CN205022847U - A high performance fixed wing uavs device for cruising monitoring - Google Patents
A high performance fixed wing uavs device for cruising monitoring Download PDFInfo
- Publication number
- CN205022847U CN205022847U CN201520713553.1U CN201520713553U CN205022847U CN 205022847 U CN205022847 U CN 205022847U CN 201520713553 U CN201520713553 U CN 201520713553U CN 205022847 U CN205022847 U CN 205022847U
- Authority
- CN
- China
- Prior art keywords
- fixed
- wing
- fuselage
- high performance
- type single
- 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.)
- Active
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The utility model provides a high performance fixed wing uavs device for cruising monitoring, the pneumatic appearance of first three some overall arrangement of the adoption formula of drawing in, two leaf screws are inserted on the motor of aircraft nose front end, the cross section of fuselage is designed for the fillet rectangle, the beam type single -vane is isometric fixes upper portion in the fuselage, the screw fixation for the end of beam type single -vane both sides has the wing tip winglet of fish shape design, the vertical fin wing adopts H type design symmetric distribution in the terminal both sides of the horizontal tail wing, whole fin is inserted and is fixed in the fuselage rear end in the stern notch inboard, the undercarriage device is fixed through the undercarriage mount and is taken off and land together with fixed wing uavs below the fuselage.
Description
Technical field
The utility model proposes a kind of High Performance fixed-wing unmanned plane device for monitoring of cruising, be related specifically to fixed-wing unmanned plane integral layout design field.
Background technology
Fixed-wing unmanned plane is as a kind of unmanned vehicle, have that flight efficiency is high, flight is fast, distance, system architecture are simple, lightweight, cost and the advantage such as operating costs is low, be applied to more and more widely and cruised in monitoring on a large scale, the data retrieval capabilities deficiency, the replacement cycle that compensate for satellite remote sensing and manned air remote sensing are long, causing the shortcomings such as data Up-to-date state difference, there is a lot of defect in the development of unmanned plane hardware: the sliding race of needs or with special retraction mechanism when taking off and land; By the impact of own load and oil mass in continuation of the journey, be faced with short defect in cruise duration; The body layout of unmanned plane is single, lift degree of utilization is low, the fixed-wing unmanned plane of many same models can only be optimized in a certain respect or promote wherein, especially when long boat, when cruising, carry out the fixed-wing unmanned plane promoted the while of lacking a kind of on a large scale in multiple performance figure.
Summary of the invention
Design of the present utility model is to propose a kind of High Performance fixed-wing unmanned plane device for monitoring of cruising, and solves problem that is short when cruising flight boat when monitoring at present, low performance.
For reaching this object, following solution is proposed:
A kind of High Performance fixed-wing unmanned plane device for monitoring of cruising, adopt drawing-in type front three-point layout aerodynamic configuration, fuselage square section is the design of fillet oblong, the middle and upper part of what beam type single-blade was isometric be fixed on fuselage, the end of beam type single-blade both sides is provided with winglet, the vertical fin wing adopts the design of H type to be symmetrically distributed in the both sides of the horizontal tail wing, and whole empennage is fixed on back body by stern notch, and two-bladed porpeller is inserted on the motor of head front end.
Further, the span of beam type single-blade is 3.35 meters, improves voyage and short take-off and landing (STOL), and increase by the voyage of 8%, for monitoring of cruising on a large scale extends cruise duration, flying height can reach height above sea level 6000 meters.
Further, winglet adopts the design of fish shape, and winglet produces yawing moment or keeps direction to stablize, and reduces air resistance during flight, improves flying speed, reduce oil consumption.
Further, vertical fin wing balance horizontal tail wing structure frequency, reduce amplitude, improve the driving efficiency of empennage, increase stability during flight, can meet 1: 500,1: 1000,1: 2000 large scale and become figure job requirements, when cruising monitoring, a vertical fin wing is destroyed, and also can not affect aircraft normal flight.
Further, fuselage bottom is provided with alighting gear fixed mount, makes fixed-wing unmanned plane that different landing gears is installed by alighting gear fixed mount, reduce the requirement to landing site, sliding race landing, catapult-assisted take-off can be met.
Preferably, the beam type single-blade of the utility model fixed-wing unmanned plane adopts timber or all steel glass material, reduces bare weight, makes mission payload can reach 15 kilograms, meet multitask, overweight equipment load requirements.
Preferably, adopt between all location and installation holes and be screwed, facilitate inspection and maintenance.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is further illustrated.
Fig. 1 is a kind of High Performance fixed-wing unmanned plane device lateral plan for monitoring of cruising of the utility model.
Fig. 2 is a kind of High Performance fixed-wing unmanned plane device birds-eye view for monitoring of cruising of the utility model.
Fig. 3 is the winglet lateral plan of a kind of High Performance fixed-wing unmanned plane device for monitoring of cruising of the utility model.
1. fuselages, 2. head, 3. screw propeller in figure, 4. beam type single-blade, 5. winglet, 6. the horizontal tail wing, 7. the vertical fin wing, 8. wing tip location and installation hole, 9. vertical fin wing location and installation hole, 10. stern notch location and installation hole, 11. stern notches, 12. alighting gear fixed mounts, 13. beam type single-blade location and installation holes.
Detailed description of the invention
Elaborate below in conjunction with accompanying drawing.
In the embodiment shown in Fig. 1, Fig. 2, two-bladed porpeller (3) is directly inserted on the motor of head (2) front end; Beam type single-blade (4) across the middle and upper part in fuselage (1), by being fixed on fuselage (1) with beam type single-blade location and installation hole (13) long screw; Landing gear is fixed on fuselage (1) landing together with fixed-wing unmanned plane below by alighting gear fixed mount (12); The vertical fin wing (7) of H type design is fixed on the end of the horizontal tail wing (6) both sides by vertical fin wing location and installation hole (9) with short screw; Whole empennage is inserted in stern notch (11) inner side, is fixed on the rear end of fuselage (1) with long screw by stern notch location and installation hole (10).
The winglet (5) of fish shape design is fixed on the end of beam type single-blade (4) both sides with short screw by wing tip location and installation hole (8) in the embodiment shown in fig. 3.
More than combine actual operation installation process, made relevant know-why and illustrated, these illustrate just in order to describe technical design of the present utility model and method of operation, and can not be interpreted as the restriction to protection domain of the present utility model in any form.Based on the explanation to this, those skilled in the art makes any amendment or equivalent variations according to technical spirit of the present utility model, all will drop in protection domain of the present utility model.
Claims (4)
1. the High Performance fixed-wing unmanned plane device for monitoring of cruising, mainly comprise fuselage (1), head (2), screw propeller (3), beam type single-blade (4), winglet (5), the horizontal tail wing (6), the vertical fin wing (7), stern notch (11), alighting gear fixed mount (12), it is characterized in that: beam type single-blade (4) is by the isometric middle and upper part being fixed on fuselage (1), beam type single-blade location and installation hole (13), landing gear is fixed on fuselage (1) landing together with fixed-wing unmanned plane below by alighting gear fixed mount (12), the square section of fuselage (1) is the design of fillet oblong, two-bladed porpeller is inserted on the motor of head front end.
2. a kind of High Performance fixed-wing unmanned plane device for monitoring of cruising according to claim 1, it is characterized in that: whole empennage is inserted in stern notch (11) inner side, is fixed on fuselage (1) rear end by stern notch location and installation hole (10).
3. a kind of High Performance fixed-wing unmanned plane device for monitoring of cruising according to claim 1, it is characterized in that: the winglet (5) being provided with the design of fish shape at the wing tip of beam type single-blade (4), winglet (5) is fixed on beam type single-blade (4) by wing tip location and installation hole (8).
4. a kind of High Performance fixed-wing unmanned plane device for monitoring of cruising according to claim 1, it is characterized in that: the vertical fin wing (7) is the design of H type, and the vertical fin wing (7) that H type designs is fixed on the horizontal tail wing (6) by vertical fin wing location and installation hole (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520713553.1U CN205022847U (en) | 2015-09-16 | 2015-09-16 | A high performance fixed wing uavs device for cruising monitoring |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520713553.1U CN205022847U (en) | 2015-09-16 | 2015-09-16 | A high performance fixed wing uavs device for cruising monitoring |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205022847U true CN205022847U (en) | 2016-02-10 |
Family
ID=55255406
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520713553.1U Active CN205022847U (en) | 2015-09-16 | 2015-09-16 | A high performance fixed wing uavs device for cruising monitoring |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205022847U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947174A (en) * | 2016-05-12 | 2016-09-21 | 中国航空工业集团公司西安飞机设计研究所 | Airplane |
| CN106516113A (en) * | 2016-10-25 | 2017-03-22 | 深圳市易飞方达科技有限公司 | Unmanned aerial vehicle |
| CN107628232A (en) * | 2017-08-11 | 2018-01-26 | 精功（绍兴）复合材料技术研发有限公司 | A kind of composite unmanned airplane empennage and its manufacture method |
| CN109466744A (en) * | 2018-11-06 | 2019-03-15 | 珠海隆华直升机科技有限公司 | Helicopter tail balance mechanism and helicopter |
-
2015
- 2015-09-16 CN CN201520713553.1U patent/CN205022847U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947174A (en) * | 2016-05-12 | 2016-09-21 | 中国航空工业集团公司西安飞机设计研究所 | Airplane |
| CN106516113A (en) * | 2016-10-25 | 2017-03-22 | 深圳市易飞方达科技有限公司 | Unmanned aerial vehicle |
| CN107628232A (en) * | 2017-08-11 | 2018-01-26 | 精功（绍兴）复合材料技术研发有限公司 | A kind of composite unmanned airplane empennage and its manufacture method |
| CN109466744A (en) * | 2018-11-06 | 2019-03-15 | 珠海隆华直升机科技有限公司 | Helicopter tail balance mechanism and helicopter |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9884682B2 (en) | Aircraft configuration | |
| CN200939356Y (en) | Small remote monitoring pilotless plane | |
| CN106741820A (en) | A kind of VTOL fixed-wing unmanned vehicle | |
| US10899447B2 (en) | Methods for improvements of the box wing aircraft concept and corresponding aircraft configuration | |
| CN205022847U (en) | A high performance fixed wing uavs device for cruising monitoring | |
| CN110254720B (en) | Solar unmanned aerial vehicle with flying wing layout | |
| CN103466074A (en) | Ship-based net collision recovery unmanned aerial vehicle | |
| CN111268089B (en) | Double-fuselage vertical take-off and landing fixed wing unmanned aerial vehicle structure | |
| US8820673B2 (en) | Rotary-wing and fixed-wing aircraft | |
| CN204399465U (en) | A kind of anury all-wing aircraft many controlsurfaces unmanned plane | |
| CN202966654U (en) | Fixed wing unmanned aerial vehicle for engineer operation | |
| CN105366049A (en) | Vertical takeoff and landing unmanned aerial vehicle | |
| CN109774916B (en) | Solar aircraft adopting three-dimensional layout design | |
| CN105905295A (en) | Vertical take-off and landing fixed wing aircraft | |
| CN108082471A (en) | A kind of variant supersonic plane | |
| CN110116802A (en) | A kind of big loading small-sized unmanned aircraft of high universalizable | |
| CN102085911A (en) | Novel flight and aircraft | |
| CN101734376B (en) | Small multipurpose unmanned aerial vehicle capable of realizing modularized load and parachute recovery | |
| CN205022854U (en) | Deformable compound aircraft | |
| CN103213683A (en) | Small multipurpose unmanned plane with oil tank embedded into blended wing body | |
| RU112154U1 (en) | MULTI-PURPOSE PLANE | |
| CN212501033U (en) | Light-duty sport aircraft of firefly | |
| CN210284611U (en) | Flying wing layout solar unmanned aerial vehicle | |
| CN203698646U (en) | Flying wing imitating rapidly ascending unmanned plane | |
| CN112623214A (en) | Amphibious unmanned transport plane based on hydrofoil technology |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information |
Inventor after: Wang Peng Inventor after: Wang Lu Inventor after: Liu Shiwen Inventor before: Wang Peng Inventor before: Han Bocai Inventor before: Zhao Yuan |
|
| COR | Change of bibliographic data |