CN108454840A - A kind of unmanned plane of wing waterproof - Google Patents
A kind of unmanned plane of wing waterproof Download PDFInfo
- Publication number
- CN108454840A CN108454840A CN201810290216.4A CN201810290216A CN108454840A CN 108454840 A CN108454840 A CN 108454840A CN 201810290216 A CN201810290216 A CN 201810290216A CN 108454840 A CN108454840 A CN 108454840A
- Authority
- CN
- China
- Prior art keywords
- wing
- fixedly connected
- power supply
- drone body
- outer casing
- 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.)
- Granted
Links
- 230000005855 radiation Effects 0.000 claims description 10
- 238000000034 method Methods 0.000 claims description 3
- 238000003466 welding Methods 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 230000003628 erosive effect Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000005286 illumination Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000000630 rising effect Effects 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
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
-
- 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
- B64D47/02—Arrangements or adaptations of signal or lighting devices
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of unmanned planes of wing waterproof, including drone body, automatically controlled holder and wing, the front surface of the drone body is provided with LED light, the LED light is fixedly connected with the drone body, it is both provided with connecting seat at left and right sides of the drone body, the connecting seat is fixedly connected with the drone body, the lateral wall of the connecting seat is provided with linking arm, the linking arm is fixedly connected with the connecting seat, and the bottom of the drone body is provided with outer casing of power supply；By the way that wing is arranged, in the junction of wing and propeller, rain cover shell is set, when unmanned plane is in rainy day flight, since rain cover shell opener part is less than the set casing of top, so that rainwater is blocked in the outside of rain cover shell, rain erosion motor internal is avoided, leads to the generation of accident, and LED light is arranged by the front surface in drone body, it is used at night convenient for unmanned plane.
Description
Technical field
The invention belongs to air vehicle technique fields, and in particular to a kind of unmanned plane of wing waterproof.
Background technology
UAV abbreviation unmanned plane is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned vehicle, unmanned plane are actually the general designation of unmanned vehicle, can be divided into from technical standpoint definition：Nobody is solid
Determine wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..
The propeller junction of original unmanned plane wing is directly connected with motor, and in the environment of the rainy day, rainwater is non-
It is often easy to be entered inside motor by junction, leads to motor damage, and original unmanned plane does not have the effect of illumination, is not easy to
Use at night.
Invention content
The purpose of the present invention is to provide a kind of unmanned planes of wing waterproof, to solve to propose nobody in above-mentioned background technology
The propeller junction of machine wing is directly connected with motor, and in the environment of the rainy day, rainwater is very easy to be entered by junction
Inside motor, lead to motor damage, and original unmanned plane does not have the effect of illumination, be not easy at night use ask
Topic.
To achieve the above object, the present invention provides the following technical solutions：A kind of unmanned plane of wing waterproof, including unmanned plane
The front surface of ontology, automatically controlled holder and wing, the drone body is provided with LED light, the LED light and the nothing
Man-machine ontology is fixedly connected, and is both provided with connecting seat at left and right sides of the drone body, the connecting seat with it is described nobody
Machine ontology is fixedly connected, and the lateral wall of the connecting seat is provided with linking arm, and the linking arm is fixedly connected with the connecting seat,
The bottom of the drone body is provided with outer casing of power supply, and the outer casing of power supply is fixedly connected with the drone body, described
Undercarriage is both provided at left and right sides of outer casing of power supply, the undercarriage is fixedly connected with the outer casing of power supply, outside the power supply
Shell is internally provided with battery, and the battery is fixedly connected with the outer casing of power supply, and the bottom setting of the outer casing of power supply is
Automatically controlled holder is stated, the automatically controlled holder is fixedly connected with the outer casing of power supply, and the bottom of the automatically controlled holder is provided with camera,
The camera is connect with the automatically controlled cloud platform rotation, and the lateral wall of the linking arm is provided with the wing, the wing with
The linking arm is fixedly connected, and the wing is internally provided with motor, and the motor is fixedly connected with the wing, the machine
Rain cover shell is provided at the top of the wing, the rain cover shell is fixedly connected with the wing, and the output end of the motor is provided with rotation
Axis, the rotary shaft and the output end of the motor are sequentially connected, and the lateral wall of the rotary shaft is provided with propeller, the spiral shell
Rotation paddle is fixedly connected with the rotary shaft, and set casing, the set casing and the rotary shaft are provided at the top of the rotary shaft
It is fixedly connected, the bottom of the wing is provided with radiation shell, and the radiation shell is fixedly connected with the wing, the radiation shell
Bottom offers the second heat emission hole, and the LED light, the camera and the motor are electrically connected with the battery.
Preferably, there are two the undercarriage is arranged altogether, the left and right two of the outer casing of power supply is fixed on by nut respectively
Side.
Preferably, the lateral wall of the outer casing of power supply offers the first heat emission hole.
Preferably, it there are four the wing is arranged altogether, and is fixed by welding on the linking arm.
Preferably, the rotary shaft is fixedly connected by flange with the propeller.
Preferably, the camera is provided with axis close to one end of the automatically controlled holder, and the camera passes through the axis
It is connect with the automatically controlled cloud platform rotation.
Preferably, the rain cover shell is cylinder, and top offers opening.
Compared with prior art, the beneficial effects of the invention are as follows：By the way that wing is arranged, in the junction of wing and propeller
Rain cover shell is set, when unmanned plane is in rainy day flight, since rain cover shell opener part is less than the set casing of top so that rainwater quilt
It blocks in the outside of rain cover shell, avoids rain erosion motor internal, lead to the generation of accident, and by drone body
LED light is arranged in front surface, is used at night convenient for unmanned plane.
Description of the drawings
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is the structural schematic diagram of wing of the present invention；
Fig. 3 is the structural schematic diagram of wing radiation shell of the present invention；
In figure：1- drone bodies, 11-LED lamps, 12- connecting seats, 13- linking arms, 14- outer casing of power supply, 15- undercarriages,
16- batteries, the first heat emission holes of 17-, the automatically controlled holders of 2-, 21- cameras, 3- wings, 31- motors, 32- rain covers shell, 33- rotations
Axis, 34- propellers, 35- set casings, 36- radiation shells, the second heat emission holes of 37-.
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.
- 3 are please referred to Fig.1, the present invention provides a kind of technical solution：A kind of unmanned plane of wing waterproof, including unmanned plane sheet
The front surface of body 1, automatically controlled holder 2 and wing 3, drone body 1 is provided with LED light 11, LED light 11 and unmanned plane sheet
Body 1 is fixedly connected, and the left and right sides of drone body 1 is both provided with connecting seat 12, and connecting seat 12 is fixed with drone body 1 to be connected
It connects, the lateral wall of connecting seat 12 is provided with linking arm 13, and linking arm 13 is fixedly connected with connecting seat 12, the bottom of drone body 1
Portion is provided with outer casing of power supply 14, and outer casing of power supply 14 is fixedly connected with drone body 1, and the left and right sides of outer casing of power supply 14 is respectively provided with
There is undercarriage 15, undercarriage 15 to be fixedly connected with outer casing of power supply 14, outer casing of power supply 14 is internally provided with battery 16, battery 16 with
Outer casing of power supply 14 is fixedly connected, and the bottom of outer casing of power supply 14 is provided with automatically controlled holder 2, and automatically controlled holder 2 is fixed with outer casing of power supply 14
The bottom of connection, automatically controlled holder 2 is provided with camera 21, and camera 21 is rotatablely connected with automatically controlled holder 2, the outside of linking arm 13
Wall is provided with wing 3, and wing 3 is fixedly connected with linking arm 13, and wing 3 is internally provided with motor 31, and motor 31 is solid with wing 3
Fixed connection, the top of wing 3 are provided with rain cover shell 32, and rain cover shell 32 is fixedly connected with wing 3, and the output end of motor 31 is provided with
Rotary shaft 33, rotary shaft 33 and the output end of motor 31 are sequentially connected, and the lateral wall of rotary shaft 33 is provided with propeller 34, spiral
Paddle 34 is fixedly connected with rotary shaft 33, and the top of rotary shaft 33 is provided with set casing 35, and set casing 35 is fixed with rotary shaft 33 to be connected
It connects, the bottom of wing 3 is provided with radiation shell 36, and radiation shell 36 is fixedly connected with wing 3, and the bottom of radiation shell 36 offers second
Heat emission hole 37, LED light 11, camera 21 and motor 31 are electrically connected with battery 16.
In the present embodiment, the setting rain cover shell 32 in the junction of wing 3 and propeller 34, when unmanned plane flies in the rainy day
When, since 32 opening portion of rain cover shell is less than the set casing 35 of top so that rainwater is blocked in the outside of rain cover shell 32, avoids
Rain erosion motor internal 31 leads to the generation of accident, and LED light 11 is arranged by the front surface in drone body 1, just
It is used at night in unmanned plane.
Further, there are two undercarriage 15 is arranged altogether, the left and right sides of outer casing of power supply 14 is fixed on by nut respectively.
In the present embodiment, by the way that undercarriage 15 is arranged, facilitate rising and falling for unmanned plane.
Further, the lateral wall of outer casing of power supply 14 offers the first heat emission hole 17.
In the present embodiment, by opening up the first heat emission hole 17, facilitate the heat dissipation of battery 16.
Further, it there are four wing 3 is arranged altogether, and is fixed by welding on linking arm 13.
In the present embodiment, wing 3 drives 1 landing of drone body by the rotation of propeller 34.
Further, rotary shaft 33 is fixedly connected by flange with propeller 34.
In the present embodiment, flange fixes propeller 34 in rotary shaft 33, easy to operate, easy for installation.
Further, camera 21 is provided with axis close to one end of automatically controlled holder 2, and camera 21 passes through axis and automatically controlled holder
2 rotation connections.
In the present embodiment, make automatically controlled holder 2 that camera 21 be driven to rotate by the way that axis is arranged.
Further, rain cover shell 32 is cylinder, and top offers opening.
In the present embodiment, rain cover shell 32 coats rotary shaft 33, and rainwater is made to be blocked in the outside of rain cover shell 32.
The model 25W of motor 31 in the present invention.
The operation principle and process for using of the present invention：After the present invention installs, LED light 11, camera 21 and motor 31
It is turned on battery 16, the junction setting rain cover shell 32 of wing 3 and propeller 34, when unmanned plane is in rainy day flight, due to hiding
32 opening portion of rain shell is less than the set casing 35 of top so that rainwater is blocked in the outside of rain cover shell 32, avoids rainwater and invades
Motor internal 31 is lost, leads to the generation of accident, and LED light 11 is arranged by the front surface in drone body 1, is convenient for unmanned plane
It is used at night.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (7)
1. a kind of unmanned plane of wing waterproof, it is characterised in that：Including drone body (1), automatically controlled holder (2) and wing (3),
The front surface of the drone body (1) is provided with LED light (11), the LED light (11) and the drone body
(1) it is fixedly connected, connecting seat (12), the connecting seat (12) and institute is both provided at left and right sides of the drone body (1)
It states drone body (1) to be fixedly connected, the lateral wall of the connecting seat (12) is provided with linking arm (13), the linking arm (13)
It is fixedly connected with the connecting seat (12), the bottom of the drone body (1) is provided with outer casing of power supply (14), outside the power supply
Shell (14) is fixedly connected with the drone body (1), and undercarriage is both provided at left and right sides of the outer casing of power supply (14)
(15), the undercarriage (15) is fixedly connected with the outer casing of power supply (14), and the outer casing of power supply (14) is internally provided with electricity
Pond (16), the battery (16) are fixedly connected with the outer casing of power supply (14), and the bottom setting of the outer casing of power supply (14) is
Automatically controlled holder (2) is stated, the automatically controlled holder (2) is fixedly connected with the outer casing of power supply (14), the bottom of the automatically controlled holder (2)
It is provided with camera (21), the camera (21) is rotatablely connected with the automatically controlled holder (2), the outside of the linking arm (13)
Wall is provided with the wing (3), and the wing (3) is fixedly connected with the linking arm (13), the inside setting of the wing (3)
There are motor (31), the motor (31) to be fixedly connected with the wing (3), rain cover shell is provided at the top of the wing (3)
(32), the rain cover shell (32) is fixedly connected with the wing (3), and the output end of the motor (31) is provided with rotary shaft
(33), the rotary shaft (33) and the output end of the motor (31) are sequentially connected, the lateral wall setting of the rotary shaft (33)
There are propeller (34), the propeller (34) to be fixedly connected with the rotary shaft (33), the top setting of the rotary shaft (33)
There are set casing (35), the set casing (35) to be fixedly connected with the rotary shaft (33), the bottom of the wing (3) is provided with scattered
Hot shell (36), the radiation shell (36) are fixedly connected with the wing (3), and the bottom of the radiation shell (36) offers second and dissipates
Hot hole (37), the LED light (11), the camera (21) and the motor (31) are electrically connected with the battery (16).
2. a kind of unmanned plane of wing waterproof according to claim 1, it is characterised in that：The undercarriage (15) is arranged altogether
There are two, the left and right sides of the outer casing of power supply (14) is fixed on by nut respectively.
3. a kind of unmanned plane of wing waterproof according to claim 1, it is characterised in that：Outside the outer casing of power supply (14)
Side wall offers the first heat emission hole (17).
4. a kind of unmanned plane of wing waterproof according to claim 1, it is characterised in that：The wing (3) is provided with altogether
Four, and be fixed by welding on the linking arm (13).
5. a kind of unmanned plane of wing waterproof according to claim 1, it is characterised in that：The rotary shaft (33) passes through method
It is blue to be fixedly connected with the propeller (34).
6. a kind of unmanned plane of wing waterproof according to claim 1, it is characterised in that：The camera (21) is close to institute
The one end for stating automatically controlled holder (2) is provided with axis, and the camera (21) is connected by the axis and automatically controlled holder (2) rotation
It connects.
7. a kind of unmanned plane of wing waterproof according to claim 1, it is characterised in that：The rain cover shell (32) is in cylinder
Shape, and top offers opening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810290216.4A CN108454840B (en) | 2018-04-03 | 2018-04-03 | Unmanned aerial vehicle with waterproof wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810290216.4A CN108454840B (en) | 2018-04-03 | 2018-04-03 | Unmanned aerial vehicle with waterproof wings |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108454840A true CN108454840A (en) | 2018-08-28 |
| CN108454840B CN108454840B (en) | 2024-05-17 |
Family
ID=63234450
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810290216.4A Active CN108454840B (en) | 2018-04-03 | 2018-04-03 | Unmanned aerial vehicle with waterproof wings |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108454840B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110217387A (en) * | 2019-06-14 | 2019-09-10 | 南京工业职业技术学院 | A kind of unmanned plane equipped with overboard safeguard structure |
| CN110588979A (en) * | 2019-10-28 | 2019-12-20 | 云南电网有限责任公司带电作业分公司 | Night emergency repair unmanned aerial vehicle carrying lighting device |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101663058B1 (en) * | 2016-04-04 | 2016-10-17 | 만진항공건설 주식회사 | Unmanned aerial vehicle for agriculture |
| KR101727019B1 (en) * | 2015-10-12 | 2017-04-14 | 최종필 | Multi-rotor-type droun with a fixed wing |
| CN206107573U (en) * | 2016-08-17 | 2017-04-19 | 姚楚鑫 | Unmanned aerial vehicle who possesses waterproof function |
| CN206446791U (en) * | 2016-09-13 | 2017-08-29 | 深圳市慧明捷科技有限公司 | A kind of police unmanned plane of many rotors |
| CN207985187U (en) * | 2018-04-03 | 2018-10-19 | 南通科技职业学院 | A kind of unmanned plane of wing waterproof |
-
2018
- 2018-04-03 CN CN201810290216.4A patent/CN108454840B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101727019B1 (en) * | 2015-10-12 | 2017-04-14 | 최종필 | Multi-rotor-type droun with a fixed wing |
| KR101663058B1 (en) * | 2016-04-04 | 2016-10-17 | 만진항공건설 주식회사 | Unmanned aerial vehicle for agriculture |
| CN206107573U (en) * | 2016-08-17 | 2017-04-19 | 姚楚鑫 | Unmanned aerial vehicle who possesses waterproof function |
| CN206446791U (en) * | 2016-09-13 | 2017-08-29 | 深圳市慧明捷科技有限公司 | A kind of police unmanned plane of many rotors |
| CN207985187U (en) * | 2018-04-03 | 2018-10-19 | 南通科技职业学院 | A kind of unmanned plane of wing waterproof |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110217387A (en) * | 2019-06-14 | 2019-09-10 | 南京工业职业技术学院 | A kind of unmanned plane equipped with overboard safeguard structure |
| CN110217387B (en) * | 2019-06-14 | 2024-01-23 | 南京工业职业技术学院 | Unmanned aerial vehicle with falling water protection architecture |
| CN110588979A (en) * | 2019-10-28 | 2019-12-20 | 云南电网有限责任公司带电作业分公司 | Night emergency repair unmanned aerial vehicle carrying lighting device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108454840B (en) | 2024-05-17 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106882377B (en) | A kind of unmanned plane for glass cleaning | |
| CN106143898B (en) | A kind of VTOL tilting rotor fixed wing aircraft | |
| WO2018233570A1 (en) | Gasoline-electric hybrid multiaxis rotor type unmanned aerial vehicle | |
| CN106240817A (en) | Submersible explorer vehicle | |
| CN108454840A (en) | A kind of unmanned plane of wing waterproof | |
| CN206984354U (en) | A kind of aircraft | |
| CN105217033A (en) | Amphibious rotor wing unmanned aerial vehicle | |
| CN204916176U (en) | Six spool agricultural unmanned aerial vehicle | |
| CN207985187U (en) | A kind of unmanned plane of wing waterproof | |
| CN105035328B (en) | Hybrid-power flight vehicle | |
| CN105109695A (en) | Multifunctional aircraft with hybrid of oil and electricity | |
| CN206417193U (en) | A kind of multi-rotor unmanned aerial vehicle aircraft | |
| CN211107984U (en) | Solar energy telescopic wing water-air dual-purpose unmanned aerial vehicle | |
| CN209351595U (en) | A kind of patrol unmanned machine control system | |
| CN209700924U (en) | A kind of unmanned plane during flying body with cage shape shielded frame | |
| CN206900643U (en) | A kind of agricultural spraying unmanned plane | |
| CN107176291A (en) | It is a kind of can VTOL solar energy unmanned plane | |
| CN209192267U (en) | A kind of multi-rotor unmanned aerial vehicle is matched to be tethered at equipment | |
| CN205801528U (en) | Solar energy aerial device | |
| CN209112422U (en) | A kind of combined type vertical take-off and landing drone easy to disassemble with vanning | |
| CN206939075U (en) | A kind of strong unmanned plane of endurance | |
| CN207417138U (en) | Multi-rotor unmanned aerial vehicle | |
| CN206394895U (en) | Oil electric mixed dynamic rotor manned aircraft | |
| CN109250141A (en) | A kind of multi-rotor unmanned aerial vehicle is matched to be tethered at equipment | |
| CN205022871U (en) | Hybrid aircraft |
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 | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |