TWI709836B - Micro detecting device - Google Patents
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Description
本案係關於一種微型偵測裝置,尤指一種利用排出流體來產生推力,進而推動具有偵測單元的飛行載具。This case is about a miniature detection device, in particular, a kind of propelling a flying vehicle with a detection unit that uses discharged fluid to generate thrust.
目前的行動載具的驅動裝置皆是以馬達、引擎、發動機等作為驅動源來帶動行動載具,但是這些傳統的驅動裝置為了達到其需求的動能,往往需要一定的體積,才得以容納其內部的核心元件,所以傳統的驅動裝置都難以縮小體積。於這個科技產品皆不斷地往微型化推動的時代,傳統的驅動裝置已經難以應用於現在的科技產品上,特別是現在的行動載具例如無人機,皆往微型化、高隱蔽性、高機動性發展,傳統的驅動裝置已經無法滿足現下微型行動載具的要求,使得目前的無人載具都難以微型化,容易受地域限制,難以普及;此外,目前的驅動裝置在運轉時,會產生擾人的噪音,也是當下驅動裝置無法攻克的難題。The current driving devices of mobile vehicles use motors, engines, engines, etc. as driving sources to drive the mobile vehicles. However, in order to achieve the required kinetic energy, these traditional driving devices often require a certain volume to accommodate their interior. It is difficult to reduce the size of traditional driving devices. In this era when technology products are constantly being miniaturized, it is difficult for traditional driving devices to be applied to current technology products, especially current mobile vehicles such as drones, which are miniaturized, highly concealed, and highly maneuverable. With the development of nature, the traditional driving device can no longer meet the requirements of the current miniature mobile vehicles, making the current unmanned vehicles difficult to miniaturize, easy to be restricted by geographical areas, and difficult to popularize; in addition, the current driving device will cause disturbances when operating. Human noise is also a problem that the current drive device cannot overcome.
有鑑於此,實乃有必要發展一種微型化的行動載具,來解決目前行動載具容易受限於環境且具有運轉時仍有噪音等問題。In view of this, it is actually necessary to develop a miniaturized mobile vehicle to solve the problems of current mobile vehicles that are easily restricted by the environment and still have noise during operation.
本案之主要目的在於提供一種微型偵測裝置,透過動力驅動器來輸送流體,再透過排出流體所產生的壓力推動飛行載具,讓飛行載具得以順利的移動,再使用設置於飛行載具上的偵測單元作偵測動作,最後將偵測結果回傳。The main purpose of this case is to provide a miniature detection device that transports fluid through a power driver, and then pushes the flight vehicle through the pressure generated by the discharged fluid, so that the flight vehicle can move smoothly, and then uses the device installed on the flight vehicle The detection unit performs a detection action, and finally returns the detection result.
為達上述目的,本案之較廣義實施態樣為提供一種微型偵測裝置,包含:一控制器,具有一第一無線通訊模組;一飛行載具,包含有:一載具主體;一處理器,容設於該載具主體內;一第二無線通訊模組,容置於該載具主體並與該處理器電連接,該第二無線通訊模組供該第一無線通訊模組連結,以接收該控制器的一控制訊號;一動力驅動器,設置於該載具主體且電連接該處理器,用以推動該載具主體;以及偵測單元,設置於該載具主體且電連接該處理器該第二無線通訊模組,並產生一偵測訊號。In order to achieve the above objective, the broader implementation of this case is to provide a miniature detection device, which includes: a controller with a first wireless communication module; a flight vehicle, including: a vehicle body; The device is housed in the main body of the carrier; a second wireless communication module is housed in the main body of the carrier and is electrically connected to the processor, and the second wireless communication module is connected to the first wireless communication module , To receive a control signal from the controller; a power driver, arranged on the vehicle body and electrically connected to the processor, for pushing the vehicle body; and a detection unit, arranged on the vehicle body and electrically connected The processor generates a detection signal for the second wireless communication module.
體現本案特徵與優點的一些典型實施例將在後段的說明中詳細敘述。應理解的是本案能夠在不同的態樣上具有各種的變化,其皆不脫離本案的範圍,且其中的說明及圖示在本質上當作說明之用,而非用以限制本案。Some typical embodiments embodying the features and advantages of this case will be described in detail in the following description. It should be understood that this case can have various changes in different aspects, all of which do not depart from the scope of the case, and the descriptions and illustrations therein are essentially for illustrative purposes, rather than limiting the case.
請參閱第1圖及第2A圖所示,第1圖為本案微型偵測裝置的示意圖,第2A圖為本案偵測裝置的方塊示意圖。本案提供一種微型偵測裝置100,包含有一控制器1及一飛行載具2。控制器1具有一操作區11及一第一無線通訊模組12,操作區11電連接第一無線通訊模組12,使用者可通過控制器1的操作區11來控制飛行載具2,操作區11將使用者輸入的指令產生一控制訊號,再通過第一無線通訊模組12發送。飛行載具2具有一載具主體21、一處理器22、一第二無線通訊模組23、一動力驅動器24以及一偵測單元25。處理器22容置於載具主體21內。第二無線通訊模組23容置於載具主體21內並與處理器22電連接,且第二無線通訊模組23與控制器1的第一無線通訊模組12連結以接收控制訊號,再將控制訊號傳遞至處理器22。動力驅動器24設置於載具主體21且電連接處理器22,使處理器22根據控制訊號來驅動動力驅動器24,推動飛行載具2開始根據控制訊號開始作動。偵測單元25設置於載具主體21且電連接處理器22與第二無線通訊模組23,偵測單元25產生一偵測訊號並傳遞至處理器22與第二無線通訊模組23。Please refer to Figure 1 and Figure 2A. Figure 1 is a schematic diagram of the miniature detection device of the present invention, and Figure 2A is a block diagram of the detection device of the present application. The present application provides a
請參閱第2B圖,第2B圖為本案動力驅動器的方塊示意圖。動力驅動器24具有複數個導流單元241、複數個導流通道242、複數個閥243及一匯流腔室244。該些導流單元241的區域形成一驅動區241A,該些導流通道242連接於該驅動區241A且與該些導流單元241相連通,用於傳遞導流單元241導入之流體,該些閥243則分別連接該些導流通道242,再連接該匯流腔室244,透過該些閥243的開啟或關閉來調控匯流腔室244內的流體與其壓力;驅動區241A內的該些導流單元241汲取流體導入該些導流通道242內,再利用該些閥243來調控匯聚於匯流腔室244的流體的流量以及壓力,最後將匯流腔室244內的流體排出,產生推力用以推動飛行載具2,使得動力驅動器24透過持續的汲取、排除流體的動作所產生的推力來推動飛行載具2位移。Please refer to Fig. 2B. Fig. 2B is a block diagram of the power drive of this case. The
其中,上述之控制器1可為一可攜式電子裝置,如智慧型手機、平板電腦、筆記型電腦等其中之一。透過可攜式電子裝置作為控制器1來控制飛行載具2的位移,以及接收飛行載具2的偵測單元25經由第二無線通訊模組23發送之偵測訊號回傳至控制器1(可攜式電子裝置),供使用者知悉。Wherein, the
此外,偵測單元25可以是一影像偵測單元,用來傳遞飛行載具2於飛行移動時所拍攝的影像,並將影像回傳至控制器1,供使用者觀測;或是偵測單元25可以是紅外線偵測單元,可用來偵測人體或是火源等;偵測單元25也可以是空氣偵測單元,用來檢測氣體的含量,確認空氣的狀況;此外,偵測單元25也可以是光學雷達偵測單元,利用光或雷射成像用以檢測。In addition, the
請先參閱第3A圖與第3B圖,第3A圖為本案導流單元之結構示意圖、第3B圖為本案致動件之結構示意圖。該些導流單元241分別包含有一基座2411、一入口板2412、一共振板2413、一間隔件2414、一致動件2415及一出口件2416。基座2411設有一流入孔2411a。入口板2412設置於基座2411的一方(如下方,並不以此為限),且入口板2412具有至少一流入口2412a,流入口2412a與基座2411的流入口2412a相通。共振板2413設置於基座2411的另一方(如上方並不以此為限),並且與入口板2412相對地間隔設置,共振板2413具有一中心穿孔2413a、一可動部2413b及一固定部2413c。中心穿孔2413a位於共振板2413的中心位置並且與基座2411的流入孔2411a垂直對應,可動部2413b則位於中心穿孔2413a的周緣並且與流入口2412a對應的區域,使得可動部2413b能夠於流入孔2411a的位置上下振動,固定部2413c位於共振板2413的周緣區域,用以固定於基座2411。間隔件2414設置於共振板2413的固定部2413c,且其中央區域凹陷與共振板2413定義出一間隔腔室2414a。致動件2415設置於間隔件2414上,具有一振動部2415a、一外框部2415b、複數個連接部2415c、複數個空隙2415d及一壓電件2415e,振動部2415a位於致動件2415的中央,並且與間隔腔室2414a垂直對應,該些連接部2415c設置於振動部2415a與外框部2415b之間,連接兩者且彈性支撐振動部2415a,該些空隙2415d形成於振動部2415a、外框部2415b與該些連接部2415c之間,供流體通過,壓電件2415e則是貼附振動部2415a。出口件2416具有一框板2416a及一蓋板2416b,框板2416a疊置於致動件2415的外框部2415b,且其中央凹陷與致動件2415的振動部2415a定義一出口腔室2416c,蓋板2416b疊置於框板2416a且其中央具有一流出口2416d;其中,壓電件2415e因壓電效應開始產生形變,故而帶動其貼附之致動件2415的振動部2415a於出口腔室2416c與間隔腔室2414a之間上下振動,藉此改變出口腔室2416c與間隔腔室2414a的容積,來改變兩者內部的壓力因而產生壓力梯度,促使流體得以由流入口2412a進入,通過流入孔2411a、中心穿孔2413a、空隙2415d,最後由流出口2416d排出,來輸送流體。Please refer to Figures 3A and 3B first. Figure 3A is a schematic diagram of the structure of the diversion unit of the project, and Figure 3B is a schematic diagram of the structure of the actuator of the project. The
請繼續參閱第3C圖至第3D圖所示,第3C圖與第3D圖為本案導流單元之作動示意圖。當壓電件2415e利用壓電效應來帶動致動件2415,請先參考第3C圖,壓電件2415e引領致動件2415的振動部2415a向上位移,且利用共振效應來同步帶動共振板2413的可動部2413b向上位移。由於振動部2415a朝向出口件2416移動,將會使間隔腔室2414a的容積大幅提升,開始汲取流入口2412a內的流體進入間隔腔室2414a,同時,由於共振板2413的可動部2413b向上移動,令基座2411的流入孔2411a內的容積提升,在加上流入孔2411a的流體開始導入間隔腔室2414a,使得流入孔2411a也同樣為負壓的狀態,透過入口板2412的流入口2412a汲取導流單元241外的流體大量進入流入孔2411a。再參考第3D圖,壓電件2415e引導致動件2415的振動部2415a向下位移,且透過共振效應同步連動共振板2413的可動部2413b向下位移。當振動部2415a向下位移時,開始擠壓間隔腔室2414a的流體急速往出口腔室2416c流動,使出口腔室2416c的壓力遽增,開始由流出口2416d排除流體。同時,由於間隔腔室2414a與出口腔室2416c的流體急速地往流出口2416d排除,使得間隔腔室2414a與出口腔室2416c內呈現負壓狀態,使流體持續地由流入口2412a進入。如此重複上述兩步驟,將使流體能夠持續的從流入口2412a進入,通過流入孔2411a、中心穿孔2413a、間隔腔室2414a、空隙2415d、出口腔室2416c,最後由流出口2416d排除,用以輸送流體。Please continue to refer to Figures 3C to 3D. Figures 3C and 3D are schematic diagrams of the operation of the diversion unit of this project. When the
請參閱第4A圖,第4A圖為本案導流單元並聯示意圖。本案之該些導流單元241可由並聯方式排列設置以形成驅動區241A。第4A圖以兩個導流單元241作說明,但不此以為限。當導流單元241以並聯方式排列時,相鄰的導流單元241可共用相同的基座2411、入口板2412、共振板2413、間隔件2414、致動件2415、出口件2416,並分別於各元件不同區域完成相關結構,當基座2411、入口板2412、共振板2413、間隔件2414、致動件2415、出口件2416堆疊後即可完成多個並聯排列之導流單元241。Please refer to Figure 4A. Figure 4A is a schematic diagram of the parallel connection of diversion units in this case. The guiding
請參閱第4B圖,第4B圖為本案導流單元串聯示意圖。本案之該些導流單元241可由串連方式排列設置,形成驅動區241A,第4B圖以兩個導流單元241作說明,但不以此為限。當導流單元241以串連方式排列時,透過一固定結構245將兩個導流單元241垂直間隔設置後固定,串聯之導流單元241之間定義出一串聯腔室2451,而固定結構245設有一串聯出口2452,使串聯後的導流單元241得以將流體導送至串聯腔室2451後,再集中於串聯出口2452一併排出。Please refer to Figure 4B. Figure 4B is a schematic diagram of the series connection of the diversion units in this project. The
請參閱第4C圖,第4C圖為本案導流單元串並聯示意圖。本案之該些導流單元241可由串並聯方式排列設置,形成驅動區241A,第4C圖以四個導流單元241作說明,但不以此為限。串並聯方式係先將導流單元241以並聯方式排列,再將並聯後的導流單元241透過固定結構245串聯起來,使串並聯後的導流單元241可將流體都先於串聯腔室2451集中,最後由串聯出口2452一併排除。Please refer to Figure 4C. Figure 4C is a schematic diagram of the series and parallel connection of the diversion units in this case. In this case, the
請先參閱第5A圖,第5A圖為本案動力驅動器之閥之第一實施例的結構示意圖。本案的閥243皆分別包含有一通道基座2431、一第一通道2432、一第二通道2433、一作動片2434、一壓電片2435及一封閉件2436。通道基座2431具有一基座表面2431a,並於基座表面2431a凹陷來形成一閥腔室2431b。第一通道2432位於通道基座2431內,第一通道2432的一端作為一進流口2432a供驅動區241A連接,另一端則與閥腔室2431b相連通。第二通道2433同樣位於通道基座2431內,且具有一連通區2433a與一出口區2433b,連通區2433a與出口區2433b相互垂直且相連通,連通區2433a位於出口區2433b與閥腔室2431b之間,其一端連通於出口區2433b,另一端連通於閥腔室2431b,使出口區2433b與閥腔室2431b相通。作動片2434設置於基座表面2431a且封蓋閥腔室2431b,作動片2434具有一第一作動表面2434a及一第二作動表面2434b。壓電片2435則是貼附於作動片2434的第一作動表面2434a。封閉件2436具有一阻塞部2436a及一連桿2436b,連桿2436b穿設於第二通道2433的連通區2433a,其一端連接阻塞部2436a,另一端連接作動片2434的第二作動表面2434b;其中,阻塞部2436a的截面積大於第二通道2433其連通區2433a的截面積,連桿2436b的長度大於第二通道2433其連通區2433a的長度。Please refer to Fig. 5A first. Fig. 5A is a structural diagram of the first embodiment of the valve of the power actuator of the present invention. The
承上所述,當壓電片2435尚未作動時,閥243為開啟狀態(如第5A圖),由於連桿2436b長度大於連通區2433a的長度與閥腔室2431b深度之和,使得當作動片2434呈水平狀時,阻塞部2436a將不會封閉第二通道2433中連通區2433a及出口區2433b相連的位置,使連通區2433a與出口區2433b彼此相通,流體得以由第一通道2432的進流口2432a進入,流入閥腔室2431b,最後通過連通區2433a與出口區2433b流出。請再參閱第5B圖,第5B圖為本案動力驅動器之閥的封閉示意圖。當壓電片2435產生形變且透過應力帶動作動片2434朝遠離通道基座2431的方向彎曲,同時將封閉件2436的連桿2436b拉起,使得封閉件2436的阻塞部2436a緊抵第二通道2433中連通區2433a及出口區2433b相連的位置,封閉連通區2433a,來使閥243關閉,透過壓電片2435來控制閥的開啟或關閉,以進一步控制流入匯流腔室244的流體其流量與壓力。As mentioned above, when the
請參閱第6A圖,第6A圖為本案本案動力驅動器之閥之第二實施例的結構示意圖。其結構與上一實施例大致相同,故不加以贅述,其差異點在於本實施例之連桿2436b長度等於連通區2433a的長度與閥腔室2431b深度之和,故壓電片2435尚未作動時,阻塞部2436a便緊抵於連通區2433a及出口區2433b相連,將連通區2433a與出口區2433b阻隔開來,流體無法通過,使閥243呈現關閉狀態,故本實施例之閥243為常閉狀態。再參閱第6B圖,當壓電片2435產生形變且透過應力帶動作動片2434朝接近通道基座2431的方向彎曲,同時推動封閉件2436的連桿2436b,使得封閉件2436的阻塞部2436a離開第二通道2433中連通區2433a及出口區2433b相連的位置,使得連通區2433a與出口區2433b相通,來使閥243開啟。此實施例與第一實施例同樣是利用壓電片2435來控制閥243的開啟或關閉,以進一步控制流入匯流腔室244的流體其流量與壓力。Please refer to Fig. 6A. Fig. 6A is a schematic structural diagram of the second embodiment of the valve of the power actuator in this case. Its structure is roughly the same as the previous embodiment, so it will not be repeated. The difference is that the length of the connecting
綜上所述,本案提供一種微型偵測裝置,利用多個導流單元搭配導流通道、閥以及匯流腔室所組成之動力驅動器,利用傳輸流體所產生的推力來推動飛行載具,使飛行載具可透過推力來移動,並透過設置於飛行載具上的偵測單元來提供相關的偵測訊號,並回傳至使用者端的控制器,利用導流單元的動力驅動器可將體積縮小、重量減輕,對於飛行載具來說更加有利,並且具有極具產業之利用價值,爰依法提出申請。In summary, this project provides a miniature detection device that uses a power driver composed of multiple diversion units with diversion channels, valves, and confluence chambers, and uses the thrust generated by the transmission fluid to propel the flying vehicle to make the flight The vehicle can be moved by thrust, and the detection unit provided on the flight vehicle provides relevant detection signals, which are transmitted back to the controller on the user side. The power driver of the guide unit can reduce the volume, Weight reduction is more advantageous for flying vehicles and has great industrial use value, so an application is filed in accordance with the law.
本案得由熟習此技術之人士任施匠思而為諸般修飾,然皆不脫如附申請專利範圍所欲保護者。This case can be modified in many ways by those who are familiar with this technology, but it is not deviated from the protection of the patent application.
100:微型偵測裝置100: Miniature detection device
1:控制器1: Controller
11:操作區11: Operating area
12:第一無線通訊模組12: The first wireless communication module
2:飛行載具2: flying vehicle
21:載具主體21: Vehicle body
22:處理器22: processor
23:第二無線通訊模組23: The second wireless communication module
24:動力驅動器24: Power Drive
241:導流單元241: Diversion unit
2411:基座2411: Pedestal
2411a:流入孔2411a: Inflow hole
2412:入口板2412: entrance plate
2412a:流入口2412a: Inlet
2413:共振板2413: Resonance plate
2413a:中心穿孔2413a: Center perforation
2413b:可動部2413b: movable part
2413c:固定部2413c: fixed part
2414:間隔件2414: spacer
2414a:間隔腔室2414a: compartment
2415:致動件2415: Actuator
2415a:振動部2415a: Vibration Department
2415b:外框部2415b: Outer frame
2415c:連接部2415c: connecting part
2415d:空隙2415d: gap
2415e:壓電件2415e: Piezoelectric
2416:出口件2416: export parts
2416a:框板2416a: frame plate
2416b:蓋板2416b: cover
2416c:出口腔室2416c: exit the oral cavity
2416d:流出口2416d: Outlet
241A:驅動區241A: Drive area
242:導流通道242: diversion channel
243:閥243: Valve
2431:通道基座2431: Channel base
2431a:基座表面2431a: Base surface
2431b:閥腔室2431b: valve chamber
2432:第一通道2432: the first channel
2432a:進流口2432a: Inlet
2433:第二通道2433: second channel
2433a:連通區2433a: Connected area
2433b:出口區2433b: export zone
2434:作動片2434: Actuator
2434a:第一作動表面2434a: first actuation surface
2434b:第二作動表面2434b: second acting surface
2435:壓電片2435: Piezoelectric sheet
2436:封閉件2436: closure
2436a:阻塞部2436a: obstruction
2436b:連桿2436b: connecting rod
244:匯流腔室244: Confluence Chamber
245:固定結構245: fixed structure
2451:串聯腔室2451: series chamber
2452:串聯出口2452: series outlet
25:偵測單元25: Detection unit
第1圖為本案微型偵測裝置的示意圖。 第2A圖為本案偵測裝置的方塊示意圖。 第2B圖為本案動力驅動器的方塊示意圖。 第3A圖為本案導流單元之結構示意圖。 第3B圖為本案致動件之結構示意圖。 第3C圖、第3D圖為本案導流單元之作動示意圖。 第4A圖為本案導流單元並聯示意圖。 第4B圖為本案導流單元串聯示意圖。 第4C圖為本案導流單元串並聯示意圖。 第5A圖為本案動力驅動器之閥之第一實施例的結構示意圖。 第5B圖為本案動力驅動器之閥之第一實施例作動示意圖。 第6A圖為本案動力驅動器之閥之第二實施例的結構示意圖。 第6B圖為本案動力驅動器之閥之第二實施例作動示意圖。 Figure 1 is a schematic diagram of the micro-detection device in this case. Figure 2A is a block diagram of the detection device in this case. Figure 2B is a block diagram of the power drive of the present invention. Figure 3A is a schematic diagram of the structure of the diversion unit of the project. Figure 3B is a schematic diagram of the structure of the actuator in this case. Figure 3C and Figure 3D are schematic diagrams of the operation of the diversion unit of this project. Figure 4A is a schematic diagram of the parallel connection of the diversion units of this project. Figure 4B is a schematic diagram of the diversion unit connected in series in this case. Figure 4C is a schematic diagram of the series and parallel connection of the diversion units in this case. Figure 5A is a schematic structural view of the first embodiment of the valve of the power actuator of the present invention. Figure 5B is a schematic diagram of the operation of the first embodiment of the valve of the power actuator of the present invention. Figure 6A is a schematic structural view of the second embodiment of the valve of the power actuator of the present invention. Figure 6B is a schematic diagram of the operation of the second embodiment of the valve of the power actuator of the present invention.
100:微型偵測裝置 100: Miniature detection device
1:控制器 1: Controller
11:操作區 11: Operating area
12:第一無線通訊模組 12: The first wireless communication module
2:飛行載具 2: flying vehicle
21:載具主體 21: Vehicle body
22:處理器 22: processor
23:第二無線通訊模組 23: The second wireless communication module
24:動力驅動器 24: Power Drive
25:偵測單元 25: Detection unit
Claims (11)
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CN112078823A (en) * | 2019-06-14 | 2020-12-15 | 研能科技股份有限公司 | Miniature detection device |
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TWM339478U (en) * | 2007-10-23 | 2008-09-01 | Shan-Le Shi | Remote-controlled airdrop flying device having imaging capturing function |
CN102105357A (en) * | 2008-05-30 | 2011-06-22 | 吉洛工业有限公司 | A flying machine comprising twin contra-rotating vertical axis propellers |
CN204822096U (en) * | 2015-06-10 | 2015-12-02 | 刘亚敏 | Unmanned aircraft |
CN205168902U (en) * | 2015-11-21 | 2016-04-20 | 深圳市易特科信息技术有限公司 | A unmanned vehicles for environment toxic gas detects |
TWM588087U (en) * | 2019-06-14 | 2019-12-21 | 研能科技股份有限公司 | Micro detecting device |
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TWM339478U (en) * | 2007-10-23 | 2008-09-01 | Shan-Le Shi | Remote-controlled airdrop flying device having imaging capturing function |
CN102105357A (en) * | 2008-05-30 | 2011-06-22 | 吉洛工业有限公司 | A flying machine comprising twin contra-rotating vertical axis propellers |
CN204822096U (en) * | 2015-06-10 | 2015-12-02 | 刘亚敏 | Unmanned aircraft |
CN205168902U (en) * | 2015-11-21 | 2016-04-20 | 深圳市易特科信息技术有限公司 | A unmanned vehicles for environment toxic gas detects |
TWM588087U (en) * | 2019-06-14 | 2019-12-21 | 研能科技股份有限公司 | Micro detecting device |
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