CN105035256B - The unmanned platform of body of carrier aircraft type high speed surface three - Google Patents

The unmanned platform of body of carrier aircraft type high speed surface three Download PDF

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Publication number
CN105035256B
CN105035256B CN201510402240.9A CN201510402240A CN105035256B CN 105035256 B CN105035256 B CN 105035256B CN 201510402240 A CN201510402240 A CN 201510402240A CN 105035256 B CN105035256 B CN 105035256B
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hull
deck
flight
high speed
glider
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CN105035256A (en
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魏成柱
王健
易宏
李英辉
张裕芳
毛立夫
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Shanghai Jiaotong University
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Shanghai Jiaotong University
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Abstract

A kind of unmanned platform of body of carrier aircraft type high speed surface three, including:The lamellar body for the glider structure that flight-deck, hull and two are symmetricly set in hull both sides, wherein:Flight-deck is arranged at the top of hull and two glider lamellar bodies, and is respectively connected with two lamellar bodies, and Multi-axis aircraft is provided with flight-deck or in hull.The present invention, which partly slides high speed monomer, wears swingboat and catamaran planing craft is combined, and expands flight-deck area, improves stability, adds sea-keeping and rapidity, ensures platform to loading the hyposensitivity of change;The unmanned platform of water surface high speed and Multi-axis aircraft are combined simultaneously, improve the use distance of Multi-axis aircraft, the unmanned platform of water surface high speed of expansion uses space, improves the overall using flexible of invention, mobility.

Description

The unmanned platform of body of carrier aircraft type high speed surface three
Technical field
The present invention relates to a kind of technology in unmanned speedboat field, specifically a kind of body of carrier aircraft type high speed surface three nobody Platform.
Background technology
With scientific and technological progress, unmanned technology obtains unprecedented development and application.Unmanned technology cost is low, and mobility is good, people Body safety guarantee is high.Unmanned air vehicle technique is widely used taking photo by plane, the field such as scout.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 Take the lead in deploying in the application of military field.In civil area, unmanned surface vehicle is in water quality detection, water sampling, marine environment Monitoring etc. has a wide range of applications.
Unmanned plane has the advantages of speed of a ship or plane is high, monitoring field is wide, mobility is high, and most popular at present is Multi-axis aircraft. Multi-axis aircraft has the characteristics of landing is flexible, mobility is high, technology maturity is high, but still suffer from cruising time it is short the problem of. Relative to unmanned surface vehicle, Multi-axis aircraft can enter many its unapproachable spatial domains and waters.Unmanned surface vehicle due to Standby and lifting hull need not be maintained to pinpoint using power, and it is low to weight sensitive, can carry more combustion Oil, therefore it has stronger a self-supplying capacity and endurance, delivered payload capability is also stronger.In addition, the target tracking algorism of Multi-axis aircraft It is ripe day by day, steadily target object can be followed to fly.Current unmanned plane and unmanned surface vehicle separately design more, if by two Person is combined together, and can make full use of respective advantage, it is contemplated that bigger efficiency will be produced.
Found by the retrieval to prior art, Chinese patent literature CN104608875A, publication date 2015.5.13, Disclose a kind of monomer and partly slide and wear swingboat, including:The hybrid introversive type of modified form wears swingboat head, semi-glding type main hull, interior Formula of inclining billow-pushed down type freeboard and totally enclosed superstructure;The hybrid introversive type of modified form is worn swingboat first packet and included:It is first post, totally enclosed Bow deck and stem freeboard, stem freeboard include:Introversion part and flared portion, wherein:Handed over flared portion introversion part Connect to form freeboard chine, the freeboard chine central fore-and-aft vertical plane projection with waterline angle γ be 1~3 °.But the technology is only Have high sea-keeping and high speed, because unmanned plane landing needs certain spatial area, too small ship top area make its carry compared with Certain difficulty be present in big Multi-axis aircraft.For single ship body compared with tri-body ship type, tri-body ship type has inborn stability advantage, Advantageously in the takeoff and landing of unmanned plane.
The content of the invention
The present invention is directed to deficiencies of the prior art, proposes a kind of unmanned platform of body of carrier aircraft type high speed surface three, Partly slide with reference to high speed Gao Naibo monomer and wear swingboat and binary high speed slide ship, form the ship type that three bodies are slided/partly slided, expand Big flight-deck area, adds stability, is advantageous to the landing of Multi-axis aircraft, ensure its muting sensitive sense to loading change Property.
The present invention is achieved by the following technical solutions:
The present invention includes:The lamellar body for the glider structure that flight-deck, hull and two are symmetricly set in hull both sides, its In:Flight-deck is arranged at the top of hull and two glider lamellar bodies, and is respectively connected with two lamellar bodies, on flight-deck or Multi-axis aircraft is provided with hull.
Described hull partly slides for high speed monomer and wears swingboat, including:The hybrid introversion of semi-glding type main hull, modified form The bow of type and the freeboard of introversion formula billow-pushed down type.
The waterline length L of described glider lamellar bodyWLSFor 0.5~0.75LWL, LWLThat is the waterline of semi-glding type main hull Length;Linewidth BWLSFor 0.3~0.5BWL, BWLThat is the width of the waterline of semi-glding type main hull;Absorb water TSFor 0.75~ 1T, T are the water line of semi-glding type main hull.
The afterbody ramping angle of described glider lamellar body is 0~17 °.
Described glider lamellar body is 0.5~1B with channel width folded by described semi-glding type main hullWL
The water line length L of described semi-glding type main hullWLIt is divided into multiple length scales.
Described Multi-axis aircraft is stopped on flight-deck according to the selection of hull demension rank, and is fixed by fixing device; Or cabin is stopped at, prevent the destruction of Exposure to Sunlight and upper wave to Multi-axis aircraft.
Described flight-deck is provided with waterproof shooting, fire water monitor, marine salvage equipment, bait dispensing device or military set It is standby.
Described semi-glding type main hull and/or glider piece are provided with propulsion plant and/or power set in vivo.
Described propulsion plant is using hydraulic propeller and half leaching oar;Described power set are the motor with lithium battery Or gasoline engine.
Technique effect
Compared with prior art, the present invention, which partly slides high speed monomer, wears swingboat and catamaran planing craft is combined, and expands Flight-deck area, improves stability, adds sea-keeping and rapidity, ensures platform to loading the hyposensitivity changed; The unmanned platform of water surface high speed and Multi-axis aircraft are combined simultaneously, improve the use distance of Multi-axis aircraft, the water surface of expansion The using flexible, the mobility that use space, improve invention entirety of unmanned platform at a high speed.
Brief description of the drawings
Fig. 1 is schematic diagram of the present invention;
Fig. 2 is side view of the present invention;
Fig. 3 is front view of the present invention;
Fig. 4 is top view of the present invention;
Fig. 5 is the cross-sectional view of position A in Fig. 2;
Fig. 6 is the cross-sectional view of position B in Fig. 2;
Fig. 7 is the cross-sectional view of position C in Fig. 2;
Fig. 8 is the cross-sectional view of position D in Fig. 2;
Fig. 9 is the cross-sectional view of position E in Fig. 2;
Figure 10 is plan of waterlines of the present invention;
Figure 11 is Multi-axis aircraft fixing device schematic diagram;
Figure 12 is Multi-axis aircraft fixture structure schematic diagram;
Figure 13 is power set schematic diagram of the present invention;
In figure:1 is main hull, and 2 be lamellar body, and 3 be superstructure, and 4 be flight-deck, and 5 be Multi-axis aircraft, and 6 is sliding for half Line main hull, 7 be bow, and 8 be freeboard, and post headed by 9,10 be bow deck, and 11 be stem freeboard, and 12 be freeboard chine, 13 be edge structure, and 14 be middle line keelson, and 15 be chin line, and 16 be waterline, and 17 be connecting bridge, and 18 be fixing device, 19 It is motor with 20,21 and 22 be propeller, and 23 and 24 be battery, and 25 and 26 be electron speed regulator, and 27 be buckle, and 28 be middle vertical profile Upper thread, 29 be steering wheel, and 30 be baseline.
Embodiment
Embodiments of the invention (1 meter level) are elaborated below, the present embodiment using technical solution of the present invention before Put and implemented, give detailed embodiment and specific operating process, but protection scope of the present invention is not limited to down The embodiment stated.Embodiment 1
As Figure 1-4, the present embodiment includes:Flight-deck 4, hull 1 and two pieces for being symmetricly set in the both sides of hull 1 Body 2, wherein:Flight-deck 4 is arranged at the top of hull 1 and two lamellar bodies 2, and is respectively connected with two lamellar bodies 2.Multiaxis flies Device 5 is stopped at flight-deck 4.
Described hull 1 is bridged by connecting bridge 17 respectively with two lamellar bodies 2.
Described hull 1 partly slides for high speed monomer and wears swingboat hull.
Described lamellar body 2 uses glider structure.
Described hull 1 is provided with superstructure 3.
Described superstructure 3 is located at the front of flight-deck 4.
Described hull 1 or lamellar body 2 are provided with power set.
Described hull 1 includes:Bow 7 and introversion formula the pressure wave of the hybrid introversive type of semi-glding type main hull 6, modified form The freeboard 8 of type.
As shown in Figure 10, the length L of the waterline 16 of described hull 1WLIt is divided into a meter level (the present embodiment), three meter levels and six Three ranks of meter level, LWLWith waterline breadth BWLRatio LWL/BWLFor 6~7, LWLWith the ratio L between water line TWL/ T is 20.5 ~23.5.
The designed water line width of described hull 1 is increased from bow to stern, is received after reaching Breadth Maximum along stern direction Contracting, the half entrance angle of the designed waterplane is 8~10 °, can further reduce ship resistance.
As shown in figure 13, described power set include:Propeller 21 or 22, motor 19 or 20, the electronics being sequentially connected Speed regulator 25 or 26 and lithium battery 23 or 24.
Described propeller 21 or 22 can be hydraulic propeller or half leaching oar.
Described power set determine according to hull rank, a meter level hull can be added using motor lithium battery or 26~ 30cc gasoline engine, three meter level hulls use 26~30cc or higher gasoline engine, and six meter level hulls then need to install high speed bavin Oil machine.
Described superstructure 3 is provided with detection device and radio transmitting device.
Can rise and fall Multi-axis aircraft 5 on described flight-deck 4, and the multiple detection modules of installation, fire-fighting may be selected when unloaded Water cannon, marine salvage equipment, bait dispensing device and military equipment etc..
Described lamellar body 2 is designed using the lamellar body of catamaran planing craft, the waterline length L of lamellar body 2WLSFor 0.5~0.75LWL, Linewidth BWLSFor 0.3~0.5BWL, absorb water TSFor 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 1CFor 0.5~1BWL, too small BCConduit be easily caused water blockoff, hinder The consequences such as power increases or dolphin jumps.
The height HB of described connecting bridge 17 can determine according to the size and modes of emplacement of selected aircraft 5.
As is illustrated by figs. 11 and 12, described flight-deck 4 is provided with several fixing devices 18, including:The He of steering wheel 29 The buckle 27 being attached thereto.
Described fixing device 18 is used for the fixed aircraft 5 being parked on flight-deck 4.
Described aircraft 5 can be built in cabin.
Changeable weight is carried on described hull 1.
Described middle line keelson 14 forms angle with baseline 29 and is easy to produce planing surface.
Knuckle and introversion the formula design of described freeboard 8 are ensureing that having while wearing wave and stealth effect for hull is enough Volume of compartment.
Body lines of the described freeboard chine 12 at the B of position is more flat with the smaller bows of angle ζ of central fore-and-aft vertical plane, mistake All it is unfavorable to the high speed of volume of compartment and hull 1 in flat bow.
Described beloid designed waterplane can further reduce ship resistance.
The openable cabin in top can be increased on the flight-deck 4 of three meter levels and six meter level hulls, prevent Exposure to Sunlight and upper wave Destruction to aircraft 5.
The present embodiment can be used as base station personnel easy to operation to carry out shaking control to aircraft 5 by remote control, and aircraft 5 flies Row height can be used as remote signal receiving terminal when higher, available for Patrol on Waters, waters it is three-dimensional monitor, water sampling and analysis, Bait is launched, the water surface images etc..

Claims (1)

  1. A kind of 1. unmanned platform of body of carrier aircraft type high speed surface three, it is characterised in that including:Flight-deck, hull and two are symmetrical The lamellar body of the glider structure of hull both sides is arranged at, wherein:Flight-deck is arranged at the upper of hull and two glider lamellar bodies Side, and be respectively connected with two lamellar bodies, Multi-axis aircraft is provided with flight-deck or in hull;
    Described hull partly slides for high speed monomer and wears swingboat, including:The hybrid introversive type of semi-glding type main hull, modified form The freeboard of bow and introversion formula billow-pushed down type;Knuckle and introversion the formula design of freeboard are ensureing that wearing for hull is unrestrained and stealth effect same When with enough volume of compartments;
    The waterline length L of described glider lamellar bodyWLSFor 0.5~0.75LWL, LWLThat is the length of the waterline of semi-glding type main hull Degree;Linewidth BWLSFor 0.3~0.5BWL, BWLThat is the width of the waterline of semi-glding type main hull;Absorb water TSFor 0.75~1T, T That is the water line of semi-glding type main hull;
    The afterbody ramping angle of described glider lamellar body is 0~17 °;
    The middle line keelson of described hull and the baseline of hull form angle and are easy to produce planing surface;
    The designed waterplane of described hull is beloid, so as to further reduce ship resistance;
    Described glider lamellar body is 0.5~1B with channel width folded by described semi-glding type main hullWL
    The water line length L of described semi-glding type main hullWLIt is divided into multiple length scales.
CN201510402240.9A 2015-07-10 2015-07-10 The unmanned platform of body of carrier aircraft type high speed surface three Expired - Fee Related CN105035256B (en)

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Publication number Priority date Publication date Assignee Title
CN106347574A (en) * 2016-09-18 2017-01-25 江苏科技大学 Planar straight wall side and double channel composite hydroplane
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
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
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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CN103770903A (en) * 2014-03-06 2014-05-07 上海交通大学 Wave absorbing type wave piercing yacht

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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
CN202124101U (en) * 2011-05-19 2012-01-25 上海船舶研究设计院 External-jumping deck structure of triple-hulled vessel
CN102785757B (en) * 2011-05-19 2015-05-27 上海船舶研究设计院 Movable side body structure of triple-hulled vessel
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