CN206569246U - Unmanned plane with waterproof casing - Google Patents
Unmanned plane with waterproof casing Download PDFInfo
- Publication number
- CN206569246U CN206569246U CN201621480184.7U CN201621480184U CN206569246U CN 206569246 U CN206569246 U CN 206569246U CN 201621480184 U CN201621480184 U CN 201621480184U CN 206569246 U CN206569246 U CN 206569246U
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- CN
- China
- Prior art keywords
- casing
- fuselage
- unmanned plane
- concave face
- horn
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Abstract
The utility model is related to the unmanned plane with waterproof casing, including：Fuselage, horn, foot stool and casing.It is mounted with image information and shoots with video-corder the gondola of part and hangs on the installing plate for being located at fuselage bottom；Flight control system is arranged on fuselage；One end of horn and the installing plate of fuselage bottom are hinged, and the other end is connected with rotor drive component；Foot stool is arranged on the installing plate of fuselage bottom；Casing includes：The drain pan that is fixedly connected with installing plate and docked with drain pan it is fixed after wrap up the upper casing of fuselage；Upper casing sets the concave face that oriented fuselage interior is drawn close；Concave face opens up heat emission hole.This has the unmanned function lifting unmanned plane water resistance of waterproof casing, it is to avoid produce fuselage immersion failure.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, the more particularly to unmanned plane with waterproof casing.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Because its action is flexible, landing environmental requirement is relatively low, and with good operating characteristics etc., it is widely used in
The numerous areas such as take photo by plane, monitor, investigating, searching and rescuing.Without driving cabin on unmanned plane, but automatic pilot, programme-control dress are installed
Put, the equipment such as information collecting device.On ground, naval vessels or machine tool remote control station personnel are by equipment such as radars, it is tracked,
Positioning, remote control, remote measurement and Digital Transmission.
The casing of existing unmanned plane does not possess water resistance typically, it is impossible to which adapting to work of the unmanned plane in rainwater environment needs
Ask.
Utility model content
The unmanned plane with waterproof casing that the application is provided, is solved or part solves unmanned plane in the prior art and prevented
The technical problem of water poor-performing, realizes lifting unmanned plane water resistance, it is to avoid produce the technique effect of fuselage immersion failure.
This application provides a kind of unmanned plane with waterproof casing, the unmanned plane includes：Rotor, rotor shaft, rotor
Drive component, gondola and flight control system, the rotor are fixedly connected with the rotor shaft；The rotor drive component and institute
Rotor shaft is stated to be fixedly connected；The unmanned plane with waterproof casing includes：
Fuselage；It is mounted with image information and shoots with video-corder the gondola of part and hangs and be located on the installing plate of the fuselage bottom；Institute
Flight control system is stated to be arranged on the fuselage；
Horn；One end of the horn and the installing plate of the fuselage bottom are hinged, the other end and the rotor driving group
Part is connected；
On foot stool, the installing plate for being arranged on the fuselage bottom；
Casing；The casing includes：The drain pan that is fixedly connected with the installing plate and docked with the drain pan it is fixed after wrap
Wrap up in the upper casing of the fuselage；The upper casing sets the concave face that the oriented fuselage interior is drawn close；The concave face opens up radiating
Hole.
Preferably, the casing opens up the pilot hole being connected for the horn with the installing plate.
Preferably, setting the fixed seat being fixedly connected with the installing plate in the pilot hole；
The end of the horn is hinged by rotating shaft with the fixed seat；
The end of the horn is connected with positioning wedged block；
Wherein, the horn is flipped up to after operating position, and the positioning wedged block coordinates with the fixed seat will be described
Horn is limited to the operating position；Now, plate face of the rotation axis of the rotor perpendicular to the installing plate.
Preferably, the horn includes：Hollow carbon fiber pipe, the pipe sleeve for being socketed in described carbon fiber pipe one end and with
The assembling block that the carbon fiber pipe other end is fixedly connected；
The end of the pipe sleeve is connected with articulated slab；
The articulated slab is hinged by the rotating shaft with the fixed seat；
The positioning wedged block is fixed on the articulated slab；
The pipe sleeve is fastened with the carbon fiber pipe by screw；
The rotor drive component is fixed on the assembling block.
Preferably, the rotor drive component includes：The motor being connected with the power supply part of the fuselage roof
And adjusted with the electricity of the motor connection；
The motor is fixed on the top or bottom of the assembling block；
The motor is connected by being located in the electric wire inside the carbon fiber pipe with the power supply part of the fuselage roof；
The electricity is adjusted to be connected by the electric wire being located in inside the carbon fiber pipe with the flight control system in the casing
Connect.
Preferably, the casing also includes：Heat sink；
The heat sink is detachably arranged in the heat emission hole.
Preferably, the heat sink is the aluminium alloy web plate for opening up multiple passages；
The aluminium alloy web plate is detachably mounted in the heat emission hole.
Preferably, there is the upper casing top upper cover plate of the first cavity volume is formed after arching upward；
The concave face is arranged on the upper cover plate；
The power supply part of the fuselage roof is located in first cavity volume.
Preferably, the quantity of the concave face is two, respectively the first concave face and the second concave face；
First concave face and second concave face are located at the both sides of the upper cover plate respectively；
The casing includes two blocks of heat sinks, respectively the first heat sink and the second heat sink；
First concave face opens up the first heat emission hole of accommodating first heat sink；
Second concave face opens up the second heat emission hole of accommodating second heat sink.
Preferably, first heat emission hole is arranged on the side of the power supply part of the fuselage roof；
Second heat emission hole is arranged on the opposite side of the power supply part of the fuselage roof.
One or more technical schemes provided herein, have at least the following technical effects or advantages：
The casing constituted as a result of the upper casing that parcel fuselage after fixation is docked by drain pan and with drain pan, in the upper of upper casing
Cover plate sets the concave face drawn close to fuselage interior, and concave face opens up heat emission hole, when unmanned plane works in rainwater environment, from upper
The rainwater slid at the top of cover plate can enter concave face top and directly drop to the lower section of heat emission hole without flowing into heat emission hole, unmanned plane
During advance, the rainwater of upper cover plate can be slipped to bottom of shell from the top of upper cover plate directly around concave face, be prevented effectively from rainwater
The part that casing internal is damaged in fuselage is entered by heat emission hole, the water resistance of unmanned plane is significantly improved.So, effectively solve
Determine the poor technical problem of unmanned plane water resistance in the prior art, realized lifting unmanned plane water resistance, it is to avoid produce
Fuselage immersion failure, while heat emission hole location layout rationally, effectively improves the technology of the power supply part radiating effect of fuselage roof
Effect.
Brief description of the drawings
The general assembly drawing for the unmanned plane with waterproof casing that Fig. 1 provides for the utility model embodiment；
Fig. 2 is casing, the installation diagram of horn in Fig. 1；
Fig. 3 is the partial enlarged drawing of horn in Fig. 1；
Fig. 4 is the partial enlarged drawing of casing in Fig. 1.
(part that each label is represented in diagram is followed successively by：1 rotor, 2 casings, 3 rotor drive components, 4 horns, 5 foot stools,
201 upper cover plates, 202 heat sinks, 203 concave faces, 205 drain pans, 401 fixed seats, 402 pipe sleeves, 403 motors, 404 assembling blocks, 405
Electricity tune, 406 carbon fiber pipes)
Embodiment
The embodiment of the present application provide the unmanned plane with waterproof casing, solve or partly solve in the prior art without
The poor technical problem of man-machine water resistance, by setting the concave face drawn close to fuselage interior in the upper casing of casing；Concave face
Heat emission hole is opened up, lifting unmanned plane water resistance is realized, it is to avoid the technique effect of fuselage immersion failure is produced.
Referring to attached Fig. 1 and 2, this application provides a kind of unmanned plane with waterproof casing, unmanned plane includes：Rotor 1, rotation
Wing axle, rotor drive component 3, gondola and flight control system, rotor 1 are fixedly connected with rotor shaft；Rotor drive component 3 and rotation
Wing axle is fixedly connected, and lift is provided to drive rotor shaft and rotor 1 to rotate to be unmanned plane；This has the unmanned plane bag of waterproof casing
Include：Fuselage, horn 4, foot stool 5 and casing 2.
It is mounted with image information and shoots with video-corder the gondola of part and hangs on the installing plate for being located at fuselage bottom；Flight control system is set
On fuselage；One end of horn 4 and the installing plate of fuselage bottom are hinged, and the other end is connected with rotor drive component 3；Foot stool 5 is set
Put on the installing plate of fuselage bottom；Casing 2 includes：The drain pan 205 that is fixedly connected with installing plate and dock fixation with drain pan 205
The upper casing of fuselage is wrapped up afterwards；Upper casing sets the concave face 203 that oriented fuselage interior is drawn close；Concave face 203 opens up heat emission hole.
Wherein, upper casing sets the concave face 203 that oriented fuselage interior is drawn close, and concave face 203 opens up heat emission hole, and unmanned plane exists
When being worked in rainwater environment, the rainwater slid from the top of upper casing can enter the top of concave face 203 and directly drop under heat emission hole
Side is without flowing into heat emission hole, and when unmanned plane advances, the rainwater of upper casing can be slipped to casing from top directly around concave face 203
2 bottoms, are prevented effectively from the part that rainwater is entered in the inside of casing 2 infringement fuselage by heat emission hole, significantly improve unmanned plane
Water resistance.
Further, referring to accompanying drawing 2, casing 2 opens up the pilot hole being connected for horn 4 with installing plate.Set in pilot hole
The fixed seat 401 being fixedly connected with installing plate；The end of horn 4 is hinged by rotating shaft with fixed seat 401；The end of horn 4 connects
It is connected to positioning wedged block；Wherein, horn 4 is flipped up to after operating position, and positioning wedged block coordinates with fixed seat 401 limits horn 4
It is scheduled on operating position；Now, plate face of the rotation axis of rotor 1 perpendicular to installing plate.By setting the turnover knot of horn 4
Structure, when the unmanned plane is transported, horn 4 is turned down to the direction of installing plate, on the one hand reduces the space-consuming of the unmanned plane, reduced
The rotor drive component 3 and rotor 1 of transport difficulty, on the other hand protection horn 4 end, it is to avoid rotor driving group in transportation
Part and rotor are damaged by collision or even horn 4 fractures.
Further, referring to accompanying drawing 2 and 3, horn 4 includes hollow carbon fiber pipe 406, is socketed in carbon fiber pipe 406 1
The pipe sleeve 402 at end and the assembling block 404 being fixedly connected with the other end of carbon fiber pipe 406；The end of pipe sleeve 402, which is connected with, to be hinged
Plate；Articulated slab is hinged by rotating shaft with fixed seat 401；Positioning wedged block is fixed on articulated slab；Pipe sleeve 402 and carbon fiber pipe 406
Fastened by screw；Rotor drive component 3 is fixed on assembling block 404.The sound construction of horn 4 being made up of said structure, weight
Amount is small, and installation and removal are very convenient, and each component manufacturing cost is low and is convenient for changing accessory.
Further, rotor drive component 3 includes：The motor 403 and and motor being connected with the power supply part of fuselage roof
The electricity of 403 connections adjusts 405；Motor 403 is fixed on the top or bottom of assembling block 404；Motor 403 is by being located in carbon fiber pipe
The power supply part connection of electric wire and fuselage roof inside 406；Electricity adjusts 405 electric wire by being located in inside carbon fiber pipe 406
It is connected with the flight control system in casing.Tie point edge of the tie point relative to foot stool 5 and installing plate of horn 4 and installing plate
The edge arranged for interval of installing plate；The space that horn 4 is overturn is not overlapped with the space that foot stool 5 is overturn.
Further, unmanned plane is provided with several horns 4；Several horns 4 are respectively symmetrically arranged in the both sides of fuselage
Position.The end of each horn 4 is connected with two rotor drive components 3；Each rotor drive component 3 is connected and driven with rotor shaft
Dynamic rotor shaft is rotated；Each rotor shaft is connected with rotor 1；Wherein, two rotors 1 of the same end of horn 4 are arranged on around phase
Same rotation axis rotation.
Further, referring to accompanying drawing 1 and 4, casing 2 also includes：Heat sink 202；Heat sink 202 is detachably arranged at radiating
Kong Zhong.Heat sink 202 is the aluminium alloy web plate for opening up multiple passages；Aluminium alloy web plate is detachably mounted in heat emission hole,
As a kind of preferred embodiment, the heat emission hole inner wall tightening of aluminium alloy web plate and upper cover plate 201, which coordinates, to be realized and fixes, install and
Convenient disassembly is quick.Aluminium alloy web plate has lightweight, the weight of the characteristics of heat-conductive characteristic is excellent, on the one hand reduction unmanned plane entirety
Amount, on the other hand improves the heat dispersion of casing 2.
Further, referring to accompanying drawing 4, there is upper casing top the upper cover plate 201 of the first cavity volume is formed after arching upward；Concave face
203 are arranged on upper cover plate 201；The power supply part of fuselage roof is located in the first cavity volume, by rationally setting upper cover plate 201
Shape, is allowed to be adapted with the power supply part position of fuselage roof.
Further, the quantity of concave face 203 is two, respectively the first concave face and the second concave face；First depression
Face and the second concave face are located at the both sides of upper cover plate 201 respectively；Casing 2 includes two blocks of heat sinks 202, respectively the first heat sink
And second heat sink；First concave face opens up the first heat emission hole of accommodating first heat sink；Second concave face opens up accommodating second
Second heat emission hole of heat sink.First heat emission hole is arranged on the side of the power supply part of fuselage roof；Second heat emission hole is arranged on
The opposite side of the power supply part of fuselage roof, power supply part is rectangular block lithium battery, and unmanned plane is in flight course, rectangular block lithium
The heat that battery is produced in the first cavity volume is distributed by the first heat sink and the second heat sink, the casing 2 is possessed good
Good radiating effect.
One or more technical schemes provided herein, have at least the following technical effects or advantages：
The casing 2 constituted as a result of the upper casing that parcel fuselage after fixation is docked by drain pan 205 and with drain pan 205, on
Shell, which includes after top is arched upward, forms the upper cover plate 201 of the first cavity volume, and sets what oriented fuselage interior was drawn close in upper cover plate 201
Concave face 203, concave face 203 opens up heat emission hole, when unmanned plane works in rainwater environment, is slid from the top of upper cover plate 201
Rainwater can enter the top of concave face 203 and directly drop to the lower section of heat emission hole without flowing into heat emission hole, when unmanned plane advances, upper lid
The rainwater of plate 201 can be slipped to the bottom of casing 2 from the top of upper cover plate 201 directly around concave face 203, be prevented effectively from rainwater and lead to
Heat emission hole is crossed into the part in the inside of casing 2 infringement fuselage, the water resistance of unmanned plane is significantly improved.Meanwhile, upper cover plate
201 the first cavity volume positions formed are corresponding with the power supply part position of fuselage roof, distinguish in the position of power supply part both sides
First heat sink and the second heat sink are set, the radiating effect of unmanned plane casing is significantly enhanced.So, efficiently solve existing
The poor technical problem of unmanned plane water resistance in technology, realizes lifting unmanned plane water resistance, it is to avoid produce fuselage immersion
Failure, while heat emission hole location layout rationally, effectively improves the technique effect of the power supply part radiating effect of fuselage roof.
Above-described embodiment, is entered to the purpose of this utility model, technical scheme and beneficial effect
One step is described in detail, be should be understood that and be the foregoing is only embodiment of the present utility model, is not used to limit
The utility model processed, all within spirit of the present utility model and principle, any modification, equivalent substitution and improvements done etc.,
It should be included within protection domain of the present utility model.
Claims (10)
1. a kind of unmanned plane with waterproof casing, the unmanned plane includes：Rotor, rotor shaft, rotor drive component, gondola and
Flight control system, the rotor is fixedly connected with the rotor shaft；The rotor drive component is fixed with the rotor shaft to be connected
Connect；Characterized in that, the unmanned plane with waterproof casing includes：
Fuselage；It is mounted with image information and shoots with video-corder the gondola of part and hangs and be located on the installing plate of the fuselage bottom；It is described to fly
Row set-up of control system is on the fuselage；
Horn；One end of the horn and the installing plate of the fuselage bottom are hinged, and the other end connects with the rotor drive component
Connect；
On foot stool, the installing plate for being arranged on the fuselage bottom；
Casing；The casing includes：The drain pan that is fixedly connected with the installing plate and docked with the drain pan it is fixed after wrap up institute
State the upper casing of fuselage；The upper casing sets the concave face that the oriented fuselage interior is drawn close；The concave face opens up heat emission hole.
2. there is the unmanned plane of waterproof casing as claimed in claim 1, it is characterised in that
The casing opens up the pilot hole being connected for the horn with the installing plate.
3. there is the unmanned plane of waterproof casing as claimed in claim 2, it is characterised in that
The fixed seat being fixedly connected with the installing plate is set in the pilot hole；
The end of the horn is hinged by rotating shaft with the fixed seat；
The end of the horn is connected with positioning wedged block；
Wherein, the horn is flipped up to after operating position, and the positioning wedged block coordinates the horn with the fixed seat
It is limited to the operating position；Now, plate face of the rotation axis of the rotor perpendicular to the installing plate.
4. there is the unmanned plane of waterproof casing as claimed in claim 3, it is characterised in that
The horn includes：Hollow carbon fiber pipe, the pipe sleeve for being socketed in described carbon fiber pipe one end and with the carbon fiber pipe
The assembling block that the other end is fixedly connected；
The end of the pipe sleeve is connected with articulated slab；
The articulated slab is hinged by the rotating shaft with the fixed seat；
The positioning wedged block is fixed on the articulated slab；
The pipe sleeve is fastened with the carbon fiber pipe by screw；
The rotor drive component is fixed on the assembling block.
5. there is the unmanned plane of waterproof casing as claimed in claim 4, it is characterised in that
The rotor drive component includes：The motor that is connected with the power supply part of the fuselage roof and with the motor connection
Electricity is adjusted；
The motor is fixed on the top or bottom of the assembling block；
The motor is connected by being located in the electric wire inside the carbon fiber pipe with the power supply part of the fuselage roof；
The electricity is adjusted to be connected by the electric wire being located in inside the carbon fiber pipe with the flight control system in the casing.
6. there is the unmanned plane of waterproof casing as claimed in claim 1, it is characterised in that
The casing also includes：Heat sink；
The heat sink is detachably arranged in the heat emission hole.
7. there is the unmanned plane of waterproof casing as claimed in claim 6, it is characterised in that
The heat sink is the aluminium alloy web plate for opening up multiple passages；
The aluminium alloy web plate is detachably mounted in the heat emission hole.
8. there is the unmanned plane of waterproof casing as claimed in claim 1, it is characterised in that
There is the upper casing top upper cover plate of the first cavity volume is formed after arching upward；
The concave face is arranged on the upper cover plate；
The power supply part of the fuselage roof is located in first cavity volume.
9. there is the unmanned plane of waterproof casing as claimed in claim 8, it is characterised in that
The quantity of the concave face is two, respectively the first concave face and the second concave face；
First concave face and second concave face are located at the both sides of the upper cover plate respectively；
The casing includes two blocks of heat sinks, respectively the first heat sink and the second heat sink；
First concave face opens up the first heat emission hole of accommodating first heat sink；
Second concave face opens up the second heat emission hole of accommodating second heat sink.
10. there is the unmanned plane of waterproof casing as claimed in claim 9, it is characterised in that
First heat emission hole is arranged on the side of the power supply part of the fuselage roof；
Second heat emission hole is arranged on the opposite side of the power supply part of the fuselage roof.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621480184.7U CN206569246U (en) | 2016-12-30 | 2016-12-30 | Unmanned plane with waterproof casing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621480184.7U CN206569246U (en) | 2016-12-30 | 2016-12-30 | Unmanned plane with waterproof casing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206569246U true CN206569246U (en) | 2017-10-20 |
Family
ID=60061625
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621480184.7U Expired - Fee Related CN206569246U (en) | 2016-12-30 | 2016-12-30 | Unmanned plane with waterproof casing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206569246U (en) |
Cited By (1)
| 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 |
-
2016
- 2016-12-30 CN CN201621480184.7U patent/CN206569246U/en not_active Expired - Fee Related
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 |
| 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 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171020 Termination date: 20181230 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |