TWM460835U - Folding ejection rack - Google Patents
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- TWM460835U TWM460835U TW102200159U TW102200159U TWM460835U TW M460835 U TWM460835 U TW M460835U TW 102200159 U TW102200159 U TW 102200159U TW 102200159 U TW102200159 U TW 102200159U TW M460835 U TWM460835 U TW M460835U
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Description
本創作主要係揭示一種彈射架,尤指折疊式的彈射架。This creation mainly reveals a type of ejection frame, especially a folding type ejection frame.
現有的無人飛行載具在起飛時,必須像一般飛機一樣先加速到起飛速度後,才能夠使飛機產生足夠的升力使飛機起飛,為使無人飛機能夠不受場地大小或地形的限制的起飛,通常會利用彈射架給予無人飛行載具輔助動力,使無人飛行載具在短時間內加速到起飛速度而起飛。When the existing unmanned aerial vehicle is taken off, it must accelerate to the take-off speed like a normal airplane before the aircraft can generate enough lift to take off the aircraft. In order to enable the unmanned aircraft to take off without being restricted by the size or terrain of the site, The ejection frame is usually used to give the unmanned aerial vehicle auxiliary power, so that the unmanned aerial vehicle accelerates to take-off speed and take off in a short time.
請參照中華人民共和國專利公開號CN101367438號之「無人飛行平台起飛彈射系統」專利案,其為一種無人飛行器的彈射系統,其包括有支架、滑軌系統、動力系統及控制系統,滑軌系統設於之架上,滑軌系統包括有導軌及滑車,動力系統包括有牽引鋼索、數個滑輪及絞盤,將無人機固定在滑車上後,滑車位於導軌的起射端的一端,滑車上及導軌的出射端皆具有滑輪,牽引鋼索通過滑輪組後而設於絞盤,當絞盤轉動而使牽引鋼索被拉伸之後,牽引鋼索能夠牽引滑車往滑軌的出射端的方向移動,期間無人機即能夠獲得起飛時所需的起飛速度。Please refer to the Patent No. CN101367438 of the People's Republic of China for the "Unmanned Flight Platform Take-off Ejection System" patent case, which is an ejection system for an unmanned aerial vehicle, which includes a bracket, a slide rail system, a power system and a control system, and a slide rail system. On the rack, the rail system includes a guide rail and a pulley. The power system includes a traction cable, a plurality of pulleys and a winch. After the drone is fixed on the trolley, the trolley is located at one end of the starting end of the guide rail, on the trolley and on the guide rail. The exit end has a pulley, and the traction cable is arranged on the winch through the pulley block. After the winch rotates and the traction cable is stretched, the traction cable can pull the trolley to move in the direction of the exit end of the slide rail, and the drone can obtain the take-off time. The required takeoff speed.
然而,此種無人飛行器的彈射系統組裝後為固定形狀,使用後欲收納時是必要拆分為多個零件分別擺放,下次要使用時則必須要再重新組裝,若不將其分解後直接收納將佔用相當大的空間,造成空間上的浪 費,在攜帶時亦不方便。However, the ejection system of such an unmanned aerial vehicle has a fixed shape after assembly, and it is necessary to split into a plurality of parts separately when used for storage, and must be reassembled again when it is to be used next time, if it is not disassembled Direct storage will take up a considerable amount of space, causing space waves Fees are also inconvenient when carrying.
有鑑於上述習知結構之缺失,本創作人乃致力於設計出一種折疊式彈射架,其係可克服上述習知結構之所有缺點。In view of the above-described deficiencies in the conventional structure, the present author is working to design a folding type ejection frame that overcomes all of the disadvantages of the above-described conventional structure.
本創作折疊式彈射架其主要目的在於,提供一種折疊式的彈射架,彈射架包括有數個支撐桿,各個支撐桿之間能夠相對樞轉或連接,使彈射架能夠在收折狀態與展開狀態之間切換,展開狀態時能夠使其中兩個支撐桿與地面呈一個銳角,無人飛行載具滑行起飛,收折狀態時所有的支撐桿經收折後皆在同一平面上,使彈射架在收納時所佔用的空間減到最小。The main purpose of the creation of the folding type ejection frame is to provide a folding type ejection frame. The ejection frame comprises a plurality of support rods, and the respective support rods can be pivoted or connected relative to each other, so that the ejection frame can be folded and unfolded. When switching between, the two support rods can be placed at an acute angle with the ground, and the unmanned flying vehicle will take off and take off. When the folding state is closed, all the support rods are folded on the same plane, so that the ejection rack is in the storage. The space occupied by the time is minimized.
其他目的、優點和本創作之新穎性將從以下詳細的描述與相關的附圖更加明顯。Other objects, advantages and novelty of the present invention will become more apparent from the following detailed description.
10‧‧‧彈射架10‧‧‧Ejection rack
20‧‧‧本體20‧‧‧ body
21‧‧‧第一支撐桿21‧‧‧First support rod
211‧‧‧樞轉部211‧‧‧ pivoting department
212‧‧‧連接部212‧‧‧Connecting Department
213‧‧‧第一端213‧‧‧ first end
214‧‧‧第二端214‧‧‧ second end
22‧‧‧第二支撐桿22‧‧‧second support rod
221‧‧‧第一樞轉部221‧‧‧First pivoting
222‧‧‧第二樞轉部222‧‧‧Second pivoting
223‧‧‧第一端223‧‧‧ first end
224‧‧‧第二端224‧‧‧ second end
23‧‧‧第三支撐桿23‧‧‧ Third support rod
231‧‧‧樞轉部231‧‧‧ pivoting department
232‧‧‧連接部232‧‧‧Connecting Department
233‧‧‧第一端233‧‧‧ first end
234‧‧‧第二端234‧‧‧ second end
235‧‧‧限位件235‧‧‧Limited parts
24‧‧‧第一連接桿24‧‧‧First connecting rod
25‧‧‧第二連接桿25‧‧‧Second connecting rod
251‧‧‧定位件251‧‧‧ Positioning parts
252‧‧‧連接端252‧‧‧Connected end
253‧‧‧尖端253‧‧‧ tip
26‧‧‧第三連接桿26‧‧‧ third connecting rod
261‧‧‧瞄準件261‧‧‧Sighting
27‧‧‧滑移件27‧‧‧Slipper
28‧‧‧固定桿28‧‧‧Fixed rod
29‧‧‧卡掣件29‧‧‧ Cards
30‧‧‧發射器30‧‧‧transmitter
31‧‧‧底板31‧‧‧floor
311‧‧‧抵靠面311‧‧‧Abutment
32‧‧‧蓋板32‧‧‧ Cover
33‧‧‧凸塊33‧‧‧Bumps
34‧‧‧間隙34‧‧‧ gap
35‧‧‧定位件35‧‧‧ Positioning parts
351‧‧‧抵靠端351‧‧‧Abutment
352‧‧‧尖端352‧‧‧ tip
90‧‧‧地板90‧‧‧floor
91‧‧‧彈性繩91‧‧‧elastic rope
92‧‧‧無人飛機92‧‧‧ Unmanned aircraft
93‧‧‧機翼93‧‧‧Wings
圖一:為本創作折疊式彈射架之立體外觀圖。Figure 1: The three-dimensional appearance of the folding frame of the creation.
圖二:為本創作折疊式彈射架之立體分解圖。Figure 2: An exploded view of the folding frame of the creation.
圖三:為本創作折疊式彈射架之使用狀態圖。Figure 3: The state of use of the folding frame of the creation.
圖四:為本創作折疊式彈射架之局部放大使用狀態圖。Figure 4: A partial enlarged state diagram of the folding frame of the present creation.
圖五:為本創作折疊式彈射架之使用狀態圖。Figure 5: The state of use of the folding frame of the creation of the present.
圖六:為本創作折疊式彈射架之操作示意圖。Figure 6: Schematic diagram of the operation of the folding frame of the creation.
圖七:為本創作折疊式彈射架之局部放大操作示意圖。Figure 7: Schematic diagram of a partial enlargement operation of the folding frame of the present creation.
圖八:為本創作折疊式彈射架之操作示意圖。Figure 8: Schematic diagram of the operation of the folding frame of the creation.
圖九:為本創作折疊式彈射架之收折狀態圖。Figure 9: The folding state diagram of the folding frame of the creation.
圖十:為本創作折疊式彈射架之收折狀態圖。Figure 10: The folding state diagram of the folding frame of the creation.
有關本創作所採用之技術、手段及其功效,茲舉一較佳實施例並配合圖式詳述如後,此僅供說明之用,在專利申請上並不受此種結構之限制。The techniques, means, and effects of the present invention are described in detail with reference to the accompanying drawings.
參照圖一及圖二所示,為本創作折疊式彈射架之立體外觀圖及立體分解圖。本創作彈射架10包括有一個本體20及一個發射器30;其中:該本體20包括有兩個第一支撐桿21、兩個第二支撐桿22及兩個第三支撐桿23,該第一支撐桿21具有一個樞轉部211及一個連接部212,該第二支撐桿22具有一個第一樞轉部221及一個第二樞轉部222,該第三支撐桿23具有一個樞轉部231及一個連接部232,該第二支撐桿22的第一樞轉部221樞設於該第一支撐桿21的樞轉部211,使該第一支撐桿21與該第二支撐桿22能夠相對樞轉,該第三支撐桿23的樞轉部231樞設於該第二支撐桿22的第二樞轉部222,使該第二支撐桿22與該第三支撐桿23能夠相對樞轉,該第三支撐桿23的連接部232選擇性的連接於該第一支撐桿21的連接部212。Referring to FIG. 1 and FIG. 2, the three-dimensional appearance and an exploded view of the folding frame of the present invention are shown. The present ejection rack 10 includes a body 20 and a transmitter 30. The body 20 includes two first support bars 21, two second support bars 22 and two third support bars 23, the first The support rod 21 has a pivoting portion 211 and a connecting portion 212. The second supporting rod 22 has a first pivoting portion 221 and a second pivoting portion 222. The third supporting rod 23 has a pivoting portion 231. And a connecting portion 232, the first pivoting portion 221 of the second supporting rod 22 is pivotally disposed on the pivoting portion 211 of the first supporting rod 21, so that the first supporting rod 21 and the second supporting rod 22 are opposite to each other. The pivoting portion 231 of the third support rod 23 is pivotally disposed on the second pivoting portion 222 of the second support rod 22 to enable the second support rod 22 and the third support rod 23 to pivot relative to each other. The connecting portion 232 of the third support rod 23 is selectively connected to the connecting portion 212 of the first support rod 21.
該本體20能夠在第一狀態與第二狀態之間進行切換,該本體20在第一狀態時,該第三支撐桿23的連接部232連接於該第一支撐桿21的連接部212,該本體20在第二狀態時,該第三支撐桿23的連接部232脫離該第一支撐桿21的連接部212。The body 20 is switchable between the first state and the second state. When the body 20 is in the first state, the connecting portion 232 of the third support rod 23 is connected to the connecting portion 212 of the first support rod 21, When the body 20 is in the second state, the connecting portion 232 of the third support rod 23 is disengaged from the connecting portion 212 of the first support rod 21 .
該第一支撐桿21包括有一個第一端213及一個第二端214,該第一支撐桿21的樞轉部211位於該第一支撐桿21的第一端213與第二端214之 間,該第一支撐桿21的第一端213能夠抵靠於地面90(請見圖三),該第二支撐桿22包括有一個第一端223及一個第二端224,該第二支撐桿22的第一樞轉部221位於該第二支撐桿22的第一端223與第二端224之間,該第二支撐桿22的第一端223能夠抵靠於地面90,該第三支撐桿23包括有一個第一端233及一個第二端234,該第三支撐桿23的樞轉部231位於該第三支撐桿23的第一端233與第二端234之間。The first support rod 21 includes a first end 213 and a second end 214. The pivoting portion 211 of the first support rod 21 is located at the first end 213 and the second end 214 of the first support rod 21. The first end 213 of the first support rod 21 can abut against the ground 90 (see FIG. 3). The second support rod 22 includes a first end 223 and a second end 224. The second support The first pivoting portion 221 of the rod 22 is located between the first end 223 and the second end 224 of the second support rod 22, and the first end 223 of the second support rod 22 can abut against the ground 90, the third The support rod 23 includes a first end 233 and a second end 234. The pivoting portion 231 of the third support rod 23 is located between the first end 233 and the second end 234 of the third support rod 23.
該本體20還包括有一個第一連接桿24、一個第二連接桿25及一個第三連接桿26,該第一連接桿24位於所述的兩個第一支撐桿21之間並同時連接於所述的兩個第一支撐桿21,使所述的兩個第一支撐桿21能夠同步與該第二支撐桿22相對樞轉,該第一連接桿24的兩端分別連接於所述的兩個第一支撐桿21的第一端213,該第一連接桿24垂直於所述的兩個第一支撐桿21,同時所述的兩個第一支撐桿21位於同一平面上且彼此平行,該第二連接桿25位於所述的兩個第二支撐桿22之間並同時連接於所述的兩個第二支撐桿22,使所述的兩個第二支撐桿22能夠同步與該第一支撐桿21或該第三支撐桿23相對樞轉,該第二連接桿25的兩端分別連接於所述的兩個第二支撐桿22的第一端223,該第二連接桿25垂直於所述的兩個第二支撐桿22,同時所述的兩個第二支撐桿22位於同一平面上且彼此平行,該第三連接桿26位於所述的兩個第三支撐桿23之間並同時連接於所述的兩個第三支撐桿23,使所述的兩個第三支撐桿23能夠同步與該第二支撐桿22相對樞轉,或同步與該第一支撐桿21相對滑移,該第三連接桿26的兩端分別連接於所述的兩個第三支撐桿23的第一端233,該第三連接桿26垂直於所述的兩個第三支撐桿23,同時所述的兩個第三支撐桿23位於同一平面上且彼此平行。The body 20 further includes a first connecting rod 24, a second connecting rod 25 and a third connecting rod 26. The first connecting rod 24 is located between the two first supporting rods 21 and is simultaneously connected to The two first support rods 21 enable the two first support rods 21 to be pivoted relative to the second support rods 22, and the two ends of the first connecting rods 24 are respectively connected to the a first end 213 of the two first support rods 21, the first connecting rod 24 is perpendicular to the two first support rods 21, while the two first support rods 21 are on the same plane and parallel to each other The second connecting rod 25 is located between the two second supporting rods 22 and is simultaneously connected to the two second supporting rods 22, so that the two second supporting rods 22 can be synchronized with the The first support rod 21 or the third support rod 23 is relatively pivoted. The two ends of the second connecting rod 25 are respectively connected to the first ends 223 of the two second support rods 22, and the second connecting rods 25 are respectively connected. It is perpendicular to the two second support rods 22, while the two second support rods 22 are on the same plane and parallel to each other. a third connecting rod 26 is located between the two third supporting rods 23 and is simultaneously connected to the two third supporting rods 23, so that the two third supporting rods 23 can be synchronized with the second The support rods 22 are relatively pivoted or synchronously slid relative to the first support rods 21, and the two ends of the third connecting rods 26 are respectively connected to the first ends 233 of the two third support rods 23, the first The three connecting rods 26 are perpendicular to the two third supporting rods 23 while the two third supporting rods 23 are on the same plane and parallel to each other.
該第一支撐桿21的連接部212位於該第一支撐桿21的第二端214,該第二支撐桿22的第二樞轉部222位於該第二支撐桿22的第二端224,該第三支撐桿23的連接部232位於該第三支撐桿23的第二端234。該本體20還包括有一個滑移件27,該滑移件27同時連接於該第一支撐桿21的連接部212及該第三支撐桿23的連接部232,使該第一支撐桿21與該第三支撐桿23能夠相對滑移。該第三支撐桿23的第二端234還設有一個限位件235,該限位件235能夠避免該滑移件27沿該第三支撐桿23軸向脫離該第三支撐桿23。The connecting portion 212 of the first support rod 21 is located at the second end 214 of the first support rod 21 , and the second pivot portion 222 of the second support rod 22 is located at the second end 224 of the second support rod 22 . The connecting portion 232 of the third support rod 23 is located at the second end 234 of the third support rod 23. The body 20 further includes a sliding member 27, which is simultaneously connected to the connecting portion 212 of the first supporting rod 21 and the connecting portion 232 of the third supporting rod 23, so that the first supporting rod 21 is The third support rod 23 is relatively slidable. The second end 234 of the third support rod 23 is further provided with a limiting member 235. The limiting member 235 can prevent the sliding member 27 from axially disengaging from the third supporting rod 23 along the third supporting rod 23.
該本體20還包括有至少一個固定桿28,該固定桿28的兩端選擇性的分別連接於該第一連接桿24及該第三連接桿26,所述的至少一個固定桿28在本實施例中數量為兩個。該本體20還包括有至少一個卡掣件29,所述的至少一個卡掣件29在本實施例中數量為兩個,所述的兩個卡掣件29分別設於所述的兩個第三支撐桿23,該卡掣件29設於該第三支撐桿23的樞轉部231與連接部232之間。The body 20 further includes at least one fixing rod 28. The two ends of the fixing rod 28 are selectively connected to the first connecting rod 24 and the third connecting rod 26, respectively. The at least one fixing rod 28 is in the present embodiment. In the example, the number is two. The body 20 further includes at least one latching member 29, the at least one latching member 29 is two in the embodiment, and the two latching members 29 are respectively disposed on the two A support rod 23 is disposed between the pivoting portion 231 of the third support rod 23 and the connecting portion 232.
該本體20的第二連接桿25還包括有一個定位件251,該定位件251包括有一個連接端252及一個相反於該連接端252的尖端253,該第二連接桿25定位件251的連接端252連接於該第二連接桿25,該第二連接桿25定位件251的尖端253能夠插設於地板90。The second connecting rod 25 of the body 20 further includes a positioning member 251. The positioning member 251 includes a connecting end 252 and a tip end 253 opposite to the connecting end 252. The second connecting rod 25 is connected with the positioning member 251. The end 252 is connected to the second connecting rod 25, and the tip end 253 of the positioning member 251 of the second connecting rod 25 can be inserted into the floor 90.
該本體20的第三連接桿26還包括有一個瞄準件261,該瞄準件261連接於該第三支撐桿26,該瞄準件261位於所述的兩個第三支撐桿23之間,且該瞄準件261與所述的兩個第三支撐桿23之間的距離相等。The third connecting rod 26 of the body 20 further includes an aiming member 261 connected to the third supporting rod 26, the aiming member 261 is located between the two third supporting rods 23, and the The distance between the aiming member 261 and the two third support rods 23 is equal.
請繼續參照圖三至圖五所示,為本創作折疊式彈射架之使用狀態圖。該發射器30包括有一個底板31及一個蓋板32,該蓋板32連接於該底 板31,該底板31於靠近該蓋板32的一側具有一個抵靠面311,該發射器30還包括有一個凸塊33,該凸塊33選擇性的凸出該底板31的抵靠面311,該凸塊33與該蓋板32之間具有一個間隙34,該蓋板32能夠相對該底板31在第一位置與第二位置之間移動,該蓋板32在第一位置時,該蓋板32遠離該底板31,該凸塊33凸出該底板31的抵靠面311,該蓋板32在第二位置時,該蓋板32靠近該底板31,該凸塊33不凸出該底板31的抵靠面311。Please continue to refer to Figure 3 to Figure 5, which is the use state diagram of the folding frame of the creation. The transmitter 30 includes a bottom plate 31 and a cover plate 32. The cover plate 32 is connected to the bottom plate. The plate 31 has an abutting surface 311 on a side close to the cover plate 32. The emitter 30 further includes a protrusion 33, and the protrusion 33 selectively protrudes from the abutting surface of the bottom plate 31. 311, the bump 33 has a gap 34 between the cover plate 32 and the cover plate 32. The cover plate 32 is movable between the first position and the second position relative to the bottom plate 31. When the cover plate 32 is in the first position, the cover plate 32 is in the first position. The cover plate 32 is away from the bottom plate 31. The protrusion 33 protrudes from the abutting surface 311 of the bottom plate 31. When the cover plate 32 is in the second position, the cover plate 32 is adjacent to the bottom plate 31. The protrusion 33 does not protrude from the bottom plate 31. The abutting surface 311 of the bottom plate 31.
同時該第一支撐桿21、該第二支撐桿22、該第三支撐桿23、該第一連接桿24、該第二連接桿25及該第三連接桿26能夠以各種不同的金屬材質或複合材料製成,如鋁合金、鎂合金、玻璃纖維、碳纖維或克維拉纖維。當該第一支撐桿21、該第二支撐桿22、該第三支撐桿23、該第一連接桿24、該第二連接桿25及該第三連接桿26以各種不同的材質製成時,能夠使該第一支撐桿21、該第二支撐桿22、該第三支撐桿23、該第一連接桿24、該第二連接桿25及該第三連接桿26具有不同的特性,獲得各種不同的機械性質。At the same time, the first support rod 21, the second support rod 22, the third support rod 23, the first connecting rod 24, the second connecting rod 25 and the third connecting rod 26 can be made of various metal materials or Made of composite materials such as aluminum alloy, magnesium alloy, glass fiber, carbon fiber or ke vera fiber. When the first support rod 21, the second support rod 22, the third support rod 23, the first connecting rod 24, the second connecting rod 25 and the third connecting rod 26 are made of various materials The first support rod 21, the second support rod 22, the third support rod 23, the first connecting rod 24, the second connecting rod 25 and the third connecting rod 26 can have different characteristics. A variety of different mechanical properties.
該發射器30連接於該本體20,該發射器30的底板31一端連接於該第一連接桿24,該底板31相反於該第一連接桿24的一端穿設有一個定位件35,該發射器30的定位件35包括有一個抵靠端351及一個相反於該抵靠端351的尖端352,該發射器30的定位件35的尖端352能夠貫穿該底板31的兩面並插設於地板90,該發射器30的定位件35的抵靠端351抵靠於該底板31。The transmitter 30 is connected to the body 20, and one end of the bottom plate 31 of the transmitter 30 is connected to the first connecting rod 24. The bottom plate 31 is opposite to the first connecting rod 24 and is provided with a positioning member 35. The positioning member 35 of the device 30 includes an abutting end 351 and a tip end 352 opposite to the abutting end 351. The tip end 352 of the positioning member 35 of the transmitter 30 can penetrate both sides of the bottom plate 31 and be inserted into the floor 90. The abutting end 351 of the positioning member 35 of the transmitter 30 abuts against the bottom plate 31.
請繼續參照圖六至圖八所示,為本創作折疊式彈射架之操作示意圖。當使用者將該彈射架10架設妥當後,所述的兩個第三支撐桿23會與地面90形成夾角,再將彈性繩91的一端固定在該彈射架10的前方,彈性繩91的另外一端具有分岔,分岔的一頭固定於該發射器30且呈緊繃狀態,彈性 繩91是勾住該發射器30中的凸塊33,分岔的另一頭則勾在無人飛機92,無人飛機92的機翼93則抵靠在所述的兩個第三支撐桿23,無人飛機92的機翼93會同時抵靠於所述的兩個卡掣件29,利用所述的兩個卡掣件29避免無人飛機92在該第三支撐桿23上滑動,同時使用者能夠觀察該瞄準件261與彈性繩91固定在該彈射架10前方一端之間的連線,無人飛機92需以該連線為基準呈對稱才能使無人飛機92以直線方向前進。Please continue to refer to Figure 6 to Figure 8, which is a schematic diagram of the operation of the folding frame. When the user erects the ejection frame 10, the two third support bars 23 form an angle with the ground 90, and one end of the elastic rope 91 is fixed in front of the ejection frame 10, and the elastic rope 91 is additionally One end has a branching, one end of the branching is fixed to the emitter 30 and is in a tight state, elastic The rope 91 is a hook 33 hooked in the transmitter 30, and the other end of the branch is hooked on the unmanned aircraft 92, and the wing 93 of the unmanned aircraft 92 abuts against the two third support bars 23, The wing 93 of the aircraft 92 will simultaneously abut against the two latching members 29, and the two latching members 29 are used to prevent the unmanned aircraft 92 from sliding on the third supporting rod 23 while the user can observe The aiming member 261 and the elastic cord 91 are fixed to the line between the front end of the ejection frame 10. The unmanned aircraft 92 needs to be symmetrical with respect to the connection to advance the unmanned aircraft 92 in a straight line direction.
當使用者操作該發射器30將固定於該發射器30的彈性繩91釋放後,使用者按壓該蓋板32後,該蓋板32往該底板31靠近,該凸塊33沉入該底板31的抵靠面311,該底板31的抵靠面311將抵推彈性繩91使彈性繩91經由該凸塊33與該蓋板32之間的間隙34脫離該凸塊33,彈性繩91將轉為拉動無人飛機92前進,使無人飛機92獲得起飛速度,使無人飛機92起飛。調整該第三支撐桿23的連接部232與該第一支撐桿21的連接部212的連接位置能夠達到調整該第三支撐桿23相對於地面90形成的角度,進而改變飛機的起飛角度。且因該彈射架10裝設有該固定桿28,能夠固定該第三支撐桿23相對於地面90的角度,同時具有增加該彈射架10結構強度的效果。After the user operates the transmitter 30 to release the elastic cord 91 fixed to the transmitter 30, after the user presses the cover 32, the cover 32 approaches the bottom plate 31, and the bump 33 sinks into the bottom plate 31. The abutting surface 311, the abutting surface 311 of the bottom plate 31 will push the elastic cord 91 to disengage the elastic cord 91 from the gap 34 between the bump 33 and the cover 32, and the elastic cord 91 will rotate. To pull the unmanned aircraft 92 forward, the unmanned aircraft 92 is allowed to take off at a take-off speed, causing the unmanned aircraft 92 to take off. Adjusting the connection position of the connecting portion 232 of the third supporting rod 23 and the connecting portion 212 of the first supporting rod 21 can adjust the angle formed by the third supporting rod 23 with respect to the ground 90, thereby changing the take-off angle of the aircraft. Moreover, since the ejecting frame 10 is provided with the fixing rod 28, the angle of the third supporting rod 23 with respect to the ground 90 can be fixed, and at the same time, the structural strength of the ejection frame 10 is increased.
請繼續參照圖九及圖十所示,為本創作折疊式彈射架之收折狀態圖。該彈射架10在非使用時,先將該第三支撐桿23的連接部232脫離該第一支撐桿21的連接部212後,使用者能夠將所述的兩個第一支撐桿21、所述的兩個第二支撐桿22及所述的兩個第三支撐桿23全數收折,收折後的該第一支撐桿21、該第二支撐桿22及該第三支撐桿23皆位於同一平面上,能夠有效減少該彈射架10所佔用的體積。Please continue to refer to Figure 9 and Figure 10 for the folding state diagram of the folding frame. When the ejection frame 10 is not in use, after the connecting portion 232 of the third supporting rod 23 is disengaged from the connecting portion 212 of the first supporting rod 21, the user can set the two first supporting rods 21 and the The two second support bars 22 and the two third support bars 23 are all folded, and the folded first support bar 21, the second support bar 22 and the third support bar 23 are located. On the same plane, the volume occupied by the ejection frame 10 can be effectively reduced.
就以上所述可以歸納出本創作具有以下優點: 1.為本創作折疊式彈射架,其中彈射架為折疊式的,彈射架包括有數個支撐桿,各個支撐桿之間能夠相對樞轉或連接,使彈射架能夠在收折狀態與展開狀態之間切換,展開狀態時能夠使其中兩個支撐桿與地面呈一個銳角,無人飛行載具滑行起飛,收折狀態時所有的支撐桿經收折後皆在同一平面上,使彈射架在收納時所佔用的空間減到最小。As far as the above is concerned, it can be concluded that this creation has the following advantages: 1. The original folding type ejection frame, wherein the ejection frame is folded, the ejection frame comprises a plurality of support rods, and the respective support rods can be relatively pivoted or connected, so that the ejection frame can be in a folded state and an unfolded state. When switching between, the two support rods can be placed at an acute angle with the ground, and the unmanned flying vehicle will take off and take off. When the folding state is folded, all the support rods are folded on the same plane, so that the ejection rack is in storage. The space occupied is minimized.
惟上所述者,僅為本創作之較佳實施例而已,當不能以之限定本創作實施之範圍,故舉凡數值之變更或等效元件及材質之置換,或依本創作申請專利範圍所作之均等變化與修飾,皆應仍屬本新型專利涵蓋之範疇。However, the above description is only for the preferred embodiment of the present invention, and the scope of the present invention cannot be limited thereto, so the change of the numerical value or the replacement of the equivalent components and materials, or the scope of patent application according to the present invention. Equal changes and modifications should remain within the scope of this new patent.
10‧‧‧彈射架10‧‧‧Ejection rack
20‧‧‧本體20‧‧‧ body
21‧‧‧第一支撐桿21‧‧‧First support rod
211‧‧‧樞轉部211‧‧‧ pivoting department
212‧‧‧連接部212‧‧‧Connecting Department
213‧‧‧第一端213‧‧‧ first end
214‧‧‧第二端214‧‧‧ second end
22‧‧‧第二支撐桿22‧‧‧second support rod
221‧‧‧第一樞轉部221‧‧‧First pivoting
222‧‧‧第二樞轉部222‧‧‧Second pivoting
223‧‧‧第一端223‧‧‧ first end
224‧‧‧第二端224‧‧‧ second end
23‧‧‧第三支撐桿23‧‧‧ Third support rod
231‧‧‧樞轉部231‧‧‧ pivoting department
232‧‧‧連接部232‧‧‧Connecting Department
233‧‧‧第一端233‧‧‧ first end
234‧‧‧第二端234‧‧‧ second end
235‧‧‧限位件235‧‧‧Limited parts
24‧‧‧第一連接桿24‧‧‧First connecting rod
25‧‧‧第二連接桿25‧‧‧Second connecting rod
251‧‧‧定位件251‧‧‧ Positioning parts
252‧‧‧連接端252‧‧‧Connected end
253‧‧‧尖端253‧‧‧ tip
26‧‧‧第三連接桿26‧‧‧ third connecting rod
261‧‧‧瞄準件261‧‧‧Sighting
27‧‧‧滑移件27‧‧‧Slipper
28‧‧‧固定桿28‧‧‧Fixed rod
29‧‧‧卡掣件29‧‧‧ Cards
30‧‧‧發射器30‧‧‧transmitter
31‧‧‧底板31‧‧‧floor
32‧‧‧蓋板32‧‧‧ Cover
35‧‧‧定位件35‧‧‧ Positioning parts
351‧‧‧抵靠端351‧‧‧Abutment
352‧‧‧尖端352‧‧‧ tip
92‧‧‧無人飛機92‧‧‧ Unmanned aircraft
93‧‧‧機翼93‧‧‧Wings
Claims (19)
Priority Applications (1)
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TW102200159U TWM460835U (en) | 2013-01-04 | 2013-01-04 | Folding ejection rack |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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TW102200159U TWM460835U (en) | 2013-01-04 | 2013-01-04 | Folding ejection rack |
Publications (1)
Publication Number | Publication Date |
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TWM460835U true TWM460835U (en) | 2013-09-01 |
Family
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TW102200159U TWM460835U (en) | 2013-01-04 | 2013-01-04 | Folding ejection rack |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10009518B2 (en) | 2015-10-30 | 2018-06-26 | Industrial Technology Research Institute | Detachable aerial photographic apparatus |
CN113694995A (en) * | 2021-08-19 | 2021-11-26 | 中国电建集团贵州电力设计研究院有限公司 | Stone crushing device and crushing method thereof |
CN115489749A (en) * | 2022-11-16 | 2022-12-20 | 成都航空职业技术学院 | Fixed wing unmanned aerial vehicle launches take-off and land integrated system |
-
2013
- 2013-01-04 TW TW102200159U patent/TWM460835U/en not_active IP Right Cessation
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10009518B2 (en) | 2015-10-30 | 2018-06-26 | Industrial Technology Research Institute | Detachable aerial photographic apparatus |
CN113694995A (en) * | 2021-08-19 | 2021-11-26 | 中国电建集团贵州电力设计研究院有限公司 | Stone crushing device and crushing method thereof |
CN115489749A (en) * | 2022-11-16 | 2022-12-20 | 成都航空职业技术学院 | Fixed wing unmanned aerial vehicle launches take-off and land integrated system |
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