CN206569244U - A kind of six rotor wing unmanned aerial vehicles of folding - Google Patents
A kind of six rotor wing unmanned aerial vehicles of folding Download PDFInfo
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- CN206569244U CN206569244U CN201621342645.4U CN201621342645U CN206569244U CN 206569244 U CN206569244 U CN 206569244U CN 201621342645 U CN201621342645 U CN 201621342645U CN 206569244 U CN206569244 U CN 206569244U
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- horn
- fuselage
- upper casing
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Abstract
The utility model provides a kind of six rotor wing unmanned aerial vehicles of folding, including motor, propeller, electricity adjust box, horn, fuselage upper casing, fuselage lower casing and undercarriage；Fuselage upper casing closing connection fuselage lower casing, fuselage upper casing is smooth streamlined curved surface；Fuselage upper casing is connected with six horns, horn includes the first horn connector and the second horn connector, the lower end of first horn connector and the second horn connector is hinged by rotary shaft, in addition to the horn stay that the opening and closing place of the first horn connector and the second horn connector is flexibly connected；Outer end connection motor, propeller and the electricity of horn adjust box；Undercarriage is connected to fuselage lower casing bottom surface sidepiece.Beneficial effect is can to reduce windage, increases the flight time, the unmanned plane of raising flight stability particularly can also have stronger adaptability under conditions of environment is relatively more severe, and horn can be folded, convenient transport and dismounting.
Description
Technical field
The utility model belongs to aerospace flight vehicle field, and flight resistance is reduced more particularly, to one kind, increases body
Stability and increase flight time, six rotor wing unmanned aerial vehicles of streamlined body.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without driving cabin on machine, but there is an automatic pilot, the equipment such as presetting apparatus.For currently on the market
Most of six rotor wing unmanned aerial vehicles are presented a kind of simple and crude without shell or shell, and in actual job, wind loading rating is poor, without streamline
The fuselage of type, flight resistance is increased in flight course, the flight time is reduced, without the simple and crude unmanned plane of shell or shell
Water-resistant performance is also poor, is unfavorable for the operation in rugged environment.
Utility model content
In view of this, the utility model is directed to a kind of six rotor wing unmanned aerial vehicles of folding, can reduce windage, and increase flies
The row time, the unmanned plane of flight stability is improved, particularly can also have stronger adaptability under conditions of environment is relatively more severe,
And horn can be folded, convenient transport and dismounting.
To reach above-mentioned purpose, what the technical solution of the utility model was realized in：
A kind of six rotor wing unmanned aerial vehicles of folding, including motor, propeller, electricity adjust box, horn, fuselage upper casing, fuselage lower casing
And undercarriage；The fuselage upper casing closing connection fuselage lower casing, the fuselage upper casing is smooth streamlined curved surface；The machine
Shell is connected with six horns with it, and the horn includes the first horn connector and the second horn connector, described first
The lower end of horn connector and the second horn connector is hinged by rotary shaft, in addition to by the first horn connector
The horn stay being flexibly connected with the opening and closing place of the second horn connector；The outer end connection motor of the horn,
The propeller and the electricity adjust box；The undercarriage is connected to the fuselage lower casing bottom surface sidepiece.
Further, the first horn connector is rotated down around the rotary shaft relative to the second horn connector
Angle be 90 degree.
Further, the fuselage upper casing is in hexagram；Each horn is connected to each of the fuselage upper casing
At coign.
Further, the side wall of the fuselage lower casing is set to battery door.
Further, the fuselage upper casing, the fuselage lower casing, the undercarriage are passed through formed in mould by composite
Mode is made.
Further, the top of the fuselage upper casing is internally provided with GPS.
Further, the horn is made up of carbon pipe, and section is rounded.
Relative to prior art, six rotor wing unmanned aerial vehicles of folding described in the utility model have the advantage that：
Fuselage upper casing and fuselage lower casing are formed using composite by Mold Making, and good forming effect is highly polished, weight
Amount is light, and fuselage upper casing is in hexagram, and surface is streamlined curved surface, the biomimetic features of similar starfish, with reducing windward
Contact area, reduces the advantage of air resistance coefficient, meets aerodynamic requirement, resistance can be reduced during practical flight
Power, increases wind resistance, makes flight more stable；Electronic equipment is all among the encirclement of fuselage upper casing and fuselage lower casing, effectively
Avoid interference of the outside adverse circumstances to electronic equipment and control device.In addition, battery door is arranged on fuselage lower casing one
Side-walls, the design and fuselage of battery compartment combine together, with certain water-proof function, also allow for changing battery, and battery
Storehouse can separate flight control system and battery, it is to avoid the electromagnetic interference of internal wiring, and heat are excessively concentrated to electric elements
Damage.
Horn uses foldable structure, gently pulls horn stay, and the first horn connector of horn connection can be around
Rotary shaft is rotated down 90 degree in the presence of the second horn connector, and the overall chi of aircraft can be reduced after completing by folding
It is very little, it is easy to store and transports.
Brief description of the drawings
Constitute a part of accompanying drawing of the present utility model to be used for providing further understanding to of the present utility model, this practicality is new
The schematic description and description of type is used to explain the utility model, does not constitute to improper restriction of the present utility model.
In accompanying drawing：
Fig. 1 is the positive structure diagram described in the utility model embodiment；
Fig. 2 is the overlooking the structure diagram described in the utility model embodiment；
Fig. 3 is the side structure schematic view described in the utility model embodiment；
Fig. 4 is the side structure schematic view such as just described in the utility model embodiment；
Fig. 5 is the foldable structure schematic diagram described in the utility model embodiment.
Description of reference numerals：
1- motors；2- propellers；3- electricity adjusts box；4- horns；5- the first horn connectors；6- the second horn connectors；7-
Fuselage upper casing；8- undercarriages；9- horn stays；10- battery doors；11- fuselage lower casings.
Embodiment
It should be noted that in the case where not conflicting, the feature in embodiment and embodiment in the utility model can
To be mutually combined.
In description of the present utility model, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", " on ", " under ",
The orientation or position relationship of the instruction such as "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer " are
Based on orientation shown in the drawings or position relationship, it is for only for ease of description the utility model and simplifies description, rather than indicate
Or imply that the device or element of meaning must have specific orientation, with specific azimuth configuration and operation, therefore be not understood that
For to limitation of the present utility model.In addition, term " first ", " second " etc. are only used for describing purpose, and it is not intended that indicating
Or imply relative importance or the implicit quantity for indicating indicated technical characteristic.Thus, " first ", " second " etc. are defined
Feature can express or implicitly include one or more this feature.In description of the present utility model, unless separately
It is described, " multiple " are meant that two or more.
, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in description of the present utility model
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integratedly
Connection；Can be mechanical connection or electrical connection；Can be joined directly together, can also be indirectly connected to by intermediary,
It can be the connection of two element internals.For the ordinary skill in the art, on being understood by concrete condition
State concrete meaning of the term in the utility model.
Describe the utility model in detail below with reference to the accompanying drawings and in conjunction with the embodiments.
As shown in Fig. 1,2,3,4,5, the utility model provides a kind of six rotor wing unmanned aerial vehicles of folding, including motor 1, spiral
Oar 2, electricity adjust box 3, horn 4, fuselage upper casing 7, fuselage lower casing 11 and undercarriage 8；The closing of fuselage upper casing 7 connection fuselage
Lower casing 11, the fuselage upper casing 7 is smooth streamlined curved surface；The fuselage upper casing 7 is connected with six horns 4, the machine
Arm 4 includes the first horn connector 5 and the second horn connector 6, the first horn connector 5 and second horn connection
The lower end of part 6 is hinged by rotary shaft, in addition to opening the first horn connector 4 and the second horn connector 5
The horn stay 9 being flexibly connected at conjunction；The outer end of the horn 4 connects the motor 1, the propeller 2 and the electricity and adjusted
Box 3；The undercarriage 8 is connected to the bottom surface sidepiece of fuselage lower casing 11.
The first horn connector 5 is around the rotary shaft, and the angle being rotated down relative to the second horn connector 6 is
90 degree.
The fuselage upper casing 7 is in hexagram；Each horn 4 is connected at each coign of the fuselage upper casing 7.
The side wall of the fuselage lower casing 11 is set to battery door 10.
The fuselage upper casing 7, the fuselage lower casing 11, the undercarriage 8 pass through formed in mould mode by composite
It is made.
The top of the fuselage upper casing 7 is internally provided with GPS.
The horn 4 is made up of carbon pipe, and section is rounded.
The course of work of this example：As shown in Figure 1,2,3, 4, a kind of smooth sweeping style is presented in whole fuselage appearance,
Smooth fairshaped fuselage is not likely to produce sinuous flow, the design that fuselage and battery compartment combine together, in flight in flight course
Resistance relative to air will be smaller, and whole electronic equipment and flight control system are arranged in fuselage interior, by opening fuselage
Upper casing 7 can realize the replacing or debugging to internal electronic equipment.Fuselage upper casing 7 and fuselage lower casing 11 are all by composite
Formed by Mold Making, lightweight, intensity is good, and air resistance coefficient is small.Horn 4 is made up of carbon pipe, and circular cross sectional shape ensures
Smoothness and reduce windage.GPS is placed in the dome interior of fuselage upper casing 7, and GPS is higher than fuselage, the electricity away from fuselage interior
Subassembly, effectively avoids the interference of signal.There is a LED blinker at battery compartment afterbody, in aircraft away from certainly
Oneself when head and tail can be distinguished according to the difference of indicator lamp.As shown in figure 5, horn stay 11 is gently pulled,
The first horn connector 5 that horn 4 is connected can be rotated down 90 around rotary shaft in the presence of the second horn connector 6
Degree, the overall dimensions of aircraft can be reduced after completing by folding, and be easy to store and transported.
Preferred embodiment of the present utility model is the foregoing is only, it is all at this not to limit the utility model
Within the spirit and principle of utility model, any modification, equivalent substitution and improvements made etc. should be included in the utility model
Protection domain within.
Claims (6)
1. a kind of six rotor wing unmanned aerial vehicles of folding, it is characterised in that：Including motor, propeller, electricity adjust box, horn, fuselage upper casing,
Fuselage lower casing and undercarriage；The fuselage upper casing closing connection fuselage lower casing, the fuselage upper casing is smooth streamlined song
Face；The fuselage upper casing is connected with six horns, and the horn includes the first horn connector and the second horn connector,
The lower end of the first horn connector and the second horn connector is hinged by rotary shaft, the first horn connector
It it is 90 degree relative to the angle that the second horn connector is rotated down, in addition to first horn is connected around the rotary shaft
The horn stay that the opening and closing place of fitting and the second horn connector is flexibly connected；The outer end of the horn connects the electricity
Machine, the propeller and the electricity adjust box；The undercarriage is connected to the fuselage lower casing bottom surface sidepiece.
2. six rotor wing unmanned aerial vehicles of folding according to claim 1, it is characterised in that：The fuselage upper casing is in Magen David
Shape；Each horn is connected at each coign of the fuselage upper casing.
3. six rotor wing unmanned aerial vehicles of folding according to claim 1, it is characterised in that：The side wall of the fuselage lower casing is set
It is set to battery door.
4. six rotor wing unmanned aerial vehicles of folding according to claim 1, it is characterised in that：The fuselage upper casing, the fuselage
Lower casing, the undercarriage are made by composite by formed in mould mode.
5. six rotor wing unmanned aerial vehicles of folding according to claim 1, it is characterised in that：Inside the top of the fuselage upper casing
It is provided with GPS.
6. six rotor wing unmanned aerial vehicles of folding according to claim 1, it is characterised in that：The horn is made up of carbon pipe, and
Section is rounded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621342645.4U CN206569244U (en) | 2016-12-08 | 2016-12-08 | A kind of six rotor wing unmanned aerial vehicles of folding |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621342645.4U CN206569244U (en) | 2016-12-08 | 2016-12-08 | A kind of six rotor wing unmanned aerial vehicles of folding |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206569244U true CN206569244U (en) | 2017-10-20 |
Family
ID=60062659
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621342645.4U Active CN206569244U (en) | 2016-12-08 | 2016-12-08 | A kind of six rotor wing unmanned aerial vehicles of folding |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206569244U (en) |
-
2016
- 2016-12-08 CN CN201621342645.4U patent/CN206569244U/en active Active
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