬維爾京群島商飛思捷投資股份有限公司 | Large drone |
-
2018
- 2018-05-03 CN CN201820649416.XU patent/CN208102333U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI716218B (en) * | 2019-12-09 | 2021-01-11 | 英屬維爾京群島商飛思捷投資股份有限公司 | Large drone |
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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: 20181116 |
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| CF01 | Termination of patent right due to non-payment of annual fee |