CN105035256A - Carrier type high-speed water three-body unmanned platform - Google Patents
Carrier type high-speed water three-body unmanned platform Download PDFInfo
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- CN105035256A CN105035256A CN201510402240.9A CN201510402240A CN105035256A CN 105035256 A CN105035256 A CN 105035256A CN 201510402240 A CN201510402240 A CN 201510402240A CN 105035256 A CN105035256 A CN 105035256A
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Abstract
The invention provides a carrier type high-speed water three-body unmanned platform. The carrier type high-speed water three-body unmanned platform comprises a flight deck, a ship body and piece bodies of planing boat structures, wherein the piece bodies are symmetrically arranged on the two sides of the ship body. The flight deck is arranged above the ship body and the two planing boat piece bodies and connected with the piece bodies. A multi-shaft aircraft is arranged on the flight deck or in the ship body. According to the carrier type high-speed water three-body unmanned platform, a high-speed single semi-planing wave-piercing ship and a double-body planing boat are combined, the area of the flight deck is enlarged, stability is improved, seakeeping and speedability are improved, and the low sensitivity to load changes of the platform is guaranteed; meanwhile the high-speed water unmanned platform and the multi-shaft aircraft are combined, the use distance of the multi-shaft aircraft is increased, the use space of the high-speed water unmanned platform is enlarged, and the use flexibility and maneuverability of the overall carrier type high-speed water three-body unmanned platform are improved.
Description
Technical field
What the present invention relates to is a kind of technology of unmanned speedboat field, the specifically unmanned platform of a kind of carrier aircraft type high speed surface three body.
Background technology
Along with scientific and technological progress, unmanned technology obtains unprecedented development and application.Unmanned technology cost is low, and manoevreability is good, and personal safety supportability is high.Unmanned air vehicle technique taking photo by plane, the field such as scouting is widely used.No matter on software and hardware, its technology maturity is very high.After unmanned plane, the development of unmanned surface vehicle enters a new upsurge.Unmanned surface vehicle has taken the lead in launching in the application of military field.At civil area, unmanned surface vehicle has a wide range of applications in water quality detection, water sampling, marine environmental monitoring etc.
Unmanned plane has the advantage that the speed of a ship or plane is high, supervision field is wide, manoevreability is high, and the most popular is Multi-axis aircraft at present.Multi-axis aircraft has the advantages that landing is flexible, manoevreability is high, technology maturity is high, but still there is short problem in cruise duration.Relative to unmanned surface vehicle, Multi-axis aircraft can enter a lot of its unapproachable spatial domain and waters.Unmanned surface vehicle is not owing to needing to use power to maintain standby and lifting hull of fixing a point, and it is low to weight sensitive, can carry more fuel oil, therefore it has stronger endurance and endurance, and delelivered payload capability is also stronger.In addition, the target tracking algorism of Multi-axis aircraft is ripe day by day, can follow object flight steadily.Current unmanned plane and unmanned surface vehicle is many designs respectively, if both combined, can make full use of respective advantage, can predict and will produce larger usefulness.
Through finding the retrieval of prior art, Chinese patent literature CN104608875A, publication date 2015.5.13, disclose a kind of monomer partly to slide and wear swingboat, comprising: the hybrid introversive type of modified form wears swingboat head, semi-glding type main body, introversion formula billow-pushed down type freeboard and fully enclosed superstructure; The hybrid introversive type of modified form is worn swingboat first packet and is drawn together: first post, fully enclosed bow deck and stem freeboard, stem freeboard comprises: introversion part and flared portion, wherein: introversion part and flared portion join and form freeboard knuckle line, this freeboard knuckle line is 1 ~ 3 ° in the projection of center buttock with the angle γ of waterline.But this technology only has high rough water quality and a high speed, because unmanned plane landing needs certain spatial area, too small ship top area makes it carry larger Multi-axis aircraft to there is certain difficulty.Single ship body is compared with tri-body ship type, and tri-body ship type has inborn stability advantage, taking off and landing advantageously in unmanned plane.
Summary of the invention
The present invention is directed to prior art above shortcomings, the unmanned platform of a kind of carrier aircraft type high speed surface three body is proposed, monomer in conjunction with high speed Gao Naibo partly slides wears swingboat and binary high speed slide ship, form the ship type that three bodies slide/partly slide, expand flight deck area, add stability, be conducive to the landing of Multi-axis aircraft, ensure that it is to the hyposensitivity loading change.
The present invention is achieved by the following technical solutions:
The present invention includes: flight deck, hull and two are symmetricly set in the lamellar body of the glider structure of hull both sides, wherein: flight deck is arranged at the top of hull and two glider lamellar bodies, and be connected respectively with two lamellar bodies, be provided with Multi-axis aircraft on flight deck or in hull.
Described hull is that high speed monomer partly slides and wears swingboat, comprising: the bow of the hybrid introversive type of semi-glding type main body, modified form and the freeboard of introversion formula billow-pushed down type.
The waterline length L of described glider lamellar body
wLSbe 0.5 ~ 0.75L
wL, L
wLthe i.e. length of the waterline of semi-glding type main body; Linewidth B
wLSbe 0.3 ~ 0.5B
wL, B
wLthe i.e. width of the waterline of semi-glding type main body; Drinking water T
sit is the floating line of 0.75 ~ 1T, T and semi-glding type main body.
The afterbody ramping angle of described glider lamellar body is 0 ~ 17 °.
Folded by described glider lamellar body and described semi-glding type main body, channel width is 0.5 ~ 1B
wL.
The length on water line L of described semi-glding type main body
wLbe divided into multiple length scale.
Described Multi-axis aircraft is selected to be stopped on flight deck according to hull demension rank, and is fixed by anchor fitting; Or be stopped at cabin, prevent Exposure to Sunlight and upper wave to the destruction of Multi-axis aircraft.
Described flight deck is provided with waterproof shooting, fire water monitor, marine salvage equipment, bait dispensing device or military equipment.
Propelling unit and/or engine installation is provided with in described semi-glding type main body and/or glider lamellar body.
Described propelling unit adopts waterjet propulsor and partly soaks oar; Described engine installation is motor with lithium cell or spark ignition engine.
Technique effect
Compared with prior art, high speed monomer partly slides and wears swingboat and catamaran planing craft combines by the present invention, expands flight deck area, improves stability, add rough water quality and rapidity, ensures that platform is to the hyposensitivity loading change; Unmanned for water surface high speed platform and Multi-axis aircraft are combined simultaneously, improve the service range of Multi-axis aircraft, the usage space of the unmanned platform of water surface high speed of expansion, improve use alerting ability, manoevreability that invention is overall.
Accompanying drawing explanation
Fig. 1 is schematic diagram of the present invention;
Fig. 2 is lateral plan of the present invention;
Fig. 3 is front elevation of the present invention;
Fig. 4 is birds-eye view of the present invention;
Fig. 5 is the cross sectional drawing of position A in Fig. 2;
Fig. 6 is the cross sectional drawing of position B in Fig. 2;
Fig. 7 is the cross sectional drawing of position C in Fig. 2;
Fig. 8 is the cross sectional drawing of position D in Fig. 2;
Fig. 9 is the cross sectional drawing of position E in Fig. 2;
Figure 10 is plan of waterlines of the present invention;
Figure 11 is Multi-axis aircraft anchor fitting schematic diagram;
Figure 12 is Multi-axis aircraft fixture structure schematic diagram;
Figure 13 is engine installation schematic diagram of the present invention;
In figure: 1 is main body, 2 is lamellar body, and 3 is superstructure, 4 is flight deck, and 5 is Multi-axis aircraft, and 6 is semi-glding type main body, 7 is bow, and 8 is freeboard, post headed by 9,10 is bow deck, and 11 is stem freeboard, and 12 is freeboard knuckle line, 13 is edge structure, and 14 is center keelson, and 15 is chin line, 16 is waterline, and 17 is connecting bridge, and 18 is anchor fitting, 19 and 20 is motor, 21 and 22 is propelling unit, and 23 and 24 is battery, and 25 and 26 is electronic governor, 27 is buckle, 28 is center buttock line, and 29 is steering wheel, and 30 is baseline.
Detailed description of the invention
Below embodiments of the invention (1 meter level) are elaborated; the present embodiment is implemented under premised on technical solution of the present invention; give detailed embodiment and concrete operating process, but protection scope of the present invention is not limited to following embodiment.Embodiment 1
As figure 1 ?shown in 4, the present embodiment comprises: flight deck 4, hull 1 and two are symmetricly set in the lamellar body 2 of hull 1 both sides, wherein: flight deck 4 is arranged at the top of hull 1 and two lamellar bodies 2, and are connected respectively with two lamellar bodies 2.Multi-axis aircraft 5 is stopped at flight deck 4.
Described hull 1 and two lamellar bodies 2 are respectively by connecting bridge 17 bridge joint.
Described hull 1 wears swingboat hull for high speed monomer partly slides.
Described lamellar body 2 adopts glider structure.
Described hull 1 is provided with superstructure 3.
Described superstructure 3 is positioned at flight deck 4 front.
Described hull 1 or lamellar body 2 are provided with engine installation.
Described hull 1 comprises: the bow 7 of the hybrid introversive type of semi-glding type main body 6, modified form and the freeboard 8 of introversion formula billow-pushed down type.
As shown in Figure 10, the length L of the waterline 16 of described hull 1
wLbe divided into a meter level (the present embodiment), three meter levels and six meter levels, three ranks, L
wLwith waterline breadth B
wLratio L
wL/ B
wLbe 6 ~ 7, L
wLwith the ratio L between floating line T
wL/ T is 20.5 ~ 23.5.
The design load water line width of described hull 1 is increased to stern by bow, and shrink along stern direction after reaching maximum width, the half entrance angle of this designed waterplane is 8 ~ 10 °, can reduce running resistance further.
As shown in figure 13, described engine installation comprises: the propelling unit 21 or 22, motor 19 or 20, electronic governor 25 or 26 and the lithium cell 23 or 24 that are connected successively.
Described propelling unit 21 or 22 can be waterjet propulsor or partly soaks oar.
Described engine installation is determined according to hull rank, and a meter level hull can adopt motor to add the spark ignition engine of lithium cell or 26 ~ 30cc, and three meter level hulls adopt the spark ignition engine of 26 ~ 30cc or higher, and six meter level hulls then need to install high speed diesel engine.
Described superstructure 3 is provided with detector and radio transmitting device.
Described flight deck 4 can rise and fall Multi-axis aircraft 5, can select to install multiple detection module, fire water monitor, marine salvage equipment, bait dispensing device and military equipment etc. time unloaded.
Described lamellar body 2 adopts the lamellar body of catamaran planing craft to design, the waterline length L of lamellar body 2
wLSbe 0.5 ~ 0.75L
wL, linewidth B
wLSbe 0.3 ~ 0.5B
wL, drinking water T
sbe 0.75 ~ 1T.
The afterbody ramping angle μ of described lamellar body 2 is 0 ~ 17 °.
Described lamellar body 2 and channel width B folded by hull 1
cbe 0.5 ~ 1B
wL, too small B
cconduit easily cause water blockoff, resistance increases or the consequence such as dolphin jumping.
The height H B of described connecting bridge 17 can determine according to the size of selected aircraft 5 and modes of emplacement.
As is illustrated by figs. 11 and 12, described flight deck 4 is provided with several anchor fittings 18, comprising: steering wheel 29 and the buckle 27 be attached thereto.
Described anchor fitting 18 is for being fixedly parked in the aircraft 5 on flight deck 4.
Described aircraft 5 can be built in cabin.
Described hull 1 carries changeable weight.
Described center keelson 14 forms angle with baseline 29 and is convenient to produce planing surface.
The knuckle of described freeboard 8 and introversion formula design ensure hull wear wave and stealth effect while there is enough volume of compartments.
The body lines of described freeboard knuckle line 12 at B place, position is more flat with the less bow of angle ζ of center buttock, and the high speed of too flat bow to volume of compartment and hull 1 is all disadvantageous.
Described beloid designed waterplane can reduce running resistance further.
The flight deck 4 of three meter levels and six meter level hulls can increase openable cabin, top, prevent Exposure to Sunlight and upper wave to the destruction of aircraft 5.
The present embodiment can be used as base station convenient operation personnel and shakes control by remote control to aircraft 5, aircraft 5 flying height can be used as remote signal receiving end time higher, can be used for Patrol on Waters, waters solid monitoring, water sampling and analysis, bait input, water surface shooting etc.
Claims (10)
1. the unmanned platform of carrier aircraft type high speed surface three body, it is characterized in that, comprise: flight deck, hull and two are symmetricly set in the lamellar body of the glider structure of hull both sides, wherein: flight deck is arranged at the top of hull and two glider lamellar bodies, and be connected respectively with two lamellar bodies, be provided with Multi-axis aircraft on flight deck or in hull.
2. the unmanned platform of carrier aircraft type high speed surface three body according to claim 1, is characterized in that, described hull is that high speed monomer partly slides and wears swingboat, comprising: the bow of the hybrid introversive type of semi-glding type main body, modified form and the freeboard of introversion formula billow-pushed down type.
3. the unmanned platform of carrier aircraft type high speed surface three body according to claim 1, is characterized in that, the waterline length L of described glider lamellar body
wLSbe 0.5 ~ 0.75L
wL, L
wLthe i.e. length of the waterline of semi-glding type main body; Linewidth B
wLSbe 0.3 ~ 0.5B
wL, B
wLthe i.e. width of the waterline of semi-glding type main body; Drinking water T
sit is the floating line of 0.75 ~ 1T, T and semi-glding type main body.
4. the unmanned platform of carrier aircraft type high speed surface three body according to claim 1 or 3, is characterized in that, the afterbody ramping angle of described glider lamellar body is 0 ~ 17 °.
5. the unmanned platform of carrier aircraft type high speed surface three body according to claim 1 or 3, is characterized in that, folded by described glider lamellar body and described semi-glding type main body, channel width is 0.5 ~ 1B
wL.
6. the unmanned platform of carrier aircraft type high speed surface three body according to Claims 2 or 3, is characterized in that, the length on water line L of described semi-glding type main body
wLbe divided into multiple length scale.
7. the unmanned platform of carrier aircraft type high speed surface three body according to claim 1, is characterized in that, described Multi-axis aircraft is selected to be stopped on flight deck according to hull demension rank, and is fixed by anchor fitting; Or be stopped at cabin, prevent Exposure to Sunlight and upper wave to the destruction of Multi-axis aircraft.
8. the unmanned platform of carrier aircraft type high speed surface three body according to claim 1, is characterized in that, described flight deck is provided with waterproof shooting, fire water monitor, marine salvage equipment, bait dispensing device or military equipment.
9. the unmanned platform of carrier aircraft type high speed surface three body according to claim 2, is characterized in that, is provided with propelling unit and/or engine installation in described semi-glding type main body and/or glider lamellar body.
10. the unmanned platform of carrier aircraft type high speed surface three body according to claim 9, is characterized in that, described propelling unit adopts waterjet propulsor and partly soaks oar; Described engine installation is motor with lithium cell or spark ignition engine.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510402240.9A CN105035256B (en) | 2015-07-10 | 2015-07-10 | The unmanned platform of body of carrier aircraft type high speed surface three |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510402240.9A CN105035256B (en) | 2015-07-10 | 2015-07-10 | The unmanned platform of body of carrier aircraft type high speed surface three |
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| Publication Number | Publication Date |
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| CN105035256A true CN105035256A (en) | 2015-11-11 |
| CN105035256B CN105035256B (en) | 2018-03-06 |
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Cited By (6)
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| CN106275302A (en) * | 2016-09-18 | 2017-01-04 | 江苏科技大学 | A kind of double flute road water surface is combined speedboat |
| CN106347574A (en) * | 2016-09-18 | 2017-01-25 | 江苏科技大学 | Planar straight wall side and double channel composite hydroplane |
| CN107380341A (en) * | 2017-06-29 | 2017-11-24 | 大连理工大学 | A kind of oil electricity three body high-speed crafts of mixing and its method of work |
| CN107662705A (en) * | 2017-10-12 | 2018-02-06 | 黄河科技学院 | A kind of marine monitoring device |
| CN108945278A (en) * | 2018-06-26 | 2018-12-07 | 广东新船重工有限公司 | A kind of catamaran |
| CN113401276A (en) * | 2021-08-04 | 2021-09-17 | 大连云海船艇科技有限公司 | Double-body channel planing boat in form of composite ship body |
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| CN102785757A (en) * | 2011-05-19 | 2012-11-21 | 上海船舶研究设计院 | Movable side body structure of triple-hulled vessel |
| CN103640675A (en) * | 2013-12-18 | 2014-03-19 | 江苏科技大学 | Amphibious unmanned surface vehicle with three bodies |
| CN103770903A (en) * | 2014-03-06 | 2014-05-07 | 上海交通大学 | Wave absorbing type wave piercing yacht |
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2015
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Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| EP0800989A1 (en) * | 1996-03-29 | 1997-10-15 | Chung Chen Clifford Shaw | Hybrid high performance water vessels |
| CN102079380A (en) * | 2010-09-17 | 2011-06-01 | 朱惠芬 | Navigation submarine ship with hydrofoil power cabins |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275302A (en) * | 2016-09-18 | 2017-01-04 | 江苏科技大学 | A kind of double flute road water surface is combined speedboat |
| CN106347574A (en) * | 2016-09-18 | 2017-01-25 | 江苏科技大学 | Planar straight wall side and double channel composite hydroplane |
| CN107380341A (en) * | 2017-06-29 | 2017-11-24 | 大连理工大学 | A kind of oil electricity three body high-speed crafts of mixing and its method of work |
| CN107380341B (en) * | 2017-06-29 | 2019-04-09 | 大连理工大学 | A kind of oil is electric to mix three-body high-speed craft and its working method |
| CN107662705A (en) * | 2017-10-12 | 2018-02-06 | 黄河科技学院 | A kind of marine monitoring device |
| CN108945278A (en) * | 2018-06-26 | 2018-12-07 | 广东新船重工有限公司 | A kind of catamaran |
| CN108945278B (en) * | 2018-06-26 | 2024-04-02 | 广东新船重工有限公司 | Catamaran |
| CN113401276A (en) * | 2021-08-04 | 2021-09-17 | 大连云海船艇科技有限公司 | Double-body channel planing boat in form of composite ship body |
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| CN105035256B (en) | 2018-03-06 |
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