TR2021012939A1

TR2021012939A1 - CYLINDRICAL UNMANNED AERIAL VEHICLE STRUCTURE

Info

Publication number: TR2021012939A1
Application number: TR2021/012939
Authority: TR
Inventors: Gurler Tugay
Original assignee: Kiraç Havacilik Teknoloji̇ Savunma Anoni̇m Şi̇rketi̇
Filing date: 2021-08-16
Publication date: 2023-02-21

Abstract

Buluş, dikey eksende uzanan silindirik bir gövdeye haiz insansız hava aracı (drone) yapısı (1) ile ilgilidir. Daha belirgin olarak mevcut buluş silindirik gövdesi sayesinde ekseni ve merkezi belli olduğundan hareket kolaylığı (manevra kabiliyeti) ve havada asılı kalma imkanı sağlayan, alt gövde (300) kısmında bulunan bayonet bağlantısı (340) sayesinde gerektiğinde bomba, havan topu vb. gibi özel ve farklı ebatlardaki mühimmat gövdeleriyle (400) irtibatlanmaya uygun modüler bir yapı sunan, mühimmatları taşıyan ve kontrol noktasından verilen talimatlar ile istenilen yere mühimmatı bırakabilen, pervaneleri kolay çıkarılıp katılabilen bir yapıda olup kol mekanizması (200) aşağıya doğru katlanırken ayak mekanizması (500) da yukarıya doğru katlanarak termos şeklini alan ve bu sayede taşıma esnasında uçuş moduna göre daha az yer kaplayarak hem taşıma kolaylığı hem de cihazın ve aksamlarının zarar görmeden muhafaza edilmesini sağlayan bir insansız hava aracı yapısı (1) ile ilgilidir.The invention relates to an unmanned aerial vehicle (drone) structure (1) with a cylindrical body extending on the vertical axis. More specifically, the present invention can be used for bombs, mortars, etc. when necessary, thanks to the bayonet connection (340) located in the lower body (300), which provides ease of movement (maneuverability) and the ability to remain suspended in the air, thanks to its cylindrical body, as its axis and center are clear. It offers a modular structure suitable for connection with special and different sized ammunition bodies (400), such as, carries the ammunition and can drop the ammunition to the desired location with the instructions given from the control point, its propellers can be easily removed and attached, and the arm mechanism (200) folds down while the foot mechanism (500) It is about an unmanned aerial vehicle structure (1) that folds upwards and takes the shape of a thermos, thus taking up less space during transportation compared to the flight mode, enabling both ease of transportation and preservation of the device and its parts without damage.

Description

TARIFNAME SILINDIRIK INSANSIZ HAVA ARACI YAPISI Teknik Alan Bulus, dikey eksende uzanan silindirik bir gövdeye haiz insansiz hava araci (drone) yapisi ile ilgilidir. Daha belirgin olarak mevcut bulus silindirik gövdesi sayesinde ekseni ve merkezi belli oldugundan hareket kolayligi (manevra kabiliyeti) ve havada asili kalma imkani saglayan, alt gövde kisminda bulunan bayonet baglantisi sayesinde gerektiginde bomba, havan topu vb. gibi özel ve farkli ebatlardaki mühimmat gövdeleriyle irtibatlanmaya uygun modüler bir yapi sunan, mühimmatlari tasiyan ve kontrol noktasindan verilen talimatlar ile istenilen yere mühimmati birakabilen, pervaneleri kolay çikarilip katilabilen bir yapida olup kol mekanizmasi asagiya dogru katlanirken ayak mekanizmasi da yukariya dogru katlanarak termos seklini alan ve bu sayede tasima esnasinda uçus moduna göre daha az yer kaplayarak hem tasima kolayligi hem de cihazin ve aksamiarinin zarar görmeden muhafaza edilmesini saglayan bir insansiz hava araci yapisi ile ilgilidir. Teknigin Bilinen Durumu Gelistirilen teknolojiyle birlikte basta askeri alanda olmak üzere pek çok alanda insansiz hava araçlari yaygin bir sekilde kullanilmaya baslamistir. Askeri alanda kullanilan insansiz hava araçlarinda ya izleme ve görüntü alma amaçli sistemler kullanilmis ya da kamikaze görevlendirmesi ile dogrudan hedef odakli ve bombayi birakirken kendisi de imha olan yapilar kullanilmistir. Insansiz hava araçlari tasidiklari bomba yüküne ve sistemlerine göre boyutlari degismektedir. Teknigin bilinen durumundaki silahli insansiz hava araçlari genellikle büyük yapilardir. Büyüklüklerinden dolayi manevra kabiliyetleri az oldugundan tasidiklari mühimmatlari istenilen yere uzak mesafeden birakirlar, bu durum hedefin tutturulmasi ihtimalini düsürmektedir. Ayrica büyük yapilar olduklarindan dolayi hedef tarafindan kolaylikla görülmekte veya duyulmakta, bunun neticesinde mühimmat hedefi vuramadan hedefin aksiyon almasi mümkün olmaktadir. Her ne kadar güçlü mühimmatlar ve güçlü sistemler kullanilsa bile hedeflerin kaçmasina olanak verdiklerinden çogunlukla hedefler iskalanmaktadir. Ayrica bu tarz silahli insansiz hava araçlari tasima modunda oldukça yer kapladigindan tasinmasina iliskin problemleri de beraberinde getirmektedir. Askeri alandaki personel için en önemli ihtiyaçlardan biri tasinabilirlik olmasina ragmen teknigin bilinen durumundaki çözümler bu ihtiyaci karsilamamaktadir. Dahasi, askeri alandaki personel için bir diger gereklilik hiz ve manevra kabiliyeti olmasina ragmen teknigin bilinen durumundaki çözümler bu ihtiyaçlara da karsilik verememektedir. yapisindan ve buna baglanabilen bir silah yapisindan bahsedilmektedir. Silindirik bir gövde ve katlanabilen kol/ayak mekanizmalarindan bahsedilmemektedir. Sonuç olarak dikey eksende uzanan silindirik gövdesi ve bu gövde üzerine katlanabilen kol/ayak mekanizmalari sayesinde kolaylikla muhafaza edilebilir ve tasinabilir bir yapi ortaya koyan, alt gövde kisminda bulunan bayonet baglantisi sayesinde gerektiginde bomba, havan topu vb. gibi özel ve farkli ebatlardaki mühimmat gövdeleriyle irtibatlanmaya uygun modüler bir yapi sunan, havada asili kalip istenilen yere istenilen mesafeden mühimmati birakabilen, ani kaçis mekanizmasi ile kendini koruyabilen, silindirik yapisi sayesinde agirlik merkezi belli olan ve bu sayede araca manevra ve hareket kabiliyeti kazandiran bir insansiz hava araci yapisina olan ihtiyaç, mevcut bulus konusu çözümün ortaya çikmasina sebep olmustur. Bulusun Amaci Ve Kisa Açiklamasi Bulusun amaci silindirik gövdesi sayesinde ekseni ve merkezi belli oldugundan hareket kolayligi (manevra kabiliyeti) ve havada asili kalma imkani saglayan, alt gövde kisminda bulunan bayonet baglantisi sayesinde gerektiginde bomba, havan topu vb. gibi özel ve farkli ebatlardaki mühimmat gövdeleriyle irtibatlanmaya uygun modüler bir yapi sunan, mühimmatlari tasiyan ve kontrol noktasindan verilen talimatlar ile istenilen yere mühimmati birakabilen, pervaneleri kolay çikarilip katilabilen bir yapida olup kol mekanizmasi asagiya dogru katlanirken ayak mekanizmasi da yukariya dogru katlanarak termos seklini alan ve bu sayede tasima esnasinda uçus moduna göre daha az yer kaplayarak hem tasima kolayligi hem de cihazin ve aksamlarinin zarar görmeden muhafaza edilmesini saglayan bir insansiz hava araci yapisi ortaya koymaktir. Bulusun bir diger amaci, askeri bölgelerde destek unsuru olmasidir. Bulus konusu insansiz hava aracinin düsmanin bulundugu bölgeye, kendisine baglanmis mühimmat ile beraber uçurularak hedefin üzerinde görünmeden beklemesi ve kontrol noktasindan kumanda edilerek istenilen bölgeye istenilen yakinliktayken tasidigi mühimmati hedefin üzerine birakmasi saglanmaktir. Bulusun bir diger amaci alt gövdenin alt kisminda bulunan bayonet baglantisi sayesinde gerektiginde bomba, havan topu vb. gibi özel ve farkli ebatlardaki mühimmat gövdeleriyle irtibatlanmaya uygun modüler bir yapi ortaya koymaktir. Bulusun bir diger amaci silindir formundaki gövde üzerine katlanabilir kol ve ayak mekanizmalari sayesinde kolay ve güvenli bir sekilde tasinabilir, muhafaza edilebilir, portatif ve daha az yer kaplayan bir drone yapisi saglamaktir. Bulusun bir diger amaci dikey silindirik yapisi sayesinde ekseni ve merkezi belli olup yerden daha kolay kalkip hareket imkani ve havada istenilen bir noktada asili kalma imkani vermektir. Bulusun bir diger amaci bellegine yüklenen özel bir yazilim ile kamikaze görevi görebilen bir yapilanma saglamaktir ancak kamikaze sisteminden farkli olarak kendini hedefle beraber imha etmek yerine, tasidigi mühimmati biraktiktan sonra ani kaçis yapabilmekte ve böylece kendi yapisini koruyabilmektedir. Sekillerin Kisa Açiklamasi Sekil 'ilde bulus konusu silindirik insansiz hava araci yapisina ait bir patlamis perspektif görünüm verilmektedir. Sekil 2'de bulus konusu insansiz hava araci yapisinin üst gövde yapisina ait bir patlamis perspektif görünüm verilmektedir. Sekil 3"de bulus konusu insansiz hava araci yapisinin alt gövde yapisina ait bir patlamis perspektif görünüm verilmektedir. Sekil 4`de bulus konusu insansiz hava araci yapisinin kol ve ayak mekanizmalarinin aracin silindirik gövdesi üzerine katlanmis haline iliskin bir perspektif görünüm verilmektedir. Sekil 5'te bulus konusu silindirik insansiz hava araci yapisinin montajli haline iliskin bir perspektif görünüm verilmektedir. Sekil 6"da bulus konusu silindirik insansiz hava araci yapisinin montajli haline iliskin bir üst görünüm verilmektedir. Sekil 7'de bulus konusu silindirik insansiz hava araci yapisinin montajli haline iliskin bir ön görünüm verilmektedir. Referans Numaralari 1. Insansiz hava araci yapisi 100. Üst gövde 110. Anten 120. Üst kapak 130. Video görüntüleme ve iletim sistem aksamlari 140. Kol baglanti kemeri 141. Üst gövde iç iskeleti 150. GPS 200. Kol mekanizmasi 300. Alt gövde 310. Dis kabuk 320. Kamera 321. Kamera yuvasi 330. Pil 331. Pil kapagi 340. Bayonet baglantisi 400. Mühimmat gövdesi 500. Ayak mekanizmasi Bulusun Detayli Açiklamasi Bulus, silindirik gövdesi sayesinde ekseni ve merkezi belli oldugundan hareket kolayligi (manevra kabiliyeti) ve havada asili kalma imkani saglayan, alt gövde (300) kisminda bulunan bayonet baglantisi (340) sayesinde gerektiginde bomba, havan topu vb. gibi özel ve farkli ebatlardaki mühimmat gövdeleriyle (500) irtibatlanmaya uygun modüler bir yapi sunan, bir ayak kemeri baglantisi ile mühimmat gövdesiyle (500) irtibatlandirilan birden fazla ayak yapisina haiz bir ayak mekanizmasina (500) ve bir kol baglanti kemeri (140) ile üst gövde (100) ve alt gövde (300) arasina irtibatlandirilan birden fazla kol ve bunlarla iliskili en az birer adet pervane yapilarina haiz bir kol mekanizmasina (200) sahip olan, mühimmatlari tasiyan ve kontrol noktasindan verilen talimatlar ile istenilen yere mühimmati birakabilen, pervaneleri kolay çikarilip katilabilen bir yapida olup kol mekanizmasi (200) asagiya dogru katlanirken ayak mekanizmasi (500) da yukariya dogru katlanarak termos seklini alan ve bu sayede tasima esnasinda uçus moduna göre daha az yer kaplayarak hem tasima kolayligi hem de cihazin ve aksamlarinin zarar görmeden muhafaza edilmesini saglayan bir insansiz hava araci yapisi (1) ile ilgilidir. Bulus konusu yöntemin uygulandigi sistem ve bilesenleri Sekil 1 de görülmektedir. Özellikle askeri açidan bir destek unsuru olarak tasarlanan bulus konusu drone yapisi, ayni amaçla kullanilan diger drone yapilarina nazaran hacimsel olarak oldukça küçüktür. Silindirik gövdesi ve bu gövde üzerine katlanabilir bir biçimde konfigüre edilmis uzuv mekanizmalari sayesinde bir yerden bir yere tasinmasi ve muhafaza edilmesi oldukça kolaydir. Sekil 1 de görüldügü üzere bulus konusu insansiz hava araci (1) genel olarak silindirik bir forma sahip olup silindirik formda bir üst gövde (100), silindirik formda bir alt gövde (300), bahsedilen üst gövde (100) ile alt gövde (300) arasina irtibatlandirilan bir kol mekanizmasi (200), söz konusu alt gövdenin (300) alt kismina bir bayonet baglantisi (340) ile iliskilendirilen silindirik formda bir mühimmat gövdesi (400) ve bahsedilen mühimmat gövdesine (400) irtibatlandirilan bir ayak mekanizmasi (500) içermektedir. Sekil 2'de bulus konusu drone yapisinin (1) üst gövde (100) kismi verilmis olup söz konusu yapi genel olarak; - sinyalleri ve gerekli bilgileri alabilmek ve iletebilmek için anten (110) yapisi, - kontrol noktasindan drone yapisinin (1 ) yerini ve gidecegi konumu belirleyebilmek için bir GPS sistemi (150), - üst gövde (100) iskeletinin dis görüntüsünü kapatmak için üst kapak yapisi (120) - görüntüleri kaydeden ve merkeze iletimini saglayan video kayit ve iletim sistemi aksamlari (130), - kol mekanizmasinin (200) üst gövde (100) ve alt gövde (300) arasina irtibatlanmasina olanak veren bir kol baglanti kemeri (140) yapilarini içermektedir. Bulus konusu drone yapisi (1) tercihen dört kola ve her bir kolda üst üste konumlanmis vaziyette ikiser tane olmak üzere toplamda sekiz pervaneye sahiptir. Kullanici tarafindan bir noktadan kumanda edilebilen söz konusu drone yapisina (1) degerli ve farkli mühimmatlar baglanmakta, baglanan bu mühimmat yapilarini kullanici kontrolü ile istenen yere tasimakta ve talimat ile de istenen yere birakmaktadir. Mühimmat birakma islemi yakin mesafeden yapilirsa, kamikaze görev özellikleri ile gelistirilen kendine özgü yazilimi sayesinde gelistirilen ani kaçis kabiliyeti ile kamikaze yapilari gibi hedefle beraber kendini imha etmemekte (ölmemekte), ani kaçis yapabilmektedir. Bulusun resimlerde gösterilen tercih edilen yapilanmasi dört kol, sekiz pervane ve daha hafif olarak dizayn edilmis bir yapisi ile ani kaçis yapabilen bir özellige sahiptir. Bunun için pervane yapilarinin motorlari güçlendirilmistir. Güçlendirilmis motor yapilarina ragmen pervane yapilari sayesinde sessiz olmasina olanak vermektedir. Güçlü motor yapilari sayesinde hizli hareket saglayan, bu sayede yakin mesafeden mühimmati birakmasi gereken durumlarda ani kaçis yapabilen ve kendi yapisini koruyabilen bir drone yapisina (1) sahiptir. Güçlendirilmis motor yapilari sayesinde mühimmati birakirken asagiya dogru sagladigi hizli hareketi ile baski yaparak birakacagi mühimmatin hizini da arttirarak hedefin kaçmasina imkan kalmadan mühimmatin amacini gerçeklestirmesi saglanmaktadir. Sekil 3'de bulus konusu drone yapisinin (1) alt gövde (300) kismi verilmis olup görüldügü - iskelet yapilarini (141) içerisinde barindiracak bir dis kabuk (310), - bahsedilen dis kabuk (310) üzerine entegre edilebilen bir kamera yuvasi (321) ve bu yuvaya konumlandirilmis en az bir kamera (320), - pil (330) ve pil kapagi (331) yapilari - istenilen mühimmat gövdesinin (400) alt gövdeye (300) irtibatlanmasina olanak saglayan bir bayonet baglantisi (340) bilesenlerini içermektedir. farkli ebatlarda mühimmata uygun çesitli mühimmat gövdeleri (400) arasindaki modüler baglantiyi saglamaktadir. Serbest bir parça olan mühimmat gövdesi (400) alt gövdenin (300) alt kismindan takilip çevrilerek drone yapisina (1) irtibatlandirilmaktadir. Mühimmat birakilip geri geldiginde yerine farkli bir mühimmat gövdesi (400) yapisi takilabilen bir yapiya haizdir. Baska bir mühimmat takmak için var olan mühimmat gövdesi (400) çikarildiktan sonra takilacak olan mühimmat gövdesinin (400) üst kismi ile alt gövdenin (300) alt kismindaki disler söz konusu bayonet baglantisi (340) vasitasiyla kavanoz kapaginin çevrilmesine benzer sekilde birbirine irtibatlandirilip sikistirilir. Bulus konusu drone yapisi (1), katlanabilir bir sekilde dizayn edilen kol (200) ve ayak (500) mekanizmalarina sahiptir. Kol mekanizmalarinda (200) bulunan pervaneler sök ve tak seklinde rahat çikarma sistemine sahiptir ve kolayca çikarilip kutuya konabilir. Pervaneleri çikarildiktan sonra kol mekanizmalari (200) kolay bir sekilde asagiya dogru katlanabilmektedir. Drone yapisinin (1) silindirik seklinin alt gövde kisminda bulunan bosluklarina, katlanan kol mekanizmalarinda (200) bulunan motorlar denk gelmektedir ve böylece kollar katlandiginda motorlar drone yapisinin (1) üstünde çikinti gibi durmamaktadir. Motor yapilarinin fazlaliklarindan ötürü silindirik yapiya egim verilerek bosluklar birakilmistir. Ayak mekanizmalari (500) mentese ile drone yapisina (1) monte edilmistir. Ayaklar (500) yukariya dogru katlanarak toparlanmaktadir. Kol ve ayak mekanizmalari katlaninca drone yapisi (1) termos gibi küçük bir sekle sahip olmakta ve bu sekilde muhafaza edilmesi ve çantada ya da elde tasinmasi kolaylasmaktadir. Bulusun tercih edilen yapilanmasinda üst gövdeye (100) bagli anten (110) yapisi bulunmaktadir. Antenler (110) mesafeler arasinda veri iletimi için kullanilmaktadir ve drone yapisinin tasinmasini kolaylastirmak için tercihen çevrilerek sökülebilir ve geri takilabilir sekilde dizayn edilmektedir. TR TR DESCRIPTION CYLINDRICAL UNMANNED AERIAL VEHICLE STRUCTURE Technical Field The invention relates to an unmanned aerial vehicle (drone) structure with a cylindrical body extending on the vertical axis. More specifically, the present invention provides ease of movement (maneuverability) and the ability to hang in the air, thanks to its cylindrical body and its axis and center, and can be used for bombs, mortars, etc. when necessary, thanks to the bayonet connection located on the lower body. It offers a modular structure suitable for connection with special ammunition bodies of different sizes, such as: It carries the ammunition and can drop the ammunition to the desired location with the instructions given from the control point, its propellers can be easily removed and joined, and while the arm mechanism folds down, the foot mechanism folds up and takes the shape of a thermos. It is about an unmanned aerial vehicle structure that takes up less space during transportation than in flight mode, allowing both ease of transportation and preservation of the device and its components without damage. Known Status of the Technology With the developed technology, unmanned aerial vehicles have begun to be widely used in many areas, especially in the military field. In unmanned aerial vehicles used in the military field, either systems for monitoring and imaging were used, or with kamikaze assignment, structures that directly focused on the target and were destroyed while dropping the bomb were used. The dimensions of unmanned aerial vehicles vary depending on the bomb load and systems they carry. Armed unmanned aerial vehicles in the state of the art are generally large structures. Since their maneuverability is low due to their size, they drop the ammunition they carry at the desired location from a long distance, which reduces the possibility of hitting the target. In addition, since they are large structures, they can be easily seen or heard by the target, and as a result, it is possible for the target to take action before the ammunition hits the target. Even though powerful ammunition and powerful systems are used, targets are often missed because they allow the targets to escape. In addition, since such armed unmanned aerial vehicles take up a lot of space in transport mode, they also bring problems related to transportation. Although one of the most important needs for military personnel is portability, state-of-the-art solutions do not meet this need. Moreover, although another requirement for personnel in the military field is speed and maneuverability, state-of-the-art solutions cannot meet these needs either. Its structure and a weapon structure that can be connected to it are mentioned. A cylindrical body and foldable arm/leg mechanisms are not mentioned. As a result, it provides an easily stored and portable structure thanks to its cylindrical body extending on the vertical axis and arm/leg mechanisms that can be folded on this body, and can be used for bombs, mortars, etc. when necessary, thanks to the bayonet connection on the lower body. It is an unmanned aerial vehicle that offers a modular structure suitable for connection with special and different-sized ammunition bodies such as, can hang in the air and drop ammunition to the desired location from a desired distance, can protect itself with a sudden escape mechanism, has a clear center of gravity thanks to its cylindrical structure and thus provides the vehicle with maneuverability and mobility. The need for an intermediary structure led to the emergence of the solution that is the subject of the present invention. Purpose and Brief Description of the Invention The purpose of the invention is to provide ease of movement (maneuverability) and the ability to hang in the air, thanks to its cylindrical body, with its axis and center being clear, and to be used for bombs, mortars, etc. when necessary, thanks to the bayonet connection located on the lower body. It offers a modular structure suitable for connection with special ammunition bodies of different sizes, such as: It carries the ammunition and can drop the ammunition to the desired location with the instructions given from the control point, its propellers can be easily removed and joined, and while the arm mechanism folds down, the foot mechanism folds up and takes the shape of a thermos. In this way, the aim is to create an unmanned aerial vehicle structure that takes up less space during transportation compared to the flight mode, allowing both ease of transportation and preservation of the device and its parts without damage. Another purpose of the invention is to be a support element in military areas. The subject of the invention is to ensure that the unmanned aerial vehicle is flown to the enemy's location with the ammunition attached to it, waits unseen over the target, and is controlled from the control point to drop the ammunition it carries onto the target while it is at the desired proximity to the desired area. Another purpose of the invention is to launch bombs, mortars, etc. when necessary, thanks to the bayonet connection located at the bottom of the lower body. It is to create a modular structure suitable for connection with ammunition bodies of special and different sizes, such as Another aim of the invention is to provide a drone structure that can be easily and safely carried, stored, portable and takes up less space, thanks to its foldable arm and foot mechanisms on a cylindrical body. Another purpose of the invention is to provide the opportunity to get up and move more easily from the ground and to hang at a desired point in the air, thanks to its vertical cylindrical structure, with a clear axis and center. Another aim of the invention is to provide a structure that can act as a kamikaze with a special software loaded into its memory. However, unlike the kamikaze system, instead of destroying itself with the target, it can make a sudden escape after releasing the ammunition it carries and thus protect its own structure. Brief Description of the Drawings The figure shows an exploded perspective view of the cylindrical unmanned aerial vehicle structure that is the subject of the invention. Figure 2 shows an exploded perspective view of the upper body structure of the unmanned aerial vehicle structure that is the subject of the invention. Figure 3 shows an exploded perspective view of the lower body structure of the unmanned aerial vehicle structure that is the subject of the invention. Figure 4 gives a perspective view of the arm and foot mechanisms of the unmanned aerial vehicle structure that is the subject of the invention folded onto the cylindrical body of the vehicle. Figure 5 shows A perspective view of the assembled cylindrical unmanned aerial vehicle structure that is the subject of the invention is given. Figure 6 shows a top view of the assembled cylindrical unmanned aerial vehicle structure that is the subject of the invention. Figure 7 shows a front view of the assembled cylindrical unmanned aerial vehicle structure of the invention. Reference Numbers 1. Unmanned aircraft structure 100. Upper body 110. Antenna 120. Upper cover 130. Video imaging and transmission system components 140. Arm attachment belt 141. Upper body internal skeleton 150. GPS 200. Arm mechanism 300. Lower body 310 . Outer shell 320. Camera 321. Camera housing 330. Battery 331. Battery cover 340. Bayonet connection 400. Ammunition body 500. Foot mechanism Detailed Description of the Invention The invention provides ease of movement (maneuverability) and in the air as its axis and center are clear thanks to its cylindrical body. Thanks to the bayonet connection (340) located on the lower body (300), which allows it to be suspended, it can be used to carry bombs, mortars, etc. when necessary. It has a foot mechanism (500) with multiple foot structures that are connected to the ammunition body (500) with a foot belt connection, and an upper body with an arm connection belt (140), which offers a modular structure suitable for connection with ammunition bodies (500) of special and different sizes, such as Having an arm mechanism (200) with multiple arms connected between the (100) and the lower body (300) and at least one propeller structure associated with them, carrying the ammunition and being able to drop the ammunition to the desired location with the instructions given from the control point, and having propellers that can be easily removed and assembled. It is an unmanned unmanned vehicle that has a structure and the arm mechanism (200) folds downwards, while the foot mechanism (500) folds upwards, taking the shape of a thermos, thus taking up less space during transportation compared to the flight mode, ensuring both ease of transportation and preservation of the device and its parts without damage. It is related to the aircraft structure (1). The system and its components where the method subject to the invention is applied can be seen in Figure 1. The drone structure of the invention, designed especially as a military support element, is quite small in volume compared to other drone structures used for the same purpose. It is very easy to carry and store from one place to another, thanks to its cylindrical body and limb mechanisms foldable on this body. As seen in Figure 1, the unmanned aerial vehicle (1) of the invention generally has a cylindrical form and consists of an upper body (100) in cylindrical form, a lower body (300) in cylindrical form, the said upper body (100) and the lower body (300). It includes an arm mechanism (200) connected between the lower body (300), a cylindrical ammunition body (400) connected to the lower part of the said lower body (300) with a bayonet connection (340), and a foot mechanism (500) connected to the said ammunition body (400). In Figure 2, the upper body (100) part of the drone structure (1) subject to the invention is given, and the structure in question is generally; - antenna (110) structure to receive and transmit signals and necessary information, - a GPS system (150) to determine the location and destination of the drone structure (1) from the control point, - upper cover structure to cover the external view of the upper body (100) skeleton. (120) - video recording and transmission system components (130) that record the images and ensure transmission to the center, - an arm connection belt (140) structures that allow the arm mechanism (200) to be connected between the upper body (100) and the lower body (300). . The drone structure (1) that is the subject of the invention preferably has four arms and a total of eight propellers, two of which are positioned one above the other on each arm. Valuable and different ammunition is connected to the said drone structure (1), which can be controlled from a point by the user, and it carries these connected ammunition structures to the desired location with user control and drops them to the desired location with instructions. If the ammunition dropping process is done from close range, the kamikaze does not self-destruct (die) with the target like kamikaze structures, and can make a sudden escape with the sudden escape ability developed thanks to its unique software developed with its mission features. The preferred embodiment of the invention shown in the pictures has a feature that allows sudden escape with four arms, eight propellers and a lighter structure. For this purpose, the engines of the propeller structures have been strengthened. Despite its reinforced engine structure, it allows it to be silent thanks to its propeller structures. It has a drone structure (1) that provides fast movement thanks to its powerful engine structure, thus being able to make sudden escapes and protect its own structure in situations where it needs to drop ammunition from close range. Thanks to its reinforced engine structure, it increases the speed of the ammunition it releases by applying pressure with its fast downward movement while releasing the ammunition, thus ensuring that the ammunition achieves its purpose without allowing the target to escape. In Figure 3, the lower body (300) part of the drone structure (1) subject to the invention is shown and it is seen - an outer shell (310) that will accommodate the skeletal structures (141), - a camera slot (321) that can be integrated on the said outer shell (310). ) and at least one camera (320) positioned in this slot, - battery (330) and battery cover (331) structures - a bayonet connection (340) components that allow the desired ammunition body (400) to be connected to the lower body (300). It provides modular connection between various ammunition bodies (400) suitable for ammunition of different sizes. The ammunition body (400), which is a free part, is attached to the lower part of the lower body (300), turned and connected to the drone structure (1). It has a structure that can be replaced with a different ammunition body (400) structure when the ammunition is dropped and returned. After the existing ammunition body (400) is removed to mount another ammunition, the upper part of the ammunition body (400) to be installed and the teeth on the lower part of the lower body (300) are connected and tightened together by means of the bayonet connection (340), similar to turning a jar lid. The drone structure (1) that is the subject of the invention has arm (200) and foot (500) mechanisms designed to be foldable. The propellers in the arm mechanisms (200) have an easy disassembly system and can be easily removed and placed in the box. After the propellers are removed, the arm mechanisms (200) can be easily folded downwards. The motors located in the folding arm mechanisms (200) correspond to the cavities in the lower body part of the cylindrical shape of the drone structure (1), and thus, when the arms are folded, the motors do not stand like a protrusion on the drone structure (1). Due to the redundancy of the engine structures, gaps were left by sloping the cylindrical structure. The foot mechanisms (500) are mounted on the drone structure (1) with a hinge. The legs (500) are folded upwards and collected. When the arm and foot mechanisms are folded, the drone structure (1) becomes small like a thermos, making it easier to store and carry in a bag or hand. In the preferred embodiment of the invention, there is an antenna (110) structure connected to the upper body (100). Antennas (110) are used for data transmission across distances and are designed to be detachable and reattachable, preferably by turning them, to facilitate transportation of the drone structure. TR TR

Claims

1. It is an unmanned aerial vehicle structure (1) and its features are; - an upper body (100) in cylindrical form, a lower body (300) in cylindrical form, an arm mechanism (200) connected between the said upper body (100) and the lower body (300), a lever mechanism (200) connected to the lower part of the said lower body (300). It is characterized by containing an ammunition body (400) in cylindrical form and a foot mechanism (500) connected to the said ammunition body (400) and - the said unmanned aerial vehicle structure (1) is characterized by having a cylindrical form extending on the vertical axis.

2. It is an unmanned aerial vehicle structure (1) according to claim 1, and its feature is; It contains a bayonet connection (340) that allows modular connection between the lower body (300) and the ammunition body (400).

3. It is an unmanned aerial vehicle structure (1) according to claim 1 or 2, and its feature is; downwards of the said arm mechanism (200); It is characterized by the fact that the foot mechanism (500) can be folded upwards onto the cylindrical unmanned aerial vehicle structure (1).