CN206569245U - A kind of six rotor wing unmanned aerial vehicles of biomimetic type body - Google Patents
A kind of six rotor wing unmanned aerial vehicles of biomimetic type body Download PDFInfo
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- CN206569245U CN206569245U CN201621343171.5U CN201621343171U CN206569245U CN 206569245 U CN206569245 U CN 206569245U CN 201621343171 U CN201621343171 U CN 201621343171U CN 206569245 U CN206569245 U CN 206569245U
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- fuselage
- undercarriage
- unmanned aerial
- type body
- aerial vehicles
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
The utility model provides a kind of six rotor wing unmanned aerial vehicles of biomimetic type body, including motor, propeller, horn, fuselage upper casing, fuselage lower casing, undercarriage cross bar, undercarriage vertical rod, battery cabin cap and electricity adjust box；Fuselage upper casing closing connection fuselage lower casing, fuselage upper casing is in hexagram, and surface is streamlined curved surface；A horn is respectively connected with six coigns of fuselage upper casing, outer end connection motor, propeller and the electricity of horn adjust box；The upper end of undercarriage vertical rod is connected to the bottom sides of fuselage lower casing, and undercarriage cross bar is connected to the lower end of undercarriage vertical rod by three-way piece.Beneficial effect can reduce windage, increase the flight time, improve the unmanned plane of flight stability, standby spy is that can also have stronger adaptability under conditions of environment is relatively more severe.
Description
Technical field
The utility model belongs to Aero-Space flight unmanned plane field, more particularly, to a kind of six rotors of biomimetic type body
Unmanned plane.
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 biomimetic type body, can reduce windage,
Increase the flight time, improve the unmanned plane of flight stability, standby spy is that can also have stronger under conditions of environment is relatively more severe
Adaptability.
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 biomimetic type body, including motor, propeller, horn, fuselage upper casing, fuselage lower casing,
Undercarriage cross bar, undercarriage vertical rod, battery cabin cap and electricity adjust box；The fuselage upper casing closing connection fuselage lower casing, it is described
Fuselage upper casing is in hexagram, and surface is streamlined curved surface；An institute is respectively connected with six coigns of the fuselage upper casing
Horn is stated, the outer end of the horn connects the motor, the propeller and the electricity and adjusts box；The upper end of the undercarriage vertical rod
The bottom sides of the fuselage lower casing are connected to, the undercarriage cross bar is connected under the undercarriage vertical rod by three-way piece
End.
Further, rotating handles is provided with the horn, the motor and the electricity adjust box around the rotating handles
120 degree of rotate counterclockwise.
Further, the undercarriage vertical rod is connected with the fuselage lower casing by gear support part.
Further, the two ends of the undercarriage cross bar are socketed with damping footmuff.
Further, the battery cabin cap is arranged in the fuselage lower casing, and the battery cabin cap separates under the fuselage
Flight control system and battery in shell.
Further, the dome interior of the fuselage upper casing is provided with GPS.
Further, the fuselage upper casing, the fuselage lower casing, the undercarriage vertical rod and the undercarriage cross bar are by multiple
Condensation material is made by formed in mould mode, and the section of the undercarriage vertical rod and the undercarriage cross bar is in circle
Shape.
Further, the horn is made up of carbon pipe, and section is rounded.
Relative to prior art, six rotor wing unmanned aerial vehicles of biomimetic type body 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 cabin cap is arranged in fuselage lower casing,
The design and fuselage of battery compartment combine together, with certain water-proof function, also allow for changing battery, and battery cabin cap can
Separate flight control system and battery, it is to avoid the electromagnetic interference of internal wiring, and heat excessively concentrate the damage to electric elements.
The rotating handles being provided with horn, can make motor and electricity adjust box around 120 degree of rotating handles rotate counterclockwise, folding
It can reduce the overall dimensions of structure after folded completion, be readily transported, quick despatch can also be carried out.
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 structural representation of the utility model folded state.
Description of reference numerals：
1- motors；2- propellers；3- damping footmuffs；4- three-way pieces；5- horns；6- rotating handleses；7- undercarriage cross bars；
8- fuselage upper casings；9- battery cabin caps；10- electricity adjusts box；11- undercarriage vertical rods；12- gear support parts；13- 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.
, 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 biomimetic type body, including motor
1st, propeller 2, horn 5, fuselage upper casing 8, fuselage lower casing 13, undercarriage cross bar 7, undercarriage vertical rod 11, battery cabin cap 9 and electricity are adjusted
Box 10；The closing of fuselage upper casing 8 connection fuselage lower casing 13, the fuselage upper casing 8 is in hexagram, and surface is streamline
Type curved surface；A horn 5 is respectively connected with six coigns of the fuselage upper casing 8, the outer end connection of the horn 5 is described
Motor 1, the propeller 2 and the electricity adjust box 10；The upper end of the undercarriage vertical rod 11 is connected to the fuselage lower casing 13
Bottom sides, the undercarriage cross bar 7 is connected to the lower end of the undercarriage vertical rod 11 by three-way piece 4.
Rotating handles 6 is provided with the horn 5, the motor 1 and the electricity adjust box 10 around the inverse time of rotating handles 6
Pin rotates 120 degree.
The undercarriage vertical rod 11 is connected with the fuselage lower casing 13 by gear support part 12.
The two ends of the undercarriage cross bar 7 are socketed with damping footmuff 3.
The battery cabin cap 9 is arranged in the fuselage lower casing 13, and the battery cabin cap 9 separates in the fuselage lower casing 13
Flight control system and battery.
The dome interior of the fuselage upper casing 8 is provided with GPS.
The fuselage upper casing 8, the fuselage lower casing 13, the undercarriage vertical rod 11 and the undercarriage cross bar 7 are by being combined
Material is made by formed in mould mode, and the section of the undercarriage vertical rod 11 and the undercarriage cross bar 7 is in circle
Shape.
The horn 5 is made up of carbon pipe, and section is rounded.
As shown in Figure 1,2,3, 4, a kind of smooth sweeping style is presented in whole fuselage appearance, and smooth fairshaped fuselage exists
Be not likely to produce sinuous flow in flight course, the design that fuselage and battery compartment combine together, in flight relative to air resistance just
Can be smaller, whole electronic equipment and flight control system are arranged in fuselage interior, can be realized to inside by opening fuselage upper casing 8
The replacing or debugging of electronic equipment.Fuselage upper casing 8 and fuselage lower casing 13 are all to be formed by composite by Mold Making, weight
Amount is light, and intensity is good, and air resistance coefficient is small.Horn 5 is made up of carbon pipe, and circular cross sectional shape ensure that smoothness and reduce wind
Resistance.GPS is placed in the dome interior of fuselage upper casing 8, and GPS is higher than fuselage, and the electronic unit away from fuselage interior is effectively avoided
The interference of signal.There is a LED blinker at the afterbody of battery cabin cap 9, can basis when aircraft is away from oneself
The difference of indicator lamp distinguishes head and tail.
As shown in figure 5, horn 5, motor 1 and electricity adjust the rotating shaft rotate counterclockwise 120 that box 10 can be at rotating handles 6
Degree, the overall dimensions of aircraft can be reduced after completing by folding, and be easy to store and transported.Under gear support part 12 and fuselage
The bottom surface of shell 13 is connected, and increases the carry ability of aircraft.
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 (8)
1. a kind of six rotor wing unmanned aerial vehicles of biomimetic type body, it is characterised in that：Including motor, propeller, horn, fuselage upper casing,
Fuselage lower casing, undercarriage cross bar, undercarriage vertical rod, battery cabin cap and electricity adjust box；The fuselage upper casing closing connection fuselage
Lower casing, the fuselage upper casing is in hexagram, and surface is streamlined curved surface；Respectively connected at six coigns of the fuselage upper casing
There is a horn, the outer end of the horn connects the motor, the propeller and the electricity and adjusts box；The erection of rising and falling
The upper end of bar is connected to the bottom sides of the fuselage lower casing, and the undercarriage cross bar is connected to the undercarriage by three-way piece
The lower end of vertical rod.
2. six rotor wing unmanned aerial vehicles of biomimetic type body according to claim 1, it is characterised in that：It is provided with the horn
Rotating handles, the motor and the electricity adjust box around 120 degree of the rotating handles rotate counterclockwise.
3. six rotor wing unmanned aerial vehicles of biomimetic type body according to claim 1, it is characterised in that：The undercarriage vertical rod and
The fuselage lower casing is connected by gear support part.
4. six rotor wing unmanned aerial vehicles of the biomimetic type body according to any one of claim 1 or 3, it is characterised in that：Described
The two ends for falling frame cross bar are socketed with damping footmuff.
5. six rotor wing unmanned aerial vehicles of biomimetic type body according to claim 1, it is characterised in that：The battery cabin cap is set
In the fuselage lower casing, the battery cabin cap separates flight control system and battery in the fuselage lower casing.
6. six rotor wing unmanned aerial vehicles of biomimetic type body according to claim 1, it is characterised in that：The circle of the fuselage upper casing
Top is internally provided with GPS.
7. six rotor wing unmanned aerial vehicles of biomimetic type body according to claim 1, it is characterised in that：The fuselage upper casing, institute
State fuselage lower casing, the undercarriage vertical rod and the undercarriage cross bar made by composite by formed in mould mode and
Into, and the section of the undercarriage vertical rod and the undercarriage cross bar is rounded.
8. six rotor wing unmanned aerial vehicles of biomimetic type body according to claim 1, it is characterised in that：The horn is by carbon pipe structure
Into, and section is rounded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621343171.5U CN206569245U (en) | 2016-12-08 | 2016-12-08 | A kind of six rotor wing unmanned aerial vehicles of biomimetic type body |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621343171.5U CN206569245U (en) | 2016-12-08 | 2016-12-08 | A kind of six rotor wing unmanned aerial vehicles of biomimetic type body |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206569245U true CN206569245U (en) | 2017-10-20 |
Family
ID=60062564
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621343171.5U Active CN206569245U (en) | 2016-12-08 | 2016-12-08 | A kind of six rotor wing unmanned aerial vehicles of biomimetic type body |
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| CN (1) | CN206569245U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020107457A1 (en) * | 2018-11-30 | 2020-06-04 | SZ DJI Technology Co., Ltd. | Foldable unmanned aerial vehicle |
-
2016
- 2016-12-08 CN CN201621343171.5U patent/CN206569245U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020107457A1 (en) * | 2018-11-30 | 2020-06-04 | SZ DJI Technology Co., Ltd. | Foldable unmanned aerial vehicle |
| JP2020083313A (en) * | 2018-11-30 | 2020-06-04 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ | Foldable unmanned aerial vehicle |
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