CN205150246U - Empty dual -purpose unmanned aerial vehicle of water - Google Patents
Empty dual -purpose unmanned aerial vehicle of water Download PDFInfo
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- CN205150246U CN205150246U CN201520802200.9U CN201520802200U CN205150246U CN 205150246 U CN205150246 U CN 205150246U CN 201520802200 U CN201520802200 U CN 201520802200U CN 205150246 U CN205150246 U CN 205150246U
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Abstract
The utility model relates to an empty dual -purpose unmanned aerial vehicle of water, including the unmanned aerial vehicle platform and install in machine on the unmanned aerial vehicle platform carries data terminal, flight control and navigation, flight driving system and surface of water navigation control system, the unmanned aerial vehicle platform including the fuselage of the ship molded lines that has surface of water navigation ware and with the wing that the fuselage is connected, the wing includes that fin and two can automatic folding flanks, flight driving system install on two flanks and connect leading screw, the fin include vertical tail and with the tailplane that vertical tail is connected, surface of water navigation control system includes that two spout the pump hydraulic jet propulsion, two spout pump hydraulic jet propulsion symmetrical arrangement install in two of the unmanned aerial vehicle platform can the automatic folding flank back lower place. The utility model discloses can realize that this unmanned aerial vehicle water is empty dual -purpose, and fine operation controls, strong adaptability are realized to the homoenergetic.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, is specifically related to the empty dual-purpose unmanned plane of a kind of water.
Background technology
Unmanned plane can make full use of that aircraft speed is fast, detection broad covered area, ageing strong, willing advantage, marine environmental monitoring is implemented in the specialized range of coastal waters, improve marine monitoring efficiency, effectively set up land, sea and air stereo monitoring system, meet the demand that accident marine site image obtains real-time, realize the target of " monitoring three-dimensional; react rapid, enforce the law and standardize and IT application in management ", may be used for spilled oil monitoring, night cruises, channel safe is patrolled, personnel search and rescue and evidence obtaining etc. of enforcing the law.Water surface unmanned plane during flying applicator platform radical function carries mission payload to implement to overhead, target area to detect or monitor, can rapidly and efficiently acquisition accident marine site sea condition information, and comprehensive, multi-angle emphasis monitoring can be carried out, for commanding and decision-making plays a significant role to important area.The aircraft platforms of amphibian unmanned plane should have the functions such as mobility strong, simple to operate, flexible safety, hedgehopping, real-time monitored, and the landing of water surface mode can be adapted to and there is the flight performance under the IFR conditions of certain coastal waters, autonomous flight can be realized, take home and the function such as spot hover.But by the impact of wave of the sea and current, the landing of extra large Mixing machine for preparation of dough is a very difficult thing.Therefore, must improve for amphibian unmanned plane, to solve above-mentioned technical matters.
Utility model content
The purpose of this utility model is solve above-mentioned technical matters and provide a kind of water empty dual-purpose unmanned plane.
For achieving the above object, the utility model adopts following technical scheme:
The empty dual-purpose unmanned plane of a kind of water, comprises unmanned aerial vehicle platform and is installed on the airborne data terminal on described unmanned aerial vehicle platform, fly control and navigationsystem, flying power system and surface navigation control system; The fuselage that described unmanned aerial vehicle platform comprises the ship molded line with navigation unit by water and the wing be connected with described fuselage; Described wing comprises empennage and two can the flank of auto-folder, and described flying power system to be arranged on described two flanks and to connect preposition screw propeller, the tailplane that described empennage comprises vertical tail and is connected with described vertical tail; Described surface navigation control system comprises two spray pump waterjet propulsors, and described two spray pump waterjet propulsors are arranged symmetrically be installed on described unmanned aerial vehicle platform two can the flank back lower place of auto-folder.
Described flight controls to include with navigationsystem to adopt MEMS sensor, acceleration pick-up, magnetic course transmitter, baroceptor, Servo-controller, embedded processor system and satellite navigation system, and described MEMS sensor, acceleration pick-up, magnetic course transmitter, baroceptor, Servo-controller, satellite navigation system are connected with described embedded processor system.
Described satellite navigation system comprises gps satellite receiver.
Described flight controls to be connected with remote control equipment (RCE) signal with navigationsystem.
Described flying power system adopts piston type twin-tub gas engine, and described piston type twin-tub gas engine connects power generation assembly.
The utility model comprises the ship molded line with navigation unit by water fuselage by unmanned aerial vehicle platform and the wing be connected with described fuselage; Described wing comprises empennage and two can the flank of auto-folder, and described flying power system to be arranged on described two flanks and to connect preposition screw propeller, the tailplane that described empennage comprises vertical tail and is connected with described vertical tail; Described surface navigation control system comprises two spray pump waterjet propulsors, described two spray pump waterjet propulsors are arranged symmetrically be installed on described unmanned aerial vehicle platform two can the flank back lower place of auto-folder, this unmanned plane water sky can be realized dual-purpose, and all can realize well operating control, strong adaptability.
Accompanying drawing explanation
The schematic side view of the empty dual-purpose unmanned plane of water that Fig. 1 provides for the utility model embodiment;
Figure 2 shows that the schematic top plan view of the empty dual-purpose unmanned plane of water that the utility model embodiment provides.
Detailed description of the invention
Below, in conjunction with example, substantive distinguishing features of the present utility model and advantage are further described, but the utility model is not limited to listed embodiment.
Shown in Fig. 1 ~ 2, the empty dual-purpose unmanned plane of a kind of water, comprises unmanned aerial vehicle platform and is installed on the airborne data terminal on described unmanned aerial vehicle platform, fly control and navigationsystem, flying power system 5 and surface navigation control system; The fuselage 1 that described unmanned aerial vehicle platform comprises the ship molded line 2 with navigation unit by water and the wing be connected with described fuselage; Described wing comprises empennage and two can the flank 4 of auto-folder, described flying power system 5 is two covers, be arranged on described two folding flank upper and lowers respectively, and connect preposition screw propeller 9, two tailplanes 8 that described empennage comprises vertical tail 7 and is connected with described vertical tail; Described surface navigation control system comprises two spray pump waterjet propulsors 3, and described two spray pump waterjet propulsors are arranged symmetrically be installed on described unmanned aerial vehicle platform two can the flank back lower place of auto-folder.
Described spray pump waterjet propulsor can adopt commercially available spray pump waterjet propulsor, as Hamilton hamilton sprays pump waterjet propulsor.
Further, on described fuselage, rear portion is provided with airborne radar 6, and concrete described airborne radar 6 is positioned at flank 4 rear, the anterior position of described empennage.
The empty dual-purpose unmanned plane of water is navigation and the aircraft of a adaptation surface navigation and airflight as its name suggests, and surface navigation requires that body has the molded line of navigation unit by water and the impact adapting to the factors such as sea is flowed, wave.Therefore in order to ensure the requirement of water empty dual-purpose unmanned plane sea navigation, body is with reference to the requirement design of the high speed unmanned boats such as unmanned boat molded line, buoyancy, weight center, block coefficient, ventral carries out landing waterborne and navigation adaptability design, and vertical fin adopts high horizontal tail layout.In order to ensure that the stability wing of the unmanned plane water surface adopts the design of automatic layboy flank.Propulsion system adopt the waterjet propulsion of spray pump waterjet propulsor mode, in water surface mode with reference to without ship water surface mode, realize unmanned plane on the water surface just, fall, turn round, the action such as hovering, achieve water sky dual-purpose, and by force handling.
Wherein, described flight controls mainly to be responsible for the scheduling of platform task and the management of resource with navigationsystem, be directly connected to information interaction and the coordination of unmanned aerial vehicle platform and operating personal, hardware configuration includes employing MEMS sensor, acceleration pick-up, magnetic course transmitter, baroceptor, Servo-controller, embedded processor system and satellite navigation system, described MEMS sensor, acceleration pick-up, magnetic course transmitter, baroceptor, Servo-controller, satellite navigation system is connected with described embedded processor system, embedded processor system is responsible for flight and is controlled, mission payload manages, information processing and the multi-sensor combined navigation of sensor resolve, detect location lay the foundation for mission payload completes target, reach the target being retrieved as center with information.
Described satellite navigation system comprises gps satellite receiver.
Wherein, described flight controls to be connected with remote control equipment (RCE) signal with navigationsystem.
Preferably, described flying power system adopts piston type twin-tub gas engine, and described piston type twin-tub gas engine connects power generation assembly.
The empty dual-purpose unmanned plane of the utility model water, after operation of finishing the work, autonomous navigation is carried out dropping to fixing marine site to task navigating area, unmanned aerial vehicle (UAV) control is entered in withdrawer device by the spray pump waterjet propulsor controlling unmanned plane.
The utility model comprises the ship molded line with navigation unit by water fuselage by unmanned aerial vehicle platform and the wing be connected with described fuselage; Described wing comprises empennage and two can the flank of auto-folder, and described flying power system to be arranged on described two flanks and to connect preposition screw propeller, the tailplane that described empennage comprises vertical tail and is connected with described vertical tail; Described surface navigation control system comprises two spray pump waterjet propulsors, described two spray pump waterjet propulsors are arranged symmetrically be installed on described unmanned aerial vehicle platform two can the flank back lower place of auto-folder, this unmanned plane water sky can be realized dual-purpose, and all can realize well operating control, strong adaptability.
The above is only preferred implementation of the present utility model; it should be pointed out that for those skilled in the art, under the prerequisite not departing from the utility model principle; can also make some improvements and modifications, these improvements and modifications also should be considered as protection domain of the present utility model.
Claims (5)
1. the empty dual-purpose unmanned plane of water, is characterized in that, comprises unmanned aerial vehicle platform and is installed on the airborne data terminal on described unmanned aerial vehicle platform, fly control and navigationsystem, flying power system and surface navigation control system; The fuselage that described unmanned aerial vehicle platform comprises the ship molded line with navigation unit by water and the wing be connected with described fuselage; Described wing comprises empennage and two can the flank of auto-folder, and described flying power system to be arranged on described two flanks and to connect preposition screw propeller, the tailplane that described empennage comprises vertical tail and is connected with described vertical tail; Described surface navigation control system comprises two spray pump waterjet propulsors, and described two spray pump waterjet propulsors are arranged symmetrically be installed on described unmanned aerial vehicle platform two can the flank back lower place of auto-folder.
2. the empty dual-purpose unmanned plane of water according to claim 1, it is characterized in that, described flight controls to include with navigationsystem to adopt MEMS sensor, acceleration pick-up, magnetic course transmitter, baroceptor, Servo-controller, embedded processor system and satellite navigation system, and described MEMS sensor, acceleration pick-up, magnetic course transmitter, baroceptor, Servo-controller, satellite navigation system are connected with described embedded processor system.
3. the empty dual-purpose unmanned plane of water according to claim 2, it is characterized in that, described satellite navigation system comprises gps satellite receiver.
4. the empty dual-purpose unmanned plane of water according to claim 3, it is characterized in that, described flight control is connected with remote control equipment (RCE) signal with navigationsystem.
5. the empty dual-purpose unmanned plane of water according to any one of Claims 1 to 4, it is characterized in that, described flying power system adopts piston type twin-tub gas engine, and described piston type twin-tub gas engine connects power generation assembly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201520802200.9U CN205150246U (en) | 2015-10-16 | 2015-10-16 | Empty dual -purpose unmanned aerial vehicle of water |
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| CN201520802200.9U CN205150246U (en) | 2015-10-16 | 2015-10-16 | Empty dual -purpose unmanned aerial vehicle of water |
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| CN205150246U true CN205150246U (en) | 2016-04-13 |
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Cited By (10)
| 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 |
| CN106114833A (en) * | 2016-07-30 | 2016-11-16 | 李勇军 | Escape water helicopter |
| CN106627010A (en) * | 2016-11-17 | 2017-05-10 | 苏州航天系统工程有限公司 | Water-air amphibious unmanned aerial vehicle |
| CN106823402A (en) * | 2017-02-03 | 2017-06-13 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special forest extinguishing model aircraft of teenager's defence education |
| CN106976367A (en) * | 2016-06-16 | 2017-07-25 | 姜忠昱 | One kind three is dwelt unmanned plane |
| CN107697287A (en) * | 2017-10-23 | 2018-02-16 | 天津飞眼无人机科技有限公司 | A kind of control system of water sky two-purpose traffic tool |
| CN107792359A (en) * | 2017-10-19 | 2018-03-13 | 西北工业大学 | A kind of empty dual-purpose unmanned plane of water |
| 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 |
| CN110107426A (en) * | 2019-05-08 | 2019-08-09 | 中国航空发动机研究院 | Across the medium flight device power device shared based on combustion chamber between grade and turbine water sky |
| CN114644112A (en) * | 2022-03-29 | 2022-06-21 | 中国电子科技南湖研究院 | Empty dual-purpose unmanned aerial vehicle of water |
-
2015
- 2015-10-16 CN CN201520802200.9U patent/CN205150246U/en active Active
Cited By (12)
| 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 |
| CN106976367A (en) * | 2016-06-16 | 2017-07-25 | 姜忠昱 | One kind three is dwelt unmanned plane |
| CN106114833A (en) * | 2016-07-30 | 2016-11-16 | 李勇军 | Escape water helicopter |
| CN106627010A (en) * | 2016-11-17 | 2017-05-10 | 苏州航天系统工程有限公司 | Water-air amphibious unmanned aerial vehicle |
| CN106823402A (en) * | 2017-02-03 | 2017-06-13 | 佛山市三水区希望火炬教育科技有限公司 | A kind of special forest extinguishing model aircraft of teenager's defence education |
| CN107792359A (en) * | 2017-10-19 | 2018-03-13 | 西北工业大学 | A kind of empty dual-purpose unmanned plane of water |
| CN107697287A (en) * | 2017-10-23 | 2018-02-16 | 天津飞眼无人机科技有限公司 | A kind of control system of water sky two-purpose traffic tool |
| CN107697287B (en) * | 2017-10-23 | 2023-05-09 | 天津飞眼无人机科技有限公司 | Control system of water-air dual-purpose vehicle |
| 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 |
| CN110107426A (en) * | 2019-05-08 | 2019-08-09 | 中国航空发动机研究院 | Across the medium flight device power device shared based on combustion chamber between grade and turbine water sky |
| CN114644112A (en) * | 2022-03-29 | 2022-06-21 | 中国电子科技南湖研究院 | Empty dual-purpose unmanned aerial vehicle of water |
| CN114644112B (en) * | 2022-03-29 | 2024-05-03 | 中国电子科技南湖研究院 | Water-air dual-purpose unmanned aerial vehicle |
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Effective date of registration: 20160815 Address after: 100013, No. 1, building 13, No. 2, Dazhong temple, Beijing, Haidian District, C203 Patentee after: Han Hai (Beijing) Technology Co., Ltd. Address before: 300457, Tianjin Binhai New Area Development Zone, Fourth Avenue, Tian Da Science and Technology Park, A1, seven floor, G room Patentee before: Tianjin HSE Co., Ltd. |