CN106042803A - Amphibious unmanned aerial vehicle - Google Patents
Amphibious unmanned aerial vehicle Download PDFInfo
- Publication number
- CN106042803A CN106042803A CN201610363528.4A CN201610363528A CN106042803A CN 106042803 A CN106042803 A CN 106042803A CN 201610363528 A CN201610363528 A CN 201610363528A CN 106042803 A CN106042803 A CN 106042803A
- Authority
- CN
- China
- Prior art keywords
- lift fan
- amphibious unmanned
- propeller
- unmanned aerial
- aerial vehicle
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Epoxy Compounds (AREA)
Abstract
The invention relates to an amphibious unmanned aerial vehicle which is composed of a vehicle body, a first lift fan, a second lift fan, a first propeller, a second propeller, undercarriages, undercarriage sliding wheels and a triangular wing. When vertical take-off and landing are needed, the first lift fan and the second lift fan can be converted so as to be perpendicular to the ground to achieve vertical take-off and landing, after the amphibious unmanned aerial vehicle ascends to the air, the angles of the first lift fan and the second lift fan are converted, and at the moment, the flight speed can be greatly increased. When the first lift fan and the second lift fan are converted to be parallel to the ground, the amphibious unmanned aerial vehicle can travel on the ground. The amphibious unmanned aerial vehicle has the beneficial effects of being multifunctional and simple in structure.
Description
Technical field
The present invention relates to a kind of unmanned plane, particularly to a kind of amphibious unmanned plane.
Background technology
Unmanned aerial vehicle has been widely applied in all trades and professions, performs such as to take photo by plane, transport, the task such as investigation.Existing nothing
The flying power of people's aircraft is limited, and function is more single.
Summary of the invention
In order to overcome the deficiency that existing unmanned plane function is more single, it not only may be used to the present invention relates to a kind of amphibious unmanned plane
Can also travel on the ground with VTOL.
The amphibious unmanned plane of the present invention by body, lift fan one, lift fan two, propeller one, propeller two, rise and fall
Frame, undercarriage pulley and dalta wing composition.Lift fan one, lift fan two are arranged on the head position of body, propeller one
With the tail position that propeller two is arranged on body, body is provided with dalta wing, the undercarriage of body is provided with four and rises and falls
Frame pulley.Lift fan one and lift fan two can be with auto-changing angles.
When needs VTOL, lift fan one, lift fan two can transform to and be perpendicular to ground to realize vertical liter
Fall, amphibious unmanned plane rise to aerial after conversion lift fan once and the angle of lift fan two at this time can be greatly improved
Flight speed.When lift fan once and lift fan two transform to when being parallel to ground that amphibious unmanned plane can be on the ground
Travel.
The amphibious unmanned plane of the present invention provides the benefit that have multifunctionality, simple in construction.
Accompanying drawing explanation
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the axonometric chart of the amphibious unmanned plane of the present invention.
Fig. 2 is the change axonometric chart of the amphibious unmanned plane of the present invention.
1. body in figure, 2. lift fan one, 3. lift fan two, 4. propeller one, 5. propeller two, 6. undercarriage,
7. undercarriage pulley, 8. dalta wing.
Detailed description of the invention
The amphibious unmanned plane of the present invention by body 1, lift fan 1, lift fan 23, propeller 1, propeller 25,
Undercarriage 6, undercarriage pulley 7 and dalta wing 8 form (as shown in Figure 1).Lift fan 1, lift fan 23 are arranged on body
The head position of 1, propeller 1 and propeller 25 are arranged on the tail position of body 1, and body 1 is provided with dalta wing 8, body
Four undercarriage pulleys 7 it are provided with on the undercarriage 6 of 1.Lift fan 1 and lift fan 23 can with auto-changing angle (as
Shown in Fig. 1).
When needs VTOL, lift fan 1, lift fan 23 can transform to and be perpendicular to ground to realize vertically
Lifting (as shown in Figure 1), at this moment amphibious unmanned plane rises to the angle of aerial rear conversion lift fan 1 and lift fan 23
Wait and just can be greatly improved flight speed.When lift fan 1 and lift fan 23 transform to amphibious nothing when being parallel to ground
Man-machine just can travel on the ground (as shown in Figure 2).
Claims (1)
1. an amphibious unmanned plane, is characterized in that amphibious unmanned plane is by body 1, lift fan 1, lift fan 23, propeller
One 4, propeller 25, undercarriage 6, undercarriage pulley 7 and dalta wing 8 form；Lift fan 1, lift fan 23 are arranged on
The head position of body 1, propeller 1 and propeller 25 are arranged on the tail position of body 1, and body 1 is provided with dalta wing 8,
Being provided with four undercarriage pulleys 7, lift fan 1 and lift fan 23 on the undercarriage 6 of body 1 can be with auto-changing angle
Degree.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610363528.4A CN106042803A (en) | 2016-05-22 | 2016-05-22 | Amphibious unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610363528.4A CN106042803A (en) | 2016-05-22 | 2016-05-22 | Amphibious unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106042803A true CN106042803A (en) | 2016-10-26 |
Family
ID=57175345
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610363528.4A Pending CN106042803A (en) | 2016-05-22 | 2016-05-22 | Amphibious unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106042803A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106882372A (en) * | 2017-03-10 | 2017-06-23 | 佛山市神风航空科技有限公司 | A kind of delta-wing aircraft of energy VTOL |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1754777A (en) * | 2004-09-30 | 2006-04-05 | 李环 | Vertical take-off and landing aircraft |
| CN103318405A (en) * | 2013-07-17 | 2013-09-25 | 国家电网公司 | Unmanned plane |
| CN103538714A (en) * | 2013-11-06 | 2014-01-29 | 张明 | Vertical take-off and landing model aircraft unmanned aerial vehicle |
| CN204110359U (en) * | 2014-09-18 | 2015-01-21 | 陈文友 | Straight putting down flies dual-purpose aircraft |
| CN205150238U (en) * | 2015-11-26 | 2016-04-13 | 郭亨浩 | Unmanned aerial vehicle |
| US20160114887A1 (en) * | 2002-10-01 | 2016-04-28 | Dylan T X Zhou | Amphibious vertical takeoff and landing unmanned system and flying car with multiple aerial and aquatic flight modes for capturing panoramic virtual reality views, interactive video and transportation with mobile and wearable application |
-
2016
- 2016-05-22 CN CN201610363528.4A patent/CN106042803A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160114887A1 (en) * | 2002-10-01 | 2016-04-28 | Dylan T X Zhou | Amphibious vertical takeoff and landing unmanned system and flying car with multiple aerial and aquatic flight modes for capturing panoramic virtual reality views, interactive video and transportation with mobile and wearable application |
| CN1754777A (en) * | 2004-09-30 | 2006-04-05 | 李环 | Vertical take-off and landing aircraft |
| CN103318405A (en) * | 2013-07-17 | 2013-09-25 | 国家电网公司 | Unmanned plane |
| CN103538714A (en) * | 2013-11-06 | 2014-01-29 | 张明 | Vertical take-off and landing model aircraft unmanned aerial vehicle |
| CN204110359U (en) * | 2014-09-18 | 2015-01-21 | 陈文友 | Straight putting down flies dual-purpose aircraft |
| CN205150238U (en) * | 2015-11-26 | 2016-04-13 | 郭亨浩 | Unmanned aerial vehicle |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106882372A (en) * | 2017-03-10 | 2017-06-23 | 佛山市神风航空科技有限公司 | A kind of delta-wing aircraft of energy VTOL |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161026 |
|
| DD01 | Delivery of document by public notice | ||
| DD01 | Delivery of document by public notice |
Addressee: Wang Jing Document name: Notification that Application Deemed to be Withdrawn |