TWI640455B - Flying device - Google Patents
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- TWI640455B TWI640455B TW106139758A TW106139758A TWI640455B TW I640455 B TWI640455 B TW I640455B TW 106139758 A TW106139758 A TW 106139758A TW 106139758 A TW106139758 A TW 106139758A TW I640455 B TWI640455 B TW I640455B
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Abstract
本發明關於一種飛行載具。該飛行載具包括一飛行本體及至少一接頭組件。該飛行本體設有至少一供定位一箱體之連結單元及一管路單元。各該接頭組件設有一插接組件及一座體組件,該插接組件選擇性地插設連通該座體組件,該插接組件及該座體組件其中一者係供設於該箱體且連通該箱體之內部、另者則係設於該飛行本體且連通該管路單元。其中,當該箱體結合定位於該飛行本體時,該插接組件插設於該座體組件,該箱體之內部透過該接頭組件而連通該管路單元。The invention relates to a flying vehicle. The flying vehicle includes a flying body and at least one joint assembly. The flight body is provided with at least one connecting unit for positioning a box body and a pipeline unit. Each of the connector assemblies is provided with a plug assembly and a body assembly. The plug assembly is selectively inserted into the base assembly, and one of the plug assembly and the base assembly is disposed in the cabinet and connected The inside of the box is provided on the flight body and communicates with the pipe unit. Wherein, when the box is coupled to the flying body, the plug component is inserted into the seat assembly, and the inside of the box communicates with the pipeline unit through the joint assembly.
Description
本發明係有關於一種飛行載具。The invention relates to a flying vehicle.
隨著科技的進步,遙控飛機也有重大突破,除了提升其飛行穩定性、操控性及結構強度以外,更對各種不同領域而附加有不同功能。舉例來說,近期之電影--看見台灣,即是將遙控飛機設計成空拍機,由鳥的觀點來俯看世界,提供不同於一般攝影的視覺效果,而受到廣大民眾喜愛,進而掀起一股空拍機的熱潮。With the advancement of technology, remote-controlled aircraft has also made major breakthroughs. In addition to improving its flight stability, handling and structural strength, it has added different functions to various fields. For example, the recent film--seeing Taiwan, is to design a remote-controlled aircraft as an aerial camera, from the bird's point of view to look down at the world, to provide a visual effect different from the general photography, and to be loved by the general public, and then pick up one The boom in the stock market.
可以理解的,遙控飛機之功用不僅可做於空拍用,更可佳貼近各種行業所需,舉例來說,傳統務農人家在噴灑農藥時,皆是身體背負藥桶而行走於田中,如台灣專利M500457即是。然而,此種噴灑方式,使得使用者常常在噴灑的過程中不斷地吸入農藥,造成身體上的傷害;並且,此噴灑方式之效率不彰、噴灑時間冗長、藥劑無法平均分布於田裡,存在亟待改善之缺弊。Understandably, the function of the remote control aircraft can be used not only for the aerial photography, but also for the needs of various industries. For example, when the traditional farmers are spraying pesticides, they are carrying the medicine barrels and walking in the fields, such as Taiwan. The patent M500457 is. However, this type of spraying causes the user to constantly inhale the pesticide during the spraying process, causing physical damage; and the spraying method is inefficient, the spraying time is long, and the medicine cannot be evenly distributed in the field, and there is Need to improve the shortcomings.
故有業者結合遙控飛機與農藥發展出另一種飛行灑藥裝置,透過遠端遙控飛行灑藥的方式來解決上述問題,如中國專利CN10349446。Therefore, some operators have developed another type of flying sprinkler device in combination with remote-controlled aircraft and pesticides, and solved the above problems by means of remote remote-controlled flight sprinkling, such as Chinese patent CN10349446.
於此專利中,參考其圖3及4、段落[0011-0017],藥箱(21)係先固定在起落架(13),之後再藉由緊固件(2、6、1)將起落架(13)固定於機身(12)底部。接著,使用藥泵(26)連通伸入藥箱(21)之腔室內的進藥管(27),接著啟動藥泵(26)抽取藥箱(21)內的農藥,進而才能將農藥運經由出藥管(28輸送至藥桿(24)上的噴嘴(25)灑出。In this patent, referring to Figures 3 and 4, paragraph [0011-0017], the medicine box (21) is first fixed to the landing gear (13), and then the landing gear is fastened by fasteners (2, 6, 1). (13) Fixed to the bottom of the fuselage (12). Next, the medicine pump (26) is used to communicate the medicine feeding tube (27) extending into the chamber of the medicine box (21), and then the medicine pump (26) is activated to take the pesticide in the medicine box (21), so that the pesticide can be transported through The nozzle (25) delivered to the medicine rod (24) is sprinkled.
換言之,此專利之技術特徵係分成二個分別獨立操作的鎖固系統及噴灑系統,使用者需要先進行鎖固定位起落架後,再啟動藥泵才能讓藥箱與藥桿連通以進行農藥噴灑,使得整個結構過於繁雜、零件眾多且操作步驟眾多。In other words, the technical features of this patent are divided into two separately operated locking systems and spraying systems. The user needs to lock the fixed landing gear first, and then start the medicine pump to connect the medicine box with the medicine rod for pesticide spraying. The whole structure is too complicated, the parts are numerous and the operation steps are numerous.
因此,有必要提供一種新穎且具有進步性之飛行載具,以解決上述之問題。Therefore, it is necessary to provide a novel and progressive flight vehicle to solve the above problems.
本發明之主要目的在於提供一種飛行載具,可以負載至少一箱體,箱體所容設之內容物可以依據需求更換(如:藥劑、汽油);並且,設計有接頭組件,讓使用者能快速將箱體之內部連通飛行載具之管路。The main object of the present invention is to provide a flying vehicle that can load at least one box, and the contents of the box can be replaced according to requirements (eg, medicine, gasoline); and a joint assembly is designed to enable the user to Quickly connect the interior of the cabinet to the piping of the flight vehicle.
為達成上述目的,本發明提供一種飛行載具,包括一飛行本體及至少一接頭組件。該飛行本體設有至少一供定位一箱體之連結單元及一管路單元。各該接頭組件設有一插接組件及一座體組件,該插接組件選擇性地插設連通該座體組件,該插接組件及該座體組件其中一者係供設於該箱體且連通該箱體之內部、另者則係設於該飛行本體且連通該管路單元。其中,當該箱體結合定位於該飛行本體時,該插接組件插設於該座體組件,該箱體之內部透過該接頭組件而直接連通該管路單元。To achieve the above object, the present invention provides a flying vehicle comprising a flying body and at least one joint assembly. The flight body is provided with at least one connecting unit for positioning a box body and a pipeline unit. Each of the connector assemblies is provided with a plug assembly and a body assembly. The plug assembly is selectively inserted into the base assembly, and one of the plug assembly and the base assembly is disposed in the cabinet and connected The inside of the box is provided on the flight body and communicates with the pipe unit. Wherein, when the box is combined and positioned on the flying body, the plug assembly is inserted into the seat assembly, and the inside of the box directly communicates with the pipeline unit through the joint assembly.
以下僅以實施例說明本發明可能之實施態樣,然並非用以限制本發明所欲保護之範疇,合先敘明。The following is a description of the possible embodiments of the present invention, and is not intended to limit the scope of the invention as claimed.
請參考圖1至圖9,其顯示本發明之一較佳實施例,本發明之飛行載具包括一飛行本體1及至少一接頭組件3。Referring to Figures 1 through 9, there is shown a preferred embodiment of the present invention. The flight carrier of the present invention includes a flight body 1 and at least one connector assembly 3.
該飛行本體1設有至少一供定位一箱體A之連結單元11及一管路單元12。各該接頭組件3設有一插接組件4及一座體組件5,該插接組件4選擇性地插設連通該座體組件5,該插接組件4及該座體組件5其中一者係供設於該箱體A且連通該箱體A之內部、另者則係設於該飛行本體1且連通該管路單元12。其中,當該箱體A結合定位於該飛行本體1時,該插接組件4插設於該座體組件5,該箱體A之內部透過該接頭組件3而直接連通該管路單元12。The flight body 1 is provided with at least one connecting unit 11 for positioning a box A and a pipe unit 12. Each of the connector assemblies 3 is provided with a plug assembly 4 and a body assembly 5. The plug assembly 4 is selectively inserted into the base assembly 5, and one of the plug assembly 4 and the base assembly 5 is provided. It is provided in the casing A and communicates with the inside of the casing A, and the other is installed in the flight body 1 and communicates with the pipeline unit 12. When the box A is coupled to the flying body 1 , the plug assembly 4 is inserted into the base assembly 5 , and the inside of the box A directly communicates with the pipe unit 12 through the joint assembly 3 .
較詳細地說,該插接組件4供設於該箱體A,該座體組件5係設於該飛行本體1,各該連結單元11包含有一滑設組件111及一基座113,該基座113供容置固定該箱體A。較佳地,該基座113係可定位地滑插於該滑設組件111,以達到快速組裝之功效。In more detail, the plug assembly 4 is disposed on the housing A, and the base assembly 5 is disposed on the flight body 1. Each of the connecting units 11 includes a sliding assembly 111 and a base 113. The seat 113 is for receiving and fixing the box A. Preferably, the base 113 is slidably inserted into the sliding assembly 111 to achieve rapid assembly.
要強調的是,由於該插接組件4係保持連通該箱體A,該座體組件5係保持連通該管路單元12,故只要將該插接組件4插設該座體組件5後,該箱體A之內部立即就可直接連通該管路單元12,而可讓該箱體A內的液體立即流入該管路單元12,無須再藉由其他汲液單元(如幫浦)來輔助連通。並且,一但該插接組件4插設該座體組件5後,該箱體A就同時定位於該飛行本體1。換言之,使用者僅需一次動作就可以同時完成鎖固定位與連通的二種不同機制,故不用再操作其他鎖固元件來定位、亦無須致動其他汲液單元,使得整個該飛行本體1之結構簡約、操作直觀又方便。It is to be emphasized that since the plug assembly 4 is kept in communication with the cabinet A, the base assembly 5 is kept in communication with the duct unit 12, so that the plug assembly 4 is inserted into the base assembly 5, The inside of the box A can directly communicate with the pipe unit 12, and the liquid in the box A can be immediately flowed into the pipe unit 12 without being assisted by other sputum units (such as pumps). Connected. Moreover, once the docking assembly 4 is inserted into the seat assembly 5, the cabinet A is simultaneously positioned on the flying body 1. In other words, the user can complete two different mechanisms of the lock fixing position and the connection at the same time in one operation, so that the other locking elements are not required to be positioned for positioning, and no other sputum unit is required to be actuated, so that the entire flight body 1 is The structure is simple, the operation is intuitive and convenient.
於本實施例中,該基座113為矩形之架體,該基座113設有二間隔排列的支撐板114,該二支撐板114供支撐該箱體A,該插接組件4係介於該二支撐板114之間。其中,考量到飛行穩定性,該至少一連結單元11之數量為二,該二連結單元11係呈對稱地設置;而考量到各該箱體A結合之平衡性,該滑設組件111較佳包含有四個滑道件112,該四滑道件112係兩兩一組的設於該飛行本體1之相對二側。另外,各該滑道件112亦可設有一限位槽115,該基座113設有可於限位槽115滑動之至少一滑凸116,藉此來提高該基座113與各該滑道件112之結合度,亦無不可。In this embodiment, the pedestal 113 is a rectangular frame body, and the pedestal 113 is provided with two spaced-apart support plates 114 for supporting the cabinet A, and the plug-in assembly 4 is interposed Between the two support plates 114. Wherein, considering the flight stability, the number of the at least one connecting unit 11 is two, and the two connecting units 11 are symmetrically disposed; and considering the balance of the combination of the respective boxes A, the sliding assembly 111 is preferably There are four slide members 112, which are disposed on opposite sides of the flight body 1 in two groups. In addition, each of the slide members 112 can also be provided with a limiting slot 115. The base 113 is provided with at least one sliding protrusion 116 that can slide on the limiting slot 115, thereby improving the base 113 and each of the sliding guides. The degree of integration of the pieces 112 is also indispensable.
更詳細地說,各該滑道件112設有至少一第一固定部71,該基座113設有至少一第二固定部72,該第一固定部71係與該第二固定部72相結合固定,藉此可避免非預期之因素造成該基座113脫離該滑設組件111的情況。舉例但不侷限於,該第一固定部71係為卡塊,該第二固定部72係為貫設於該基座113之孔洞,該第一及第二固定部71, 72相互卡抵固定。In more detail, each of the slide members 112 is provided with at least one first fixing portion 71. The base 113 is provided with at least one second fixing portion 72, and the first fixing portion 71 is coupled to the second fixing portion 72. The fixing is combined, thereby preventing unintended factors from causing the susceptor 113 to be detached from the sliding assembly 111. For example, but not limited to, the first fixing portion 71 is a block, and the second fixing portion 72 is a hole that is disposed in the base 113. The first and second fixing portions 71, 72 are fixed to each other. .
值得一提的是,該管路單元12可以係該飛行本體1之油路管路,此時,只要於各該箱體A內置入油體後,各該箱體A就可以當作是備用油槽讓該飛行載具有更充足之燃料,以有效延長飛行時間。或是,該飛行本體1另設有一噴灑組件6,該噴灑組件6設有該管路單元12,各該箱體A承有藥劑,此時該飛行載具則可進行農藥噴灑。故操作者可以在較遠之地方操控而不會有吸入大量藥劑之風險;並且,藥劑由農田上方噴灑而下可較為平均分布且噴灑面積較廣泛,而能充分且有效率地使用藥劑,減少所使用之分量。當然,各該箱體A之承載物並不侷限於流體,亦可為細小之固體等其他物體型態。It is worth mentioning that the pipeline unit 12 can be the oil pipeline of the flight body 1. At this time, as long as the oil body is built in each of the cabinets A, each of the cabinets A can be regarded as a backup. The oil sump allows the flight to carry more fuel to effectively extend flight time. Alternatively, the flight body 1 is further provided with a spray assembly 6, the spray assembly 6 is provided with the pipeline unit 12, and each of the tanks A is provided with a medicament, and at this time, the flight carrier can be sprayed with pesticides. Therefore, the operator can control at a remote place without the risk of inhaling a large amount of medicine; and the medicine can be sprayed from above the farmland to be evenly distributed and the spray area is wider, and the medicament can be fully and efficiently used, thereby reducing The amount used. Of course, the load of each of the cases A is not limited to a fluid, and may be other object types such as a small solid.
接著,對該接頭組件3之構造做進一步之說明,該插接組件4設有一供設於該箱體A之本體41、一擋件42及一桿件43,該本體41圍構出一供連通該箱體A之內部的通道45,該擋件42可選擇性地阻斷該通道45連通該箱體A之內部,該桿件43連接該擋件42且可移動地插設於該通道45。該座體組件5設有一座體51及一頂件52,該座體51設有一結合部511及一內部空間513,該內部空間513連通該管路單元12,該頂件52容設於該內部空間513。其中,當該箱體A結合定位於該飛行本體1時,該本體41插設且定位於該結合部511,該通道45連通該內部空間513,且該頂件52抵頂該桿件43而使該擋件42未阻斷該通道45。The structure of the joint assembly 3 is further described. The plug assembly 4 is provided with a body 41, a stop member 42 and a rod member 43 disposed on the box body A. a passage 45 communicating with the inside of the box A, the blocking member 42 selectively blocking the passage 45 from communicating with the inside of the box A, the rod member 43 connecting the blocking member 42 and movably inserted in the passage 45. The base assembly 5 is provided with a body 51 and a top member 52. The base body 51 is provided with a joint portion 511 and an inner space 513. The inner space 513 communicates with the pipeline unit 12, and the top member 52 is accommodated therein. Internal space 513. When the box A is coupled to the flying body 1 , the body 41 is inserted and positioned on the joint portion 511 , the passage 45 communicates with the inner space 513 , and the top member 52 abuts the rod member 43 . The stop 42 is not blocked by the stop 42.
更進一步地說,該插接組件4另設有一第一彈性件91,該第一彈性件91連接該本體41及該桿件43,使該擋件42常態性阻斷該通道45連通該箱體A之內部。而該座體組件5另設有一第二彈性件92,該頂件52係可移動地設於該內部空間513,該結合部511設有一供外界連通該內部空間513之開口512,該第二彈性件92連接該座體51及該頂件52,使該頂件52常態性封閉該開口512。只有當該箱體A結合定位於該飛行本體1時,該本體41由該開口512伸入該內部空間513壓抵該頂件52至一預定位置,才會使該頂件52未封閉該開口512,同時,使該擋件42未阻斷該通道45。雙向連動開啟及封閉的結構設計,能確保該接頭組件3只有該箱體A結合定位於該飛行本體1時才能連通,能有效避免該箱體A之物體非注意而移動至外界,並阻隔該管路單元12連通外界,防止雜物進入該管路單元12或是不良揮發物散逸而出(如油、藥劑)的情況發生,確保於使用上有較佳之安全性。Further, the plug assembly 4 is further provided with a first elastic member 91. The first elastic member 91 connects the body 41 and the rod member 43 such that the blocking member 42 normally blocks the passage 45 from communicating with the box. The inside of body A. The base member 5 is further provided with a second elastic member 92. The top member 52 is movably disposed in the inner space 513. The joint portion 511 is provided with an opening 512 for external communication with the inner space 513. The elastic member 92 connects the seat body 51 and the top member 52 such that the top member 52 normally closes the opening 512. Only when the case A is coupled to the flight body 1 , the body 41 extends from the opening 512 into the inner space 513 and presses against the top piece 52 to a predetermined position, so that the top piece 52 does not close the opening. 512, at the same time, the stop 42 is not blocked by the passage 45. The two-way linkage opening and closing structure design ensures that the joint assembly 3 can only be connected when the box A is combined and positioned on the flight body 1, and can effectively prevent the object of the box A from moving to the outside without being noticed, and blocking the The pipeline unit 12 communicates with the outside world to prevent impurities from entering the pipeline unit 12 or the occurrence of bad volatiles (such as oil and chemicals), thereby ensuring better safety in use.
於本實施例中,該擋件42係為蓋設於該本體41之蓋件;而為了快速組裝,該本體41另設有一供螺鎖於該箱體A之螺接部411、及一位於該通道45之裝設部412,該裝設部412貫設有一安裝孔413及複數通孔414,該桿件43穿設過該安裝孔413,該第一彈性件91套設於該桿件43,且該第一彈性件91之一端連接該裝設部412、該第一彈性件91之另端連接一鎖件44,該鎖件44可移動地螺接於該桿件43。該座體組件5另設有一限位件53及一支撐件54,該限位件53固設於該座體51,該第二彈性件92套設於該限位件53,該支撐件54之一端組接於該頂件52、該支撐件54之另端可移動地插設於限位件53及該座體51,當該箱體A結合定位於該飛行本體1時,該限位件53移動至該預定位置而抵頂該頂件52。In the present embodiment, the blocking member 42 is a cover member that is disposed on the body 41. For quick assembly, the body 41 is further provided with a screwing portion 411 for screwing to the housing A, and a The mounting portion 412 of the channel 45 is disposed with a mounting hole 413 and a plurality of through holes 414. The rod member 43 passes through the mounting hole 413. The first elastic member 91 is sleeved on the rod member. The one end of the first elastic member 91 is connected to the mounting portion 412, and the other end of the first elastic member 91 is connected to a locking member 44. The locking member 44 is movably screwed to the rod member 43. The base member 5 is further provided with a limiting member 53 and a supporting member 54 . The limiting member 53 is fixed to the seat body 51 , and the second elastic member 92 is sleeved on the limiting member 53 . The supporting member 54 is further disposed on the limiting member 53 . One end is connected to the top piece 52, and the other end of the support member 54 is movably inserted into the limiting member 53 and the seat body 51. When the box A is combined and positioned on the flying body 1, the limit is The piece 53 is moved to the predetermined position to abut the top piece 52.
較佳地,該插接組件4另設有至少一第一止漏件81,各該第一止漏件81設於該本體41,當該箱體A結合定位於該飛行本體1時,各該第一止漏件81係夾設該結合部511及該本體41之間,能有效防止物體(如流體)從縫隙中跑至外界。並且,透過各該第一止漏件81能使該本體41與該結合部511呈緊配合結合關係,而有較佳之結合。Preferably, the plug assembly 4 is further provided with at least one first stop member 81. Each of the first stop members 81 is disposed on the body 41. When the box A is coupled to the flight body 1, each The first leakage preventing member 81 is interposed between the joint portion 511 and the body 41, and can effectively prevent an object (such as a fluid) from running from the gap to the outside. Moreover, the main body 41 and the joint portion 511 can be tightly coupled and coupled through the first stop member 81, and a preferred combination is obtained.
要補充的是,該本體41另貫設有至少一連通該通道45之貫孔415,該頂件52設有一頭部521及一身部522,當該箱體A結合定位於該飛行本體1時,該頭部521係伸入該通道45抵頂該桿件43,該身部522抵接於該本體41,該通道45藉由各該貫孔415連通該內部空間513。較仔細地說,該頂件52另設有一底部523,一第二止漏件82套設於該身部522,且當該本體41未插設入該結合部511時,該第二止漏件82係介於該結合部511與該底部523之間,以提高密封度。更仔細地說,以垂直該插接組件4與該座體組件5之插接方向觀之,該頂件52概呈「凸」字型。It is to be noted that the body 41 is further provided with at least one through hole 415 which communicates with the passage 45. The top piece 52 is provided with a head portion 521 and a body portion 522. When the box body A is combined and positioned on the flight body 1 The head portion 521 extends into the channel 45 to abut the rod member 43 . The body portion 522 abuts the body 41 , and the passage 45 communicates with the inner space 513 through the through holes 415 . More specifically, the top member 52 is further provided with a bottom portion 523, and a second stop member 82 is sleeved on the body portion 522. When the body portion 41 is not inserted into the joint portion 511, the second stop leaking The member 82 is interposed between the joint portion 511 and the bottom portion 523 to improve the degree of sealing. More specifically, the top member 52 is substantially "convex" in view of the direction in which the plug assembly 4 is perpendicular to the mating direction of the base assembly 5.
綜上,本發明飛行載具能夠快速組接箱體,並依據需求不同而於箱體內填裝不同物體,如要長時間飛行,則於箱體裝置燃油;若要進行噴灑作業,則可放置藥劑於箱體。In summary, the flying carrier of the present invention can quickly assemble the box body and fill different objects in the box according to different requirements. If the aircraft is to be flying for a long time, the fuel is installed in the box body; if the spraying operation is to be carried out, the space can be placed. The medicine is in the box.
並且,接頭組件係常態性地處於封閉狀態,能防止箱體內物體移動至外界,且可避免雜物進入管路單元或是避免管路單元之不良揮發物散逸出,只有當該箱體結合定位於該飛行本體時,該插接組件插設於該座體組件時,才會同時雙向開啟,能夠有較佳安全的使用機制。Moreover, the joint component is normally in a closed state, which can prevent the object in the box from moving to the outside, and can prevent the foreign matter from entering the pipeline unit or avoid the leakage of the bad volatiles of the pipeline unit, only when the cabinet is combined and positioned. When the flying body is inserted into the flying body, the plug assembly can be opened in both directions at the same time, and a better and safe use mechanism can be obtained.
<TABLE border="1" borderColor="#000000" width="85%"><TBODY><tr><td> 1:飛行本體 11:連結單元 111:滑設組件 112:滑道件 113:基座 114:支撐板 115:限位槽 116:滑凸 12:管路單元 3:接頭組件 4:插接組件 41:本體 411:螺接部 412:裝設部 413:安裝孔 414:通孔 415:貫孔 42:擋件 43:桿件 44:鎖件 </td><td> 45:通道 5:座體組件 51:座體 511:結合部 512:開口 513:內部空間 52:頂件 521:頭部 522:身部 523:底部 53:限位件 54:支撐件 6:噴灑組件 71:第一固定部 72:第二固定部 81:第一止漏件 82:第二止漏件 91:第一彈性件 92:第二彈性件 A:箱體 </td></tr></TBODY></TABLE><TABLE border="1" borderColor="#000000" width="85%"><TBODY><tr><td> 1: Flight body 11: Connection unit 111: Sliding assembly 112: Slide member 113: Base Seat 114: support plate 115: limit groove 116: slide 12: pipe unit 3: joint assembly 4: plug assembly 41: body 411: screw portion 412: mounting portion 413: mounting hole 414: through hole 415 :through hole 42: stopper 43: rod 44: lock piece </td><td> 45: channel 5: seat body assembly 51: seat body 511: joint portion 512: opening 513: inner space 52: top piece 521 : Head 522: Body 523: Bottom 53: Limiting member 54: Supporting member 6: Spraying assembly 71: First fixing portion 72: Second fixing portion 81: First stopping member 82: Second stopping member 91 : first elastic member 92: second elastic member A: cabinet </td></tr></TBODY></TABLE>
圖1為本發明一較佳實施例之立體圖。 圖2為圖1之局部分解圖。 圖3為圖1之側視剖面圖。 圖4為圖3之局部剖面放大圖。 圖5為圖3之另一局部剖面放大圖。 圖6為本發明一較佳實施例之接頭組件。 圖7為圖6之分解圖。 圖8及圖9為本發明一較佳實施例之接頭組件的剖面作動圖。1 is a perspective view of a preferred embodiment of the present invention. Figure 2 is a partial exploded view of Figure 1. Figure 3 is a side cross-sectional view of Figure 1. Figure 4 is an enlarged partial cross-sectional view of Figure 3. Figure 5 is another partial cross-sectional enlarged view of Figure 3. Figure 6 shows a joint assembly in accordance with a preferred embodiment of the present invention. Figure 7 is an exploded view of Figure 6. 8 and 9 are cross-sectional views of a joint assembly in accordance with a preferred embodiment of the present invention.
Claims (6)
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TW106139758A TWI640455B (en) | 2017-04-26 | 2017-04-26 | Flying device |
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TW106139758A TWI640455B (en) | 2017-04-26 | 2017-04-26 | Flying device |
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CN105015782A (en) * | 2015-08-17 | 2015-11-04 | 山东卫士植保机械有限公司 | Aviation nozzle |
CN205727786U (en) * | 2016-06-30 | 2016-11-30 | 北方天途航空技术发展(北京)有限公司 | Unmanned plane pesticide spraying system |
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JPH068888A (en) * | 1991-06-05 | 1994-01-18 | Minoru Higa | Levitation device |
JPH0986499A (en) * | 1995-09-25 | 1997-03-31 | Fuji Robin Ind Ltd | Chemical spraying device for remote control type helicopter |
WO2005123503A1 (en) * | 2004-06-20 | 2005-12-29 | Colin Pay | Injection variable rate chemical distribution |
JP2012153168A (en) * | 2011-01-21 | 2012-08-16 | New Delta Industrial Co Ltd | Chemical liquid dispersing device of unmanned helicopter |
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