CN107554778A - A kind of land and water unmanned plane of VTOL - Google Patents
A kind of land and water unmanned plane of VTOL Download PDFInfo
- Publication number
- CN107554778A CN107554778A CN201710783026.1A CN201710783026A CN107554778A CN 107554778 A CN107554778 A CN 107554778A CN 201710783026 A CN201710783026 A CN 201710783026A CN 107554778 A CN107554778 A CN 107554778A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- land
- unmanned plane
- water
- vtol
- 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.)
- Withdrawn
Links
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
A kind of land and water unmanned plane of VTOL, belongs to vehicle technology field, more particularly to a kind of unmanned plane, including fuselage, wing, empennage, hull, steering wheel, undercarriage, and described fuselage includes detector, controller, central processing unit and motor；Described motor is located at fuselage endpiece, and described wing is connected with fuselage, positioned at nosing；Described propeller is located at body upper；After described empennage is located at fuselage；Described hull is located at below fuselage；Described steering wheel is located at hull rear end, and described undercarriage is located at below fuselage.The present invention takes full advantage of the rotary power of propeller, enable land and water unmanned plane VTOL, save take-off venue when land is taken off, save the time when the water surface takes off, simultaneously when running into the sea of complexity, it can in a short time fly to and be hidden in the air, improve land and water unmanned plane survival ability and operating efficiency.
Description
Technical field
A kind of land and water unmanned plane of VTOL, belong to vehicle technology field, more particularly to a kind of unmanned plane.
Background technology
Traditional land and water unmanned plane above water uses the layout of fixed wing aircraft, including fuselage, wing and empennage, under water
Part is laid out using Ship Structure, can carry bigger load.Traditional land and water unmanned plane is adapted to the navigation in calmness, but not
Navigate by water beneficial on the sea of complexity, when traditional land and water unmanned plane runs into the weather for having stormy waves, just can not navigate by water so that tradition
Land and water unmanned plane application it is smaller.
The content of the invention
The purpose of the present invention is to overcome the above-mentioned deficiency of traditional land and water unmanned plane, invent a kind of land and water of VTOL nobody
Machine.
A kind of land and water unmanned plane of VTOL, including fuselage, wing, empennage, hull, steering wheel, undercarriage.
Described fuselage includes detector, controller, central processing unit and motor；Before described detector is located at fuselage
Section, for detecting the situation on sea；Described controller is located at middle fuselage；Described central processing unit is located at middle fuselage,
On the right side of controller；Described motor is located at fuselage endpiece, and the energy is provided for unmanned plane.
Described wing is divided into left wing and right flank, and left wing and right flank are connected with fuselage, positioned at nosing, left wing and right flank
Symmetrical distribution；Described propeller is located at body upper, and propeller is located at the surface of wing；Described empennage is located at
After fuselage；Described hull is located at below fuselage, can be in surface navigation；Described steering wheel is located at hull rear end, is unmanned plane
Power is provided in surface navigation；Described undercarriage is located at below fuselage.
Preferably, a kind of land and water unmanned plane of described VTOL also includes wireless camera, radar and GPS.
A kind of land and water unmanned plane operation principle of VTOL is：When taking off on land, central controller, which receives, to take off
Instruction, information is transmitted to controller, controller control propeller starts, and motor gives propeller to provide electric energy, passes through propeller
The power brought enables land and water unmanned plane to take off vertically；When land and water, unmanned plane needs to drop to sea navigation, controller
Control propeller is stopped operating, and land and water unmanned plane is slowly slided and dropped on the water surface by left wing and right flank, then controller control
Steering wheel processed starts, and the power in surface navigation is provided for land and water unmanned plane；When land and water unmanned plane needs to take off from the water surface, control
Device control flaps office closes, and starts propeller and provides power for taking off vertically for land and water unmanned plane；When land and water, unmanned plane needs to land
During to ground, controller control propeller slowly lands so that the unmanned function vertical landing in land and water to ground；When land and water unmanned plane
When on sea, navigation runs into wave；Can be taken off vertically by propeller-driven land and water unmanned plane, circumvent wave, wait wave later again
The water surface is dropped to continue to navigate by water.
The present invention takes full advantage of the rotary power of propeller so that land and water unmanned plane can VTOL, save
Take-off venue when land is taken off, the time when the water surface takes off is saved, while when running into the sea of complexity, can
Fly to and hidden in the air in a short time, improve land and water unmanned plane survival ability and operating efficiency.
Brief description of the drawings
Fig. 1 is a kind of schematic top plan view of the land and water unmanned plane of VTOL；Fig. 2 be a kind of land and water of VTOL nobody
The left view schematic diagram of machine.
In figure, 1- fuselages, 2- detectors, 3- controllers, 4- central processing units, 5- motors, 6- wings, 7- left wings, the 8- right sides
The wing, 9- propellers, 10- empennages, 11- hulls, 12- steering wheels, 13- undercarriages.
Embodiment
The present invention is illustrated in conjunction with accompanying drawing：A kind of land and water unmanned plane of VTOL, including fuselage 1, machine
The wing 6, empennage 10, hull 11, steering wheel 12, undercarriage 13.
Described fuselage 1 includes detector 2, controller 3, central processing unit 4 and motor 5；Described detector 2 is located at machine
The leading portion of body 1, for detecting the situation on sea；Described controller 3 is located at the stage casing of fuselage 1；Described central processing unit 4 is located at machine
The stage casing of body 1, the right side of controller 3；Described motor 5 is located at the endpiece of fuselage 1, and the energy is provided for unmanned plane.
Described wing 6 divides to be connected for left wing 7 and right flank 8, left wing 7 and right flank 8 with fuselage 1, left positioned at the leading portion of fuselage 1
The 8 symmetrical distribution of the wing 7 and right flank；Described propeller 9 is located at body upper, and propeller 9 is located at the surface of wing 6；
After described empennage 10 is located at fuselage 1；Described hull 11 is located at the lower section of fuselage 1, can be in surface navigation；Described steering wheel 12
Positioned at the rear end of hull 11, power is provided in surface navigation for unmanned plane；Described undercarriage 13 is located at the lower section of fuselage 1.
A kind of land and water unmanned plane of described VTOL also includes wireless camera, radar and GPS.
A kind of land and water unmanned plane operation principle of VTOL is：When taking off on land, central controller 3, which receives, to take off
Instruction, information is transmitted to controller 3, controller 3 controls propeller 9 to start, and motor 5 provides electric energy to propeller 9, passes through spiral shell
The power that rotation oar 9 is brought enables land and water unmanned plane to take off vertically；When land and water, unmanned plane needs to drop to sea navigation, control
Device 3 processed controls propeller 9 to stop operating, and land and water unmanned plane is slowly slided by left wing 7 and right flank 8 and dropped on the water surface, then
Controller 3 controls steering wheel 12 to start, and the power in surface navigation is provided for land and water unmanned plane；When land and water unmanned plane is needed from the water surface
When taking off, controller 3 controls steering wheel 12 to close, and starts propeller 9 and provides power for taking off vertically for land and water unmanned plane；Work as land and water
When unmanned plane needs to drop to ground, controller 3 controls propeller 9 slowly to land so that the unmanned function vertical landing in land and water is arrived
Ground；When land and water unmanned plane runs into wave in sea navigation；By propeller 9 land and water unmanned plane can be driven to take off vertically, kept away
Wave is crossed, waits wave to drop to the water surface again later and continues to navigate by water.
Claims (4)
- A kind of 1. land and water unmanned plane of VTOL, it is characterised in that：Including fuselage（1）, wing（6）, empennage（10）, hull （11）, steering wheel（12）, undercarriage（13）；Described fuselage（1）Including detector（2）, controller（3）, central processing unit（4）With Motor（5）；Described detector（2）Positioned at fuselage（1）Leading portion；Described controller（3）Positioned at fuselage（1）Stage casing；Described Central processing unit（4）Positioned at fuselage（1）Stage casing, controller（3）Right side；Described motor（5）Positioned at fuselage（1）Endpiece；It is described Wing（6）It is divided into left wing（7）And right flank（8）, left wing（7）And right flank（8）With fuselage（1）It is connected, positioned at fuselage（1）Leading portion； Described propeller（9）Positioned at body upper；Described empennage（10）Positioned at fuselage（1）Afterwards；Described hull（11）Positioned at machine Body（1）Lower section, can be in surface navigation；Described steering wheel（12）Positioned at hull（11）Rear end；Described undercarriage（13）It is located at Fuselage（1）Lower section.
- A kind of 2. land and water unmanned plane of VTOL according to claim 1, it is characterised in that：Left wing（7）And right flank（8） Symmetrical distribution.
- A kind of 3. land and water unmanned plane of VTOL according to claim 1 or 2, it is characterised in that：Described one kind is hung down The land and water unmanned plane of straight landing also includes wireless camera, radar and GPS.
- A kind of 4. land and water unmanned plane of VTOL according to claim 1 or 2, it is characterised in that：The propeller（9） Positioned at wing（6）Surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710783026.1A CN107554778A (en) | 2017-09-03 | 2017-09-03 | A kind of land and water unmanned plane of VTOL |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710783026.1A CN107554778A (en) | 2017-09-03 | 2017-09-03 | A kind of land and water unmanned plane of VTOL |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107554778A true CN107554778A (en) | 2018-01-09 |
Family
ID=60978836
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710783026.1A Withdrawn CN107554778A (en) | 2017-09-03 | 2017-09-03 | A kind of land and water unmanned plane of VTOL |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107554778A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1202861A (en) * | 1995-10-24 | 1998-12-23 | 汉斯·J·伯恩 | Hybrid aircraft |
| CN102166931A (en) * | 2011-06-08 | 2011-08-31 | 陈昌志 | New energy multifunctional airplane |
| CN205293087U (en) * | 2015-12-25 | 2016-06-08 | 天津全华时代航天科技发展有限公司 | VTOL tandem wing unmanned aerial vehicle |
| CN105818980A (en) * | 2016-05-06 | 2016-08-03 | 刘行伟 | Novel large-lift-force vertical take-off and landing aircraft |
| CN106103274A (en) * | 2015-07-02 | 2016-11-09 | 深圳市大疆创新科技有限公司 | Unmanned plane, its control system and method, and unmanned plane landing control method |
| CN106494608A (en) * | 2015-09-06 | 2017-03-15 | 陈康 | Many shrouded propeller variable geometry Electric aircrafts |
-
2017
- 2017-09-03 CN CN201710783026.1A patent/CN107554778A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1202861A (en) * | 1995-10-24 | 1998-12-23 | 汉斯·J·伯恩 | Hybrid aircraft |
| CN102166931A (en) * | 2011-06-08 | 2011-08-31 | 陈昌志 | New energy multifunctional airplane |
| CN106103274A (en) * | 2015-07-02 | 2016-11-09 | 深圳市大疆创新科技有限公司 | Unmanned plane, its control system and method, and unmanned plane landing control method |
| CN106494608A (en) * | 2015-09-06 | 2017-03-15 | 陈康 | Many shrouded propeller variable geometry Electric aircrafts |
| CN205293087U (en) * | 2015-12-25 | 2016-06-08 | 天津全华时代航天科技发展有限公司 | VTOL tandem wing unmanned aerial vehicle |
| CN105818980A (en) * | 2016-05-06 | 2016-08-03 | 刘行伟 | Novel large-lift-force vertical take-off and landing aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107554783A (en) | A kind of amphibious unmanned plane of VTOL | |
| CN107696811A (en) | A kind of VTOL amphibious unmanned plane of more power | |
| CN205131644U (en) | Four -axis glide vehicle | |
| CN106379525A (en) | Wing connected unmanned plane | |
| CN105882942B (en) | A kind of high-efficient low-speed aircraft | |
| CN207072429U (en) | One kind vertical lift tilting rotor wing unmanned aerial vehicle | |
| CN206231620U (en) | One kind connects wing unmanned plane | |
| CN109263975A (en) | A kind of VTOL amphibian | |
| CN105217026A (en) | A kind of compound type aircraft | |
| CN105173060B (en) | A kind of pair of oar Convertiplane | |
| CN205499349U (en) | Electronic unmanned helicopter of compound thrust | |
| CN107953987A (en) | A kind of serial mixed power vector promotes air-sea detection carrying platform | |
| CN107521661A (en) | A kind of rotatable more amphibious unmanned planes of power VTOL of wing | |
| CN107499504A (en) | A kind of amphibious unmanned plane of rotatable VTOL of wing | |
| CN107554778A (en) | A kind of land and water unmanned plane of VTOL | |
| CN106741933A (en) | A kind of amphibious unmanned plane | |
| CN107539470A (en) | A kind of four oars amphibious unmanned plane of VTOL | |
| CN109263969A (en) | A kind of amphibious aircraft of VTOL | |
| CN206900368U (en) | Imitate air cushion composite wing ship in ground | |
| CN206841716U (en) | A kind of fixed-wing unmanned plane | |
| CN107685857A (en) | A kind of four rotation land and water unmanned planes of vertical lift | |
| CN201678041U (en) | Circulating flapping-wing flying vehicle | |
| CN205131654U (en) | Compound aircraft | |
| CN107458601A (en) | A kind of amphibious unmanned plane of the VTOL with auxiliary power | |
| CN105197230A (en) | Aircraft provided with double rotor wings |
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 | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20181022 Address after: 528000 201L two (1 / two) of Feng Jie street, Chao'an Road, Zu Miao street, Chancheng District, Guangdong, China (residence declaration) Applicant after: Foshan Jiayun Aviation Technology Co. Ltd. Address before: 528000 201Q two (1 / two) of Feng Jie street, Chao'an Road, Zu Miao street, Chancheng District, Guangdong, China (residence declaration) Applicant before: Foshan flying Technology Co., Ltd. |
|
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180109 |