CN107554783A - A kind of amphibious unmanned plane of VTOL - Google Patents

A kind of amphibious unmanned plane of VTOL Download PDF

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Publication number
CN107554783A
CN107554783A CN201710782976.2A CN201710782976A CN107554783A CN 107554783 A CN107554783 A CN 107554783A CN 201710782976 A CN201710782976 A CN 201710782976A CN 107554783 A CN107554783 A CN 107554783A
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CN
China
Prior art keywords
fuselage
unmanned plane
amphibious unmanned
vtol
connecting rod
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Pending
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CN201710782976.2A
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Chinese (zh)
Inventor
罗哲远
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Foshan Longcheng Technology Co Ltd
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Foshan Longcheng Technology Co Ltd
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Priority to CN201710782976.2A priority Critical patent/CN107554783A/en
Publication of CN107554783A publication Critical patent/CN107554783A/en
Pending legal-status Critical Current

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Abstract

A kind of amphibious unmanned plane of VTOL, belong to vehicle technology field, more particularly to a kind of amphibious unmanned plane of VTOL, including fuselage, wing, empennage, hull, steering wheel and undercarriage.Described fuselage includes detector, controller, central processing unit and motor;Described fuselage also includes connecting rod and propeller, and the connecting rod has four, and nosing each side has one, and back body each side has one, and a propeller is all connected in each connecting rod.The present invention takes full advantage of the rotary power of four propellers, enable amphibious unmanned plane VTOL, save take-off venue when land is taken off, save the time when the water surface takes off, simultaneously when running into the sea of complexity, it can in a short time fly to and be hidden in the air, improve amphibious unmanned plane survival ability and operating efficiency.

Description

A kind of amphibious unmanned plane of VTOL
Technical field
A kind of amphibious unmanned plane of VTOL, belong to vehicle technology field, more particularly to a kind of VTOL Amphibious unmanned plane.
Background technology
Traditional amphibious unmanned plane above water uses the layout of fixed wing aircraft, including fuselage, wing and empennage, Underwater portion is laid out using Ship Structure, can carry bigger load.Traditional amphibious unmanned plane is adapted in calmness Navigation, but be unfavorable for navigating by water on the sea of complexity, when traditional amphibious unmanned plane runs into the weather for having stormy waves, just can not Navigation so that the application of traditional amphibious unmanned plane is smaller.
The content of the invention
The purpose of the present invention is to overcome the above-mentioned deficiency of the amphibious unmanned plane of tradition, invents a kind of land and water of VTOL Amphibious unmanned plane.
A kind of amphibious unmanned plane of VTOL, including fuselage, wing, empennage, hull, steering wheel and undercarriage.
Described fuselage includes detector, controller, central processing unit and motor;Before described detector is located at fuselage Section, for detecting the situation on sea;Described controller is located at middle fuselage;Described central processing unit is located at middle fuselage, On the right side of controller;Described motor is located at fuselage endpiece, and the energy is provided for unmanned plane.
Described fuselage also includes connecting rod and propeller, and the connecting rod has four, and nosing each side has One, back body each side has one, and a propeller is all connected in each connecting rod, for it is amphibious nobody Machine provides the power of vertical lift.
Described wing is divided into left wing and right flank, and left wing and right flank are connected with fuselage, positioned at nosing, left wing and right flank Symmetrical distribution;After described empennage is located at fuselage;Described hull is located at below fuselage, can be in surface navigation;Institute The steering wheel stated is located at hull rear end, and power is provided in surface navigation for unmanned plane;Described undercarriage is located at below fuselage.
Preferably, a kind of amphibious unmanned plane of described VTOL also includes wireless camera, radar and GPS.
A kind of amphibious unmanned plane of described VTOL so works:When taking off on land, center control Device processed receives the instruction taken off, and information is transmitted to controller, controller controls four propellers to start, and motor gives four propellers Electric energy is provided, the amphibious unmanned plane of power brought by four propellers can take off vertically;When amphibious nothing Man-machine when needing to drop to sea navigation, controller controls four propellers to stop operating, and amphibious unmanned plane relies on two Wing is slowly slided and dropped on the water surface, and then controller control steering wheel starts, and provides for amphibious unmanned plane and is navigated in the water surface Capable power;When amphibious unmanned plane needs to take off from the water surface, controller control flaps office closes, and starts four propellers and is Taking off vertically for amphibious unmanned plane provides power;When amphibious unmanned plane needs to drop to ground, controller control Four propellers slowly land so that amphibious unmanned function vertical landing to ground;When amphibious unmanned plane is on sea When navigation runs into wave;It can be taken off vertically by four amphibious unmanned planes of propeller-driven, circumvent wave, wait wave mistake The water surface is dropped to again afterwards to continue to navigate by water.
The present invention takes full advantage of the rotary power of four propellers so that amphibious unmanned plane can VTOL, Take-off venue when land is taken off is saved, saves the time when the water surface takes off, while in the sea for running into complexity During face, it can in a short time fly to and be hidden in the air, improve amphibious unmanned plane survival ability and operating efficiency.
Brief description of the drawings
Fig. 1 is a kind of schematic top plan view of the amphibious unmanned plane of VTOL;Fig. 2 is a kind of land and water of VTOL The left view schematic diagram of amphibious unmanned plane.
In figure, 1- fuselages, 2- detectors, 3- controllers, 4- central processing units, 5- motors, 6- left wings, 7- right flanks, 8- companies Extension bar, 9- propellers, 10- empennages, 11- hulls, 12- steering wheels, 13- undercarriages.
Embodiment
The present invention is illustrated in conjunction with accompanying drawing:A kind of amphibious unmanned plane of VTOL, including fuselage 1st, wing, empennage 10, hull 11, steering wheel 12 and undercarriage 13.
Described fuselage 1 includes detector 2, controller 3, central processing unit 4 and motor 5;Described detector 2 is located at machine The leading portion of body 1, for detecting the situation on sea;Described controller 3 is located at the stage casing of fuselage 1;Described central processing unit 4 is located at machine The stage casing of body 1, the right side of controller 3;Described motor 5 is located at the endpiece of fuselage 1, and the energy is provided for unmanned plane.
Described fuselage 1 also includes connecting rod 8 and propeller 9, and the connecting rod 8 has four, the nosing left and right sides Respectively there is one, back body each side has one, and a propeller 9 is all connected in each connecting rod 8, is land and water two Unmanned plane of dwelling provides the power of vertical lift.
Described wing is divided into left wing 6 and right flank 7, and left wing 6 and right flank 7 are connected with fuselage 1, positioned at the leading portion of fuselage 1, left wing 6 and 7 symmetrical distribution of right flank;Described left wing 6 is identical with the structure of right flank 7.After described empennage 10 is located at fuselage 1;Institute The hull 11 stated is located at the lower section of fuselage 1, can be in surface navigation;Described steering wheel 12 is located at the rear end of hull 11, exists for unmanned plane Surface navigation provides power;Described undercarriage 13 is located at the lower section of fuselage 1.
A kind of amphibious unmanned plane of described VTOL so works:When taking off on land, center control Device 3 processed receives the instruction taken off, and information is transmitted to controller 3, controller 3 controls four propellers 9 to start, and motor 5 gives four Propeller 9 provides electric energy, and the amphibious unmanned plane of power brought by four propellers 9 can take off vertically;Work as water When the amphibious unmanned plane in land needs to drop to sea navigation, controller 3 controls four propellers 9 to stop operating, it is amphibious nobody Machine is slowly slided by two wings and dropped on the water surface, and then controller 3 controls steering wheel 12 to start, and is amphibious unmanned plane Power in surface navigation is provided;When amphibious unmanned plane needs to take off from the water surface, controller 3 controls steering wheel 12 to close, Start four propellers 9 and provide power for taking off vertically for amphibious unmanned plane;When amphibious unmanned plane needs to drop to During ground, controller 3 controls four propellers 9 slowly to land so that amphibious unmanned function vertical landing to ground;Work as water The amphibious unmanned plane in land is when sea navigation runs into wave;By four propellers 9 amphibious unmanned plane can be driven vertically to rise Fly, circumvent wave, wait wave to drop to the water surface again later and continue to navigate by water.

Claims (2)

1. a kind of amphibious unmanned plane of VTOL, including fuselage(1), wing, empennage(10), hull(11), steering wheel (12)And undercarriage(13), it is characterised in that:Described fuselage(1)Including detector(2), controller(3), central processing unit (4)And motor(5);Described detector(2)Positioned at fuselage(1)Leading portion;Described controller(3)Positioned at fuselage(1)Stage casing;Institute The central processing unit stated(4)Positioned at fuselage(1)Stage casing, controller(3)Right side;Described motor(5)Positioned at fuselage(1)Endpiece; Described fuselage(1)Also include connecting rod(8)And propeller(9), the connecting rod(8)There are four, fuselage(1)Leading portion or so two Side respectively has one, fuselage(1)Rear end each side has one, each connecting rod(8)On be all connected to a propeller (9);Described wing is divided into left wing(6)And right flank(7), left wing(6)And right flank(7)With fuselage(1)It is connected, positioned at fuselage(1) Leading portion, left wing(6)And right flank(7)Symmetrical distribution;Described empennage(10)Positioned at fuselage(1)Afterwards;Described hull (11)Positioned at fuselage(1)Lower section;Described steering wheel(12)Positioned at hull(11)Rear end;Described undercarriage(13)Positioned at fuselage (1)Lower section.
A kind of 2. amphibious unmanned plane of VTOL according to claim 1, it is characterised in that:It is described amphibious Unmanned plane also includes wireless camera, radar and GPS.
CN201710782976.2A 2017-09-03 2017-09-03 A kind of amphibious unmanned plane of VTOL Pending CN107554783A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110077588A (en) * 2019-04-22 2019-08-02 大连理工大学 It is a kind of can the sea, land and air latent four of VTOL dwell aircraft
CN110722942A (en) * 2019-11-14 2020-01-24 复旦大学 Multifunctional amphibious unmanned aerial vehicle
CN110775265A (en) * 2019-10-28 2020-02-11 上海交通大学 Oil-electricity hybrid driving amphibious aircraft and control method thereof
CN111152923A (en) * 2020-01-07 2020-05-15 长江水利委员会长江科学院 Underwater terrain measuring device based on vertical take-off and landing fixed wing amphibious unmanned aerial vehicle
CN112027078A (en) * 2020-09-16 2020-12-04 郑州航空工业管理学院 Amphibious composite wing unmanned aerial vehicle and control method thereof
CN113093770A (en) * 2021-03-30 2021-07-09 华南理工大学 Wave evaluation-based multi-rotor unmanned spacecraft water surface takeoff control method

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1202861A (en) * 1995-10-24 1998-12-23 汉斯·J·伯恩 Hybrid aircraft
CN102166931A (en) * 2011-06-08 2011-08-31 陈昌志 New energy multifunctional airplane
CN105346718A (en) * 2015-09-29 2016-02-24 上海圣尧智能科技有限公司 Vertical take-off and landing unmanned plane
CN106103274A (en) * 2015-07-02 2016-11-09 深圳市大疆创新科技有限公司 Unmanned plane, its control system and method, and unmanned plane landing control method
CN106494608A (en) * 2015-09-06 2017-03-15 陈康 Many shrouded propeller variable geometry Electric aircrafts
CN106956773A (en) * 2017-04-07 2017-07-18 南昌航空大学 Tilting rotor formula VUAV and its control method

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1202861A (en) * 1995-10-24 1998-12-23 汉斯·J·伯恩 Hybrid aircraft
CN102166931A (en) * 2011-06-08 2011-08-31 陈昌志 New energy multifunctional airplane
CN106103274A (en) * 2015-07-02 2016-11-09 深圳市大疆创新科技有限公司 Unmanned plane, its control system and method, and unmanned plane landing control method
CN106494608A (en) * 2015-09-06 2017-03-15 陈康 Many shrouded propeller variable geometry Electric aircrafts
CN105346718A (en) * 2015-09-29 2016-02-24 上海圣尧智能科技有限公司 Vertical take-off and landing unmanned plane
CN106956773A (en) * 2017-04-07 2017-07-18 南昌航空大学 Tilting rotor formula VUAV and its control method

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110077588A (en) * 2019-04-22 2019-08-02 大连理工大学 It is a kind of can the sea, land and air latent four of VTOL dwell aircraft
CN110077588B (en) * 2019-04-22 2022-05-20 大连理工大学 Sea, land and air submerged four-purpose aircraft capable of taking off and landing vertically
CN110775265A (en) * 2019-10-28 2020-02-11 上海交通大学 Oil-electricity hybrid driving amphibious aircraft and control method thereof
CN110722942A (en) * 2019-11-14 2020-01-24 复旦大学 Multifunctional amphibious unmanned aerial vehicle
CN111152923A (en) * 2020-01-07 2020-05-15 长江水利委员会长江科学院 Underwater terrain measuring device based on vertical take-off and landing fixed wing amphibious unmanned aerial vehicle
CN111152923B (en) * 2020-01-07 2021-06-25 长江水利委员会长江科学院 Underwater terrain measuring device based on vertical take-off and landing fixed wing amphibious unmanned aerial vehicle
CN112027078A (en) * 2020-09-16 2020-12-04 郑州航空工业管理学院 Amphibious composite wing unmanned aerial vehicle and control method thereof
CN112027078B (en) * 2020-09-16 2022-06-07 郑州航空工业管理学院 Amphibious composite wing unmanned aerial vehicle and control method thereof
CN113093770A (en) * 2021-03-30 2021-07-09 华南理工大学 Wave evaluation-based multi-rotor unmanned spacecraft water surface takeoff control method

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Application publication date: 20180109

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