CN106240795A - The fine six collapsible unmanned planes of axle of carbon - Google Patents
The fine six collapsible unmanned planes of axle of carbon Download PDFInfo
- Publication number
- CN106240795A CN106240795A CN201610886151.0A CN201610886151A CN106240795A CN 106240795 A CN106240795 A CN 106240795A CN 201610886151 A CN201610886151 A CN 201610886151A CN 106240795 A CN106240795 A CN 106240795A
- Authority
- CN
- China
- Prior art keywords
- porous plate
- upper shell
- adjutage
- carbon
- axle
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
Abstract
The fine six collapsible unmanned planes of axle of a kind of carbon, it includes: main body, and it has the lower house and upper shell being connected, and upper shell has six relative to the adjutage outwards radially arranged in the middle part of upper shell；Being provided with folding part and pulling buckle portion between each adjutage and slurry arm, described folding part has the first inlay and the second inlay being hinged；First inlay is sheathed on the inner chamber of adjutage, and second is sheathed on the inner chamber of slurry arm, allows slurry arm rotate to change between deployed condition and folded state relative to adjutage by means of folding part；Every paddle arm is relatively distant from one end formation motor installation cavity of described main body；Blade mechanism, it rotation section including connecting motor, both sides, rotation section are all equiped with blade；Lower house and upper shell combination form cavity volume；Cavity volume is built-in includes the side porous plate that porous plate is relative with described upper porous plate, the lower porous plate being connected to side porous plate and porous barrier, and they combinations are formed and are available for cage chamber and the many square channels that air-flow communicates.
Description
[technical field]
The present invention relates to the fine six collapsible unmanned planes of axle of a kind of carbon.
[background technology]
According to market survey and patent retrieval, find existing unmanned plane structure complex, install inconvenience, body heat radiation not good enough,
Weight is relatively big, directly affects flying power and the safety of unmanned plane, and it is big that horn awing exists flight vibrations, Er Qiecun
Unreasonable in folding mode, transport is with inconvenient to carry.
In order to overcome above-mentioned problem, we have developed the fine six collapsible unmanned planes of axle of a kind of carbon.
[summary of the invention]
Purpose of the present invention technical problem to be solved is intended to provide a kind of carbon the fine six collapsible unmanned planes of axle, its structure pole
For simple, install and swift to operate, stable, the length in service life of flying, safe and reliable, lightweight, good heat dissipation, cruising time
The features such as length, and elegant in appearance.Therefore, it is technical, practicality and the product of the equal top grade of economy.
To achieve these goals, the technical solution used in the present invention: the fine six collapsible unmanned planes of axle of a kind of carbon, its bag
Include:
Main body, it has the lower house and upper shell being connected, and upper shell has six outside relative in the middle part of upper shell
The adjutage radially arranged；
Be provided with folding part and pulling buckle portion between each adjutage and slurry arm, described folding part have the first inlay of being hinged and
Second inlay；First inlay is sheathed on the inner chamber of adjutage, and second is sheathed on the inner chamber of slurry arm, allows by means of folding part and starches arm phase
Adjutage is rotated to change between deployed condition and folded state；
Every paddle arm is relatively distant from one end formation motor installation cavity of described main body；
Blade mechanism, it rotation section including connecting motor, both sides, rotation section are all equiped with blade；
Lower house and upper shell combination form cavity volume；The built-in side including that porous plate is relative with described upper porous plate of cavity volume is many
Orifice plate, the lower porous plate being connected to side porous plate and porous barrier, they combinations are formed and are available for cage chamber that air-flow communicates and in many ways
Passage；
Power supply and control portion, it is installed in cage intracavity, realizes being prone to heat radiation and strengthening main body intensity by means of many square channels.
In one or more embodiments of the invention, described upper shell is removably equiped with lid.
In one or more embodiments of the invention, described lower house, upper shell, upper porous plate, side porous plate, lower many
Orifice plate, porous barrier and slurry arm all use carbon fibre material to make.
In one or more embodiments of the invention, described pulling buckle portion includes that the hook being installed in paddle arm and being assembled in is prolonged
The button of semi-girder.
In one or more embodiments of the invention, described main body has to the spike extended out.
In one or more embodiments of the invention, described paddle arm is symmetrical arranged, the motor steering of adjacent two paddle arm
On the contrary, described spike connects folding mounting blocks.
The present invention is produced beneficial effect compared with background technology:
Owing to have employed above-mentioned technical scheme, its structure is extremely simple, install and swift to operate, fly stable, make
By features such as life-span length, safe and reliable, lightweight, good heat dissipation, length in cruising time, and elegant in appearance.Therefore, it is technology
Property, practicality and the product of the equal top grade of economy.
[accompanying drawing explanation]
Fig. 1 is the perspective view of the fine six collapsible unmanned planes of axle of carbon in one embodiment of the invention；
Fig. 2 is deployed condition one structural representation of the fine six collapsible unmanned planes of axle of carbon in one embodiment of the invention；
Fig. 3 is deployed condition two structural representation of the fine six collapsible unmanned planes of axle of carbon in one embodiment of the invention；
Fig. 4 is enlarged drawing at A in Fig. 2；
Fig. 5 is enlarged drawing at B in Fig. 3；
Fig. 6 is enlarged drawing at C in Fig. 2.
[detailed description of the invention]
Embodiments of the invention are described below in detail, and described embodiment example is shown in the drawings, the most identical
Or similar label represents same or similar element or has the element of same or like function.
In describing the invention, it should be noted that for the noun of locality, if any term " " center ", " laterally ", " longitudinally ", " length
Degree ", " width ", " thickness ", " on ", D score, "front", "rear", "left", "right", " vertically ", " level ", " top ", " end ", " interior ",
The indicating position such as " outward ", " clockwise ", " counterclockwise " and position relationship are based on orientation shown in the drawings or position relationship, are only
For the ease of describing the present invention and simplifying description rather than instruction or imply that the device of indication or element must have specific side
Position, with particular orientation structure and operation, it is impossible to be interpreted as limit the present invention concrete protection domain.
Additionally, be only used for describing purpose if any term " first ", " second ", and it is not intended that indicate or hint relative importance
Or imply the quantity indicating technical characteristic.Thus, define " first ", " second " feature can be expressed or implicit include one
Or multiple this feature, in the present description, " at least " is meant that one or more, unless otherwise the most concrete
Limit.In the present invention, except as otherwise clear stipulaties and restriction, " assemble " if any term, broad sense should be made in " being connected ", " connection " term
Go to understand, connect for example, it may be fixing, it is also possible to be to removably connect, or be integrally connected；Can also be to be mechanically connected；
Can be to be joined directly together, it is also possible to be to be connected by intermediary, can be that two element internals are connected.General for this area
For logical technical staff, above-mentioned term concrete meaning in the present invention can be understood as the case may be.
In the present invention, unless otherwise prescribed and limit, fisrt feature second feature it " on " or D score can include the
One directly contacts with second feature, it is also possible to include that fisrt feature and second feature are not directly contact but by between them
Other characterisation contact.And, fisrt feature second feature " on ", " under " and " above " include that fisrt feature is second
Directly over feature and oblique upper, or be only the height representing fisrt feature level height higher than second feature.Fisrt feature exists
Second feature " on ", " under " and " below " include that fisrt feature immediately below second feature or obliquely downward, or is merely representative of
Fisrt feature level height is less than second feature.
Being incorporated into foregoing, those skilled in the art can carry out adaptive regulation and understanding, in the lump with reference to explanation
The accompanying drawing of book, by being further described the detailed description of the invention of the present invention, makes technical scheme and useful
Effect is clearer, clear and definite.It is exemplary for describing embodiment below with reference to accompanying drawing, it is intended to explain the present invention, and can not
It is interpreted as limitation of the present invention.
Refer to shown by Fig. 1-6, it provides preferably embodiment to be the fine six collapsible nothings of axle of a kind of carbon for the present invention
Man-machine, it includes: main body 1, slurry arm 2, folding part 3, pulling buckle portion 4, blade mechanism 5 and power supply and control portion 6 etc. assemble,
Wherein main body 1 has the lower house 11 and upper shell 12 being connected, upper shell 11 have six relative to upper shell 11 in the middle part of
The adjutage 111 outwards radially arranged；
Being provided with folding part 3 and pulling buckle portion 4 between each adjutage 111 and slurry arm 2, described folding part 3 has the be hinged
One inlay 31 and the second inlay 32；Described first inlay 31 is sheathed on the inner chamber of adjutage 111, and slurry arm is located at by described second set 32
Inner chamber, by means of folding part 3 allow slurry arm 2 relative to adjutage 111 rotate with between deployed condition and folded state change；
Under deployed condition, the hook 41 being installed in paddle arm and the button 42 phase hanging support being assembled in adjutage coordinate, and occur without arm during aircraft
Vibrations, stable；Volume after folding can be realized less, it is easy to carry and transport.
Every paddle arm 2 is relatively distant from one end formation motor installation cavity 21 of described main body 1；Blade mechanism 5 includes connecting
The rotation section 52 of motor 51, both sides, rotation section 52 are all equiped with blade 53；Lower house 11 and upper shell 12 combination form cavity volume；
Cavity volume is built-in includes side porous plate 14 that porous plate 13 is relative with described upper porous plate 13, be connected to side porous plate 14 times
Porous plate 15 and porous barrier 16, they combinations are formed and are available for cage chamber and the many square channels that air-flow communicates；Power supply and control portion 6 fill
It is located at cage intracavity, realizes being prone to heat radiation and strengthening main body intensity by means of many square channels.The comprehensive ventilation and heat of many square channels,
Can effectively alleviate weight and with material simultaneously, also facilitate wiring connect and install.
Lid 17 removably it is equiped with on described upper shell 11.Described lower house 12, upper shell 11, upper porous plate 13,
Side porous plate 14, lower porous plate 15, porous barrier 16 and slurry arm 2 etc. all can use carbon fibre material to make, and weight greatly subtracts
Light, have and relatively extend cruising time, manoeuvrable degree strengthens.Described main body 1 has to the spike 18 extended out.Respectively
Paddle arm 2 and the symmetry being oppositely arranged, the motor steering of adjacent two paddle arm 2 is contrary, and described spike 18 connects folding mounting blocks
19。
Summary content and understanding referring to all accompanying drawings in the lump, its structure of the present embodiment is extremely simple, install and grasp
Make quick, the feature such as stable, the length in service life of flying, safe and reliable, lightweight, good heat dissipation, length in cruising time, Er Qiemei
See generous.Therefore, it is technical, practicality and the product of the equal top grade of economy.
In the description of description, reference term " embodiment ", " preferably ", " example ", " concrete example " or " one
A little examples " etc. description means to combine this embodiment or example describes specific features, structure, material or feature, be contained in
In at least one embodiment of the present invention or example, the schematic representation for above-mentioned term not necessarily refers in this manual
It is identical embodiment or example.And, the specific features of description, structure, material or feature can at any one or
Multiple embodiments or example combine in a suitable manner.
By above-mentioned structure and the description of principle, person of ordinary skill in the field should be appreciated that the present invention not office
It is limited to above-mentioned detailed description of the invention, uses the improvement of techniques well known and replacement to all fall within this on the basis of the present invention
Bright protection domain, should be limited it by each claim.
Claims (6)
1. the fine six collapsible unmanned planes of axle of carbon, it is characterised in that it includes:
Main body, it has the lower house and upper shell being connected, and upper shell has six outside relative in the middle part of upper shell
The adjutage radially arranged；
Be provided with folding part and pulling buckle portion between each adjutage and slurry arm, described folding part have the first inlay of being hinged and
Second inlay；First inlay is sheathed on the inner chamber of adjutage, and second is sheathed on the inner chamber of slurry arm, allows by means of folding part and starches arm phase
Adjutage is rotated to change between deployed condition and folded state；
Every paddle arm is relatively distant from one end formation motor installation cavity of described main body；
Blade mechanism, it rotation section including connecting motor, both sides, rotation section are all equiped with blade；
Lower house and upper shell combination form cavity volume；The built-in side including that porous plate is relative with described upper porous plate of cavity volume is many
Orifice plate, the lower porous plate being connected to side porous plate and porous barrier, they combinations are formed and are available for cage chamber that air-flow communicates and in many ways
Passage；
Power supply and control portion, it is installed in cage intracavity, realizes being prone to heat radiation and strengthening main body intensity by means of many square channels.
The fine six collapsible unmanned planes of axle of carbon the most according to claim 1, it is characterised in that: on described upper shell removably
It is equiped with lid.
The fine six collapsible unmanned planes of axle of carbon the most according to claim 2, it is characterised in that: described lower house, upper shell, on
Porous plate, side porous plate, lower porous plate, porous barrier and slurry arm all use carbon fibre material to make.
The fine six collapsible unmanned planes of axle of carbon the most according to claim 3, it is characterised in that: described pulling buckle portion includes being installed in
The hook of paddle arm and be assembled in the button of adjutage.
The fine six collapsible unmanned planes of axle of carbon the most according to claim 4, it is characterised in that: described main body has to extension
A spike out.
The fine six collapsible unmanned planes of axle of carbon the most according to claim 5, it is characterised in that: described paddle arm is symmetrical arranged, phase
The motor steering of adjacent two paddle arm is contrary, and described spike connects folding mounting blocks.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610886151.0A CN106240795A (en) | 2016-10-11 | 2016-10-11 | The fine six collapsible unmanned planes of axle of carbon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610886151.0A CN106240795A (en) | 2016-10-11 | 2016-10-11 | The fine six collapsible unmanned planes of axle of carbon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106240795A true CN106240795A (en) | 2016-12-21 |
Family
ID=57612347
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610886151.0A Pending CN106240795A (en) | 2016-10-11 | 2016-10-11 | The fine six collapsible unmanned planes of axle of carbon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106240795A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107521685A (en) * | 2017-09-20 | 2017-12-29 | 首航国翼（武汉）科技有限公司 | Foldable multiaxis unmanned plane |
| DE102019128202B4 (en) | 2019-10-18 | 2023-12-07 | Emqopter GmbH | System and method for ad-hoc configuration of a modular multicopter |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2233393A2 (en) * | 2009-03-23 | 2010-09-29 | Gregor Schnoell | Locking system |
| CN204056294U (en) * | 2014-09-12 | 2014-12-31 | 西北工业大学明德学院 | A kind of collapsible four axle multi-rotor aerocrafts |
| CN104386249A (en) * | 2014-11-17 | 2015-03-04 | 马鞍山市靓马航空科技有限公司 | Multi-rotor unmanned aerial vehicle for fast surveying and surveying method of multi-rotor unmanned aerial vehicle |
| CN105035318A (en) * | 2015-09-01 | 2015-11-11 | 湖南云顶智能科技有限公司 | Multi-rotor unmanned aerial vehicle |
| CN204916176U (en) * | 2015-09-15 | 2015-12-30 | 湖南翼航无人机科技有限公司 | Six spool agricultural unmanned aerial vehicle |
| CN205044951U (en) * | 2015-10-22 | 2016-02-24 | 深圳市科卫泰实业发展有限公司 | Folding many rotor unmanned aerial vehicle of horn |
| CN105366048A (en) * | 2015-11-30 | 2016-03-02 | 湖北易瓦特科技股份有限公司 | Multi-rotor unmanned aerial vehicle |
| US20160122016A1 (en) * | 2014-10-30 | 2016-05-05 | Ecole Polytechnique Federale De Lausanne (Epfl) | Foldable and self-deployable aerial vehicle |
| CN206141811U (en) * | 2016-10-11 | 2017-05-03 | 中山市卡邦碳纤维材料制品有限公司 | Six spool fine foldable unmanned aerial vehicle in carbon |
-
2016
- 2016-10-11 CN CN201610886151.0A patent/CN106240795A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2233393A2 (en) * | 2009-03-23 | 2010-09-29 | Gregor Schnoell | Locking system |
| CN204056294U (en) * | 2014-09-12 | 2014-12-31 | 西北工业大学明德学院 | A kind of collapsible four axle multi-rotor aerocrafts |
| US20160122016A1 (en) * | 2014-10-30 | 2016-05-05 | Ecole Polytechnique Federale De Lausanne (Epfl) | Foldable and self-deployable aerial vehicle |
| CN104386249A (en) * | 2014-11-17 | 2015-03-04 | 马鞍山市靓马航空科技有限公司 | Multi-rotor unmanned aerial vehicle for fast surveying and surveying method of multi-rotor unmanned aerial vehicle |
| CN105035318A (en) * | 2015-09-01 | 2015-11-11 | 湖南云顶智能科技有限公司 | Multi-rotor unmanned aerial vehicle |
| CN204916176U (en) * | 2015-09-15 | 2015-12-30 | 湖南翼航无人机科技有限公司 | Six spool agricultural unmanned aerial vehicle |
| CN205044951U (en) * | 2015-10-22 | 2016-02-24 | 深圳市科卫泰实业发展有限公司 | Folding many rotor unmanned aerial vehicle of horn |
| CN105366048A (en) * | 2015-11-30 | 2016-03-02 | 湖北易瓦特科技股份有限公司 | Multi-rotor unmanned aerial vehicle |
| CN206141811U (en) * | 2016-10-11 | 2017-05-03 | 中山市卡邦碳纤维材料制品有限公司 | Six spool fine foldable unmanned aerial vehicle in carbon |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107521685A (en) * | 2017-09-20 | 2017-12-29 | 首航国翼（武汉）科技有限公司 | Foldable multiaxis unmanned plane |
| DE102019128202B4 (en) | 2019-10-18 | 2023-12-07 | Emqopter GmbH | System and method for ad-hoc configuration of a modular multicopter |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206141811U (en) | Six spool fine foldable unmanned aerial vehicle in carbon | |
| CN106240795A (en) | The fine six collapsible unmanned planes of axle of carbon | |
| CN205872469U (en) | Unmanned aerial vehicle that can long -range input object | |
| CN106005357A (en) | Multipurpose unmanned aerial vehicle | |
| CN206813288U (en) | A kind of unmanned plane of plug type horn | |
| CN207334515U (en) | A kind of assembly type lamp stand | |
| CN206417177U (en) | Machine body cover and unmanned plane | |
| CN106121047B (en) | Source of the gas room | |
| CN205839618U (en) | Automatically reset road cone | |
| CN207000811U (en) | Foldable structure and unmanned plane | |
| CN204464785U (en) | A kind of multifunction power cabinet | |
| CN205440857U (en) | Helicopter skid formula undercarriage | |
| CN210777787U (en) | Elevator maintenance warning sign | |
| CN206528617U (en) | A kind of plant protection unmanned plane radiating water-proof ventilation road structure | |
| CN208216984U (en) | multi-rotor unmanned aerial vehicle | |
| CN209553085U (en) | A kind of vehicle roof box Unclosing structure | |
| CN206417122U (en) | Scooter bar assembly and the scooter that can freely assemble based on the car bar assembly | |
| CN207613338U (en) | Multifunctional trolley case | |
| CN207174301U (en) | One kind has multi-functional solar energy takeaway box | |
| CN206984335U (en) | A kind of medicine-chest rises and falls posture plant protection unmanned plane | |
| CN205854463U (en) | The unmanned aerial vehicle of diversification purposes | |
| CN106005468A (en) | Integrated all-in-one unmanned aerial vehicle with trolley | |
| CN207045746U (en) | A kind of cloakroom | |
| CN209487107U (en) | A kind of warning sign | |
| CN207580012U (en) | Vehicle seat and riding cycle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161221 |
|
| RJ01 | Rejection of invention patent application after publication |