CN110203407A - Six rotor wing unmanned aerial vehicle transmission component mounting structures and installation method - Google Patents
Six rotor wing unmanned aerial vehicle transmission component mounting structures and installation method Download PDFInfo
- Publication number
- CN110203407A CN110203407A CN201910512088.8A CN201910512088A CN110203407A CN 110203407 A CN110203407 A CN 110203407A CN 201910512088 A CN201910512088 A CN 201910512088A CN 110203407 A CN110203407 A CN 110203407A
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- Prior art keywords
- motor
- propeller
- attachment base
- output shaft
- transmission component
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- 238000009434 installation Methods 0.000 title claims abstract description 22
- 230000005540 biological transmission Effects 0.000 title claims abstract description 20
- 238000000034 method Methods 0.000 title claims abstract description 9
- 238000010586 diagram Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Classifications
-
- 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
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
- B64D35/04—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Catching Or Destruction (AREA)
Abstract
The present invention relates to a kind of six rotor wing unmanned aerial vehicle transmission component mounting structures and installation methods, including drone body, it is mounted on the propeller of the armed lever outer end of drone body, armed lever outer end top is provided with mounting groove, propeller is located above armed lever outer end, motor is fixedly installed in mounting groove, the output shaft end of motor connects propeller, filling block is filled between the output shaft periphery of motor and mounting groove, filling block is sleeved on the output shaft of motor, the output shaft of motor, the propeller coaxial heart, the output shaft end of motor is equipped with attachment base, several connecting columns being vertically arranged are evenly distributed on attachment base, the through-hole with connecting column grafting is correspondingly arranged on propeller, the tapped through hole for wearing attachment base is vertically arranged in connecting column, after connecting column and propeller grafting, bolt wears tapped through hole, and pass through nut for attachment base and propeller Connection locking, this transmission component mounting structure is simple, and design is rationally, easy for installation, improves the stability of propeller.
Description
Technical field
The present invention relates to a kind of six rotor wing unmanned aerial vehicle transmission component mounting structures and installation methods.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, can be divided into from technical standpoint definition: unmanned helicopter, nobody six gyroplanes, unmanned multi-rotor aerocraft,
This several major class of unmanned airship, unmanned parasol.
Field is relatively broad being related to currently on the market for unmanned plane, and the development of unmanned plane increases the growth effect of major industry
Rate, wherein six gyroplanes are relatively conventional in the market.
There is installation inconvenience, while unmanned plane armed lever and spiral shell in the transmission component of six gyroplanes currently on the market
Connect single between rotation paddle, connection is whole unstable.
Summary of the invention
The present invention proposes six rotor wing unmanned aerial vehicle transmission component mounting structures of one kind and installation method.
The solution adopted by the present invention to solve the technical problem is that a kind of six rotor wing unmanned aerial vehicle transmission component mounting structures, packet
The propeller of drone body, the armed lever outer end for being mounted on drone body is included, armed lever outer end top is provided with mounting groove,
Propeller is located above armed lever outer end, and motor is fixedly installed in mounting groove, and the output shaft end of motor connects propeller, motor
Output shaft periphery and mounting groove between be filled with filling block, filling block is sleeved on the output shaft of motor, the output shaft of motor,
The propeller coaxial heart, the output shaft end of motor are equipped with attachment base, and several connecting columns being vertically arranged are evenly distributed on attachment base,
It is correspondingly arranged on the through-hole with connecting column grafting on propeller, the tapped through hole for wearing attachment base is vertically arranged in connecting column, connects
After column and propeller grafting, bolt wears tapped through hole, and attachment base is connect locking with propeller by nut.
Further, it is provided with installation protrusion on the shell of the motor, is provided in mounting groove and is carried out with installation protrusion
The shell of the recess portion of grafting, motor locks through screw or bolt and armed lever.
Further, one is made in attachment base and connecting column.
Further, the output shaft of attachment base and motor is bolted or is made one.
Further, drone body lower end is fixedly installed with support frame.
A kind of installation method of six rotor wing unmanned aerial vehicles transmission component mounting structure: to the peace of the armed lever outer end of drone body
Motor is installed in tankage, after the recess portion grafting in installation protrusion and mounting groove, motor locking is being installed by screw or bolt
In slot；Filling is sleeved on the output shaft of motor, attachment base then is installed in the output shaft end in motor；By propeller with
Attachment base is then connect locking with propeller by bolt, nut, to complete to install by the connecting column grafting on attachment base.
Compared with prior art, the invention has the following advantages: structure is simple, design is rationally, easy for installation, improves
The stability of propeller.
Detailed description of the invention
The invention patent is further illustrated with reference to the accompanying drawing.
Fig. 1 is the main view of drone body；
Fig. 2 is the top view of drone body；
Fig. 3 is transmission component structural schematic diagram；
Fig. 4 is partial enlargement structural representation at A in Fig. 1.
In figure: 1- drone body；2- armed lever；3- support frame；4- motor；5- mounting groove；6- propeller；7- motor it is defeated
Shaft；8- connecting rod；9- attachment base；10- through-hole；11- bolt；12- filling block.
Specific embodiment
The present invention is further described with reference to the accompanying drawings and detailed description.
As shown in Figs 1-4, a kind of six rotor wing unmanned aerial vehicle transmission component mounting structures, including drone body, it is mounted on nothing
The propeller of the armed lever outer end of man-machine ontology, armed lever outer end top are provided with mounting groove, and propeller is located on armed lever outer end
It is square, motor is fixedly installed in mounting groove, the output shaft end of motor connects propeller, the output shaft periphery of motor and mounting groove
Between be filled with filling block, filling block is sleeved on the output shaft of motor, output shaft, the propeller coaxial heart of motor, motor
Output shaft end is equipped with attachment base, and several connecting columns being vertically arranged are evenly distributed on attachment base, are correspondingly arranged on propeller
With the through-hole of connecting column grafting, it is vertically arranged the tapped through hole for wearing attachment base in connecting column, after connecting column and propeller grafting, spiral shell
Bolt wears tapped through hole, and attachment base is connect locking with propeller by nut, and multiple connecting columns are corresponding on propeller
Through-hole grafting baking locks bolt, forms multiple spot and fixes, and keeps whole fixation more stable, increases the stability of propeller installation.
In the present embodiment, the inside dimension of the filling block and the output shaft outer dimension of motor are coincide, and filling block
Maximum radius and the differential of radius of mounting groove be bordering on zero so that filling block is by the hole between the output shaft and mounting groove of motor
Gap region is entirely filled, to increase the stability of device.
In the present embodiment, it is provided with installation protrusion on the shell of the motor, is provided in mounting groove and installation protrusion
The recess portion of grafting is carried out, the shell of motor locks through screw or bolt and armed lever.
In the present embodiment, when installing transmission component, motor is fastened through the recess portion in installation protrusion and mounting groove, motor
Movable filling block is directly socketed on output shaft, filling block is directly completely contacted with mounting groove inner wall, while being not in inclined
The phenomenon that shifting, realizes location and installation.
In the present embodiment, one is made in attachment base and connecting column.
In the present embodiment, the output shaft of attachment base and motor is bolted or is made one.
In the present embodiment, drone body lower end is fixedly installed with support frame.
A kind of installation method of six rotor wing unmanned aerial vehicles transmission component mounting structure: to the peace of the armed lever outer end of drone body
Motor is installed in tankage, after the recess portion grafting in installation protrusion and mounting groove, motor locking is being installed by screw or bolt
In slot；Filling is sleeved on the output shaft of motor, attachment base then is installed in the output shaft end in motor；By propeller with
Attachment base is then connect locking with propeller by bolt, nut, to complete to install by the connecting column grafting on attachment base.
In the description of the present invention, it is to be understood that, term " length ", " width ", "upper", "lower", "front", "rear",
The orientation or positional relationship of the instructions such as "left", "right", "vertical", "horizontal", "top", "bottom" "inner", "outside" is based on attached drawing institute
The orientation or positional relationship shown, is merely for convenience of description of the present invention and simplification of the description, rather than the dress of indication or suggestion meaning
It sets or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as to limit of the invention
System.In addition, in the description of the present invention, the meaning of " plurality " is two or more, unless otherwise specifically defined.
The content being not described in detail in this explanation belongs to the prior art well known to professional and technical personnel in the field.
Above-listed preferred embodiment, has been further described the object, technical solutions and advantages of the present invention, is answered
Understand, the foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Within mind and principle, any modification, equivalent replacement, improvement and so on be should all be included in the protection scope of the present invention.
Claims (6)
1. a kind of six rotor wing unmanned aerial vehicle transmission component mounting structures, including drone body, it is mounted on the armed lever of drone body
The propeller of outer end, it is characterised in that: armed lever outer end top is provided with mounting groove, and propeller is located above armed lever outer end,
Be fixedly installed with motor in mounting groove, the output shaft end of motor connects propeller, the output shaft periphery of motor and mounting groove it
Between be filled with filling block, filling block is sleeved on the output shaft of motor, output shaft, the propeller coaxial heart of motor, motor it is defeated
Shaft end is equipped with attachment base out, and several connecting columns being vertically arranged are evenly distributed on attachment base, be correspondingly arranged on propeller with
The through-hole of connecting column grafting, is vertically arranged the tapped through hole for wearing attachment base in connecting column, after connecting column and propeller grafting, bolt
Tapped through hole is worn, and attachment base is connect with propeller by locking by nut.
2. six rotor wing unmanned aerial vehicles transmission component mounting structure according to claim 1, it is characterised in that: the shell of the motor
Be provided with installation protrusion on body, be provided with the recess portion for carrying out grafting with installation protrusion in mounting groove, the shell of motor through screw or
Bolt and armed lever lock.
3. six rotor wing unmanned aerial vehicles transmission component mounting structure according to claim 1, it is characterised in that: attachment base with connect
One is made in column.
4. six rotor wing unmanned aerial vehicles transmission component mounting structure according to claim 3, it is characterised in that: attachment base and motor
Output shaft be bolted or be made one.
5. six rotor wing unmanned aerial vehicles transmission component mounting structure according to claim 1, it is characterised in that: under drone body
End is fixedly installed with support frame.
6. a kind of installation method of six rotor wing unmanned aerial vehicle transmission component mounting structures, using six rotor as claimed in claim 2
Unmanned plane transmission component mounting structure, it is characterised in that: install motor into the mounting groove of the armed lever outer end of drone body, pacify
After filling the recess portion grafting in protrusion and mounting groove, motor is locked in mounting groove by screw or bolt；Filling is sleeved on
On the output shaft of motor, attachment base then is installed in the output shaft end in motor；By the connecting column on propeller and attachment base
Attachment base is then connect locking with propeller by bolt, nut, to complete to install by grafting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910512088.8A CN110203407A (en) | 2019-06-13 | 2019-06-13 | Six rotor wing unmanned aerial vehicle transmission component mounting structures and installation method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910512088.8A CN110203407A (en) | 2019-06-13 | 2019-06-13 | Six rotor wing unmanned aerial vehicle transmission component mounting structures and installation method |
Publications (1)
| Publication Number | Publication Date |
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| CN110203407A true CN110203407A (en) | 2019-09-06 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910512088.8A Pending CN110203407A (en) | 2019-06-13 | 2019-06-13 | Six rotor wing unmanned aerial vehicle transmission component mounting structures and installation method |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110587306A (en) * | 2019-10-27 | 2019-12-20 | 陈芳 | Automatic production line for aerial rotating flying gyro |
| CN110758713A (en) * | 2019-11-22 | 2020-02-07 | 复旦大学 | Unmanned aerial vehicle rotor wing, rotor wing assembling method and rotor wing type unmanned aerial vehicle |
| CN112027075A (en) * | 2020-09-15 | 2020-12-04 | 惠州众合航空科技有限公司 | Vertical lifting wing for unmanned aerial vehicle |
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| CN204507263U (en) * | 2015-04-08 | 2015-07-29 | 辽宁力德航空科技有限公司 | Unmanned plane mounting structure for propeller |
| CN206202707U (en) * | 2016-12-04 | 2017-05-31 | 新疆海讯达电子科技有限公司 | A kind of unmanned plane propeller safety guard |
| CN206218207U (en) * | 2016-12-05 | 2017-06-06 | 深圳光启空间技术有限公司 | Mounting structure for propeller and aircraft |
| CN208248493U (en) * | 2018-06-04 | 2018-12-18 | 广州市华科尔科技股份有限公司 | A kind of rotor assemblies of multi-rotor unmanned aerial vehicle |
| WO2019027195A1 (en) * | 2017-08-03 | 2019-02-07 | 엘지이노텍 주식회사 | Drone motor |
| CN210133294U (en) * | 2019-06-13 | 2020-03-10 | 福州大学 | Six rotor unmanned aerial vehicle transmission assembly mounting structure |
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2019
- 2019-06-13 CN CN201910512088.8A patent/CN110203407A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN204507263U (en) * | 2015-04-08 | 2015-07-29 | 辽宁力德航空科技有限公司 | Unmanned plane mounting structure for propeller |
| CN206202707U (en) * | 2016-12-04 | 2017-05-31 | 新疆海讯达电子科技有限公司 | A kind of unmanned plane propeller safety guard |
| CN206218207U (en) * | 2016-12-05 | 2017-06-06 | 深圳光启空间技术有限公司 | Mounting structure for propeller and aircraft |
| WO2019027195A1 (en) * | 2017-08-03 | 2019-02-07 | 엘지이노텍 주식회사 | Drone motor |
| CN208248493U (en) * | 2018-06-04 | 2018-12-18 | 广州市华科尔科技股份有限公司 | A kind of rotor assemblies of multi-rotor unmanned aerial vehicle |
| CN210133294U (en) * | 2019-06-13 | 2020-03-10 | 福州大学 | Six rotor unmanned aerial vehicle transmission assembly mounting structure |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110587306A (en) * | 2019-10-27 | 2019-12-20 | 陈芳 | Automatic production line for aerial rotating flying gyro |
| CN110587306B (en) * | 2019-10-27 | 2021-09-21 | 南京六合高新建设发展有限公司 | Automatic production line for aerial rotating flying gyro |
| CN110758713A (en) * | 2019-11-22 | 2020-02-07 | 复旦大学 | Unmanned aerial vehicle rotor wing, rotor wing assembling method and rotor wing type unmanned aerial vehicle |
| CN112027075A (en) * | 2020-09-15 | 2020-12-04 | 惠州众合航空科技有限公司 | Vertical lifting wing for unmanned aerial vehicle |
| CN112027075B (en) * | 2020-09-15 | 2022-04-29 | 惠州众合航空科技有限公司 | Vertical lifting wing for unmanned aerial vehicle |
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| 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: 20190906 |