CN107323661A - A kind of axle aircraft of multifunctional portable six - Google Patents
A kind of axle aircraft of multifunctional portable six Download PDFInfo
- Publication number
- CN107323661A CN107323661A CN201710531503.5A CN201710531503A CN107323661A CN 107323661 A CN107323661 A CN 107323661A CN 201710531503 A CN201710531503 A CN 201710531503A CN 107323661 A CN107323661 A CN 107323661A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- multifunctional portable
- axle aircraft
- carbon fiber
- side wall
- 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
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 21
- 239000004917 carbon fiber Substances 0.000 claims abstract description 21
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract description 21
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 18
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 17
- 238000013016 damping Methods 0.000 claims description 8
- 229910000838 Al alloy Inorganic materials 0.000 claims description 7
- 239000000956 alloy Substances 0.000 claims description 6
- 230000005540 biological transmission Effects 0.000 claims description 6
- 238000009434 installation Methods 0.000 claims description 5
- 239000000463 material Substances 0.000 claims description 3
- 238000013461 design Methods 0.000 abstract description 3
- 238000012545 processing Methods 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000013507 mapping Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 208000010138 Diastema Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 210000000475 diastema Anatomy 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000001629 suppression Effects 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/06—Undercarriages fixed
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Purses, Travelling Bags, Baskets, Or Suitcases (AREA)
Abstract
The invention discloses a kind of axle aircraft of multifunctional portable six, including fuselage, the body upper, which is provided with below antenna, fuselage to be provided with below drawer plate, drawer plate by resilient pin, is provided with H type foot stools；Fuselage surrounding is uniformly provided with six carbon beam fixed seats, and carbon beam fixed seat both sides are provided with side wall, and side wall is connected by axle with fuselage；Horn carbon fiber pipe is connected by spinner with carbon beam fixed seat, and the midpoint of horn carbon fiber pipe and side wall contact surface is provided with projection；Multiple bay plate is installed, fuselage roof is provided with above detachable top cover, top cover and is welded with handheld ring on fuselage.The present invention is reasonable in design, is designed using 6 axles, and take-off weight is high, using full carbon fiber fuselage, and fuselage weight is light, can belongings it is many；Using folding horn, good portability；Fixed H-shaped foot stool, the dust-proof processing of fuselage main body improves stability and reliability.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, specifically a kind of axle aircraft of multifunctional portable six.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned aircraft that presetting apparatus is manipulated.Unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, nobody
Machine is divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+sector application is that unmanned plane has really just been needed；At present taking photo by plane, agriculture
Industry, plant protection, miniature auto heterodyne, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric power
The application in inspection, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded the purposes of unmanned plane in itself, flourishing state
Family is also in actively extension sector application and development unmanned air vehicle technique.
Existing unmanned aerial vehicle body is generally metal material, and fuselage is heavier, and the thing that can be carried is few.Volume is larger, inconvenience
Take.Function Extension can not be carried out, the functional parts that can be carried are fewer.
The content of the invention
It is an object of the invention to provide a kind of axle aircraft of multifunctional portable six, to solve to propose in above-mentioned background technology
The problem of.
To achieve the above object, the present invention provides following technical scheme：
A kind of axle aircraft of multifunctional portable six, including fuselage, the body upper, which is provided with below antenna, fuselage, passes through elasticity
Latch is provided with below drawer plate, drawer plate and is provided with H type foot stools；Fuselage surrounding is uniformly provided with six carbon beam fixed seats, carbon beam
Fixed seat both sides are provided with side wall, and side wall is connected by axle with fuselage；Horn carbon fiber pipe is connected by spinner with carbon beam fixed seat,
The midpoint of horn carbon fiber pipe and side wall contact surface is provided with projection；Multiple bay plate is installed, fuselage roof is installed on fuselage
Have and be welded with handheld ring above detachable top cover, top cover.
It is used as further scheme of the invention：The motor cabinet is aluminum alloy material.
It is used as further scheme of the invention：The spinner is aluminum alloy material.
It is used as further scheme of the invention：Damping washer is provided between the night bolt and drawer plate.
It is used as further scheme of the invention：The damping washer is quality of rubber materials.
It is used as further scheme of the invention：The external diameter of the horn carbon fiber pipe is 30mm.
It is used as further scheme of the invention：The carbon beam fixed seat is inclined upwardly 5 °.
It is used as further scheme of the invention：The detachable base of the H types foot stool bottom carry, it is described detachable
Pipe clamp is fixed with base, pipe clamp is fixedly connected with the threaded rod on H type foot stools.
It is used as further scheme of the invention：The motor cabinet bottom is reserved with pencil transmission mouth, pencil transmission mouth
Shower nozzle is installed.
It is used as further scheme of the invention：Foot stool installation position is reserved with the fuselage.
Compared with prior art, the beneficial effects of the invention are as follows：The present invention is reasonable in design, is designed using 6 axles, take-off weight
Height, using full carbon fiber fuselage, fuselage weight is light, can belongings it is many；Using folding horn, good portability；Fixed H-shaped pin
Frame, the dust-proof processing of fuselage main body improves stability and reliability.
Brief description of the drawings
Fig. 1 is structural representation of the invention.
Fig. 2 is the structural representation of motor cabinet in the present invention.
Fig. 3 is horn carbon fiber pipe in the present invention and the attachment structure schematic diagram of carbon beam fixed seat.
Fig. 4 is the structural representation of night bolt in the present invention.
Fig. 5 is the structural representation of damping washer in the present invention.
Fig. 6 is the structural representation of multiple bay plate in the present invention.
Fig. 7 is the structural representation of top cover in the present invention.
Fig. 8 is the structural representation of motor cabinet bottom.
Fig. 9 is the structural representation that shower nozzle is provided with motor cabinet.
Figure 10 is
In figure：1- motors, 2- motor cabinets, 3- reserves mounting groove position, and 4- carbon beam fixed seats, 5- sides wall, 6- spinners, 7- horns carbon is fine
Dimension pipe, 8- night bolts, 9- damping washers, 10- multiple bay plates, 11- top covers, 12- handheld rings, 13- fuselages, 14- antennas,
15-H type foot stools, 16- shower nozzles, 17- pencils transmission mouth, 18- foot stools installation position.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.It is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
Fig. 1~10, a kind of axle aircraft of multifunctional portable six, including fuselage 13 are referred to, the top of fuselage 13 is installed
There is antenna 14, the lower section of fuselage 13 is provided with below drawer plate, drawer plate by resilient pin 8 and is provided with H types foot stool 15；Fuselage 13
Surrounding is uniformly provided with six carbon beam fixed seats 4, and the both sides of carbon beam fixed seat 4 are provided with side wall 5, and side wall 5 is connected by axle with fuselage 13,
Being folded down for horn carbon fiber pipe 7 can be achieved, high fitness ensures in the operating condition to play external environment condition certain isolation
Effect；Horn carbon fiber pipe 7 is connected by spinner 6 with carbon beam fixed seat 4, is tieed up in the case where horn carbon fiber pipe 7 is in deployed condition
Pulling force is held, the midpoint of horn carbon fiber pipe 7 and the contact surface of side wall 5 is provided with projection, and convenient use person's fix in position is prevented effectively from void
Position and the risk that loosening is produced under the effect of certain external force；Multiple bay plate 10 is installed, compatible first regards on fuselage 13
Angle camera and a variety of mappings are singly anti-；The top of fuselage 13 is provided with detachable top cover 11, convenient to fly in control, electric tune, battery etc.
The installing/dismounting that portion is built；The top of top cover 11 is welded with handheld ring 12, is convenient for carrying.
Further, motor cabinet 2 of the present invention is aluminum alloy material, can provide the reliability for unmanned plane dynamical system
Fastening mounting platform, the compatible outer diameter 30mm standard carbon fiber arm of force.
Further, spinner 6 of the present invention is aluminum alloy material, and pulling force is maintained in the case where horn is in deployed condition,
The midpoint small design protrusion of spiral arm contact surface, convenient use person's fix in position is prevented effectively from diastema and in certain outer masterpiece
With the lower risk for producing and loosening.
Further, damping washer 9 is provided between night bolt 8 and drawer plate of the present invention, aircraft is effectively reduced
The damage that the vibrations landed are brought to integral body.
Further, damping washer 9 of the present invention is quality of rubber materials, with good effectiveness in vibration suppression.
Further, the external diameter of horn carbon fiber pipe 7 of the present invention is 30mm, lightweight, high mechanical strength.
Further, carbon beam fixed seat 4 of the present invention is inclined upwardly 5 °, optimizing pneumatic layout, using friction and insertion
Horn carbon fiber pipe 7 is fixed spacing mode, it is ensured that horn carbon fiber pipe 7 will not be because rotating production in the case where working long hours
The raw influence to aeroperformance provides stability dual redundant simultaneously.
Further, it is solid on the detachable base of bottom carry of H types foot stool 15 of the present invention, the detachable base
Surely pipe clamp is provided with, pipe clamp is fixedly connected with the threaded rod on H types foot stool 15；Replacing X-CAMX series heads, can load Sony
All series are micro- singly to meet different demands.
Further, the bottom of motor cabinet 2 of the present invention is reserved with pencil transmission mouth 17, pencil transmission mouth 17 and is provided with
Shower nozzle 16, can be achieved the machine of taking photo by plane to the conversion of fog machine.
Further, foot stool installation position 18 is reserved with fuselage 13 of the present invention, can be used in bottom board replacing head.
The present invention uses 6 axles, carries integrated aluminium alloy electric support, full carbon fiber fuselage, and use carbon fiber pipe conduct
Horn, fuselage weight is light, power collocation 12S batteries, substantially increases the power of aircraft, improves take-off weight, fuselage main body
Dust-proof processing, good protection is carried out to the part of aircraft.Motor cabinet meets the installation rule of 3508 ~ 8312 grade brushless electric machines
Model, strong applicability.By setting reserved mounting groove position, it is allowed to subsequently support the multidirectional avoidance sensor of large-scale unmanned plane, LED lamplight
Deng the extension of functor.
The present invention can carry out installing functional module additional according to actual needs, and practicality is very good, disclosure satisfy that the overwhelming majority
The need of work of current unmanned plane during flying device.
It is obvious to a person skilled in the art that the invention is not restricted to the details of above-mentioned one exemplary embodiment, Er Qie
In the case of without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter
From the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, the scope of the present invention is by appended power
Profit is required rather than described above is limited, it is intended that all in the implication and scope of the equivalency of claim by falling
Change is included in the present invention.Any reference in claim should not be considered as to the claim involved by limitation.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that for clarity, those skilled in the art should
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It may be appreciated other embodiment.
Claims (10)
1. a kind of axle aircraft of multifunctional portable six, including fuselage, it is characterised in that：The body upper is provided with antenna, machine
It is provided with below body by resilient pin below drawer plate, drawer plate and H type foot stools is installed；Fuselage surrounding is uniformly provided with six carbon
Bar fixed seat, carbon beam fixed seat both sides are provided with side wall, and side wall is connected by axle with fuselage；Horn carbon fiber pipe passes through spinner and carbon
Bar fixed seat is connected, and the midpoint of horn carbon fiber pipe and side wall contact surface is provided with projection；Multiple bay plate is installed on fuselage,
Fuselage roof is provided with above detachable top cover, top cover and is welded with handheld ring.
2. the axle aircraft of multifunctional portable six according to claim 1, it is characterised in that：The motor cabinet is aluminium alloy material
Matter.
3. the axle aircraft of multifunctional portable six according to claim 1, it is characterised in that：The spinner is aluminium alloy material
Matter.
4. the axle aircraft of multifunctional portable six according to claim 1, it is characterised in that：The night bolt and drawer plate
Between be provided with damping washer.
5. the axle aircraft of multifunctional portable six according to claim 4, it is characterised in that：The damping washer is rubber material
Matter.
6. the axle aircraft of multifunctional portable six according to claim 1, it is characterised in that：Outside the horn carbon fiber pipe
Footpath is 30mm.
7. the axle aircraft of multifunctional portable six according to claim 1, it is characterised in that：The carbon beam fixed seat is to updip
Oblique 5 °.
8. the axle aircraft of multifunctional portable six according to claim 1, it is characterised in that：H types foot stool bottom carry
Pipe clamp is fixed with detachable base, the detachable base, pipe clamp is fixedly connected with the threaded rod on H type foot stools.
9. the axle aircraft of multifunctional portable six according to claim 1, it is characterised in that：The motor cabinet bottom is reserved with
Pencil transmits and is provided with shower nozzle on mouth, pencil transmission mouth.
10. the axle aircraft of multifunctional portable six according to claim 1, it is characterised in that：Pin is reserved with the fuselage
Frame installation position.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710531503.5A CN107323661A (en) | 2017-07-03 | 2017-07-03 | A kind of axle aircraft of multifunctional portable six |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710531503.5A CN107323661A (en) | 2017-07-03 | 2017-07-03 | A kind of axle aircraft of multifunctional portable six |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107323661A true CN107323661A (en) | 2017-11-07 |
Family
ID=60197800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710531503.5A Pending CN107323661A (en) | 2017-07-03 | 2017-07-03 | A kind of axle aircraft of multifunctional portable six |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107323661A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101456035B1 (en) * | 2014-09-06 | 2014-11-04 | 최종필 | The rotor arm device of multi-rotor type drone |
| KR101527544B1 (en) * | 2015-01-10 | 2015-06-10 | 최종필 | The multi-rotor type folding drone |
| CN205256650U (en) * | 2015-12-07 | 2016-05-25 | 天津全华时代航天科技发展有限公司 | Rotor beta structure |
| CN205273839U (en) * | 2015-11-30 | 2016-06-01 | 湖北易瓦特科技股份有限公司 | Unmanned aerial vehicle with folding assembly |
| CN205707294U (en) * | 2016-06-27 | 2016-11-23 | 浙江智天科技有限公司 | Folding piece in a kind of horn on Multi-axis aircraft |
| CN205906203U (en) * | 2016-08-24 | 2017-01-25 | 四川建筑职业技术学院 | H type structure can two -way deformation unmanned aerial vehicle |
| CN106379522A (en) * | 2016-10-26 | 2017-02-08 | 辽宁电力建设监理有限公司 | Long-endurance aircraft |
| 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 |
| CN106628158A (en) * | 2017-02-28 | 2017-05-10 | 罗熠 | Antiriot unmanned aerial vehicle |
-
2017
- 2017-07-03 CN CN201710531503.5A patent/CN107323661A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101456035B1 (en) * | 2014-09-06 | 2014-11-04 | 최종필 | The rotor arm device of multi-rotor type drone |
| KR101527544B1 (en) * | 2015-01-10 | 2015-06-10 | 최종필 | The multi-rotor type folding drone |
| CN205273839U (en) * | 2015-11-30 | 2016-06-01 | 湖北易瓦特科技股份有限公司 | Unmanned aerial vehicle with folding assembly |
| CN205256650U (en) * | 2015-12-07 | 2016-05-25 | 天津全华时代航天科技发展有限公司 | Rotor beta structure |
| CN205707294U (en) * | 2016-06-27 | 2016-11-23 | 浙江智天科技有限公司 | Folding piece in a kind of horn on Multi-axis aircraft |
| CN205906203U (en) * | 2016-08-24 | 2017-01-25 | 四川建筑职业技术学院 | H type structure can two -way deformation 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 |
| CN106379522A (en) * | 2016-10-26 | 2017-02-08 | 辽宁电力建设监理有限公司 | Long-endurance aircraft |
| CN106628158A (en) * | 2017-02-28 | 2017-05-10 | 罗熠 | Antiriot unmanned aerial vehicle |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
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Application publication date: 20171107 |