CN108248852A - Exerciser is passed through in unmanned plane racing - Google Patents
Exerciser is passed through in unmanned plane racing Download PDFInfo
- Publication number
- CN108248852A CN108248852A CN201810162774.2A CN201810162774A CN108248852A CN 108248852 A CN108248852 A CN 108248852A CN 201810162774 A CN201810162774 A CN 201810162774A CN 108248852 A CN108248852 A CN 108248852A
- Authority
- CN
- China
- Prior art keywords
- armlet
- rectangle
- circular rotor
- exerciser
- unmanned plane
- 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
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 10
- 238000000034 method Methods 0.000 abstract description 3
- 230000006378 damage Effects 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000000306 component Substances 0.000 description 1
- 239000008358 core component Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 230000008569 process Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- 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)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Rehabilitation Tools (AREA)
Abstract
The present invention relates to unmanned air vehicle technique fields more particularly to a kind of unmanned plane racing to pass through exerciser, including upper rectangle armlet, lower rectangle armlet, upper circular rotor armlet, lower circular rotor armlet, motor and propeller；The angular position of inside four of the upper rectangle armlet is connected with the upper circular rotor armlet respectively；The angular position of inside four of the lower rectangle armlet is connected with the lower circular rotor armlet respectively；Bottom plate there are one being set in the center of descended rectangle armlet, the both sides of the bottom plate are connected with reinforcing plate respectively；It is linked together between the upper rectangle armlet and lower rectangle armlet by connecting pole；The motor is four, and in the reinforcing plate for the center position for being separately mounted to lower circular rotor armlet, the output terminal of motor is equipped with the propeller.By the unique design to rack shape, the stability and reliability of body are enhanced, reduces duties, improves the safety of flight.
Description
Technical field
The present invention relates to unmanned air vehicle technique fields more particularly to a kind of unmanned plane racing to pass through exerciser.
Background technology
FPV full name " First Person View ", FPV are often referred to the unmanned plane by first person control flight,
Also known as pass through machine.Stablize from general big well known pursuit it is different with the machine of taking photo by plane of shooting ability, FPV pursuits be speed,
Flexibly and flight experience.And first person manipulation is carried out by image transmission system, realizes and is virtually perfectly combined with real.
Tradition, which passes through rack, to be formed using straight panel horn, the fine polygon central plate of four axis of carbon, and shortcoming is that stability is inadequate, focus point control
It makes bad, is unfavorable for battery and flies control protection, and battery can contact ground friction is promoted to cause to damage when putting, by collision
When can cause fly control and the of short duration failure of critical component.In flight racing, the movement of more rotors all relies on the speed of propeller
Change and adjustment torque, the leakage of blade are easy to lead to flight safety, lead to air crash.And the mechanical structure of more rotors
Reliability is low, and without movable part in mechanism, abrasion is also easy to produce in flight course.Electron speed regulator, battery, blade and fly control
Damage is easy to replace so that it is easy to replace.
Invention content
It is an object of the invention to overcome the shortcomings of above-mentioned technology, and a kind of unmanned plane racing is provided and passes through exerciser, energy
It enough protects unmanned plane blade and flies control.
The present invention to achieve the above object, using following technical scheme：Exerciser, feature are passed through in a kind of unmanned plane racing
It is：Including upper rectangle armlet, lower rectangle armlet, upper circular rotor armlet, lower circular rotor armlet, motor and spiral
Paddle；The angular position of inside four of the upper rectangle armlet is connected with the upper circular rotor armlet respectively；Under described
The angular position of inside four of rectangle armlet is connected with the lower circular rotor armlet respectively；In descended rectangle armlet
Center is set there are one bottom plate, and the both sides of the bottom plate are connected with reinforcing plate respectively, the reinforcing plate extend to it is lower just
Round rotor armlet is interior and is classified as the semicircle of two same sizes；Lead between the upper rectangle armlet and lower rectangle armlet
Connecting pole is crossed to link together；The motor be four, be separately mounted to lower circular rotor armlet center position plus
On strong plate, the output terminal of motor is equipped with the propeller；Controller and battery are installed on the bottom plate.
Preferably, two blocks of camera head protecting plates are equipped between the upper rectangle armlet, lower rectangle armlet, are taken the photograph at described two pieces
As being equipped with camera between head protection plate.
Preferably, it is linked together between the upper circular rotor armlet, lower circular rotor armlet by connecting pole.
Preferably, the angle of inside four of the upper rectangle armlet and lower rectangle armlet is respectively chamfering, chamfering radian with
Upper circular rotor armlet is identical with the radian of lower circular rotor armlet.
The beneficial effects of the invention are as follows:Relative to the prior art, by the unique design to rack shape, for protecting nothing
Man-machine blade and the fixing device (electricity is mechanical, electrical to be adjusted, flies control etc.) for flying control, enhance the stability and reliability of body, reduce duties
Property improves the safety of flight.Technological process is reduced, simple for structure firm, layout is reasonable, and installation and removal are convenient, peace
It is complete reliable.
Description of the drawings
Fig. 1 looks up exploded view for the present invention's；
Fig. 2 is the top exploded view of the present invention；
Fig. 3 is the stereogram of the present invention.
Specific embodiment
Below in conjunction with the accompanying drawings and the preferred embodiment specific embodiment that the present invention will be described in detail.As shown in Figure 1-Figure 3, one
Exerciser is passed through in kind unmanned plane racing, including upper rectangle armlet 1, lower rectangle armlet 2, upper circular rotor armlet 3, lower circular
Rotor armlet 4, motor 5 and propeller 6；Upper rectangle armlet 1, lower rectangle armlet 2, upper circular rotor armlet 3, lower circular
Rotor armlet 4 is laminated by epoxy resin by carbon cloth and bonded, and forms carbon fiber board, then form one by CNC cutting process
Body high-strength carbon fiber rack.The angular position of inside four of the upper rectangle armlet is connected with the upper positive round respectively
Shape rotor armlet；The angular position of inside four of the lower rectangle armlet is connected with the lower circular rotor shield respectively
Arm；It being set in the center of descended rectangle armlet there are one bottom plate 7, the both sides of the bottom plate are connected with reinforcing plate 8 respectively,
The reinforcing plate extends in lower circular rotor armlet and is classified as the semicircle of two same sizes；The upper rectangle shield
It is linked together between arm and lower rectangle armlet by connecting pole 9；The motor is four, is separately mounted to lower circular rotor
In the reinforcing plate of the center position of armlet, the output terminal of motor is equipped with the propeller；Control is installed on the bottom plate
Device and battery 10.Upper rectangle armlet, lower rectangle armlet, upper circular rotor armlet, lower circular rotor armlet play simultaneously
The purpose of the intermediate blade of protection.The solar panel of independent design connection, it is therefore intended that battery is hidden within machine frame inside, so as to reduce
Injury of the aircraft air crash to battery.It can also achieve the effect that lower the center of gravity.
Upper circular rotor armlet and lower circular rotor armlet can protect blade and motor, upper rectangle armlet and lower square
Shape armlet can make whole more secured, and core component such as battery and electric control part among rack are all by upper circular rotor
Armlet, lower circular rotor armlet are protected, and effectively unmanned plane is integrally all protected.
As Figure 2-3, two blocks of camera head protecting plates 11 are equipped between the upper rectangle armlet, lower rectangle armlet, in institute
It states and camera 12 is installed between two blocks of camera head protecting plates.The upper circular rotor armlet, lower circular rotor armlet it
Between linked together by connecting pole.The motor is brushless motor, is additionally provided with to control motor speed in the motor
Electron speed regulator.The flight control system, battery, GPS positioning module and equipment of taking photo by plane are fixedly mounted by insulated screw
On the fixation bottom plate of frame central position, the flight control system, GPS positioning module and take photo by plane equipment and fixed bottom plate
Contain signal line in connecting line road.
The above is only the preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art
For member, various improvements and modifications may be made without departing from the principle of the present invention, these improvements and modifications also should
It is considered as protection scope of the present invention.
Claims (4)
1. exerciser is passed through in a kind of unmanned plane racing, it is characterised in that：Including upper rectangle armlet, lower rectangle armlet, upper circular
Rotor armlet, lower circular rotor armlet, motor and propeller；The angular position difference of inside four of the upper rectangle armlet
It is connected with the upper circular rotor armlet；The angular position of inside four of the lower rectangle armlet is connected with respectively
The lower circular rotor armlet；It is set in the center of descended rectangle armlet there are one bottom plate, the both sides of the bottom plate are distinguished
Reinforcing plate is connected with, the reinforcing plate extends in lower circular rotor armlet and be classified as the half of two same sizes
It is round；It is linked together between the upper rectangle armlet and lower rectangle armlet by connecting pole；The motor is four, is pacified respectively
In the reinforcing plate of the center position of lower circular rotor armlet, the output terminal of motor is equipped with the propeller；It is described
Controller and battery are installed on bottom plate.
2. exerciser is passed through in unmanned plane racing according to claim 1, it is characterised in that：The upper rectangle armlet, lower square
Two blocks of camera head protecting plates are equipped between shape armlet, camera is installed between two blocks of camera head protecting plates.
3. exerciser is passed through in unmanned plane racing according to claim 1, it is characterised in that：The upper circular rotor shield
It is linked together between arm, lower circular rotor armlet by connecting pole.
4. exerciser is passed through in unmanned plane racing according to claim 1, it is characterised in that：The upper rectangle armlet and lower square
The angle of inside four of shape armlet is respectively chamfering, chamfering radian and upper circular rotor armlet and lower circular rotor armlet
Radian is identical.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810162774.2A CN108248852A (en) | 2018-02-26 | 2018-02-26 | Exerciser is passed through in unmanned plane racing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810162774.2A CN108248852A (en) | 2018-02-26 | 2018-02-26 | Exerciser is passed through in unmanned plane racing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108248852A true CN108248852A (en) | 2018-07-06 |
Family
ID=62745404
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810162774.2A Pending CN108248852A (en) | 2018-02-26 | 2018-02-26 | Exerciser is passed through in unmanned plane racing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108248852A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109625254A (en) * | 2018-12-28 | 2019-04-16 | 浙江星米体育有限公司 | Sports class unmanned plane |
| CN112874753A (en) * | 2021-02-18 | 2021-06-01 | 陶霖密 | Integrated platy laminated rack unmanned aerial vehicle |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203111495U (en) * | 2012-11-16 | 2013-08-07 | 哈尔滨飞机工业集团有限责任公司 | Helicopter tail speed-reducer cowling |
| CN105366045A (en) * | 2015-12-17 | 2016-03-02 | 湖南云顶智能科技有限公司 | Multi-rotor-wing unmanned aerial vehicle |
| US20160229530A1 (en) * | 2014-11-24 | 2016-08-11 | Amazon Technologies, Inc. | Unmanned aerial vehicle protective frame configuration |
| CN107618650A (en) * | 2017-09-18 | 2018-01-23 | 北海勇士三维科技有限公司 | 3D printing unmanned plane frame and unmanned plane |
| CN208119429U (en) * | 2018-02-26 | 2018-11-20 | 天津中德应用技术大学 | Exerciser is passed through in unmanned plane racing |
-
2018
- 2018-02-26 CN CN201810162774.2A patent/CN108248852A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203111495U (en) * | 2012-11-16 | 2013-08-07 | 哈尔滨飞机工业集团有限责任公司 | Helicopter tail speed-reducer cowling |
| US20160229530A1 (en) * | 2014-11-24 | 2016-08-11 | Amazon Technologies, Inc. | Unmanned aerial vehicle protective frame configuration |
| CN105366045A (en) * | 2015-12-17 | 2016-03-02 | 湖南云顶智能科技有限公司 | Multi-rotor-wing unmanned aerial vehicle |
| CN107618650A (en) * | 2017-09-18 | 2018-01-23 | 北海勇士三维科技有限公司 | 3D printing unmanned plane frame and unmanned plane |
| CN208119429U (en) * | 2018-02-26 | 2018-11-20 | 天津中德应用技术大学 | Exerciser is passed through in unmanned plane racing |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109625254A (en) * | 2018-12-28 | 2019-04-16 | 浙江星米体育有限公司 | Sports class unmanned plane |
| CN112874753A (en) * | 2021-02-18 | 2021-06-01 | 陶霖密 | Integrated platy laminated rack unmanned aerial vehicle |
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| 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 | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180706 |