CN108528694A - A kind of novel unmanned plane - Google Patents
A kind of novel unmanned plane Download PDFInfo
- Publication number
- CN108528694A CN108528694A CN201710332985.1A CN201710332985A CN108528694A CN 108528694 A CN108528694 A CN 108528694A CN 201710332985 A CN201710332985 A CN 201710332985A CN 108528694 A CN108528694 A CN 108528694A
- Authority
- CN
- China
- Prior art keywords
- laminate
- rack
- motor
- unmanned plane
- horn
- 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
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 14
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 14
- 229910000975 Carbon steel Inorganic materials 0.000 claims description 3
- 239000010962 carbon steel Substances 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 3
- 230000005611 electricity Effects 0.000 description 3
- 238000007689 inspection Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 125000006850 spacer group Chemical group 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
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- 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
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of novel unmanned planes, including carbon pipe horn, motor, propeller and rack, four sides of the rack are installed with carbon pipe horn, and rack by the first laminate and second layer board group at, the side of first laminate and the second laminate is provided with side plate, it is provided with horn pipe clamp between first laminate and four corners of the second laminate, and horn pipe clamp is fixed on by M3 screws on the first laminate and the second laminate, it is provided with battery tray above the rack, and battery is provided with above battery tray, GPS signal antenna is arranged in the side of the battery, one end of the carbon pipe horn is provided with motor cabinet, and the both sides up and down of motor cabinet are both provided with motor, it is provided with propeller on the output end of the motor.The present invention uses three ply board duplex, and the first laminate of side plate firm link, the second laminate, overall structure is more secured, and internal circuit is effectively protected, more beautiful.
Description
Technical field
The present invention relates to air vehicle technique field, specifically a kind of novel unmanned plane.
Background technology
Overhead transmission line frame scale is growing in recent years, since its coverage area is wide, it is multiple to pass through region landform
Miscellaneous and natural environment is severe, and modern power systems safety and stability fortune cannot be increasingly met by the way of artificial regular visit
Capable needs.The overhead transmission line inspection work that develops into of unmanned air vehicle technique provides new platform.Utilize UAV flight
Inspection device carries out line walking, realizes, safety patrol inspection quick to transmission line of electricity.
Four axis of majority, six axis aircraft, coaxial double-oar aircraft at present.Due to the use of electric drive, fuselage is overweight, continuation of the journey
Energy force difference, undercarriage cannot be packed up, and cruise is taken pictures there are dead angle, and holder has a single function, and there are limitations.
Invention content
The purpose of the present invention is to provide a kind of novel unmanned planes, to solve unmanned plane in the prior art due to the use of electricity
Power drive, fuselage is overweight, and cruising ability is poor, and undercarriage cannot be packed up, and cruise is taken pictures there are dead angle, and holder has a single function, and exists
The problems such as limitation.
To achieve the above object, the present invention provides the following technical solutions：
Four sides of a kind of novel unmanned plane, including carbon pipe horn, motor, propeller and rack, the rack are fixedly mounted
Have a carbon pipe horn, and rack by the first laminate and second layer board group at the side of first laminate and the second laminate is provided with
It is provided with horn pipe clamp between four corners of side plate, first laminate and the second laminate, and horn pipe clamp passes through M3 screws
It is fixed on the first laminate and the second laminate, battery tray, and the top setting of battery tray is provided with above the rack
There are battery, the side of the battery that GPS signal antenna is set, one end of the carbon pipe horn is provided with motor cabinet, and motor cabinet
Both sides up and down be both provided with motor, propeller is provided on the output end of the motor, in-built electrical is provided on the motor
It adjusts, the bottom of the rack is provided with third laminate, and is provided with holder below third laminate, and cloud is provided at the top of holder
The two bottom sides of platform Quick Release plate, the third laminate are provided with operation of landing gear.
Further, the motor and propeller are uniaxial connect.
Further, it is provided with holder block on the holder Quick Release plate to disassemble, and holder block is disassembled and consolidated across third laminate
It is fixed.
Further, the operation of landing gear passes through limit pin connection with third laminate.
Further, the propeller using 1047 the positive and negative paddle of high efficiency, and propeller select carbon steel material system
At.
Further, the rack is internally provided with flight controller, and flight controller selects embedded STM32 mono-
Piece movement piece.
Compared with prior art, the beneficial effects of the invention are as follows：
Using three ply board duplex, the first laminate of side plate firm link, the second laminate, overall structure is more secured, interior
Portion's circuit is effectively protected, more beautiful；
Increase horn pipe clamp and the first laminate, the second laminate contact area increases unmanned plane stability, using upper and lower screw
It is fixed simultaneously, it is convenient to overhaul；
Using single shaft, paddle designs altogether, and horn torque is offset by double paddles, reduces unmanned plane volume, easy to carry；
Holder Quick-dismantle component optimizes, and Quick-dismantle component can carry arbitrary holder, increase such unmanned plane versatility；
So that undercarriage is not exclusively packed up with spacer pin by optimizing operation of landing gear, is limited in propeller on holder
Under, successfully solve shooting blind angle amount, undercarriage propeller collision problem.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of novel unmanned plane of the present invention；
Fig. 2 is a kind of side view of novel unmanned plane of the present invention；
Fig. 3 is a kind of structural schematic diagram of the propeller of novel unmanned plane of the present invention；
Fig. 4 is a kind of structural schematic diagram of the rack of novel unmanned plane of the present invention；
Fig. 5 is a kind of structural schematic diagram of the holder of novel unmanned plane of the present invention.
In figure：1, in-built electrical tune；2, motor cabinet；3, carbon pipe horn；4, horn pipe clamp；5, motor；6, propeller；7、GPS
Signal antenna；8, the first laminate；9, the second laminate；10, battery tray；11, battery；12, holder；13, third laminate；14, cloud
Platform Fast detachable unit；15, operation of landing gear；16, side plate；17, M3 screws；18, rack；19, holder Quick Release plate.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Please refer to Fig.1~5, in the embodiment of the present invention, a kind of novel unmanned plane, including carbon pipe horn 3, motor 5, propeller
6 and rack 18, four sides of the rack 18 are installed with carbon pipe horn 3, and rack 18 is by the first laminate 8 and the second laminate 9
Composition, the side of first laminate, 8 and second laminate 9 are provided with side plate 16, increase the first laminate 8 and second by side plate 16
Contact area between laminate 9 is provided with horn pipe clamp 4 between four corners of first laminate, 8 and second laminate 9, and
Horn pipe clamp 4 is fixed on by M3 screws 17 on the first laminate 8 and the second laminate 9, and the top of the rack 18 is provided with battery
Pallet 10, and the top of battery tray 10 is provided with battery 11, the side setting GPS signal antenna 7 of the battery 11, the carbon
One end of pipe horn 3 is provided with motor cabinet 2, and the both sides up and down of motor cabinet 2 are both provided with motor 5, the output end of the motor 5
On be provided with propeller 6, in-built electrical tune 1 is provided on the motor 5, pass through in-built electrical tune 1 adjust two motors 5 output work
Rate makes the velocity of rotation of upper and lower two propellers 6 be consistent, and the bottom of the rack 18 is provided with third laminate 13, and
13 lower section of three ply board is provided with holder 12, and the top of holder 12 is provided with holder Quick Release plate 19, the bottom of the third laminate 13
Portion both sides are provided with operation of landing gear 15.
The motor 5 and propeller 6 be it is uniaxial connect, holder block is provided on the holder Quick Release plate 19 and disassembles 14, and
Holder block disassembles 14 and third laminate 13 is passed through to fix, and the operation of landing gear 15 is with third laminate 13 by limiting pin connection, institute
Propeller 6 is stated using the 1047 positive and negative paddle of high efficiency, and propeller 6 selects carbon steel material to be made, the rack 18 it is interior
Portion is provided with flight controller, and flight controller selects embedded STM32 singlechip chips.
The present invention operation principle be：The novel unmanned plane in use, the first laminate 8 in rack 18 and
Between two laminates 9 setting for control device, by motor driving electric wire connect with motor 5 across carbon pipe horn 3, avoid electric wire
It is exposed to improve the service life of circuit outside, it is conveniently replaceable in the top of the first laminate 8 by being arranged battery 11, original-pack
When battery is without electricity, battery is directly replaced, original-pack battery is removed into charging, cruising ability is improved, also avoids battery in unmanned plane
It is damaged in drop event, control signal is received by GPS signal antenna, signal is fed back into the control device inside rack 18,
The motor 5 adjusted on four axis is driven the rotation of propeller 6 to adjust flying height and the direction of unmanned plane by control device, is passed through
Cooperation being rapidly assembled and disassembled convenient for holder 12 of holder Quick Release plate 19 and holder Fast detachable unit 14.
It is obvious to a person skilled in the art that invention is not limited to the details of the above exemplary embodiments, 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, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the present invention is by appended power
Profit requires rather than above description limits, it is intended that all by what is fallen within the meaning and scope of the equivalent requirements of the claims
Variation is included within the present invention.Any reference signs in the claims should not be construed as limiting the involved claims.
Claims (6)
1. a kind of novel unmanned plane, including carbon pipe horn (3), motor (5), propeller (6) and rack (18), which is characterized in that
Four sides of the rack (18) are installed with carbon pipe horn (3), and rack (18) is by the first laminate (8) and the second laminate (9)
The side of composition, first laminate (8) and the second laminate (9) is provided with side plate (16), first laminate (8) and the second layer
Horn pipe clamp (4) is provided between four corners of plate (9), and horn pipe clamp (4) is fixed on first layer by M3 screws (17)
On plate (8) and the second laminate (9), battery tray (10) is provided with above the rack (18), and battery tray (10) is upper
Side is provided with battery (11), and the side setting GPS signal antenna (7) of the battery (11), one end of the carbon pipe horn (3) is set
It is equipped with motor cabinet (2), and the both sides up and down of motor cabinet (2) are both provided with motor (5), are arranged on the output end of the motor (5)
There is propeller (6), in-built electrical tune (1) is provided on the motor (5), the bottom of the rack (18) is provided with third laminate
(13), it and below third laminate (13) is provided with holder (12), and is provided with holder Quick Release plate (19), institute at the top of holder (12)
The two bottom sides for stating third laminate (13) are provided with operation of landing gear (15).
2. a kind of novel unmanned plane according to claim 1, which is characterized in that the motor (5) and propeller (6) is singly
Axis connection.
3. a kind of novel unmanned plane according to claim 1, which is characterized in that be provided on the holder Quick Release plate (19)
Holder block is disassembled (14), and holder block is disassembled (14) and fixed across third laminate (13).
4. a kind of novel unmanned plane according to claim 1, which is characterized in that the operation of landing gear (15) and third layer
Plate (13) is by limiting pin connection.
5. a kind of novel unmanned plane according to claim 1, which is characterized in that the propeller (6) is using 1047
The positive and negative paddle of high efficiency, and propeller (6) select carbon steel material be made.
6. a kind of novel unmanned plane according to claim 1, which is characterized in that being internally provided with for the rack (18) is winged
Line control unit, and flight controller selects embedded STM32 singlechip chips.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710332985.1A CN108528694A (en) | 2017-05-12 | 2017-05-12 | A kind of novel unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710332985.1A CN108528694A (en) | 2017-05-12 | 2017-05-12 | A kind of novel unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108528694A true CN108528694A (en) | 2018-09-14 |
Family
ID=63489628
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710332985.1A Pending CN108528694A (en) | 2017-05-12 | 2017-05-12 | A kind of novel unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108528694A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104149971A (en) * | 2013-05-13 | 2014-11-19 | 湖北易瓦特科技有限公司 | Unmanned plane |
| CN203996886U (en) * | 2014-06-30 | 2014-12-10 | 上海汇联皆景信息科技有限公司 | A kind of four axle eight oars aircraft of taking photo by plane |
| CN205131646U (en) * | 2015-11-16 | 2016-04-06 | 湖南云顶智能科技有限公司 | Big load unmanned aerial vehicle |
| CN105857603A (en) * | 2016-04-08 | 2016-08-17 | 四川克瑞斯航空科技有限公司 | Multi-rotor wing unmanned aerial vehicle of which booms can be folded |
| US20160325834A1 (en) * | 2015-05-07 | 2016-11-10 | Curtis Asa Foster | In-flight battery recharging system for an unmanned aerial vehicle |
-
2017
- 2017-05-12 CN CN201710332985.1A patent/CN108528694A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104149971A (en) * | 2013-05-13 | 2014-11-19 | 湖北易瓦特科技有限公司 | Unmanned plane |
| CN203996886U (en) * | 2014-06-30 | 2014-12-10 | 上海汇联皆景信息科技有限公司 | A kind of four axle eight oars aircraft of taking photo by plane |
| US20160325834A1 (en) * | 2015-05-07 | 2016-11-10 | Curtis Asa Foster | In-flight battery recharging system for an unmanned aerial vehicle |
| CN205131646U (en) * | 2015-11-16 | 2016-04-06 | 湖南云顶智能科技有限公司 | Big load unmanned aerial vehicle |
| CN105857603A (en) * | 2016-04-08 | 2016-08-17 | 四川克瑞斯航空科技有限公司 | Multi-rotor wing unmanned aerial vehicle of which booms can be folded |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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 |
Application publication date: 20180914 |
|
| RJ01 | Rejection of invention patent application after publication |