CN107458601A - A kind of amphibious unmanned plane of the VTOL with auxiliary power - Google Patents
A kind of amphibious unmanned plane of the VTOL with auxiliary power Download PDFInfo
- Publication number
- CN107458601A CN107458601A CN201710782977.7A CN201710782977A CN107458601A CN 107458601 A CN107458601 A CN 107458601A CN 201710782977 A CN201710782977 A CN 201710782977A CN 107458601 A CN107458601 A CN 107458601A
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- CN
- China
- Prior art keywords
- propeller
- hull
- unmanned plane
- controller
- fuselage
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- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
- B64C35/008—Amphibious sea planes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
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- 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
Abstract
A kind of amphibious unmanned plane of the VTOL with auxiliary power, belong to vehicle technology field, more particularly to a kind of amphibious unmanned plane of the VTOL with auxiliary power, including fuselage, wing, empennage, hull, steering wheel and undercarriage.Described fuselage includes detector, controller, central processing unit and motor;Described left secondary hull is identical with right secondary boat body structure;Described left secondary hull also includes the first controller, second controller, swivelling chute and rail groove.The present invention takes full advantage of the rotary power of four propellers so that amphibious unmanned plane can VTOL, save take-off venue when land is taken off;Meanwhile propeller provides auxiliary power for amphibious unmanned plane, the speed of navigation is added, saves the substantial amounts of time;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 the VTOL with auxiliary power, belongs to vehicle technology field, more particularly to one
The kind amphibious unmanned plane of the VTOL with auxiliary power.
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.The landing of traditional amphibious unmanned plane is also required to
Runway, the departure time are longer.Traditional amphibious unmanned plane is adapted to the navigation in calmness, but is unfavorable for navigating on the sea of complexity
OK, when traditional amphibious unmanned plane runs into the weather for having stormy waves, just can not navigate by water so that it is traditional it is amphibious nobody
The application of machine 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, a kind of hanging down with auxiliary power of invention
The amphibious unmanned plane of straight landing.
A kind of amphibious unmanned plane of the VTOL with auxiliary power, 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 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 left wing includes left secondary hull, positioned at the middle part of left wing;Described left secondary hull includes the
One propeller and the second propeller, the first propeller are located at left secondary hull front end, and the second propeller is located at the rear end of left secondary hull;
Described right flank includes right secondary boat body, positioned at the middle part of right flank;Described right secondary boat body includes the 3rd propeller and the 4th
Propeller, the 3rd propeller are located at the front end of right secondary boat body, and quadruple screw propeller is located at the rear end of right secondary boat body;Described left wing and
Right flank structure is identical;Four described propeller arrangements are identical.
Described left secondary hull is identical with right secondary boat body structure;Described left secondary hull also includes the first controller, second
Controller, swivelling chute and rail groove;The first described controller is located at the leading portion of left secondary hull, for controlling the first propeller
Rotation;Described second controller is located at the back segment of left secondary hull, for controlling the lifting of the second propeller;Described swivelling chute
Positioned at the front end of left secondary hull, the rotation for the first spiral provides space;Described rail groove is located at the rear end of left secondary hull, is
The lifting of second propeller provides space.
After described empennage is located at fuselage;Described hull is located at below fuselage, can be in surface navigation;Described steering wheel
Positioned at hull rear end, power is provided in surface navigation for unmanned plane;Described undercarriage is located at below fuselage.
Preferably, a kind of described amphibious unmanned plane of the VTOL with auxiliary power also include wireless camera,
Radar and GPS.
A kind of propeller rotary course of described amphibious unmanned plane of the VTOL with auxiliary power:When land and water two
When unmanned plane of dwelling drops to surface navigation, four propellers of amphibious unmanned plane stop operating, and central processing unit is information
Controller, the first controller and second controller are transmitted to, controller control steering wheel rotates, and the first controller controls the first propeller
90 ° are rotated toward horizontal direction, then restarts the first propeller, as auxiliary power;Second controller also controls second simultaneously
Propeller declines along rail groove, and similarly, the 3rd propeller of right secondary boat body is also rotated by 90 ° toward horizontal direction, as second
Auxiliary power, quadruple screw propeller just decline along rail groove.
A kind of course of work of described amphibious unmanned plane of the VTOL with auxiliary power:Take off on land
When, central controller receives the instruction taken off, and information is transmitted to controller, controller controls four propellers to start, and motor is given
Four propellers provide electric energy, and the amphibious unmanned plane of power brought by four propellers can take off vertically;When
When amphibious unmanned plane needs to drop to sea navigation, controller controls four propellers to stop operating, it is amphibious nobody
Machine is slowly slided by two wings and dropped on the water surface, and then controller control steering wheel starts, and is carried for amphibious unmanned plane
For the active force in surface navigation, meanwhile, the first propeller and the 3rd propeller are rotated by 90 ° toward horizontal direction, there is provided two are auxiliary
Power-assist power, the second propeller and quadruple screw propeller decline along rail groove;When amphibious unmanned plane needs to take off from the water surface,
Controller control flaps office closes, meanwhile, control the first propeller and the 3rd propeller propeller to be rotated toward horizontal vertical direction
90 °, the second propeller and quadruple screw propeller is controlled to be ramped up along rail groove, it is amphibious nothing then to start four propellers
Man-machine taking off vertically provides power;When amphibious unmanned plane needs to drop to ground, controller controls four propellers
Slowly landing so that amphibious unmanned function vertical landing to ground;When amphibious unmanned plane, on sea, navigation runs into sea
When unrestrained;It can be taken off vertically by four amphibious unmanned planes of propeller-driven, circumvent wave, wait wave to drop to again later
The water surface continues 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;Meanwhile propeller is land and water two
Unmanned plane of dwelling provides auxiliary power, adds the speed of navigation, saves the substantial amounts of time;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.
Brief description of the drawings
Fig. 1 is a kind of schematic top plan view of the amphibious unmanned plane of the VTOL with auxiliary power;Fig. 2 is one kind with auxiliary
The left view schematic diagram of the amphibious unmanned plane of VTOL of power-assist power;Fig. 3 is vertical view of the left secondary hull without propeller of the present invention
Schematic diagram;Fig. 4 is the left view schematic diagram after the left width hull propeller rotation of the present invention and decline.
In figure, 1- fuselages, 2- detectors, 3- controllers, 4- central processing units, 5- motors, 6- left wings, 7- right flanks, a 8- left sides
Secondary hull, the propellers of 9- first, the propellers of 10- second, 11- right secondary boat bodies, the propellers of 12- the 3rd, 13- quadruple screw propellers, 14-
Empennage, 15- hulls, 16- steering wheels, 17- undercarriages, the controllers of 18- first, 19- second controllers, 20- swivelling chutes, 21- tracks
Groove.
Embodiment
The present invention is illustrated in conjunction with accompanying drawing:A kind of VTOL with auxiliary power it is amphibious nobody
Machine, including fuselage 1, wing, empennage 14, hull 15, steering wheel 16 and undercarriage 17.
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 is divided into
Left wing 6 and right flank, left wing 6 and right flank 7 are connected with fuselage 1, positioned at the leading portion of fuselage 1, the 7 symmetrical distribution of left wing 6 and right flank;
Described left wing 6 includes left secondary hull 8, positioned at the middle part of left wing 6;Described left secondary hull 8 includes the He of the first propeller 9
Second propeller 10, the first propeller 9 are located at the front end of left secondary hull 8, and the second propeller 10 is located at the rear end of left secondary hull 8;Institute
The right flank 7 stated includes right secondary boat body 11, positioned at the middle part of right flank 7;Described right secondary boat body 11 includes the 3rd propeller 12
With quadruple screw propeller 13, the 3rd propeller 12 is located at the front end of right secondary boat body 11, and quadruple screw propeller 13 is located at right secondary boat body 11
Rear end;Described left wing 6 is identical with the structure of right flank 7;Described left secondary hull 8 is identical with the structure of right secondary boat body 11;Described four
Individual propeller arrangement is identical.
Now the left width hull of the present invention is illustrated:Described left secondary hull 8 also includes the first controller 18, second
Controller 19, swivelling chute 20 and rail groove 21;The first described controller 18 is located at the leading portion of left secondary hull 8, for controlling the
The rotation of one propeller 9;Described second controller 19 is located at the back segment of left secondary hull 8, for controlling the second propeller 10
Lifting;Described swivelling chute 20 is located at the front end of left secondary hull 8, and the rotation for the first spiral provides space;Described rail groove
21 are located at the rear end of left secondary hull 8, and the lifting for the second propeller 10 provides space.
After described empennage 14 is located at fuselage 1;Described hull 15 is located at the lower section of fuselage 1, can be in surface navigation;It is described
Steering wheel 16 be located at the rear end of hull 15, provide power in surface navigation for unmanned plane;Described undercarriage 17 is located under fuselage 1
Side.
A kind of described amphibious unmanned plane of the VTOL with auxiliary power also include wireless camera, radar and
GPS。
A kind of propeller rotary course of described amphibious unmanned plane of the VTOL with auxiliary power:When land and water two
When unmanned plane of dwelling drops to surface navigation, four propellers of amphibious unmanned plane stop operating, and central processing unit 4 is information
It is transmitted to controller 3, the first controller 18 and second controller 19, controller 3 controls steering wheel to rotate, the first controller 18 control the
One propeller 9 rotates 90 ° toward horizontal direction, then restarts the first propeller 9, as auxiliary power;Second controller simultaneously
19 also control the second propeller 10 to decline along rail groove 21, and similarly, the 3rd propeller 12 of right secondary boat body 11 is also toward level side
To being rotated by 90 °, as second auxiliary power, quadruple screw propeller 14 just declines along rail groove 21.
A kind of described amphibious unmanned plane of the VTOL with auxiliary power so works:Take off on land
When, central controller 3 receives the instruction taken off, and information is transmitted to controller 3, controller 3 controls four propellers to start, motor
5 provide electric energy to four propellers, and the amphibious unmanned plane of power brought by four propellers can take off vertically;
When amphibious unmanned plane needs to drop to sea navigation, controller 3 controls four propellers to stop operating, amphibious nothing
Man-machine slowly to slide and drops on the water surface by two wings, then controller 3 controls steering wheel 16 to start, for it is amphibious nobody
Machine provides the active force in surface navigation, meanwhile, the first propeller 9 and the 3rd propeller 12 are rotated by 90 ° toward horizontal direction, there is provided
Two auxiliary powers, the second propeller 10 and quadruple screw propeller 13 decline along rail groove 21;When amphibious unmanned plane needs
When being taken off from the water surface, controller 3 controls steering wheel 16 to close, meanwhile, four propellers of control are rotated by 90 ° toward horizontal vertical direction,
Start four propellers and provide power for taking off vertically for amphibious unmanned plane;When amphibious unmanned plane needs to drop to ground
During face, controller 3 controls four propellers slowly to land so that amphibious unmanned function vertical landing to ground;Work as land and water
Amphibious unmanned plane is when sea navigation runs into wave;It can be taken off vertically by four amphibious unmanned planes of propeller-driven,
Wave is circumvented, waits wave to drop to the water surface again later and continues to navigate by water.
Claims (2)
1. a kind of amphibious unmanned plane of the VTOL with auxiliary power, including fuselage(1), wing, empennage(14), hull
(15), steering wheel(16)And undercarriage(17), it is characterised in that:Described fuselage(1)Including detector(2), controller(3), in
Central processor(4)And 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 machine
Body(1)Endpiece;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 machine
Body(1)Leading portion, left wing(6)And right flank(7)Symmetrical distribution;Described left wing(6)Including left secondary hull(8), positioned at a left side
The wing(6)Middle part;Described left secondary hull(8)Including the first propeller(9)With the second propeller(10), the first propeller
(9)Positioned at left secondary hull(8)Front end, the second propeller(10)Positioned at left secondary hull(8)Rear end;Described right flank(7)Including
Right secondary boat body(11), positioned at right flank(7)Middle part;Described right secondary boat body(11)Including the 3rd propeller(12)With the 4th
Propeller(13), the 3rd propeller(12)Positioned at right secondary boat body(11)Front end, quadruple screw propeller(13)Positioned at right secondary boat body
(11)Rear end;Described left wing(6)And right flank(7)Structure is identical;Four described propeller arrangements are identical;Described left secondary
Hull(8)With right secondary boat body(11)Structure is identical;Described left secondary hull(8)Also include the first controller(18), second control
Device(19), swivelling chute(20)And rail groove(21);The first described controller(18)Positioned at left secondary hull(8)Leading portion;It is described
Second controller(19)Positioned at left secondary hull(8)Back segment;Described swivelling chute(20)Positioned at left secondary hull(8)Front end;
Described rail groove(21)Positioned at left secondary hull(8)Rear end;Described empennage(14)Positioned at fuselage(1)Afterwards;Described hull
(15)Positioned at fuselage(1)Lower section;Described steering wheel(16)Positioned at hull(15)Rear end;Described undercarriage(17)Positioned at fuselage
(1)Lower section.
A kind of 2. amphibious unmanned plane of the VTOL with auxiliary power according to claim 1, it is characterised in that:Institute
Stating amphibious unmanned plane also includes wireless camera, radar and GPS.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201710782977.7A CN107458601A (en) | 2017-09-03 | 2017-09-03 | A kind of amphibious unmanned plane of the VTOL with auxiliary power |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201710782977.7A CN107458601A (en) | 2017-09-03 | 2017-09-03 | A kind of amphibious unmanned plane of the VTOL with auxiliary power |
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Publication Number | Publication Date |
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CN107458601A true CN107458601A (en) | 2017-12-12 |
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ID=60551733
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CN201710782977.7A Withdrawn CN107458601A (en) | 2017-09-03 | 2017-09-03 | A kind of amphibious unmanned plane of the VTOL with auxiliary power |
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Citations (5)
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 |
CN106516110A (en) * | 2016-12-22 | 2017-03-22 | 中国海洋大学 | Water-air amphibious glider capable of vertically taking-off, landing and flying |
-
2017
- 2017-09-03 CN CN201710782977.7A patent/CN107458601A/en not_active Withdrawn
Patent Citations (5)
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 |
CN106516110A (en) * | 2016-12-22 | 2017-03-22 | 中国海洋大学 | Water-air amphibious glider capable of vertically taking-off, landing and flying |
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Application publication date: 20171212 |