WO2024065915A1 - 一种检测被动式房屋碳排放的装置 - Google Patents

一种检测被动式房屋碳排放的装置 Download PDF

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Publication number
WO2024065915A1
WO2024065915A1 PCT/CN2022/127277 CN2022127277W WO2024065915A1 WO 2024065915 A1 WO2024065915 A1 WO 2024065915A1 CN 2022127277 W CN2022127277 W CN 2022127277W WO 2024065915 A1 WO2024065915 A1 WO 2024065915A1
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assembly
guide
metal
carbon emissions
split
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PCT/CN2022/127277
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English (en)
French (fr)
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鲍海君
汪凝
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浙大城市学院
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Publication of WO2024065915A1 publication Critical patent/WO2024065915A1/zh

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U60/00—Undercarriages
    • B64U60/40—Undercarriages foldable or retractable
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N33/00—Investigating or analysing materials by specific methods not covered by groups G01N1/00 - G01N31/00
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications

Definitions

  • the present invention relates to the technical field of carbon emission detection equipment, and in particular to a device for detecting carbon emission of a passive house.
  • Passive houses also known as passive energy-saving houses, are energy-saving buildings built based on passive design. Passive houses can adjust the indoor temperature to a suitable level with very little energy consumption, which is very environmentally friendly. During the use of passive houses, carbon emissions will be emitted from their exhaust vents. When passive houses are put into production, carbon emissions from passive houses need to be tested. However, when testing carbon emissions from passive houses, it is necessary to manually climb to the outlet and then use instruments to test it, which is very inconvenient and dangerous. No corresponding improvements have been made to this defect.
  • the present invention provides a device for detecting carbon emissions of passive houses.
  • a device for detecting carbon emissions of passive houses which is arranged on the metal rain cap on the top of the chimney. It includes a drone, a guide assembly and two landing gear assemblies.
  • the two landing gear assemblies are arranged at the bottom of the drone, and the guide assembly is arranged at the bottom of the two landing gear assemblies, and the guide assembly includes two split assemblies.
  • the two split assemblies correspond to the two landing gear assemblies one by one, and the split assembly is linked to the landing gear assembly.
  • the split assembly includes a plurality of guide metal rings and connecting belts from small to large.
  • the connecting belt is arranged between two adjacent guide metal rings, and the plurality of guide metal rings are movably connected to each other. It also includes a fixed grab assembly, which is movably arranged at the bottom of the drone.
  • the landing support assembly comprises a ring seat, a clamping joint, a bracket seat and a transverse telescopic rod.
  • the transverse telescopic rod is transversely arranged at the bottom of the drone, and the bracket seat is arranged on the movable end of the transverse telescopic rod.
  • the clamping joint is arranged at the bottom of the bracket seat, and the ring seat is detachably clamped on the clamping joint.
  • the ring seat is connected to the split assembly.
  • the landing support assembly further comprises an electromagnet, and the electromagnet is arranged on the support seat. Two electromagnets located on different support seats attract each other.
  • the fixed grabbing assembly includes a metal cap head and a main conductor.
  • One end of the main conductor is arranged at the bottom of the drone, and the other end is detachably connected to the metal cap head.
  • the metal cap head is linked to the split assembly.
  • the fixed grabbing assembly further comprises four air detectors and an inwardly curved multi-segment folding frame.
  • the four multi-segment folding frames are hinged on the metal cap head at equal angles with the metal cap head as the center.
  • the air detector is arranged on one end of the multi-segment folding frame away from the metal cap head.
  • the fixed grabbing assembly further comprises four guide plates.
  • the guide plates are arranged on the outside of the air detector.
  • the width of the guide plates is greater than the gap distance between two adjacent guide metal rings.
  • it further comprises two cassettes and a cassette holder, wherein the cassette holder is arranged on the guide metal ring with the smallest caliber.
  • One end of the cassette is detachably connected to the cassette holder, and the other end is connected to the metal cap head.
  • the split assembly further comprises a plurality of secondary conductors, which correspond one to one with the plurality of guide metal rings, one end of the secondary conductor being electrically connected to the guide metal ring, and the other end being connected in series with the metal cap head through the main conductor.
  • it further comprises a plurality of abutment plates and telescopic rods, wherein the plurality of telescopic rods correspond to the plurality of air detectors one by one.
  • the telescopic rods are vertically arranged on the drone, and the movable ends of the telescopic rods pass through the drone and extend to the bottom of the drone.
  • the abutment plates are arranged on the movable ends of the telescopic rods.
  • the abutment plates correspond to the air detectors.
  • the present invention provides a device for detecting carbon emissions from passive houses. It has the following beneficial effects:
  • the device for detecting carbon emissions of passive houses cooperates with each other through the drone, the guide assembly and the two landing bracket assemblies.
  • the present invention can use the drone to deliver the carbon emission detection device to the chimney and fix it, and can also effectively avoid the shielding of the metal rain cap on the chimney and allow the detector to smoothly correspond to the chimney outlet. It is greatly convenient for personnel to use.
  • FIG1 is a first stereogram of the present invention
  • FIG2 is a second stereoscopic view of the present invention.
  • FIG3 is a third stereogram of the present invention.
  • FIG4 is a front cross-sectional view of the present invention.
  • FIG5 is a perspective view of a first partial component of the present invention.
  • FIG6 is a front view of a first partial component of the present invention.
  • FIG7 is a perspective view of a second partial component of the present invention.
  • FIG8 is a perspective view of a third partial component of the present invention.
  • FIG. 9 is an enlarged view of point A in FIG. 2 of the present invention.
  • the embodiment of the present invention provides a device for detecting carbon emissions of passive houses, as shown in Figures 1-9, which is arranged on the metal rain cap 2 on the top of the chimney 1. It includes a drone 5, a guide assembly 3 and two landing gear assemblies 6. The two landing gear assemblies 6 are arranged at the bottom of the drone 5, and the guide assembly 3 is arranged at the bottom of the two landing gear assemblies 6.
  • the guide assembly 3 includes two split assemblies 7. The two split assemblies 7 correspond to the two landing gear assemblies 6 one by one, and the split assembly 7 is linked to the landing gear assembly 6.
  • the split assembly 7 includes a plurality of guide metal rings 11 from small to large and a connecting belt 17.
  • the connecting belt 17 is arranged between two adjacent guide metal rings 11, and the plurality of guide metal rings 11 are movably connected to each other. It also includes a fixed grab assembly 16, which is movably arranged at the bottom of the drone 5.
  • the diameter of the metal rain cap 2 can be measured physically through the guide metal rings 11 of different sizes and contacting with the outer surface of the metal rain cap 2. In this way, it is convenient to adjust the fixed grabbing assembly 16, effectively ensuring that the air detector 15 corresponds to the air outlet of (1), which is convenient for personnel to use.
  • the landing support assembly 6 includes a ring seat 9, a clamping joint 13, a bracket seat 12 and a transverse telescopic rod 10.
  • the transverse telescopic rod 10 is transversely arranged at the bottom of the UAV 5, and the bracket seat 12 is arranged on the movable end of the transverse telescopic rod 10.
  • the clamping joint 13 is arranged at the bottom of the bracket seat 12, and the ring seat 9 is detachably clamped on the clamping joint 13.
  • the ring seat 9 is connected to the split assembly 7.
  • the landing support assembly 6 further comprises an electromagnet 8, which is arranged on a support seat 12. Two electromagnets 8 located on different support seats 12 attract each other.
  • the fixed grab assembly 16 includes a metal cap head 18 and a main conductor 19. One end of the main conductor 19 is arranged at the bottom of the drone 5, and the other end is detachably connected to the metal cap head 18. The metal cap head 18 is linked to the split assembly 7.
  • the fixed grab assembly 16 also includes four air detectors 15 and an inwardly curved multi-section folding frame 21.
  • the four multi-section folding frames 21 are hinged to the metal cap head 18 at equal angles with the metal cap head 18 as the center.
  • the air detector 15 is arranged on one end of the multi-section folding frame 21 away from the metal cap head 18.
  • the fixed grab assembly 16 further comprises four guide plates 22.
  • the guide plates 22 are arranged on the outside of the air detector 15.
  • the width of the guide plates 22 is greater than the gap distance between two adjacent guide metal rings 11.
  • the guide plate 22 when the multi-stage folding frame 21 is pressed down and bent, the guide plate 22 is subjected to a lateral force and is simultaneously stuck by the guide metal ring 11, thereby preventing the multi-stage folding frame 21 from being stuck.
  • the utility model also comprises two cassettes 23 and a cassette seat 24, wherein the cassette seat 24 is arranged on the guide metal ring 11 with the smallest diameter.
  • One end of the cassette 23 is detachably connected with the cassette seat 24, and the other end is connected with the metal cap head 18.
  • the split component 7 further includes a plurality of secondary conductors 20.
  • the plurality of secondary conductors 20 correspond one to one with the plurality of guide metal rings 11.
  • One end of the secondary conductor 20 is electrically connected to the guide metal ring 11, and the other end is connected in series with the metal cap head 18 through the main conductor 19.
  • the plurality of secondary wires 20 are connected to the guide metal rings 11, so that during the continuous falling process of the drone 5, the guide metal rings 11 of different sizes fall on the metal rain cap 2 in sequence.
  • the nearest guide metal ring 11 does not fall on the metal rain cap 2, that is, the electrical circuit of the guide metal ring 11 is not connected, and is in a disconnected state, so the edge position of the metal rain cap 2 is determined by powering off and on. This facilitates the position adjustment of the air detector 16 and ensures its detection effect.
  • the invention also includes a plurality of abutment plates 14 and telescopic rods 4, and the plurality of telescopic rods 4 correspond to a plurality of air detectors 15.
  • the telescopic rods 4 are vertically arranged on the drone 5, and the movable ends of the telescopic rods 4 pass through the drone 5 and extend to the bottom of the drone 5.
  • the abutment plates 14 are arranged on the movable ends of the telescopic rods 4.
  • the abutment plates 14 correspond to the air detectors 15.
  • the present invention can then judge the actual area of the metal rain cap 2 by the passage on the specific guide metal ring 11, and then press and bend the multi-segment folding frame 21 through the telescopic rod 4 according to the feedback, so that the distance from the multi-segment folding frame 21 to the metal cap head 18 is close to the radius of the metal rain cap 2, and then control the card seat 24 to disconnect the card belt 23 from the card seat 24, and at the same time disconnect the main wire 19 from the metal cap head 18.
  • the electromagnet 8 is powered off, and the horizontal telescopic rod 10 is controlled to extend, forcing the two split components 7 to separate, thereby exposing the fixed grabbing component 16 located in the two split components 7, and then under the action of gravity, the multi-segment folding frame 21 flips over, so that the air detector 15 just corresponds to the air outlet between the metal rain cap 2 and the chimney 1.
  • the device for detecting carbon emissions of passive houses cooperates with each other through the drone 5, the guide assembly 3 and the two landing bracket assemblies 6.
  • the present invention can use the drone to deliver the carbon emission detection device to the chimney 1 and fix it, and can also effectively avoid the shielding of the metal rain cap 2 on the chimney 1 and allow the detector to smoothly correspond to the air outlet of the chimney 1, which greatly facilitates the use of personnel.

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Abstract

一种检测被动式房屋碳排放的装置，设置在烟囱（1）顶部的金属防雨帽（2）上，包括无人机（5）、导向组件（3）和两个起落支架组件（6），两个起落支架组件（6）设置在无人机（5）的底部，所述导向组件（3）设置在两个起落支架组件（6）的底部，所述导向组件（3）包括两个分体组件（7），所述两个分体组件（7）与两个起落支架组件（6）一一对应，所述分体组件（7）与起落支架组件（6）联动连接。该检测被动式房屋碳排放的装置，通过设置的无人机（5）、导向组件（3）和两个起落支架组件（6）相互配合，具有利用无人机（5）将碳排放检测装置送到烟囱（1）并固定的功能，同时也可以有效避开烟囱（1）上的金属防雨帽（2）的遮挡并让空气检测器（15）顺利与烟囱（1）的出风口相对应，大大方便人员的使用。

Description

一种检测被动式房屋碳排放的装置 技术领域
本发明涉及碳排放检测设备技术领域，具体为一种检测被动式房屋碳排放的装置。
背景技术
被动式房屋又可称为被动式节能屋，是基于被动式设计而建造的节能建筑物，被动式房屋可以用非常小的能耗将室内调节到合适的温度，非常环保，被动式房屋在使用的过程中，其排风口中会进行碳排放，在被动式房屋投入生产时，需要对被动式房屋的碳排放进行检测。但是目前在对被动式房屋的碳排放进行检测时，需要人工攀爬到出风口的位置，然后用仪器对其进行检测工作，十分的不便，而且还具有危险性，没有对此缺陷进行相应的改进。
发明内容
(一)解决的技术问题
针对现有技术的不足，本发明提供了一种检测被动式房屋碳排放的装置。
(二)技术方案
为实现以上目的，本发明通过以下技术方案予以实现：一种检测被动式房屋碳排放的装置，设置在烟囱顶部的金属防雨帽上。包括无人机、导向组件和两个起落支架组件。两个起落支架组件设置在无人机的底部，所述导向组件设置在两个起落支架组件的底部，所述导向组件包括两个分体组件。所述两个分体组件与两个起落支架组件一一对应，所述分体组件与起落支架组件联动连接。所述分体组件包括多个由小到大的导向金属环和连接带。所述连接带设置在两个相邻导向金属环之间，多个导向金属环相互活动套接。还包括固定抓取组件，所述固定抓取组件活动设置在无人机的底部。
优选的，所述起落支架组件包括环座、卡接头、支架座和横向伸缩杆。所述横向伸缩杆横向设置在无人机的底部，所述支架座设置在横向伸缩杆的 活动端上。所述卡接头设置在支架座的底部，所述环座可拆卸式卡接在卡接头上。所述环座与分体组件相连。
优选的，所述起落支架组件还包括电磁铁，所述电磁铁设置在支架座上。两个位于不同支架座上的电磁铁相互吸引。
优选的，所述固定抓取组件包括金属帽头和主导线。所述主导线的一端设置在无人机的底部，另一端与金属帽头可拆卸式卡接。所述金属帽头与分体组件联动连接。
优选的，所述固定抓取组件还包括四个空气检测器和向内弯曲多段折叠架。所述四个多段折叠架以金属帽头为中心等角度铰接在金属帽头上。所述空气检测器设置在多段折叠架远离金属帽头的一端上。
优选的，所述固定抓取组件还包括四个导向板。所述导向板设置在空气检测器的外侧。所述导向板的宽度大于相邻两个导向金属环之间的缝隙距离。
优选的，还包括两个卡带和卡座，所述卡座设置在口径最小的导向金属环上。所述卡带的一端与卡座可拆卸式卡接，另一端与金属帽头相连。
优选的，所述分体组件还包括多个副导线。多个副导线与多个导向金属环一一对应。所述副导线的一端与导向金属环电性连接，另一端通过主导线与金属帽头串联。
优选的，还包括多个抵板和伸缩杆，多个伸缩杆与多个空气检测器一一对应。所述伸缩杆竖直设置在无人机上，所述伸缩杆的活动端穿过无人机并延伸至无人机的底部。所述抵板设置在伸缩杆的活动端上。所述抵板与空气检测器相对应。
(三)有益效果
本发明提供了一种检测被动式房屋碳排放的装置。具备以下有益效果：
1、该检测被动式房屋碳排放的装置，通过设置的无人机、导向组件和两个起落支架组件相互配合。可以让本发明具有利用无人机将碳排放检测装置 送到烟囱并固定的功能，同时也可以有效避开烟囱上的金属防雨帽的遮挡并让该检测器顺利与烟囱的出风口相对应。大大方便人员的使用。
附图说明
图1为本发明第一立体图；
图2为本发明第二立体图；
图3为本发明第三立体图；
图4为本发明正面剖视图；
图5为本发明第一局部部件立体图；
图6为本发明第一局部部件正视图；
图7为本发明第二局部部件立体图；
图8为本发明第三局部部件立体图；
图9为本发明图2中A处放大图。
图中：1烟囱、2金属防雨帽、3导向组件、4伸缩杆、5无人机、6起落支架组件、7分体组件、8电磁铁、9环座、10横向伸缩杆、11导向金属环、12支架座、13卡接头、14抵板、15空气检测器、16固定抓取组件、17连接带、18金属帽头、19主导线、20副导线、21多段折叠架、22导向板、23卡带、24卡座。
具体实施方式
本发明实施例提供一种检测被动式房屋碳排放的装置，如图1-9所示，设置在烟囱1顶部的金属防雨帽2上。包括无人机5、导向组件3和两个起落支架组件6。两个起落支架组件6设置在无人机5的底部，导向组件3设置在两个起落支架组件6的底部，导向组件3包括两个分体组件7。两个分体组件7与两个起落支架组件6一一对应，分体组件7与起落支架组件6联动连接。分体组件7包括多个由小到大的导向金属环11和连接带17。连接带17设置在两个相邻导向金属环11之间，多个导向金属环11相互活动套接。还包括 固定抓取组件16，固定抓取组件16活动设置在无人机5的底部。
通过设置的多个由小到大的导向金属环11和连接带17相互配合，这样一来，通过不同尺寸的导向金属环11并与金属防雨帽2的外表面接触，进而可以通过物理方式测量金属防雨帽2的直径。这样一来，方便对固定抓取组件16进行调节，有效保证将空气检测器15与(1)的出风口相对应，方便人员的使用。
起落支架组件6包括环座9、卡接头13、支架座12和横向伸缩杆10。横向伸缩杆10横向设置在无人机5的底部，支架座12设置在横向伸缩杆10的活动端上。卡接头13设置在支架座12的底部，环座9可拆卸式卡接在卡接头13上。环座9与分体组件7相连。
起落支架组件6还包括电磁铁8，电磁铁8设置在支架座12上。两个位于不同支架座12上的电磁铁8相互吸引。
固定抓取组件16包括金属帽头18和主导线19。主导线19的一端设置在无人机5的底部，另一端与金属帽头18可拆卸式卡接。金属帽头18与分体组件7联动连接。
固定抓取组件16还包括四个空气检测器15和向内弯曲多段折叠架21。四个多段折叠架21以金属帽头18为中心等角度铰接在金属帽头18上。空气检测器15设置在多段折叠架21远离金属帽头18的一端上。
固定抓取组件16还包括四个导向板22。导向板22设置在空气检测器15的外侧。导向板22的宽度大于相邻两个导向金属环11之间的缝隙距离。
通过设置的导向板22，可以在对多段折叠架21进行下压弯折时，导向板22会受到横向力，同时受到导向金属环11卡住。防止多段折叠架21被卡住。
还包括两个卡带23和卡座24，卡座24设置在口径最小的导向金属环11上。卡带23的一端与卡座24可拆卸式卡接，另一端与金属帽头18相连。
分体组件7还包括多个副导线20。多个副导线20与多个导向金属环11 一一对应。副导线20的一端与导向金属环11电性连接，另一端通过主导线19与金属帽头18串联。
通过设置的多个副导线20与导向金属环11相连，这样在无人机5不断下落过程中，不同尺寸的导向金属环11依次落在金属防雨帽2上，当最近一个导向金属环11没有落在金属防雨帽2时，即该导向金属环11的电回路没有联通，进而处于断开状态，因此通过断电通电来判断金属防雨帽2的边缘位置。方便对空气检测器16的位置调节。保证其检测效果。
还包括多个抵板14和伸缩杆4，多个伸缩杆4与多个空气检测器15一一对应。伸缩杆4竖直设置在无人机5上，伸缩杆4的活动端穿过无人机5并延伸至无人机5的底部。抵板14设置在伸缩杆4的活动端上。抵板14与空气检测器15相对应。
工作原理：当遇到带有金属防雨帽2的烟囱1时，控制无人机5悬停空中，接着将固定抓取组件16与主导线19卡接固定。控制无人机5移动到金属防雨帽2的正上方，控制金属帽头18与金属防雨帽2的帽尖上，同时无人机5缓缓下落，此时位于低处的导向金属环11依次与金属防雨帽2相接触，由于金属防雨帽2为金属制，因此当电流从副导线20移动到导向金属环11，接着导向金属防雨帽2，再与金属帽头18相通，在通过主导线19完成通电回路。进而方便本发明在可以通过具体哪个导向金属环11上的通路，来判断金属防雨帽2的实际面积，在根据其反馈，通过伸缩杆4压弯多段折叠架21，进而让多段折叠架21到金属帽头18的距离与金属防雨帽2半径相近，接着控制卡座24使得卡带23与卡座24断开，同时断开主导线19与金属帽头18的连接。接着电磁铁8断电，控制横向伸缩杆10伸出，迫使两个分体组件7分离，进而让位于两个分体组件7之中的固定抓取组件16露出，接着在重力作用下，多段折叠架21翻转，让空气检测器15刚好与金属防雨帽2和烟囱1之前的出风口对应。
综上所述，该检测被动式房屋碳排放的装置，通过设置的无人机5、导向组件3和两个起落支架组件6相互配合。可以让本发明具有利用无人机将碳排放检测装置送到烟囱1并固定的功能，同时也可以有效避开烟囱1上的金属防雨帽2的遮挡并让该检测器顺利与烟囱1的出风口相对应。大大方便人员的使用。

Claims (9)

  1. 一种检测被动式房屋碳排放的装置，设置在烟囱(1)顶部的金属防雨帽(2)上，其特征在于：包括无人机(5)、导向组件(3)和两个起落支架组件(6)，两个起落支架组件(6)设置在无人机(5)的底部，所述导向组件(3)设置在两个起落支架组件(6)的底部，所述导向组件(3)包括两个分体组件(7)，所述两个分体组件(7)与两个起落支架组件(6)一一对应，所述分体组件(7)与起落支架组件(6)联动连接，所述分体组件(7)包括多个由小到大的导向金属环(11)和连接带(17)，所述连接带(17)设置在两个相邻导向金属环(11)之间，多个导向金属环(11)相互活动套接，还包括固定抓取组件(16)，所述固定抓取组件(16)活动设置在无人机(5)的底部。
  2. 根据权利要求1所述的一种检测被动式房屋碳排放的装置，其特征在于：所述起落支架组件(6)包括环座(9)、卡接头(13)、支架座(12)和横向伸缩杆(10)，所述横向伸缩杆(10)横向设置在无人机(5)的底部，所述支架座(12)设置在横向伸缩杆(10)的活动端上，所述卡接头(13)设置在支架座(12)的底部，所述环座(9)可拆卸式卡接在卡接头(13)上，所述环座(9)与分体组件(7)相连。
  3. 根据权利要求2所述的一种检测被动式房屋碳排放的装置，其特征在于：所述起落支架组件(6)还包括电磁铁(8)，所述电磁铁(8)设置在支架座(12)上，两个位于不同支架座(12)上的电磁铁(8)相互吸引。
  4. 根据权利要求3所述的一种检测被动式房屋碳排放的装置，其特征在于：所述固定抓取组件(16)包括金属帽头(18)和主导线(19)，所述主导线(19)的一端设置在无人机(5)的底部，另一端与金属帽头(18)可拆卸式卡接，所述金属帽头(18)与分体组件(7)联动连接。
  5. 根据权利要求4所述的一种检测被动式房屋碳排放的装置，其特征在于：所述固定抓取组件(16)还包括四个空气检测器(15)和向内弯曲多段 折叠架(21)，所述四个多段折叠架(21)以金属帽头(18)为中心等角度铰接在金属帽头(18)上，所述空气检测器(15)设置在多段折叠架(21)远离金属帽头(18)的一端上。
  6. 根据权利要求5所述的一种检测被动式房屋碳排放的装置，其特征在于：所述固定抓取组件(16)还包括四个导向板(22)，所述导向板(22)设置在空气检测器(15)的外侧，所述导向板(22)的宽度大于相邻两个导向金属环(11)之间的缝隙距离。
  7. 根据权利要求6所述的一种检测被动式房屋碳排放的装置，其特征在于：还包括两个卡带(23)和卡座(24)，所述卡座(24)设置在口径最小的导向金属环(11)上，所述卡带(23)的一端与卡座(24)可拆卸式卡接，另一端与金属帽头(18)相连。
  8. 根据权利要求7所述的一种检测被动式房屋碳排放的装置，其特征在于：所述分体组件(7)还包括多个副导线(20)，多个副导线(20)与多个导向金属环(11)一一对应，所述副导线(20)的一端与导向金属环(11)电性连接，另一端通过主导线(19)与金属帽头(18)串联。
  9. 根据权利要求8所述的一种检测被动式房屋碳排放的装置，其特征在于：还包括多个抵板(14)和伸缩杆(4)，多个伸缩杆(4)与多个空气检测器(15)一一对应，所述伸缩杆(4)竖直设置在无人机(5)上，所述伸缩杆(4)的活动端穿过无人机(5)并延伸至无人机(5)的底部，所述抵板(14)设置在伸缩杆(4)的活动端上，所述抵板(14)与空气检测器(15)相对应。
PCT/CN2022/127277 2022-09-28 2022-10-25 一种检测被动式房屋碳排放的装置 WO2024065915A1 (zh)

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