TR201722780A2 - AUTONOMOUS UNMANNED AERIAL VEHICLE INTEGRATION AND SYSTEM CAPABLE OF HYBRID SPRAYING - Google Patents
AUTONOMOUS UNMANNED AERIAL VEHICLE INTEGRATION AND SYSTEM CAPABLE OF HYBRID SPRAYING Download PDFInfo
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- TR201722780A2 TR201722780A2 TR2017/22780A TR201722780A TR201722780A2 TR 201722780 A2 TR201722780 A2 TR 201722780A2 TR 2017/22780 A TR2017/22780 A TR 2017/22780A TR 201722780 A TR201722780 A TR 201722780A TR 201722780 A2 TR201722780 A2 TR 201722780A2
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- unmanned aerial
- aerial vehicle
- motor
- spraying
- multirotor
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- 238000005507 spraying Methods 0.000 title claims abstract description 20
- 230000010354 integration Effects 0.000 title description 2
- 239000007788 liquid Substances 0.000 claims description 7
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 4
- 230000005540 biological transmission Effects 0.000 claims description 2
- 238000003973 irrigation Methods 0.000 abstract description 7
- 230000002262 irrigation Effects 0.000 abstract description 7
- 239000007921 spray Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 238000005265 energy consumption Methods 0.000 description 2
- 239000000575 pesticide Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000010152 pollination Effects 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
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- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01B—SOIL WORKING IN AGRICULTURE OR FORESTRY; PARTS, DETAILS, OR ACCESSORIES OF AGRICULTURAL MACHINES OR IMPLEMENTS, IN GENERAL
- A01B79/00—Methods for working soil
- A01B79/005—Precision agriculture
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01C—PLANTING; SOWING; FERTILISING
- A01C21/00—Methods of fertilising, sowing or planting
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/20—Vertical take-off and landing [VTOL] aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/40—UAVs specially adapted for particular uses or applications for agriculture or forestry operations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/45—UAVs specially adapted for particular uses or applications for releasing liquids or powders in-flight, e.g. crop-dusting
Abstract
Buluş, tarımsal amaçlarla sulama ya da ilaçlama yapabilen farklı kanat yapılarına sahip bir otonom insansız hava aracına ilişkindir. Buluşa konu insansız hava aracı sisteminin farklı kanat yapılarına sahip olması sayesinde, ileri yönde oluşan hareketlerde kanatların kaldırıcı kuvvet oluşturması ile daha az enerji harcanarak ileri manevra yapılmasını, daha uzun uçuş süresi ve uçuş menzili elde edilmesini ve geniş spreyleme alanına sahip olunmasını sağlamaktadır.The invention relates to an autonomous unmanned aerial vehicle with different wing structures capable of irrigation or spraying for agricultural purposes. Since the unmanned aircraft system of the present invention has different wing structures, it enables the forward maneuvering with less energy consumed by the lifting of the wings in forward movements, providing longer flight time and flight range and having a large spraying area.
Description
TARIFNAME HIBRIT SPREYLEME YAPABILEN OTONOM INSANSIZ HAVA ARACI ENTEGRESI VE SISTEMI Bulusun Konusu Bulus, tarimsal amaçlarla sulama ya da ilaçlama yapabilen farkli kanat yapilarina sahip, hibrit spreyleme yapabilen otonom insansiz hava araci entegresi ve sistemine iliskindir. DESCRIPTION AUTONOMOUS UNMANNED AERIAL VEHICLE WITH HYBRID SPRAYING INTEGRATED AND SYSTEM Subject of the Invention Invention, irrigation or pesticide application for agricultural purposes. with different wing structures, capable of hybrid spraying It relates to autonomous unmanned aerial vehicle integration and system.
Teknigin Bilinen Durumu Tarimsal alanlarda zirai ilaçlama ya da sulama yapmak ya da herhangi bir durum için havadan spreyleme yapmak amaciyla insanli veya insansiz hava araci sistemleri kullanilmaktadir. State of the Art To carry out agricultural spraying or irrigation in agricultural areas, or for aerial spraying for any situation manned or unmanned aerial vehicle systems are used.
Fakat insanli araçlarin boyutu, maliyeti ve olusturdugu karbon ayak izi, bitkiler üzerinde biraktigi zararli egzoz kalintilari gibi sorunlar sebebiyle son zamanlarda insansiz hava araçlarina olan ilgi artmistir. Önceki teknikte, insansiz hava araci sistemleri için quadcopter, hexacopter, oktocopter veya helikopter kullanilmaktadir. Araçlarin gövdelerinde gerekli görülen yerde bulunan depodan alinan sivi motorlarda olusan rüzgar veya basinç farki ile püskürtülmektedir. Bu sistem de her ne kadar belirli bir miktarda yük tasinabiliyor olsa da gerekli pratik kullanisliligi saglayamamaktadir. Bu sistemlerde mevcut olan püskürtme alanlarinin tek seferde taradigi etki alanlarinin sinirli olmasi dezavantaj yaratmaktadir. However, the size, cost and nature of manned vehicles carbon footprint, harmful exhaust it leaves on plants unmanned recently due to problems such as The interest in aircraft has increased. In the prior art, for unmanned aerial vehicle systems quadcopter, hexacopter, octocopter or helicopter is used. Necessary on the bodies of vehicles the wind in the liquid motors taken from the warehouse on the ground or sprayed with pressure difference. What is this system Although a certain amount of cargo can be carried, it is necessary cannot provide practical use. In these systems the effect that the existing spray areas are scanned in one go limited areas create a disadvantage.
Hava araci sistemlerinde, enerjinin büyük bir kisminin kalkis ve inislerde harcandigi bilinmektedir. Buna göre, özellikle döner kanatli sistemlerin sürekli seviyelerini korumak için tek kuvvet olusturacak itkiyi motorlardan saglamakta oldugu görülmektedir. Bu durumda, hava araci sistemlerinde kalkis sirasinda ilave bir kuvvete ihtiyaç duyulmaktadir. Bu sayede, daha az enerji harcanarak kalkis saglanacak. ve kazanilan enerji ile daha uzun bir uçus menzili elde edilecektir. Ancak, teknigin bilinen durumunda bu amaç dogrultusunda gelistirilen hava araci sistemleri bulunmamaktadir. In aircraft systems, most of the energy is taken off. and is known to be spent on the descents. Accordingly, especially to maintain constant levels of rotary vane systems that it provides the thrust that will create the only force from the engines. is seen. In this case, the aircraft systems take-off additional force is required. In this way, take-off will be achieved by consuming less energy. and earned A longer flight range will be achieved with energy. However, developed for this purpose in the state of the art There are no aircraft systems.
Teknigin bilinen durumunda yer alan dokümanlara örnek olarak asagida açiklanan dokümanlar verilebilir. Examples of documents in the state of the art The documents described below can be given.
CN205239920U sayili faydali model dokümanina konu bulus, tarimsal spreylemenin kalitesini ve verimliligini artirmak amaciyla gelistirilmis bir insansiz hava aracina iliskindir. The invention, which is the subject of the utility model document numbered CN205239920U, improve the quality and efficiency of agricultural spraying It relates to an unmanned aerial vehicle developed for the purpose of
Bulusa konu bu insansiz hava aracinin avantajlari, su tankinin içerisinde bulunan su pompasi sayesinde püskürtücülerden iletilen suyun akis hizinin ve spreyleme alaninin arttirilmasi ve rüzgardan etkilenmeyen yüksek kalitede spreyleme performansi elde edilmesi olarak siralanabilir. The advantages of this unmanned aerial vehicle, which is the subject of the invention, are from the sprayers thanks to the water pump in it. the flow rate of the delivered water and the spray area. high quality, not affected by wind It can be listed as obtaining spraying performance.
Fakat bu bulusta aracin kalkis gücüne destek olacak sabit kanatlar yer almamaktadir. However, in this invention, there is a constant that will support the starting power of the vehicle. wings are not included.
CNlO6069596A. nolu dokümana konu bulus, en genel haliyle, tarimsal sulama faaliyetleri için gelistirilmis bir insansiz hava aracina iliskindir. Bulusa konu insansiz hava araci, bir gövde, uçus mekanizmasi, güç mekanizmasi, sulama mekanizmasi ve destek çerçevesi içermektedir. Tarimsal alanlarda insansiz hava araci kullanima yönelik olan bu patent dokümaninda, aracin kolay hareket etmesine, havalanmasina ya da püskürtme alan genisletilerek daha genis bir etki alanina sahip olunmasina iliskin bir gelistirmeden bahsedilmemektedir. CN106069596A. The invention, which is the subject of the document no., in its most general form, An unmanned aerial vehicle developed for agricultural irrigation activities. pertaining to the aircraft. The subject of the invention is the unmanned aerial vehicle, a fuselage, flight mechanism, power mechanism, irrigation mechanism and support frame. unmanned in agricultural areas In this patent document for aircraft use, allowing the vehicle to move easily, take off or spray. by expanding the area to have a wider range of influence No development is mentioned.
Bilgileri verilen bu dokümanlarda anlatilan buluslarin, kalkis gücüne destek verecek kanat yapisina ya da daha genis alana spreyleme saglayacak bir püskürtme sistemi yapisina iliskin gelistirmelere sahip olmadigi böylelikle teknigin bilinen durumunda yer alan dezavantajlarin devam ettigi görülmektedir. Bu durumda, bu dezavantajlari ortadan kaldiracak inis kalkislarda daha az enerji harcayan, daha ekonomik bir spreyleme sistemine sahip bir insansiz hava araci sistemine ihtiyaç duyulmaktadir. The inventions described in these documents, the information of which is given, wing structure or wider to support take-off power a spray system structure that will provide spraying to the area. Thus, the technique does not have the related developments. known disadvantages persist is seen. In this case, these disadvantages are eliminated. consuming less energy in take-offs and landings, an unmanned aerial vehicle with an economical spraying system system is needed.
Basvuruya konu bulus, bu dezavantajlari ortadan kaldiracak kalkis gücüne destek saglayacak egimli yüzeylere ve püskürtme alanini genisletecek yapiya sahip kanatlar içeren hibrit spreyleme yapabilen bir otonom insansiz hava araci sistemi sunmaktadir. The invention subject to the application will eliminate these disadvantages. Inclined surfaces and spraying to support the take-off power hybrid with wings to expand its range an autonomous drone system capable of spraying offers.
Bulusun Detayli Açiklamasi Bulus, tarimsal amaçlarla sulama ya da ilaçlama yapabilen farkli kanat yapilarina sahip bir otonom insansiz hava aracina iliskindir. Söz konusu bulus, hem hareketli(döner) hem sabit yapilara sahip olmasi sayesinde, ileri yönde olusan hareketlerde kanatlarin kaldirici kuvvet olusturmasi ile daha az enerji harcanarak ileri manevra yapilmasini ve daha uzun uçus süresi ve uçus menzili elde edilmesini saglamaktadir. Detailed Description of the Invention Invention, irrigation or pesticide application for agricultural purposes. an autonomous unmanned aerial vehicle with different wing structures is related. The invention in question is both mobile (rotating) and stationary. Thanks to its structures, the forward-looking with the lifting force of the wings in the movements, It allows forward maneuvering with less energy consumption and longer It provides flight time and flight range.
Döner kanatli (12) yapisi ile dikey kalkis kolayligi ve sabit kanatli (4) yapisi ile süzülebilme imkani sunmaktadir. Bulusa konu insansiz hava aracinda, istenilen genislikte ve aralikta siralanabilen fiskiye (2) elemanlari bulunmaktadir. Bu fiskiye (2) elemanlari sayesinde, aracin kullanini amacina göre (sulama ya da ilaçlama gibi) depoda (5) bekletilen sivinin disari salinimi gerçeklestirilmektedir. Bulus ile fiskiye (2) elemanlarinin gelistirilmesi sonucu, daha genis bir alana sivi salinimi yapilarak etki alani genisletilmektedir. Ease of vertical take-off with its rotating wing (12) structure and stable It offers the possibility of gliding with its winged (4) structure. find it The subject is in the unmanned aerial vehicle, in the desired width and range. There are sprinkler (2) elements that can be sorted. This Thanks to the sprinkler (2) elements, the vehicle can be used for its intended purpose. kept in the warehouse (5) (such as irrigation or spraying) according to the fluid is released out. with the invention As a result of the improvement of the fountain (2) elements, a wider area of influence by releasing liquid to an area is being expanded.
Basvuruya ait bulusa konu insansiz hava araci, en temel haliyle, gerekli mekanik enerjiyi saglayan multirotor motor (1), spreyleme ile sivinin iletimini saglayan fiskiyeler (2), motor tutacaklari (3), sabit kanat (4) spreyleme yapilacak siviyi barindiran depo (tank) (5), depo (5) içerisinde bulunan siviyi fiskiyelere (2) ileten pompa, dikey kalkis hareketli motor (6), servo motor ve pin seti (7), ESC motor kontrolcüsü (8), Li-Po Batarya (9), aracin uçusu ve kontrolünden sorumlu olan otonom uçus kontrol sistemi (10) ve multirotor pervaneleri (ll) elemanlarindan olusmaktadir. The unmanned aerial vehicle, which is the subject of the invention of the application, is the most basic Thus, the multirotor motor providing the necessary mechanical energy (1), sprinklers that provide the transmission of liquid by spraying (2), motor handles (3), fixed blade (4) to be sprayed the tank (tank) (5) containing the liquid, the tank (5) The pump, which transmits the liquid to the fountains (2), has vertical lift action. motor (6), servo motor and pin set (7), ESC motor controller (8), Li-Po Battery (9), responsible for the flight and control of the vehicle autonomous flight control system (10) and multirotor It consists of propellers (ll) elements.
Bulusun bir yapilandirmasinda, depo (5) araç üzerinde gövdenin agirlik merkezine yakin bir bölgede bulunmaktadir. In one embodiment of the invention, the tank (5) is on the vehicle. It is located in a region close to the center of gravity of the body.
Otononi uçus kontrol sistemi (10), gerekli kararlara göre sonuçlar vererek aracin istenen sekilde görevini icra etmesini saglamaktadir. Multirotor pervaneleri (11), multirotor` motor (1) için kullanilan pervanelerdir. Servo motorlar bir yüzeyi veya yapiyi kontrol etmek için kullanilmaktadir. The autonomous flight control system (10) By giving results, the vehicle performs its task as desired. makes it possible. Multirotor propellers (11), These are the propellers used for the multirotor' motor (1). Servo motors to control a surface or structure is used.
Bulusun bir yapilandirmasinda, gerekli elektrik enerjisinin depolandigi Lityum-Polimer piller (Li-Po Batarya (9)) kullanilmaktadir. In one embodiment of the invention, the required electrical energy Lithium-Polymer batteries (Li-Po Battery (9)) is used.
Bulusun bir yapilandirmasinda, sabit kanatli (4) yapinin altina yerlestirilen fiskiyelerin (2) arasinda bulunan açikliklar kullanim amacina göre ayarlanabilmektedir. Bu açikliklarin ve yerlestirilen fiskiye (2) sayisinin ayarlanmasi gerekli pratikligi saglamaktadir. In one embodiment of the invention, the fixed wing (4) structure located between the sprinklers (2) placed under openings can be adjusted according to the purpose of use. This of the openings and the number of sprinklers (2) placed adjustment provides the necessary practicality.
Bulusa konu insansiz hava aracinin önemli özellikleri, döner kanatlara (12) ek olarak kalkis gücüne destek veren egimli yüzeylere sahip sabit kanatlar (4) içermesi ve sabit kanatlarin (4) altinda bir uçtan diger uca kadar yerlestirilmis olan fiskiyelere (2) sahip olmasidir. Bulusa konu insansiz hava aracinin hem döner kanatli (12) hem sabit kanatli (4) yapiya sahip olmasi (hibrit olmasi); ileriye dogru olusan hareketlerde kanadin kaldirici kuvvet olusturmasi sayesinde daha az enerji harcanmasini, ileriye manevra yapilmasini ve uçus zamanina bir miktar katki saglayarak uçus menzilinin arttirilmasini saglamaktadir. Insansiz hava aracinin sahip oldugu döner kanatlar (12) ile dikey kalkis(VTOL) yapabilen ve sabit kanatlar (4) ile süzülebilen bir yapiya sahip olmasi araca önceki teknikte var olan enerji tüketimine yönelik problemlerin ortadan kaldirilmasina büyük katki saglamaktadir. The important features of the unmanned aerial vehicle subject to the invention are In addition to the wings (12), it is inclined to support the take-off power. fixed blades (4) with surfaces and under the wings (4) from one end to the other It has sprinklers (2) placed on it. find it The subject is unmanned aerial vehicle with both rotary wing (12) and fixed having a winged (4) structure (hybrid); forward creating a lifting force of the wing in the movements that occur Thanks to less energy consumption, forward maneuvering flight by making some contribution to the flight time and it increases the range. unmanned air vertical with the rotating blades (12) of the vehicle. capable of take-off (VTOL) and gliding with fixed wings (4) having a structure gives the vehicle the energy existing in the previous art. great effort to eliminate the problems related to consumption it contributes.
Bulusa konu sistemin sahip oldugu sabit kanatlar (4), genis alanda spreyleme imkani tanimasinin yaninda aracin ileriye dogru olusan hizlardan dogan tasima kuvvetine katki saglamaktadir. Sabit kanat (4) yapilari egimli yüzeylerden meydana gelmekte olup, bir airfoil kanat yapisi içermektedir. The fixed wings (4) of the inventive system are wide In addition to the possibility of spraying in the area, the vehicle can be moved forward. Contribution to the transport force arising from the correct velocities it provides. Fixed blade (4) structures are made of inclined surfaces. consists of an airfoil blade structure.
Bu kanat yapisi sayesinde Bernoulli ilkesinden faydalanarak aracin ileriye dogru hizlanmasinda kanattan kaldirma kuvveti kazanmasi saglanmaktadir. Kazanilan bu kuvvet sayesinde multirotor Hmtorlara UJ ve nmltirotor pervanelerine (ll) gereken yük azaltilmakta ve verimlilige katki saglanmaktadir. Thanks to this wing structure, it takes advantage of Bernoulli's principle. lift from the wing when accelerating the vehicle forward is assured to win. Thanks to this strength gained to multirotor Hmtors UJ and nmltirotor propellers (ll) the required load is reduced and it contributes to efficiency.
Bulusa konu gelistirilen insansiz hava araci sisteminin enerji kazancina yönelik sagladigi avantajlarin yaninda, sahip oldugu genis sabit kanatlarin (4) alt kisminin boylu boyunca dizilmis fiskiyelerden (2) olusmasi sayesinde, spreyleme yapilacak etki alaninda artis saglanmaktadir. Sabit kanatlarin (4) kullanimi, daha fazla fiskiye (2) yerlestirilmesi için bir alan olusturmakta. ve daha fazla fiskiye (2) kullanilmasi ise insansiz hava aracinin bir seferde daha fazla alani tarayarak spreyleme yapmasina olanak tanimaktadir. Özetle bulus, tarimsal spreyleme için multirotorlu otonom bir insansiz hava araci olup; dikey kalkis yapabilmesini saglayan birden fazla döner kanat (12) ve bu döner kanatlara (12) bagli birden fazla dikey kalkis hareketli motor (6), kanattan kaldirma kuvveti kazanilmasina imkan veren egimli yüzeylere (airfoil kanat yapisina) sahip bir sabit kanat (4) sistemi, spreyleme için sabit kanatlarin (4) üzerinde aralikli olarak yer alan fiskiyeler (2) içermektedir. The unmanned aerial vehicle system developed as the subject of the invention In addition to the advantages it provides for energy gain, the length of the lower part of the wide fixed wings (4) it has Thanks to the fact that it consists of sprinklers (2) lined up along it, an increase in the effect area to be sprayed is provided. Still use of blades (4), more sprinklers (2) It creates an area for placement. and more Using the sprinkler (2) is a part of the unmanned aerial vehicle. Allows it to spray by scanning more areas at once. knows. In summary, the invention is an autonomous multirotor for agricultural spraying. is an unmanned aerial vehicle; enabling vertical take-off more than one rotating blade (12) and connected to these rotating blades (12) more than one vertical take-off motor (6), from the wing on inclined surfaces that allow gaining buoyancy a fixed wing (4) system with (airfoil wing structure), intermittently on the fixed vanes (4) for spraying The fountains (2) are located.
Bulusa konu sistemin sahip oldugu bu avantajlara ilave olarak, bitkileri havadan nemlendirmede kullanilmasi ve bitkilerin tozlasma olayina katkida bulunmasi gibi özelliklerinin bulundugu belirtilebilir. In addition to these advantages of the inventive system, use of plants to humidify plants from the air and properties such as contributing to pollination can be specified.
Sekillerin Açiklamalari Sekil-1 Bulusa Konu Insansiz Hava Aracinin Üst Yüzden Görünümü Sekil-2 Bulusa Konu Insansiz Hava Aracinin Perspektif Görünümü Sekil-3 Bulusa Konu Insansiz Hava Aracinin Ön Yüzden Görünümü Sekil-4 Bulusa Konu Insansiz Hava Aracinin Yan Yüzden Görünümü Sekil-5 Bulusa Konu Insansiz Hava Aracinin Patlatilmis Görünümü Sekillerde Yer Alan Referans Numaralarinin Açiklamalari .Multirotor motor . Fiskiye .Motor tutacaklari .Sabit kanat .Depo(tank) .Dikey kalkis hareketli motor .Servo motor ve pin seti .ESC motor kontrolcüsü .Li-Po Batarya . Otonom uçus kontrol sistemi 11. Multirotor pervanesi 12. Döner kanatlar Descriptions of Figures Figure-1 Top Side View of the Unmanned Aerial Vehicle Subject to the Invention Figure-2 Perspective of the Unmanned Aerial Vehicle Subject to the Invention view Figure-3 Front Side View of the Unmanned Aerial Vehicle Subject to the Invention Figure-4 Side View of the Unmanned Aerial Vehicle Subject to the Invention Figure-5 Explosion of the Unmanned Aerial Vehicle Subject to the Invention view Explanations of Reference Numbers in the Figures .Multirotor motor . Fountain .Engine holders .Fixed wing .Storage(tank) .Vertical start-up motor .Servo motor and pin set .ESC motor controller .Li-Po Battery . autonomous flight control system 11. Multirotor propeller 12. Rotating wings
Claims (1)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TR2017/22780A TR201722780A2 (en) | 2017-12-29 | 2017-12-29 | AUTONOMOUS UNMANNED AERIAL VEHICLE INTEGRATION AND SYSTEM CAPABLE OF HYBRID SPRAYING |
| PCT/TR2018/050951 WO2019212439A2 (en) | 2017-12-29 | 2018-12-31 | Autonomous unmanned aerial vehicle integration and system performing hybrid spraying |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TR2017/22780A TR201722780A2 (en) | 2017-12-29 | 2017-12-29 | AUTONOMOUS UNMANNED AERIAL VEHICLE INTEGRATION AND SYSTEM CAPABLE OF HYBRID SPRAYING |
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| Publication Number | Publication Date |
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| TR201722780A2 true TR201722780A2 (en) | 2018-03-21 |
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| TR2017/22780A TR201722780A2 (en) | 2017-12-29 | 2017-12-29 | AUTONOMOUS UNMANNED AERIAL VEHICLE INTEGRATION AND SYSTEM CAPABLE OF HYBRID SPRAYING |
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| WO (1) | WO2019212439A2 (en) |
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| US11919630B2 (en) * | 2019-08-16 | 2024-03-05 | Textron Systems Corporation | Separated lift-thrust VTOL aircraft with articulated rotors |
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| IL199009A (en) * | 2009-05-27 | 2013-11-28 | Israel Aerospace Ind Ltd | Air vehicle |
| US10183744B2 (en) * | 2016-02-10 | 2019-01-22 | Lockheed Martin Corporation | Magnetic orientation detent |
| CN206255196U (en) * | 2016-12-13 | 2017-06-16 | 广东合即得能源科技有限公司 | A kind of fixed-wing unmanned plane for spraying insecticide |
| CN206476119U (en) * | 2017-02-15 | 2017-09-08 | 江西中轻智能设备有限公司 | It is a kind of from rotor plant protection unmanned plane |
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| WO2019212439A2 (en) | 2019-11-07 |
| WO2019212439A3 (en) | 2019-12-05 |
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