CN109353501A - Shoe formula aquatic unmanned aerial vehicle - Google Patents
Shoe formula aquatic unmanned aerial vehicle Download PDFInfo
- Publication number
- CN109353501A CN109353501A CN201811352653.0A CN201811352653A CN109353501A CN 109353501 A CN109353501 A CN 109353501A CN 201811352653 A CN201811352653 A CN 201811352653A CN 109353501 A CN109353501 A CN 109353501A
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- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- shoe
- fuselage
- wing
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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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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 11
- 238000011835 investigation Methods 0.000 abstract description 6
- 230000000007 visual effect Effects 0.000 abstract description 4
- 238000005096 rolling process Methods 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000004064 recycling Methods 0.000 description 2
- 230000037396 body weight Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 201000009482 yaws Diseases 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of shoe formula aquatic unmanned aerial vehicles, including fuselage, it is installed on the wing that body upper extends along fuselage central axes two sides, the electric pod being installed below fore-body, it is installed on the airscrew engine of afterbody, the radome fairing being fixed on fuselage, the shoe being connect with radome fairing, further include the empennage being connected with shoe, is connected to the floating drum extended obliquely below fuselage along central axes two sides.The shoe formula aquatic unmanned aerial vehicle has reliable and stable structure and the openr investigation visual field, can float on the water surface and landing.
Description
Technical field
The present invention relates to aquatic unmanned aerial vehicle fields, more particularly to a kind of shoe formula aquatic unmanned aerial vehicle.
Background technique
Unmanned air vehicle technique is quickly grown at present, is all widely used in many fields such as military, civil, existing nothing
It is man-machine generally to recycle and draw in the net to recycle using undercarriage, if unmanned plane encounters fortuitous event and cannot look for when executing marine task
To suitable landing environment, then will crash after unmanned plane depleted of energy.Therefore, be faced with cannot be in water for traditional unmanned plane
Face landing, when sail, are inconvenient to the problems such as recycling.Meanwhile also having this body weight big, the disadvantages of payload is small.
Therefore, it is necessary to a kind of new technical solutions to solve the above technical problems.
Summary of the invention
To solve the deficiencies in the prior art, the present invention proposes a kind of shoe formula aquatic unmanned aerial vehicle, the shoe formula it is waterborne nobody
Machine has reliable and stable structure and the openr investigation visual field, can float on the water surface and landing.
In order to achieve the above objectives, the present invention adopts the following technical scheme that: a kind of shoe formula aquatic unmanned aerial vehicle, feature
It is, including fuselage, is installed on the wing that body upper extends along fuselage central axes two sides, the electricity being installed below fore-body
Sub- gondola is installed on the airscrew engine of afterbody, the radome fairing being fixed on fuselage, the shoe connecting with radome fairing,
Further include the empennage being connected with shoe, is connected to the floating drum extended obliquely below fuselage along central axes two sides.
In a specific embodiment, the empennage is U-shaped empennage, and the U-shaped empennage includes horizontal tail, is located at described flat
Tail both ends are approximately perpendicular to the left vertical fin of the horizontal tail, and right vertical fin is separately mounted to left vertical fin, the left direction on right vertical fin
Rudder, right direction rudder, and the pitching rudder being mounted in horizontal tail.
In a specific embodiment, the number of the floating drum includes two, and described two floating drums pass through floating drum respectively
Connecting rod is connect with fuselage.
In a specific embodiment, the floating drum is ship shape.
In a specific embodiment, the wing extended along fuselage central axes two sides includes port wing and right machine
The wing, and the left side aileron and right side aileron that are separately positioned on port wing and starboard wing.
In a specific embodiment, the length D of the wing is 4.824m.
In a specific embodiment, the top of the left vertical fin and right vertical fin and the bottom distance H of fuselage are
1.76m。
In a specific embodiment, the length A of the shoe formula unmanned plane is 5.096m.
Shoe formula aquatic unmanned aerial vehicle proposed by the present invention, floating drum and shoe use so that unmanned plane has tail boom airplane
Equally reliable and stable structure and the openr investigation visual field, the water surface landing ability with seaplane.Compared to same
Traditional unmanned plane, possesses larger range of investigation ability and stronger survival ability, and unmanned plane of the present invention has both seaplane, tail
The characteristic of support formula aircraft or foilcraft, Quick-speed low-resistance landing waterborne, is slided when the water surface is long.
At military aspect, shoe formula aquatic unmanned aerial vehicle realizes that the recycling of unmanned plane universe has executed by water surface landing ability
Task may not necessarily return to naval vessel or roadbed base, can directly land and wait subsequent recovery on the water, possess bigger distance
Investigation ability.
At civilian aspect, shoe formula aquatic unmanned aerial vehicle is suitable for photography waterborne, seaplane simulated training.
Detailed description of the invention
Fig. 1 is the schematic diagram of shoe formula aquatic unmanned aerial vehicle of the invention.
Fig. 2 is the front view of shoe formula aquatic unmanned aerial vehicle of the invention；
Fig. 3 is the main view of shoe formula aquatic unmanned aerial vehicle of the invention；
Fig. 4 is the top view of shoe formula aquatic unmanned aerial vehicle of the invention.
Specific embodiment
The preferred embodiment of apparatus of the present invention and method is described in further detail with reference to the accompanying drawing.
As shown in Figure 1, a kind of shoe formula aquatic unmanned aerial vehicle, including fuselage 1,1 top of fuselage is installed on along 1 central axes of fuselage
The wing 5 that two sides extend, is installed on the electric pod 2 of 1 lower front of fuselage, is installed on the airscrew engine of 1 tail portion of fuselage
12, power is provided for unmanned plane, the radome fairing 13 being fixed on fuselage 1, the shoe 6 connecting with radome fairing 13 further includes and tail
The connected empennage of support 6 is connected to the floating drum 3 that 1 lower section of fuselage extends obliquely along central axes two sides.Shoe 6 can make unmanned plane
Possess more stable structure and the openr investigation visual field.
As shown in Figure 1 and Figure 4, empennage is U-shaped empennage, and U-shaped empennage includes horizontal tail 9, is approximately perpendicular to the left vertical fin of horizontal tail 9
10, right vertical fin 7 is separately positioned on left vertical fin 10, the left direction rudder 11 on right vertical fin 7, right direction rudder 8, and setting and exists
Pitching rudder 16 in horizontal tail 9.The transverse and longitudinal stability of the U-shaped adjustable unmanned plane of empennage, while the pitching to control unmanned plane,
Rolling and yawing rotation.
As shown in Figure 1,1 rear portion of fuselage is arranged in shoe 6, diameter is significantly less than the cab body construction of fuselage 1, partially plays rear machine
The effect of body, end is equipped with empennage, therefore plays the role of the arm of force again.The advantages of shoe 6, is that structure is more stable, reliability
It is higher, especially scounting aeroplane using the topology layout of back-pushed shoe benefit be rear engine driving propeller 12 not
The sight of ferreting device can be blocked.
As shown in Fig. 2, the number of floating drum 3 includes two, which is connected by floating drum connecting rod 4 and fuselage 1 respectively
It connects.The floating drum 3 is ship shape, unmanned plane can be made in floating on water and landing using ship shape floating drum, it is waterborne can to enhance shoe formula
Stability of the unmanned plane in floating on water.In a specific embodiment, the length D of wing is 4.824m.
As shown in figure 3, in a specific embodiment, the bottom at the top and fuselage 1 of left vertical fin 7 and right vertical fin 8
Distance H is 1.76m, and electric pod 2 is mounted on 1 front of fuselage, that is, the lower section of head.
As shown in figure 4, including port wing and starboard wing along the wing 5 that 1 central axes two sides of fuselage extend, and it is respectively set
Left side aileron 14 and right side aileron 15 on port wing and starboard wing.The length A of entire unmanned plane is 5.096m.
When unmanned plane hydroplaning or the water surface take off, floating drum 3 guarantees that fuselage 1 is not contacted with the water surface in hydroplaning.Nobody
When machine surface navigation carries out directional control, pass through left direction rudder 11 and right direction rudder 8 and left side aileron 14 and right side aileron
15 linkage controls yaw to realize, right direction rudder 11 and right direction rudder 8 deflect to the left, and left side aileron 14 deflects down together
When right side aileron 15 upward deflect then unmanned plane and deflected to the right to left drift, left direction rudder 11 and right direction rudder 8, left side pair
The wing 14 upward deflects while right side aileron 15 deflects down, and unmanned plane yaws to the right.Unmanned plane surface navigation carries out pitch control
When, it is realized by control pitching rudder 16, pitching rudder 16 deflects down, and aircraft is bowed, and pitching rudder 16 up deflects then unmanned plane
It comes back.When unmanned plane surface navigation carries out roll guidance, realized by the linkage of control left side aileron 14 and right side aileron 15,
Left side aileron 14 upward deflects while right side aileron 15 is deflected down and upward deflected, unmanned plane rolling clockwise, left side aileron 14
It deflects down while right side aileron 15 upward deflects, rolling that aircraft is counterclockwise.Yaw, pitching and rolling when unmanned plane airflight
It moves consistent with working principle when hydroplaning.
The basic principles, main features and advantages of the invention have been shown and described above.The technical staff of the industry should
Understand, the invention is not limited in any way for examples detailed above, all skills obtained by the way of equivalent substitution or equivalent transformation
Art scheme, falls within the scope of protection of the present invention.
Claims (8)
1. a kind of shoe formula aquatic unmanned aerial vehicle, which is characterized in that including fuselage, be installed on body upper along fuselage central axes two sides
The wing of extension, the electric pod being installed below fore-body are installed on the airscrew engine of afterbody, are fixed on machine
Radome fairing with it, the shoe connecting with radome fairing further include the empennage being connected with shoe, are connected to below fuselage along central axes
The floating drum that two sides extend obliquely.
2. shoe formula aquatic unmanned aerial vehicle according to claim 1, which is characterized in that the empennage is U-shaped empennage, the U
Type tail includes horizontal tail, and the left vertical fin of the horizontal tail is approximately perpendicular to positioned at horizontal tail both ends, and right vertical fin is separately mounted to left hang down
Tail, the left direction rudder on right vertical fin, right direction rudder, and the pitching rudder being mounted in horizontal tail.
3. shoe formula aquatic unmanned aerial vehicle according to claim 1, which is characterized in that the number of the floating drum includes two,
Described two floating drums pass through floating drum connecting rod respectively and connect with fuselage.
4. shoe formula aquatic unmanned aerial vehicle according to claim 1, which is characterized in that the floating drum is ship shape.
5. shoe formula aquatic unmanned aerial vehicle according to claim 1, which is characterized in that described to extend along fuselage central axes two sides
Wing include port wing and starboard wing, and the left side aileron and right side aileron that are separately positioned on port wing and starboard wing.
6. shoe formula aquatic unmanned aerial vehicle according to claim 1, which is characterized in that the length D of the wing is 4.824m.
7. shoe formula aquatic unmanned aerial vehicle according to claim 2, which is characterized in that the top of the left vertical fin and right vertical fin
Bottom distance H with fuselage is 1.76m.
8. shoe formula aquatic unmanned aerial vehicle according to claim 1, which is characterized in that the length A of the shoe formula unmanned plane
For 5.096m.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811352653.0A CN109353501A (en) | 2018-11-14 | 2018-11-14 | Shoe formula aquatic unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811352653.0A CN109353501A (en) | 2018-11-14 | 2018-11-14 | Shoe formula aquatic unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109353501A true CN109353501A (en) | 2019-02-19 |
Family
ID=65345193
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811352653.0A Pending CN109353501A (en) | 2018-11-14 | 2018-11-14 | Shoe formula aquatic unmanned aerial vehicle |
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| Country | Link |
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| CN (1) | CN109353501A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN207225638U (en) * | 2017-09-04 | 2018-04-13 | 上海优伟斯智能系统有限公司 | A kind of inside cabin loads the amphibious fixed-wing logistics unmanned vehicle of cargo |
| CN207346074U (en) * | 2017-11-03 | 2018-05-11 | 西安冰果智能航空科技有限公司 | A kind of double shoe VTOL fixed-wing unmanned planes of normal arrangement |
| CN108128453A (en) * | 2018-01-08 | 2018-06-08 | 浙江大学 | A kind of air-sea dual-purpose solar unmanned plane and its control method |
| CN207725616U (en) * | 2018-01-08 | 2018-08-14 | 浙江大学 | Double coaxial tilting rotor wing unmanned aerial vehicles of shoe formula |
| CN108502172A (en) * | 2018-05-30 | 2018-09-07 | 佛山市神风航空科技有限公司 | A kind of seaplane for rescue of patrolling on the sea |
| CN209290683U (en) * | 2018-11-14 | 2019-08-23 | 南京航空航天大学 | Shoe formula aquatic unmanned aerial vehicle |
-
2018
- 2018-11-14 CN CN201811352653.0A patent/CN109353501A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN207225638U (en) * | 2017-09-04 | 2018-04-13 | 上海优伟斯智能系统有限公司 | A kind of inside cabin loads the amphibious fixed-wing logistics unmanned vehicle of cargo |
| CN207346074U (en) * | 2017-11-03 | 2018-05-11 | 西安冰果智能航空科技有限公司 | A kind of double shoe VTOL fixed-wing unmanned planes of normal arrangement |
| CN108128453A (en) * | 2018-01-08 | 2018-06-08 | 浙江大学 | A kind of air-sea dual-purpose solar unmanned plane and its control method |
| CN207725616U (en) * | 2018-01-08 | 2018-08-14 | 浙江大学 | Double coaxial tilting rotor wing unmanned aerial vehicles of shoe formula |
| CN108502172A (en) * | 2018-05-30 | 2018-09-07 | 佛山市神风航空科技有限公司 | A kind of seaplane for rescue of patrolling on the sea |
| CN209290683U (en) * | 2018-11-14 | 2019-08-23 | 南京航空航天大学 | Shoe formula aquatic unmanned aerial vehicle |
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