CN205131666U - Unmanned aerial vehicle that takes off and land on water - Google Patents
Unmanned aerial vehicle that takes off and land on water Download PDFInfo
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- CN205131666U CN205131666U CN201520802335.5U CN201520802335U CN205131666U CN 205131666 U CN205131666 U CN 205131666U CN 201520802335 U CN201520802335 U CN 201520802335U CN 205131666 U CN205131666 U CN 205131666U
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Abstract
The utility model relates to an unmanned aerial vehicle that takes off and land on water, including the unmanned aerial vehicle platform and install in flight control, navigation, driving system, airborne radar and spiral propulsion system on water on the unmanned aerial vehicle platform, spiral propulsion system on water passes through the control line and connects the screw propulsion controller, spiral propulsion system on water includes left -hand screw propeller and right spiral propeller, left -hand screw propeller and right spiral propeller symmetrical arrangement install in the both sides below of unmanned aerial vehicle platform, the left -hand screw propeller is the same with right spiral propeller structure, the size is unanimous. The utility model discloses lean on screw propulsion ware work under water when making unmanned aerial vehicle on water take off on the surface of water, satisfy the aircraft surface of water and control the requirement, solved current unmanned aerial vehicle on water take off and land the environment harshness, take off and land airborne big, retrieve the problem that the difficulty expected much.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, is specifically related to a kind of landing unmanned plane waterborne.
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.The radical function of aircraft platforms 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 can carry out comprehensive, multi-angle emphasis to important area and monitor, for commanding and decision-making plays a significant role.Aircraft platforms 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 existing unmanned plane is also not suitable for the landing of the high sea situation water surface and can reclaims fast, therefore develops a kind of unmanned plane of applicable Horizontal Take-off and Landing, to solve the requirement of unmanned plane water surface landing under harsh environment, has a very important role and meaning.
Utility model content
The purpose of this utility model is solve above-mentioned technical matters and provide a kind of landing unmanned plane waterborne.
For achieving the above object, the utility model adopts following technical scheme:
A kind of landing unmanned plane waterborne, comprises unmanned aerial vehicle platform and is installed on flight control system, navigationsystem, power system, airborne radar and the screw propulsion system waterborne on described unmanned aerial vehicle platform; Described screw propulsion system waterborne connects screw propulsion controller by control line; Described screw propulsion system waterborne comprises left auger and right auger, and described left auger and right auger are arranged symmetrically with the down either side being installed on described unmanned aerial vehicle platform; Described left auger is identical with right auger structure, in the same size.
Described spiral propeller and right auger comprise housing, can positive and negative rotation screw propeller and be placed in screw propulsion electrical source of power in described housing, screw drives motor and be connected the drive element of described screw drives motor and described screw propeller; Streamlined reefer housing is provided with outside described screw propeller.
Described screw propeller adopts 4 leaf shrouded propellers.
Described spiral propeller is fixed on described unmanned aerial vehicle platform by the C-type clamp be connected with described housing with right auger.
Described screw propulsion electrical source of power adopts dc-battery, and described screw drives motor adopts DC brushless motor.
The wing that described unmanned aerial vehicle platform comprises fuselage and is connected with described fuselage; Described wing comprises empennage and two flanks, described power system adopts propeller turbine, described propeller turbine to be arranged on described two flanks and to connect screw propeller, the tailplane that described empennage comprises vertical tail and is connected with described vertical tail.
The utility model by installing screw propulsion system waterborne on unmanned aerial vehicle platform, described screw propulsion system waterborne comprises left auger and right auger, described left auger and right auger are arranged symmetrically with the down either side being installed on described unmanned aerial vehicle platform, by spiral propeller work under water when aquatic unmanned aerial vehicle can be made to take off on the water surface, thus meet aircraft water surface manipulation request.
Accompanying drawing explanation
The structural representation of the landing unmanned plane waterborne that Fig. 1 provides for the utility model embodiment.
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 Figure 1, a kind of landing unmanned plane waterborne, comprises unmanned aerial vehicle platform 1 and is installed on flight control system, navigationsystem, power system 4, airborne radar 8 and the screw propulsion system 2 waterborne on described unmanned aerial vehicle platform; Described screw propulsion system waterborne connects screw propulsion controller by control line 24; Described screw propulsion system waterborne comprises left auger and right auger, and described left auger and right auger are arranged symmetrically with the down either side being installed on described unmanned aerial vehicle platform; Described left auger is identical with right auger structure, in the same size.
Concrete, described spiral propeller and right auger include housing 21, can positive and negative rotation screw propeller and be placed in screw propulsion electrical source of power in described housing, screw drives motor and be connected the drive element of described screw drives motor and described screw propeller; Streamlined reefer housing 22 is provided with outside described screw propeller.
Concrete, described screw propeller adopts 4 leaf shrouded propellers.
During installation, described spiral propeller is fixed on described unmanned aerial vehicle platform 1 by the C-type clamp 23 be connected with described housing 21 with right auger.
Concrete, described screw propulsion electrical source of power adopts dc-battery, and described screw drives motor adopts DC brushless motor.
In the utility model embodiment, the wing that described unmanned aerial vehicle platform comprises the fuselage of the water people unmanned boat type of the ship molded line with sailing device on water or body and is connected with described fuselage; Described wing comprises empennage and two flanks 3, described power system 4 adopts propeller turbine, described propeller turbine to be arranged on described two flanks and to connect screw propeller 5, the tailplane 7 that described empennage comprises vertical tail 6 and is connected with described vertical tail.
The maximum difference of the utility model and common water surface landing unmanned plane is that unmanned water machine leans on spiral propeller work under water to meet aircraft water surface manipulation request when the water surface takes off.
During work, the angle of rake landing unmanned plane mode of operation waterborne of band underwater propeller is consistent with common unmanned plane mode of operation adopts remote manual control to operate and autonomous flight operations two kinds of operation modes.But need to increase during the remote manual control operation of band propeller landing unmanned plane waterborne and switch handle, adopt water sailing pattern when working on the water, make unmanned plane enter departure location, direction of taking off accurately carry out taking off prepare after switch to the common pattern of taking off and take off.Fly to adopt autonomous sail mode to certain height.Otherwise during landing.
The utility model mainly solves the current harshness of water machine landing environment both at home and abroad with the aquatic unmanned aerial vehicle of spiral propeller waterborne, landing is dropped from the air greatly, reclaim difficulty requires high object, when taking off from the water surface with spiral propeller unmanned plane waterborne, the work such as spiral propeller rotating under water, speed governing complete the action such as flipper turn, reversing, positive car of the water surface, so that unmanned fast searching to take off navigation channel to the best, ensure the safety of taking off; With spiral propeller unmanned plane waterborne from when the water surface (particularly narrow) unmanned plane underwater propeller propelling unit when dropping to the water surface manually controller enter unmanned plane accurately and reclaim in grabber, complete the quick recovery of unmanned plane.
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 (6)
1. a landing unmanned plane waterborne, is characterized in that, comprises unmanned aerial vehicle platform and is installed on flight control system, navigationsystem, power system, airborne radar and the screw propulsion system waterborne on described unmanned aerial vehicle platform; Described screw propulsion system waterborne connects screw propulsion controller by control line; Described screw propulsion system waterborne comprises left auger and right auger, and described left auger and right auger are arranged symmetrically with the down either side being installed on described unmanned aerial vehicle platform; Described left auger is identical with right auger structure, in the same size.
2. landing unmanned plane waterborne according to claim 1, it is characterized in that, described spiral propeller and right auger comprise housing, can positive and negative rotation screw propeller and be placed in screw propulsion electrical source of power in described housing, screw drives motor and be connected the drive element of described screw drives motor and described screw propeller; Streamlined reefer housing is provided with outside described screw propeller.
3. landing unmanned plane waterborne according to claim 2, it is characterized in that, described screw propeller adopts 4 leaf shrouded propellers.
4. landing unmanned plane waterborne according to claim 3, it is characterized in that, described spiral propeller is fixed on described unmanned aerial vehicle platform by the C-type clamp be connected with described housing with right auger.
5. landing unmanned plane waterborne according to claim 2, is characterized in that, described screw propulsion electrical source of power adopts dc-battery, and described screw drives motor adopts DC brushless motor.
6. landing unmanned plane waterborne according to claim 1, is characterized in that, the fuselage that described unmanned aerial vehicle platform comprises the ship molded line with sailing device on water and the wing be connected with described fuselage; Described wing comprises empennage and two flanks, described power system adopts propeller turbine, described propeller turbine to be arranged on described two flanks and to connect screw propeller, the tailplane that described empennage comprises vertical tail and is connected with described vertical tail.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520802335.5U CN205131666U (en) | 2015-10-16 | 2015-10-16 | Unmanned aerial vehicle that takes off and land on water |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520802335.5U CN205131666U (en) | 2015-10-16 | 2015-10-16 | Unmanned aerial vehicle that takes off and land on water |
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| CN205131666U true CN205131666U (en) | 2016-04-06 |
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| CN201520802335.5U Active CN205131666U (en) | 2015-10-16 | 2015-10-16 | Unmanned aerial vehicle that takes off and land on water |
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Cited By (2)
| 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 |
-
2015
- 2015-10-16 CN CN201520802335.5U patent/CN205131666U/en active Active
Cited By (2)
| 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 |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
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. |