CN107521661A - A kind of rotatable more amphibious unmanned planes of power VTOL of wing - Google Patents
A kind of rotatable more amphibious unmanned planes of power VTOL of wing Download PDFInfo
- Publication number
- CN107521661A CN107521661A CN201710782981.3A CN201710782981A CN107521661A CN 107521661 A CN107521661 A CN 107521661A CN 201710782981 A CN201710782981 A CN 201710782981A CN 107521661 A CN107521661 A CN 107521661A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- wing
- amphibious unmanned
- tailplane
- stage 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
-
- 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
- B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
A kind of rotatable more amphibious unmanned planes of power VTOL of wing, belong to vehicle technology field, more particularly to a kind of rotatable more amphibious unmanned planes of power VTOL of wing, including fuselage, wing, empennage, hull and undercarriage.Described fuselage is symmetrical, and described fuselage is symmetrical, includes self-locking device and connecting rod on the left of described fuselage, described self-locking device is located at the stage casing of fuselage, positioned at the top of connecting rod and left, described connecting rod is located at the stage casing of fuselage, and stage casing is embedded in fuselage interior;Both ends are embedded in inside wing so that fuselage is connected with wing.The present invention take full advantage of wing rotation ability so that amphibious unmanned plane can VTOL, save take-off venue when land is taken off, save the time when the water surface takes off;When running into the sea of complexity, it also 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 rotatable more amphibious unmanned planes of power VTOL of wing, belong to vehicle technology field, especially
It is related to a kind of rotatable more amphibious unmanned planes of power VTOL of wing.
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, and it is rotatable more to invent a kind of wing
The amphibious unmanned plane of power VTOL.
A kind of rotatable more amphibious unmanned planes of power VTOL of wing, including fuselage, wing, empennage, hull
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 is symmetrical, includes self-locking device and connecting rod, described self-locking device on the left of described fuselage
Positioned at the stage casing of fuselage, positioned at the top of connecting rod and left, eight altogether, wing when being lifted for fixed vertical;Institute
The connecting rod stated is located at the stage casing of fuselage, and stage casing is embedded in fuselage interior;Both ends are embedded in inside wing so that fuselage and wing
It is connected.
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 also carries propeller, positioned at the middle part of left wing;Described left wing and right flank structure
It is identical;Described empennage is divided into port tailplane and starboard tailplane, and port tailplane and starboard tailplane are connected with fuselage, positioned at aft body, left tail
The wing and the symmetrical distribution of starboard tailplane;Described port tailplane also carries propeller, positioned at the middle part of port tailplane;A described left side
Empennage is identical with the structure of starboard tailplane.
Described hull is located at below fuselage, can be in surface navigation;Described undercarriage is located at below fuselage.
Preferably, a kind of rotatable more amphibious unmanned planes of power VTOL of described wing also include wirelessly taking the photograph
As head, radar and GPS.
The wing and empennage of a kind of rotatable more amphibious unmanned planes of power VTOL of described wing rotate through
Journey:When amphibious unmanned plane drops to surface navigation, instruction is transmitted to controller, controller control wing by central processing unit
Be rotated by 90 ° with the leading edge of empennage toward vertical direction so that amphibious unmanned plane slowly drops to the water surface, then again wing and
Empennage, which is gone back to, to be come, and starts propeller, amphibious unmanned plane just can be in surface navigation.
A kind of rotatable more amphibious unmanned planes of power VTOL of described wing so work:On land
On when taking off, central controller receives the instruction taken off, and information is transmitted to the leading edge of controller, controller control wing and empennage
It is rotated by 90 ° toward vertical direction, motor provides electric energy, the power land and water two brought by two propellers to two propellers
Unmanned plane of dwelling can take off vertically;When amphibious unmanned plane needs to drop to sea navigation, controller controls two spirals
Oar stops operating, meanwhile, controller control wing and the leading edge of empennage are rotated by 90 ° toward vertical direction so that it is amphibious nobody
Machine slowly drops to the water surface;When amphibious unmanned plane needs to take off from the water surface, controller controls two propellers to close,
Then the leading edge of wing and empennage is rotated by 90 ° toward vertical direction, then restarts two propellers so that it is amphibious nobody
Machine can take off vertically on the water surface;When amphibious unmanned plane runs into wave in sea navigation;Wing and tail can be passed through
The leading edge of the wing is revolved toward after 90 ° of vertical direction turn, is taken off vertically to circumvent wave, is waited wave to drop to the water surface again later and is continued to navigate
OK.
The present invention take full advantage of wing and empennage rotation ability 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;When running into the sea of complexity,
Also 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 rotatable more amphibious unmanned planes of power VTOL of wing;Fig. 2 is this
Left view schematic diagram of the invention without wing;Fig. 3 is the schematic top plan view that the present invention deploys.
In figure, 1- fuselages, 2- detectors, 3- controllers, 4- central processing units, 5- motors, 6- left wings, 7- right flanks, 8- is certainly
Locking device, 9- connecting rods, 10- propellers, 12- port tailplanes, 13- starboard tailplanes, 14- hulls, 15- undercarriages.
Embodiment
The present invention is illustrated in conjunction with accompanying drawing:A kind of rotatable more power VTOL of wing are amphibious
Unmanned plane, including fuselage 1, wing, empennage, hull 14 and undercarriage 15.
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 or so
Symmetrically.
Described fuselage 1 is symmetrical, and now the structure in the left side of fuselage 1 is illustrated:The described left side of fuselage 1 includes
Self-locking device 8 and connecting rod 9, described self-locking device 8 are located at the stage casing of fuselage 1, positioned at the top of connecting rod 9 and left, one
Totally eight, wing when being lifted for fixed vertical;Described connecting rod 9 is located at the stage casing of fuselage 1, and stage casing is embedded in fuselage
Inside 1;Both ends are embedded in inside wing so that fuselage 1 is connected with wing.
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 right flank be in 7 symmetrical distributions;Described left wing 6 also carries propeller 10, positioned at the middle part of left wing 6;A described left side
The wing 6 is identical with the structure of right flank 7;Described empennage is divided into port tailplane 12 and starboard tailplane 13, port tailplane 12 and starboard tailplane 13 and fuselage 1
It is connected, positioned at the back segment of fuselage 1, the 13 symmetrical distribution of port tailplane 12 and starboard tailplane;Described port tailplane 12 also carries propeller
10, positioned at the middle part of port tailplane 12;Described port tailplane 12 is identical with the structure of starboard tailplane 13.
Described hull 14 is located at the lower section of fuselage 1, can be in surface navigation;Described undercarriage 15 is located at the lower section of fuselage 1.
A kind of amphibious unmanned plane wing of the rotatable more power VTOL of described wing and empennage rotary course:
When amphibious unmanned plane drops to surface navigation, instruction is transmitted to controller 3 by central processing unit 4, and controller 3 controls wing
Be rotated by 90 ° with the leading edge of empennage toward vertical direction so that amphibious unmanned plane slowly drops to the water surface, then again wing and
Empennage, which is gone back to, to be come, and starts propeller, amphibious unmanned plane just can be in surface navigation.
The rotatable more amphibious unmanned planes of power VTOL of described a kind of wing and empennage so work:
When taking off on land, central controller 3 receives the instruction taken off, and information is transmitted to controller 3, controller 3 control wing and
The leading edge of empennage is rotated by 90 ° toward vertical direction, and motor 5 provides electric energy to two propellers, is brought by two propellers dynamic
Power enables amphibious unmanned plane to take off vertically;When amphibious unmanned plane needs to drop to sea navigation, controller 3
Two propellers of control stop operating, meanwhile, controller 3 controls the leading edge of wing and empennage to be rotated by 90 ° toward vertical direction so that
Amphibious unmanned plane slowly drops to the water surface;When amphibious unmanned plane needs to take off from the water surface, the control of controller 3 two
Individual propeller is closed, and then the leading edge of wing and empennage is rotated by 90 ° toward vertical direction, then restarts two propellers, makes
Obtaining amphibious unmanned plane can take off vertically on the water surface;When amphibious unmanned plane runs into wave in sea navigation;Can
Revolved after turning 90 ° toward vertical direction, taken off vertically to circumvent wave with the leading edge by wing and empennage, wait wave to land again later
Continue to navigate by water to the water surface.
Claims (2)
1. a kind of rotatable more amphibious unmanned planes of power VTOL of wing, including fuselage(1), wing, empennage, hull
(14)And undercarriage(15), 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)Symmetrical, described fuselage(1)Left side includes self-locking device(8)And connecting rod(9), described self-locking
Device(8)Positioned at fuselage(1)Stage casing, positioned at connecting rod(9)Top and left, eight altogether;Described connecting rod(9)Position
In fuselage(1)Stage casing, stage casing is embedded in fuselage(1)It is internal;Both ends are embedded in inside wing so that fuselage(1)With wing phase
Connection;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 left wing(6)Also carry propeller(10), positioned at left wing(6)
Middle part;Described left wing(6)With right flank(7)Structure is identical;Described empennage is divided into port tailplane(12)And starboard tailplane
(13), port tailplane(12)And starboard tailplane(13)With fuselage(1)It is connected, positioned at fuselage(1)Back segment, port tailplane(12)And starboard tailplane
(13)Symmetrical distribution;Described port tailplane(12)Also carry propeller(10), positioned at port tailplane(12)Middle part;Institute
The port tailplane stated(12)With starboard tailplane(13)Structure it is identical;Described hull(14)Positioned at fuselage(1)Lower section;Described rises and falls
Frame(15)Positioned at fuselage(1)Lower section.
2. the rotatable more amphibious unmanned planes of power VTOL of a kind of wing according to claim 1, its feature
It is:The amphibious unmanned plane also includes wireless camera, radar and GPS.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710782981.3A CN107521661A (en) | 2017-09-03 | 2017-09-03 | A kind of rotatable more amphibious unmanned planes of power VTOL of wing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710782981.3A CN107521661A (en) | 2017-09-03 | 2017-09-03 | A kind of rotatable more amphibious unmanned planes of power VTOL of wing |
Publications (1)
Publication Number | Publication Date |
---|---|
CN107521661A true CN107521661A (en) | 2017-12-29 |
Family
ID=60683481
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710782981.3A Withdrawn CN107521661A (en) | 2017-09-03 | 2017-09-03 | A kind of rotatable more amphibious unmanned planes of power VTOL of wing |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN107521661A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108583912A (en) * | 2018-01-29 | 2018-09-28 | 杭州迅蚁网络科技有限公司 | A kind of tail sitting posture unmanned vertical flight |
CN109131879A (en) * | 2018-07-26 | 2019-01-04 | 合肥学院 | A kind of ocean garbage reclamation robot |
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 |
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 |
CN106628168A (en) * | 2016-11-30 | 2017-05-10 | 北京天宇新超航空科技有限公司 | Novel tilt rotor aircraft |
CN106828913A (en) * | 2017-01-09 | 2017-06-13 | 北京猎鹰无人机科技有限公司 | A kind of VUAV |
-
2017
- 2017-09-03 CN CN201710782981.3A patent/CN107521661A/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 |
CN106628168A (en) * | 2016-11-30 | 2017-05-10 | 北京天宇新超航空科技有限公司 | Novel tilt rotor aircraft |
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 |
CN106828913A (en) * | 2017-01-09 | 2017-06-13 | 北京猎鹰无人机科技有限公司 | A kind of VUAV |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108583912A (en) * | 2018-01-29 | 2018-09-28 | 杭州迅蚁网络科技有限公司 | A kind of tail sitting posture unmanned vertical flight |
CN109131879A (en) * | 2018-07-26 | 2019-01-04 | 合肥学院 | A kind of ocean garbage reclamation robot |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN104589938B (en) | A kind of imitative flying fish variable configuration is across medium aircraft | |
CN107554783A (en) | A kind of amphibious unmanned plane of VTOL | |
CN110775264B (en) | Water-air amphibious unmanned aircraft and control method thereof | |
CN107696811A (en) | A kind of VTOL amphibious unmanned plane of more power | |
CN109018271B (en) | Novel large-span hybrid drive unmanned underwater vehicle | |
US20120298789A1 (en) | Aircraft | |
CN108656885A (en) | Tilting rotor air-sea amphibious robot | |
CN109878666A (en) | A kind of leading edge rotational circle column type wing control underwater towed vehicle, | |
Alzu'bi et al. | Evaluation of an aerial quadcopter power-plant for underwater operation | |
CN109017181A (en) | A kind of small-scale underwater vehicle device carriage by air is laid and recovery system | |
CN110254710A (en) | A kind of empty amphibious unmanned plane of mixing wing water of two-stage displacement | |
CN206984354U (en) | A kind of aircraft | |
CN209617425U (en) | A kind of underwater unmanned vehicle vector propulsion device | |
CN109383727A (en) | A kind of nearly vector expression underwater robot propeller | |
CN107521661A (en) | A kind of rotatable more amphibious unmanned planes of power VTOL of wing | |
CN107176297A (en) | A kind of aircraft | |
CN110722941A (en) | Rotor type water-air crossing amphibious aircraft and use method thereof | |
RU139040U1 (en) | AIRCRAFT "LANNER" | |
CN107499504A (en) | A kind of amphibious unmanned plane of rotatable VTOL of wing | |
CN203753403U (en) | Water-air dual-purpose ship | |
CN106184692A (en) | A kind of flying wing type hybrid lift dirigible of the dismantled and assembled power that verts | |
CN205113714U (en) | Dual -purpose unmanned navigation ware device under water in air | |
CN202357821U (en) | Wing-variable micro amphibian flight vehicle | |
CN107539470A (en) | A kind of four oars amphibious unmanned plane of VTOL | |
CN207045646U (en) | Nearly vector expression underwater robot propeller |
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 | ||
WW01 | Invention patent application withdrawn after publication | ||
WW01 | Invention patent application withdrawn after publication |
Application publication date: 20171229 |