CN107554783A - A kind of amphibious unmanned plane of VTOL - Google Patents
A kind of amphibious unmanned plane of VTOL Download PDFInfo
- Publication number
- CN107554783A CN107554783A CN201710782976.2A CN201710782976A CN107554783A CN 107554783 A CN107554783 A CN 107554783A CN 201710782976 A CN201710782976 A CN 201710782976A CN 107554783 A CN107554783 A CN 107554783A
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- fuselage
- unmanned plane
- amphibious unmanned
- vtol
- connecting rod
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Abstract
A kind of amphibious unmanned plane of VTOL, belong to vehicle technology field, more particularly to a kind of amphibious unmanned plane of VTOL, including fuselage, wing, empennage, hull, steering wheel and undercarriage.Described fuselage includes detector, controller, central processing unit and motor；Described fuselage also includes connecting rod and propeller, and the connecting rod has four, and nosing each side has one, and back body each side has one, and a propeller is all connected in each connecting rod.The present invention takes full advantage of the rotary power of four propellers, enable amphibious 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 amphibious unmanned plane survival ability and operating efficiency.
Description
Technical field
A kind of amphibious unmanned plane of VTOL, belong to vehicle technology field, more particularly to a kind of VTOL
Amphibious unmanned plane.
Background technology
Traditional amphibious unmanned plane above water uses the layout of fixed wing aircraft, including fuselage, wing and empennage,
Underwater portion is laid out using Ship Structure, can carry bigger load.Traditional amphibious unmanned plane is adapted in calmness
Navigation, but be unfavorable for navigating by water on the sea of complexity, when traditional amphibious unmanned plane runs into the weather for having stormy waves, just can not
Navigation so that the application of traditional amphibious unmanned plane is smaller.
The content of the invention
The purpose of the present invention is to overcome the above-mentioned deficiency of the amphibious unmanned plane of tradition, invents a kind of land and water of VTOL
Amphibious unmanned plane.
A kind of amphibious unmanned plane of VTOL, including fuselage, wing, empennage, hull, steering wheel and 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 fuselage also includes connecting rod and propeller, and the connecting rod has four, and nosing each side has
One, back body each side has one, and a propeller is all connected in each connecting rod, for it is amphibious nobody
Machine provides the power of vertical lift.
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；After described empennage is located at fuselage；Described hull is located at below fuselage, can be in surface navigation；Institute
The steering wheel stated is located at hull rear end, and power is provided in surface navigation for unmanned plane；Described undercarriage is located at below fuselage.
Preferably, a kind of amphibious unmanned plane of described VTOL also includes wireless camera, radar and GPS.
A kind of amphibious unmanned plane of described VTOL so works：When taking off on land, center control
Device processed receives the instruction taken off, and information is transmitted to controller, controller controls four propellers to start, and motor gives four propellers
Electric energy is provided, the amphibious unmanned plane of power brought by four propellers can take off vertically；When amphibious nothing
Man-machine when needing to drop to sea navigation, controller controls four propellers to stop operating, and amphibious unmanned plane relies on two
Wing is slowly slided and dropped on the water surface, and then controller control steering wheel starts, and provides for amphibious unmanned plane and is navigated in the water surface
Capable power；When amphibious unmanned plane needs to take off from the water surface, controller control flaps office closes, and starts four propellers and is
Taking off vertically for amphibious unmanned plane provides power；When amphibious unmanned plane needs to drop to ground, controller control
Four propellers slowly land so that amphibious unmanned function vertical landing to ground；When amphibious unmanned plane is on sea
When navigation runs into wave；It can be taken off vertically by four amphibious unmanned planes of propeller-driven, circumvent wave, wait wave mistake
The water surface is dropped to again afterwards to continue to navigate by water.
The present invention takes full advantage of the rotary power of four propellers so that amphibious unmanned plane can VTOL,
Take-off venue when land is taken off is saved, saves the time when the water surface takes off, while in the sea for running into complexity
During face, it can in a short time fly to and be hidden in the air, improve amphibious unmanned plane survival ability and operating efficiency.
Brief description of the drawings
Fig. 1 is a kind of schematic top plan view of the amphibious unmanned plane of VTOL；Fig. 2 is a kind of land and water of VTOL
The left view schematic diagram of amphibious unmanned plane.
In figure, 1- fuselages, 2- detectors, 3- controllers, 4- central processing units, 5- motors, 6- left wings, 7- right flanks, 8- companies
Extension bar, 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 amphibious unmanned plane of VTOL, including fuselage
1st, wing, empennage 10, hull 11, steering wheel 12 and 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 fuselage 1 also includes connecting rod 8 and propeller 9, and the connecting rod 8 has four, the nosing left and right sides
Respectively there is one, back body each side has one, and a propeller 9 is all connected in each connecting rod 8, is land and water two
Unmanned plane of dwelling provides the power of vertical lift.
Described wing is divided into left wing 6 and right flank 7, and left wing 6 and right flank 7 are connected with fuselage 1, positioned at the leading portion of fuselage 1, left wing
6 and 7 symmetrical distribution of right flank；Described left wing 6 is identical with the structure of right flank 7.After described empennage 10 is located at fuselage 1；Institute
The hull 11 stated is located at the lower section of fuselage 1, can be in surface navigation；Described steering wheel 12 is located at the rear end of hull 11, exists for unmanned plane
Surface navigation provides power；Described undercarriage 13 is located at the lower section of fuselage 1.
A kind of amphibious unmanned plane of described VTOL so works：When taking off on land, center control
Device 3 processed receives the instruction taken off, and information is transmitted to controller 3, controller 3 controls four propellers 9 to start, and motor 5 gives four
Propeller 9 provides electric energy, and the amphibious unmanned plane of power brought by four propellers 9 can take off vertically；Work as water
When the amphibious unmanned plane in land needs to drop to sea navigation, controller 3 controls four propellers 9 to stop operating, it is amphibious nobody
Machine is slowly slided by two wings and dropped on the water surface, and then controller 3 controls steering wheel 12 to start, and is amphibious unmanned plane
Power in surface navigation is provided；When amphibious unmanned plane needs to take off from the water surface, controller 3 controls steering wheel 12 to close,
Start four propellers 9 and provide power for taking off vertically for amphibious unmanned plane；When amphibious unmanned plane needs to drop to
During ground, controller 3 controls four propellers 9 slowly to land so that amphibious unmanned function vertical landing to ground；Work as water
The amphibious unmanned plane in land is when sea navigation runs into wave；By four propellers 9 amphibious unmanned plane can be driven vertically to rise
Fly, circumvent wave, wait wave to drop to the water surface again later and continue to navigate by water.
Claims (2)
1. a kind of amphibious unmanned plane of VTOL, including fuselage（1）, wing, empennage（10）, hull（11）, steering wheel
（12）And undercarriage（13）, it is characterised in that：Described fuselage（1）Including detector（2）, controller（3）, central processing unit
（4）And motor（5）；Described detector（2）Positioned at fuselage（1）Leading portion；Described controller（3）Positioned at fuselage（1）Stage casing；Institute
The central processing unit stated（4）Positioned at fuselage（1）Stage casing, controller（3）Right side；Described motor（5）Positioned at fuselage（1）Endpiece；
Described fuselage（1）Also include connecting rod（8）And propeller（9）, the connecting rod（8）There are four, fuselage（1）Leading portion or so two
Side respectively has one, fuselage（1）Rear end each side has one, each connecting rod（8）On be all connected to a propeller
（9）；Described wing is divided into left wing（6）And right flank（7）, left wing（6）And right flank（7）With fuselage（1）It is connected, positioned at fuselage（1）
Leading portion, left wing（6）And right flank（7）Symmetrical distribution；Described empennage（10）Positioned at fuselage（1）Afterwards；Described hull
（11）Positioned at fuselage（1）Lower section；Described steering wheel（12）Positioned at hull（11）Rear end；Described undercarriage（13）Positioned at fuselage
（1）Lower section.
A kind of 2. amphibious unmanned plane of VTOL according to claim 1, it is characterised in that：It is described amphibious
Unmanned plane also includes wireless camera, radar and GPS.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710782976.2A CN107554783A (en) | 2017-09-03 | 2017-09-03 | A kind of amphibious unmanned plane of VTOL |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710782976.2A CN107554783A (en) | 2017-09-03 | 2017-09-03 | A kind of amphibious unmanned plane of VTOL |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107554783A true CN107554783A (en) | 2018-01-09 |
Family
ID=60977906
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710782976.2A Pending CN107554783A (en) | 2017-09-03 | 2017-09-03 | A kind of amphibious unmanned plane of VTOL |
Country Status (1)
| Country | Link |
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| CN (1) | CN107554783A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110077588A (en) * | 2019-04-22 | 2019-08-02 | 大连理工大学 | It is a kind of can the sea, land and air latent four of VTOL dwell aircraft |
| CN110722942A (en) * | 2019-11-14 | 2020-01-24 | 复旦大学 | Multifunctional amphibious unmanned aerial vehicle |
| CN110775265A (en) * | 2019-10-28 | 2020-02-11 | 上海交通大学 | Oil-electricity hybrid driving amphibious aircraft and control method thereof |
| CN111152923A (en) * | 2020-01-07 | 2020-05-15 | 长江水利委员会长江科学院 | Underwater terrain measuring device based on vertical take-off and landing fixed wing amphibious unmanned aerial vehicle |
| CN112027078A (en) * | 2020-09-16 | 2020-12-04 | 郑州航空工业管理学院 | Amphibious composite wing unmanned aerial vehicle and control method thereof |
| CN113093770A (en) * | 2021-03-30 | 2021-07-09 | 华南理工大学 | Wave evaluation-based multi-rotor unmanned spacecraft water surface takeoff control method |
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 |
| CN105346718A (en) * | 2015-09-29 | 2016-02-24 | 上海圣尧智能科技有限公司 | Vertical take-off and landing unmanned plane |
| 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 |
| CN106956773A (en) * | 2017-04-07 | 2017-07-18 | 南昌航空大学 | Tilting rotor formula VUAV and its control method |
-
2017
- 2017-09-03 CN CN201710782976.2A patent/CN107554783A/en active Pending
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 |
| CN105346718A (en) * | 2015-09-29 | 2016-02-24 | 上海圣尧智能科技有限公司 | Vertical take-off and landing unmanned plane |
| CN106956773A (en) * | 2017-04-07 | 2017-07-18 | 南昌航空大学 | Tilting rotor formula VUAV and its control method |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110077588A (en) * | 2019-04-22 | 2019-08-02 | 大连理工大学 | It is a kind of can the sea, land and air latent four of VTOL dwell aircraft |
| CN110077588B (en) * | 2019-04-22 | 2022-05-20 | 大连理工大学 | Sea, land and air submerged four-purpose aircraft capable of taking off and landing vertically |
| CN110775265A (en) * | 2019-10-28 | 2020-02-11 | 上海交通大学 | Oil-electricity hybrid driving amphibious aircraft and control method thereof |
| CN110722942A (en) * | 2019-11-14 | 2020-01-24 | 复旦大学 | Multifunctional amphibious unmanned aerial vehicle |
| CN111152923A (en) * | 2020-01-07 | 2020-05-15 | 长江水利委员会长江科学院 | Underwater terrain measuring device based on vertical take-off and landing fixed wing amphibious unmanned aerial vehicle |
| CN111152923B (en) * | 2020-01-07 | 2021-06-25 | 长江水利委员会长江科学院 | Underwater terrain measuring device based on vertical take-off and landing fixed wing amphibious unmanned aerial vehicle |
| CN112027078A (en) * | 2020-09-16 | 2020-12-04 | 郑州航空工业管理学院 | Amphibious composite wing unmanned aerial vehicle and control method thereof |
| CN112027078B (en) * | 2020-09-16 | 2022-06-07 | 郑州航空工业管理学院 | Amphibious composite wing unmanned aerial vehicle and control method thereof |
| CN113093770A (en) * | 2021-03-30 | 2021-07-09 | 华南理工大学 | Wave evaluation-based multi-rotor unmanned spacecraft water surface takeoff control method |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180109 |
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| RJ01 | Rejection of invention patent application after publication |