[go: up one dir, main page]

CN105300890A - Gas detection system - Google Patents

Gas detection system Download PDF

Info

Publication number
CN105300890A
CN105300890A CN201510771433.1A CN201510771433A CN105300890A CN 105300890 A CN105300890 A CN 105300890A CN 201510771433 A CN201510771433 A CN 201510771433A CN 105300890 A CN105300890 A CN 105300890A
Authority
CN
China
Prior art keywords
laser
ground
laser light
gas detection
flight
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201510771433.1A
Other languages
Chinese (zh)
Inventor
邢浩
蔡明亮
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ENN Science and Technology Development Co Ltd
Original Assignee
ENN Science and Technology Development Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by ENN Science and Technology Development Co Ltd filed Critical ENN Science and Technology Development Co Ltd
Priority to CN201510771433.1A priority Critical patent/CN105300890A/en
Publication of CN105300890A publication Critical patent/CN105300890A/en
Pending legal-status Critical Current

Links

Landscapes

  • Investigating Or Analysing Materials By Optical Means (AREA)

Abstract

本发明提供了一种气体检测系统。该系统包括地面系统和飞行系统,地面系统包括光电探测器和数据处理装置;飞行系统包括飞行装置、激光发射装置和光路转换装置;激光发射装置用于向被检测区域发射激光;光路转换装置用于接收反射回的激光并转向至光电探测器;光电探测器用于接收反射激光并转换成反射激光参数电信号;数据处理装置用于接收反射激光参数电信号和激光发射装置发射的发射激光参数电信号并进行分析确定被检测区域的气体成分和/或含量。本发明较方便地对空中管路的气体泄漏情况进行检测,及时了解空中管路的泄漏情况,当飞行装置出现问题时仅需更换光学转换装置和激光发射装置即可,降低了高空检测成本。

The invention provides a gas detection system. The system includes a ground system and a flight system, the ground system includes a photoelectric detector and a data processing device; the flight system includes a flight device, a laser emitting device and an optical path conversion device; the laser emitting device is used to emit laser light to the detected area; the optical path conversion device is used It is used to receive the reflected laser light and turn it to the photodetector; the photodetector is used to receive the reflected laser light and convert it into the reflected laser parameter electrical signal; the data processing device is used to receive the reflected laser parameter electrical signal and the emitted laser parameter electrical signal emitted by the laser transmitter The signal is analyzed to determine the gas composition and/or content of the detected area. The invention more conveniently detects the gas leakage situation of the aerial pipeline, understands the leakage situation of the aerial pipeline in time, only needs to replace the optical conversion device and the laser emitting device when the flying device has a problem, and reduces the high-altitude detection cost.

Description

气体检测系统Gas detection system

技术领域 technical field

本发明涉及检测技术领域,具体而言,涉及一种气体检测系统。 The invention relates to the technical field of detection, in particular to a gas detection system.

背景技术 Background technique

随着经济的发展,燃气在工业、民用上的应用也越来越广泛,燃气作为一种能源,燃气管道的泄漏不仅会造成经济损失,而且也可能引起人身伤害,因此,燃气检测作为预防措施显得尤为重要。目前,常用的检测方法是通过燃气检测仪,但由于燃气检测仪的检测效率低、速度慢,难以满足实际应用的需要,尤其是对于一些特殊的应用场所,例如,化工领域的架空管路、高层建筑燃气管路等置于空中的管路更是难以检测。 With the development of the economy, the application of gas in industry and civil use is becoming more and more extensive. As a kind of energy, the leakage of gas pipelines will not only cause economic losses, but also may cause personal injury. Therefore, gas detection is used as a preventive measure appears to be particularly important. At present, the commonly used detection method is through gas detectors, but due to the low detection efficiency and slow speed of gas detectors, it is difficult to meet the needs of practical applications, especially for some special applications, such as overhead pipelines in the chemical industry, Pipelines placed in the air, such as gas pipelines in high-rise buildings, are even more difficult to detect.

发明内容 Contents of the invention

鉴于此,本发明提出了一种气体检测系统,旨在解决现有技术中对置于空中的管路是否泄漏难以检测的问题。 In view of this, the present invention proposes a gas detection system, aiming to solve the problem in the prior art that it is difficult to detect whether a pipeline placed in the air is leaking.

一个方面,本发明提出了一种气体检测系统,该系统包括:地面系统和飞行系统;其中,所述地面系统包括光电探测器和数据处理装置;所述飞行系统包括飞行装置及设置于所述飞行装置的激光发射装置和光路转换装置;所述激光发射装置用于向被检测区域发射激光;所述光路转换装置用于接收所述被检测区域反射回的激光并转向至光电探测器;所述光电探测器用于接收所述反射回的激光并转换成反射激光参数电信号;所述数据处理装置与所述光电探测器相连接,用于接收所述反射激光参数电信号,并根据所述发射激光参数电信号和预先存储的所述激光发射装置的发射激光参数电信号确定被检测区域的气体成分和/或含量。 In one aspect, the present invention provides a gas detection system, which includes: a ground system and a flight system; wherein, the ground system includes a photoelectric detector and a data processing device; the flight system includes a flight device and is arranged on the The laser emitting device and the optical path conversion device of the flying device; the laser emitting device is used to emit laser light to the detected area; the optical path conversion device is used to receive the laser light reflected back from the detected area and turn it to the photodetector; the The photodetector is used to receive the reflected laser light and convert it into a reflected laser parameter electrical signal; the data processing device is connected to the photoelectric detector to receive the reflected laser parameter electrical signal, and according to the The gas component and/or content of the detected area is determined by the laser emission parameter electric signal and the pre-stored emission laser parameter electric signal of the laser emission device.

进一步地,上述气体检测系统中,所述激光发射装置为单波长激光发射装置。 Further, in the above gas detection system, the laser emitting device is a single-wavelength laser emitting device.

进一步地,上述气体检测系统中,所述激光发射装置发射的激光通过空气或光纤传播至所述光路转换装置。 Further, in the above gas detection system, the laser light emitted by the laser emitting device is transmitted to the optical path conversion device through air or optical fiber.

进一步地,上述气体检测系统中,所述光路转换装置接收的所述被检测区域反射回的激光通过空气或光纤传播至光电探测器。 Further, in the above gas detection system, the laser light received by the optical path conversion device and reflected back by the detected area is transmitted to the photodetector through air or optical fiber.

进一步地,上述气体检测系统还包括:地面车载,所述光电探测器和数据处理装置设置于所述地面车载。 Further, the above-mentioned gas detection system further includes: a ground vehicle, the photoelectric detector and data processing device are arranged on the ground vehicle.

进一步地,上述气体检测系统还包括:第一定位系统,用于确定所述飞行装置置于所述地面系统上方的预设范围内,以使所述光电探测器接收所述激光发射装置转向的反射激光。 Further, the above-mentioned gas detection system further includes: a first positioning system, configured to determine that the flying device is placed within a preset range above the ground system, so that the photodetector receives the steering position of the laser emitting device. Reflect the laser.

进一步地,上述气体检测系统中,所述第一定位系统包括:激光器,设置于所述地面系统,用于向所述飞行装置发射激光;感光板,设置于所述飞行装置的底部,用于接收所述发光装置发射的激光,并返回感光电信号;接收装置,设置于地面系统,用于接收返回的所述感光电信号并根据返回的所述感光电信号确定所述飞行装置是否处于所述地面系统上方的预设范围内。 Further, in the above-mentioned gas detection system, the first positioning system includes: a laser, arranged on the ground system, for emitting laser light to the flying device; a photosensitive plate, arranged at the bottom of the flying device, for receiving the laser light emitted by the light-emitting device, and returning the photosensitive signal; the receiving device is arranged on the ground system, and is used to receive the returned photosensitive signal and determine whether the flying device is in the position according to the returned photosensitive signal. within a preset range above the ground system described above.

进一步地,上述气体检测系统中,所述第一定位系统包括:第一GPS系统、第二GPS系统和控制装置;其中,所述第一GPS系统设置于地面系统,用于定位地面系统的位置;所述第二GPS系统设置于飞行系统,用于定位飞行系统的位置;控制装置,与所述第一GPS系统和所述第二GPS系统电连接,用于接收所述地面系统和所述飞行系统的位置,以及控制所述飞行系统以使所述飞行系统置于所述地面系统上方的预设范围内。 Further, in the above gas detection system, the first positioning system includes: a first GPS system, a second GPS system and a control device; wherein, the first GPS system is set on the ground system for locating the position of the ground system The second GPS system is set on the flight system for locating the position of the flight system; the control device is electrically connected with the first GPS system and the second GPS system, and is used to receive the ground system and the The location of the flight system, and controlling the flight system to place the flight system within a predetermined range above the ground system.

进一步地,上述气体检测系统还包括:第二定位系统,设置于所述飞行装置,用于保证所述飞行装置与被检测区域之间的距离在预设距离范围内。 Further, the above gas detection system further includes: a second positioning system, arranged on the flying device, for ensuring that the distance between the flying device and the detected area is within a preset distance range.

进一步地,上述气体检测系统中,所述第二定位系统还用于在反射距离小于预设距离时发出检测异常报警信号;所述反射距离为所述光路转换装置与被检测区域内的激光反射点之间的距离中的距离。 Further, in the above gas detection system, the second positioning system is also used to send an abnormal detection alarm signal when the reflection distance is less than a preset distance; the reflection distance is the distance between the optical path conversion device and the laser reflection in the detected area The distance in distance between points.

本发明提供的气体检测系统通过激光发射装置发射的激光对被检测区域的气体进行检测,并且该气体检测系统分为地面系统和飞行系统两部分,飞行系统携带激光发射装置和光路转换装置至空中,可以对空中的管路直接进行检测,与现有技术相比,本发明可以比较方便地对空中管路的气体泄漏情况进行检测,以便及时了解空中管路的泄漏情况。此外,当飞行装置出现问题时仅需更换光学转换装置和激光发射装置即可,有效地降低了高空气体检测的成本。 The gas detection system provided by the present invention detects the gas in the detected area through the laser emitted by the laser emitting device, and the gas detection system is divided into two parts: the ground system and the flight system, and the flight system carries the laser emitting device and the optical path conversion device to the air , can directly detect the pipeline in the air, compared with the prior art, the present invention can more conveniently detect the gas leakage of the pipeline in the sky, so as to know the leakage of the pipeline in the sky in time. In addition, when there is a problem with the flying device, only the optical conversion device and the laser emitting device need to be replaced, which effectively reduces the cost of high-altitude gas detection.

附图说明 Description of drawings

通过阅读下文优选实施方式的详细描述,各种其他的优点和益处对于本领域普通技术人员将变得清楚明了。附图仅用于示出优选实施方式的目的,而并不认为是对本发明的限制。而且在整个附图中,用相同的参考符号表示相同的部件。在附图中: Various other advantages and benefits will become apparent to those of ordinary skill in the art upon reading the following detailed description of the preferred embodiment. The drawings are only for the purpose of illustrating a preferred embodiment and are not to be considered as limiting the invention. Also throughout the drawings, the same reference numerals are used to designate the same parts. In the attached picture:

图1为本发明实施例提供的气体检测系统的结构框图; Fig. 1 is a structural block diagram of a gas detection system provided by an embodiment of the present invention;

图2为本发明实施例提供的气体检测系统的工作状态图。 Fig. 2 is a working state diagram of the gas detection system provided by the embodiment of the present invention.

具体实施方式 detailed description

下面将参照附图更详细地描述本公开的示例性实施例。虽然附图中显示了本公开的示例性实施例,然而应当理解,可以以各种形式实现本公开而不应被这里阐述的实施例所限制。相反,提供这些实施例是为了能够更透彻地理解本公开,并且能够将本公开的范围完整的传达给本领域的技术人员。需要说明的是,在不冲突的情况下,本发明中的实施例及实施例中的特征可以相互组合。下面将参考附图并结合实施例来详细说明本发明。 Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

参见图1,图1为本发明实施例提供的气体检测系统的结构框图。如图所示,该检测系统包括:地面系统1和飞行系统2。其中,地面系统1设置在地面上,飞行系统2可以在空中飞行,本实施例通过地面系统1和飞行系统2的配合来完成检测。 Referring to FIG. 1 , FIG. 1 is a structural block diagram of a gas detection system provided by an embodiment of the present invention. As shown in the figure, the detection system includes: a ground system 1 and a flight system 2 . Wherein, the ground system 1 is set on the ground, and the flight system 2 can fly in the air. In this embodiment, the detection is completed through the cooperation of the ground system 1 and the flight system 2 .

飞行系统2可以包括飞行装置21、激光发射装置23和光路转换装置22。飞行装置21可以为飞行器,例如直升机、无人机等。激光发射装置23用于直接向被检测区域发射激光,具体实施时,激光发射装置11可以为激光器。激光发射装置11具体发射的波长可以根据被检测气体进行选择,例如,当检测气体为甲烷时采用激光工作波长为1653.7nm,因为甲烷气体可以吸收该波长的激光。光路转换装置22用于接收被检测区域反射回的激光,以及变换被检测区域反射回的激光的传播方向,以使反射回的激光向地面系统1传播。具体实施时,光路转换装置22接收的被检测区域反射回的激光可以通过空气或光纤传播至光电探测器13。需要说明的是,具体实施时,光路转换装置22可以由凹镜、透镜、棱镜等光学器件组成,光学转换装置22只要能够实现转向的目的即可,具体实施方式多样,本实施例对其不做任何限定。 The flying system 2 may include a flying device 21 , a laser emitting device 23 and an optical path conversion device 22 . The flying device 21 may be an aircraft, such as a helicopter, a drone, and the like. The laser emitting device 23 is used to directly emit laser light to the area to be detected. In specific implementation, the laser emitting device 11 may be a laser. The wavelength emitted by the laser emitting device 11 can be selected according to the detected gas. For example, when the detected gas is methane, the working wavelength of the laser is 1653.7nm, because methane gas can absorb laser light of this wavelength. The optical path conversion device 22 is used for receiving the laser light reflected back from the detected area, and changing the propagation direction of the laser light reflected back by the detected area, so that the reflected laser light propagates to the ground system 1 . During specific implementation, the laser light received by the optical path conversion device 22 and reflected back by the detected area may be transmitted to the photodetector 13 through air or optical fiber. It should be noted that, during specific implementation, the optical path conversion device 22 can be composed of optical devices such as concave mirrors, lenses, and prisms. As long as the optical conversion device 22 can achieve the purpose of turning, there are various specific implementation methods, and this embodiment does not address it. Make any restrictions.

地面系统1可以包括光电探测器13和数据处理装置12。光电探测器13用于接收反射回的激光并转换成反射激光参数电信号;数据处理装置12与光电探测器13相连接,用于接收反射激光参数电信号;数据处理装置12内还预先存储有激光发射装置11发射的发射激光参数电信号,数据处理装置12根据预先存储的发射激光参数电信号和接收的反射激光参数电信号确定被检测区域的气体成分和/或含量。其中,发射激光参数电信号和反射激光参数电信号可以包括激光的波长、强度等信息,数据处理装置12可以根据接收到的反射回的激光损失的波长和强度损耗来得出各气体的组成和含量。数据处理装置12可以通过分析激光光谱的波长信息确定被检测气体的组成,反射回的激光强度损耗等信息得出被检测气体中各组分含量,分析方法可以采用本领域技术人员所熟知的三级鉴别法、整体解析法等其他分析方法等。需要说明的是,发射激光参数和反射激光参数的具体包括的参数类型可以根据实际情况来确定,本实施例对此不作任何限定。具体实施时,数据处理装置12可以为单片机、DSP、计算机等。 The ground system 1 may comprise a photodetector 13 and a data processing device 12 . The photodetector 13 is used to receive the reflected laser light and convert it into a reflected laser parameter electric signal; the data processing device 12 is connected to the photoelectric detector 13 for receiving the reflected laser parameter electric signal; the data processing device 12 also pre-stores The laser emitting device 11 transmits the emitted laser parameter electric signal, and the data processing device 12 determines the gas composition and/or content of the detected area according to the pre-stored emitted laser parameter electric signal and the received reflected laser parameter electric signal. Wherein, the transmitted laser parameter electrical signal and the reflected laser parameter electrical signal may include information such as the wavelength and intensity of the laser, and the data processing device 12 may obtain the composition and content of each gas according to the wavelength and intensity loss of the received reflected laser loss . The data processing device 12 can determine the composition of the gas to be detected by analyzing the wavelength information of the laser spectrum, and obtain the content of each component in the gas to be detected by information such as the intensity loss of the reflected laser light. The analysis method can adopt three methods well known to those skilled in the art. Level identification method, overall analysis method and other analysis methods, etc. It should be noted that the types of parameters specifically included in the emission laser parameters and the reflection laser parameters may be determined according to actual conditions, which is not limited in this embodiment. During specific implementation, the data processing device 12 may be a single-chip microcomputer, a DSP, a computer, and the like.

本实施例的工作原理为:对于某种特定的气体,可以吸收特定波长的激光,本发明实施例利用气体的该特性对气体进行检测。例如,甲烷可以吸收波长为1653.7nm的激光,当检测甲烷时,使激光发射装置11发射波长为1653.7nm的激光,该波长的激光射向被检测区域时,如果该被检测区域内有甲烷气体,则甲烷气体会全部或部分吸收该波长的激光,通过甲烷气体反射回的激光将不再有该波长的激光或者该波长的激光会减弱;如果该被检测区域内没有甲烷气体,则该波长的激光不会被吸收。可以看出,根据该特性,通过对发射激光和被检测区域反射回的激光进行分析,即可确定被检测区域内的气体成分。此外,甲烷吸收气体时,也会造成激光强度损耗,而不同气体对激光造成损耗的能力不同,所以通过分析激光强度的损耗便可以确定气体的含量。 The working principle of this embodiment is: for a specific gas, laser light with a specific wavelength can be absorbed, and the embodiment of the present invention uses this characteristic of the gas to detect the gas. For example, methane can absorb laser light with a wavelength of 1653.7nm. When methane is detected, the laser emitting device 11 is made to emit a laser light with a wavelength of 1653.7nm. , then the methane gas will absorb all or part of the laser light of this wavelength, and the laser light reflected back by the methane gas will no longer have the laser light of this wavelength or the laser light of this wavelength will be weakened; if there is no methane gas in the detected area, then the laser light of this wavelength The laser light will not be absorbed. It can be seen that according to this characteristic, the gas composition in the detected area can be determined by analyzing the emitted laser light and the reflected laser light from the detected area. In addition, when methane absorbs gas, it will also cause loss of laser intensity, and different gases have different abilities to cause loss of laser light, so the gas content can be determined by analyzing the loss of laser intensity.

本实施例的工作过程为:启动飞行装置21,飞行装置21携带激光发射装置23和光路装换装置22上升至被检测区域附近,然后飞行装置21调整位置,进而调整光路转换装置22的位置,以使光电探测器13可以接收到光路转换装置22转向后的反射激光,待调整好飞行装置21的位置后,开始检测,此时,由激光发射装置11发射的激光直接射向被检测区域,激光被待检测气体反射,反射回的激光通过光路转换装置22进行变向,变向后的激光在空气或光纤介质中传播,传输至光电探测器13,光电探测器13将该反射激光信号转换为电信号,并传送给数据处理装置12,数据处理装置12对将该激光和激光发射装置11发射的激光进行分析得到被检测气体的成分和/或含量。 The working process of this embodiment is: start the flying device 21, the flying device 21 carries the laser emitting device 23 and the optical path replacement device 22 and rises to the vicinity of the detected area, then the flying device 21 adjusts the position, and then adjusts the position of the optical path conversion device 22, So that the photodetector 13 can receive the reflected laser light after the optical path conversion device 22 turns, and after the position of the flying device 21 is adjusted, the detection starts. At this time, the laser emitted by the laser emitting device 11 directly shoots to the detected area. The laser is reflected by the gas to be detected, and the reflected laser is redirected through the optical path conversion device 22. The redirected laser propagates in the air or optical fiber medium and is transmitted to the photodetector 13. The photodetector 13 converts the reflected laser signal It is an electrical signal, which is sent to the data processing device 12, and the data processing device 12 analyzes the laser and the laser emitted by the laser emitting device 11 to obtain the composition and/or content of the gas to be detected.

本实施例中提供的气体检测系统通过激光发射装置发射的激光对被检测区域的气体进行检测,并且该气体检测系统分为地面系统1和飞行系统2两部分,飞行系统2携带激光发射装置23和光路转换装置22至空中,可以对空中的管路直接进行检测,与现有技术相比,本实施例可以比较方便地对空中管路的气体泄漏情况进行检测,以便及时了解空中管路的泄漏情况。此外,当飞行装置12出现问题时仅需更换光学转换装置22和激光发射装置21即可,有效地降低了高空气体检测的成本。 The gas detection system provided in this embodiment detects the gas in the detected area through the laser emitted by the laser emitting device, and the gas detection system is divided into two parts: the ground system 1 and the flight system 2, and the flight system 2 carries the laser emitting device 23 And the optical path conversion device 22 to the air, can directly detect the pipeline in the air, compared with the prior art, this embodiment can more conveniently detect the gas leakage of the pipeline in the air, so as to know the status of the pipeline in the air in time Leakage. In addition, when there is a problem with the flying device 12, only the optical conversion device 22 and the laser emitting device 21 need to be replaced, which effectively reduces the cost of high-altitude gas detection.

上述实施例中,激光发射装置23可以为单波长激光发射装置,即该激光发射装置只能发射一种波长的激光。由于该激光发射装置只能发射一种波长的激光,所以只能对一种气体进行检测,但由于单波长激光发射装置重量较轻,比较容易携带入空中,而且可以直接将发射的激光照射在被检测区域,检测精度也比较高。可以看出,本实施例将重量较重的数据处理装置12设置在地面上,而只是将重量较轻的光路转换装置22和只能发射单波长的激光发射装置23通过飞行装置21携带到空中,通过该方法将核心较重的设备转移到地面,从而减轻飞行装置21携带的重量,增加飞行装置21的续航能力,可以一次完成较大区域的气体检测。此外,对于数据处理装置12而言,检测精度越高,重量也会越重。由于本实施例中的数据处理装置12置于地面,可以选择精度较高的数据处理装置12,进而提高气体的检测精度。 In the above embodiments, the laser emitting device 23 may be a single-wavelength laser emitting device, that is, the laser emitting device can only emit laser light of one wavelength. Since the laser emitting device can only emit laser light of one wavelength, it can only detect one gas, but because the single-wavelength laser emitting device is light in weight, it is easier to carry into the air, and can directly irradiate the emitted laser light on the The detected area has a relatively high detection accuracy. It can be seen that in this embodiment, the heavy data processing device 12 is placed on the ground, and only the light path conversion device 22 and the laser emitting device 23 that can only emit a single wavelength are carried into the air through the flying device 21 Through this method, the core heavy equipment is transferred to the ground, thereby reducing the weight carried by the flying device 21, increasing the endurance of the flying device 21, and completing gas detection in a larger area at one time. In addition, for the data processing device 12 , the higher the detection accuracy, the heavier the weight. Since the data processing device 12 in this embodiment is placed on the ground, a data processing device 12 with higher accuracy can be selected, thereby improving the gas detection accuracy.

上述各实施例中还可以包括:地面车载。其中,光电探测器13和数据处理装置12均设置于该地面车载。具体地,地面车载可以为可移动的机动车辆等,光电探测器13和数据处理装置12设置在该地面车载上。可以看出,地面车载的移动,可以带动地面系统1在地面上向任意位置移动,方便调整地面系统1的位置,可以大大地提高检测效率。 The above embodiments may also include: ground vehicles. Wherein, the photodetector 13 and the data processing device 12 are both arranged on the ground vehicle. Specifically, the ground vehicle may be a movable motor vehicle, etc., and the photodetector 13 and the data processing device 12 are arranged on the ground vehicle. It can be seen that the movement of the vehicle on the ground can drive the ground system 1 to move to any position on the ground, which facilitates the adjustment of the position of the ground system 1 and greatly improves the detection efficiency.

参见图1、图2,为了使激光发射装置11和光电探测器13可以与光路转换装置22更好地对应,上述各实施例中还可以增设:第一定位系统。其中,第一定位系统用于确定飞行装置21置于地面系统1上方的预设范围内,以光电探测器13可以接受到光路转换装置22转向的被检测区域反射回的激光。 Referring to FIG. 1 and FIG. 2 , in order to make the laser emitting device 11 and the photodetector 13 better correspond to the optical path conversion device 22 , in each of the above embodiments, a first positioning system can also be added. Wherein, the first positioning system is used to determine that the flying device 21 is placed within a preset range above the ground system 1 , so that the photodetector 13 can receive the laser light reflected back from the detected area where the optical path conversion device 22 turns.

在本发明的一种实施方式中,第一定位系统可以包括:激光器、感光板和接收装置。其中,激光器设置于地面系统1中的车载上,用于向飞行装置21的底部发射激光;感光板可以设置于飞行装置21的底部,用于接收激光器发射的激光并返回感光电信号;接收装置也设置在地面系统1上,用于接收返回的该感光电信号以及根据返回的该感光电信号确定飞行装置21是否在预设范围内,当飞行装置21不在预设范围内时,接收装置接收不到感光电信号。地面系统1以一定频率发射垂直定位激光校正地面系统1与飞行装置21的垂直位置,具体实施时,可以采用激光快速定位系统,例如每秒100次以上定位信号。 In one embodiment of the present invention, the first positioning system may include: a laser, a photosensitive plate, and a receiving device. Wherein, the laser device is arranged on the vehicle in the ground system 1, and is used to emit laser light to the bottom of the flying device 21; the photosensitive plate can be arranged on the bottom of the flying device 21, and is used to receive the laser light emitted by the laser device and return the sensing photoelectric signal; the receiving device It is also arranged on the ground system 1 to receive the returned photosensitive signal and determine whether the flying device 21 is within the preset range according to the returned photosensitive signal. When the flying device 21 is not within the preset range, the receiving device receives There is no photosensitive signal. The ground system 1 emits a vertical positioning laser at a certain frequency to correct the vertical position of the ground system 1 and the flying device 21. During specific implementation, a laser rapid positioning system can be used, for example, more than 100 positioning signals per second.

在本发明的另一种实施方式中,第一定位系统可以包括第一GPS系统、第二GPS系统和控制装置。其中,第一GPS系统设置于地面系统1,用于定位地面系统1的位置;第二GPS系统设置于飞行系统2,用于定位飞行系统的位置;控制装置与第一GPS系统和第二GPS系统电连接,用于接收地面系统1和飞行系统2的位置,以及控制飞行系统1以使飞行系统2置于地面系统1上方的预设范围内。具体实施时,控制装置可以与飞行装置21中的控制系统相连接,当飞行装置21超出预设范围时,控制装置给飞行装置21发送位置调节信号,飞行装置21根据该位置调节信号调节位置至预设范围内。 In another embodiment of the present invention, the first positioning system may include a first GPS system, a second GPS system and a control device. Wherein, the first GPS system is arranged on the ground system 1, and is used for positioning the position of the ground system 1; the second GPS system is arranged on the flight system 2, and is used for positioning the position of the flight system; the control device is connected with the first GPS system and the second GPS The system is electrically connected for receiving the positions of the ground system 1 and the flight system 2 , and controlling the flight system 1 so that the flight system 2 is placed within a preset range above the ground system 1 . During specific implementation, the control device can be connected with the control system in the flight device 21. When the flight device 21 exceeds the preset range, the control device sends a position adjustment signal to the flight device 21, and the flight device 21 adjusts the position according to the position adjustment signal. within the preset range.

需要说明的是,具体实施时,预设范围可以根据实际情况来确定,本实施例对其不做任何限定。 It should be noted that during specific implementation, the preset range may be determined according to actual conditions, which is not limited in this embodiment.

可以看出,本实施例通过第一定位系统来对飞行装置21进行定位,可以保证光电探测器可以接收到被检测区域反射回的激光。 It can be seen that in this embodiment, the flying device 21 is positioned by the first positioning system, which can ensure that the photodetector can receive the laser light reflected back from the detected area.

为了达到较好的检测效果,还可以对上述实施例做进一步改进,增设:第二定位系统。其中,第二定位系统设置于飞行装置21,用于保证飞行装置21与被检测区域之间的距离在预设距离内。具体地,第二定位系统可以包括激光器和接收装置。激光器向被检测器发射激光,被检测区域对激光器发射的激光进行反射,接收装置接收被检测区域反射回的激光,并根据接收的反射回的激光确定飞行装置21与被检测区域之间的距离。 In order to achieve a better detection effect, the above embodiment can be further improved by adding a second positioning system. Wherein, the second positioning system is arranged on the flying device 21 to ensure that the distance between the flying device 21 and the detected area is within a preset distance. Specifically, the second positioning system may include a laser and a receiving device. The laser emits laser light to the detected device, and the detected area reflects the laser light emitted by the laser device, and the receiving device receives the reflected laser light from the detected area, and determines the distance between the flying device 21 and the detected area according to the received reflected laser light .

本实施例中,通过第二定位系统可以保证飞行装置21与被检测区域之间在预设距离内,进而更好地保证了检测的效果。 In this embodiment, the second positioning system can ensure that the distance between the flying device 21 and the detected area is within a preset distance, thereby better ensuring the detection effect.

上述实施例中,第二定位系统还用于在反射距离小于预设距离时发出检测异常报警信号;反射距离为光路转换装置22与被检测区域内的激光反射点之间的距离。例如,对于居民楼内燃气管道的检测而言,假设飞行装置21与居民楼之间的距离为10米,而该居民楼的纵深为4米,则反射距离应为10米到14米之间。如果反射距离为10米,则认为激光可能被该居民楼窗户处的窗帘所阻挡,判断检测有误,发出异常报警信号。 In the above embodiment, the second positioning system is also used to send out an abnormal detection alarm signal when the reflection distance is less than the preset distance; the reflection distance is the distance between the optical path conversion device 22 and the laser reflection point in the detected area. For example, for the detection of gas pipelines in a residential building, assuming that the distance between the flying device 21 and the residential building is 10 meters, and the depth of the residential building is 4 meters, the reflection distance should be between 10 meters and 14 meters. . If the reflection distance is 10 meters, it is considered that the laser light may be blocked by the curtain at the window of the residential building, it is judged that the detection is wrong, and an abnormal alarm signal is sent.

下面以检测居民楼内是否有甲烷气体为例,对本发明实施例做更为详细的说明: Take the detection of whether there is methane gas in a residential building as an example below to describe the embodiment of the present invention in more detail:

激光发射装置选用二极管激光器,飞行装置选用无人机,光路转换装置可以选用棱镜。光路转换装置中的棱镜安装在无人机的下端,安装时,要保证一定的角度,该角度主要是为了保证激光经过光路转换装置时要发生全反射,以使激光沿竖直方向照射向光电探测器13,全反射角度可以根据公式来确定,其中,c为临界角,n为折射率,使激光以临界角入射棱镜,棱镜可以选用材质为玻璃的棱镜,玻璃的临界角为:32-42°。安装时,使棱镜透光边与地面垂直成45°角,并将棱镜安装固定保证无人机续航期间该角度不变,该种安装方式可以保证激光射向棱镜后能够全反射水平射向被检测区域。此外,还要在地面系统中组装好光电探测器13和数据处理装置12。 A diode laser is used for the laser emitting device, a drone is used for the flying device, and a prism can be used for the optical path conversion device. The prism in the optical path conversion device is installed at the lower end of the UAV. When installing, a certain angle must be ensured. This angle is mainly to ensure that the laser beam passes through the optical path conversion device to undergo total reflection, so that the laser light is irradiated to the photoelectric sensor along the vertical direction. Detector 13, the total reflection angle can be determined according to the formula, wherein, c is the critical angle, and n is the refractive index, so that the laser light is incident on the prism at the critical angle, and the prism can be a prism made of glass, and the critical angle of the glass is: 32- 42°. When installing, make the light-transmitting side of the prism vertical to the ground at an angle of 45°, and install and fix the prism to ensure that the angle remains unchanged during the drone’s battery life. Detection area. In addition, the photodetector 13 and the data processing device 12 must be assembled in the ground system.

由于甲烷气吸收波长为1653.7nm,所以检测时,先将激光发射装置11的激光发射波长调节在1653.7nm附近,然后调整无人机的飞行位置,使第一定位系统中的激光器发射的激光能够射在无人机下端的感光板上,此时光路转换装置转向的激光可以被光电探测器接收,无人机在该位置停稳,然后激光发射装置向被检测区域发射激光,激光器发射出的激光水平射向被检测区域,激光被待测气体反射,反射回的被吸收的激光通过光路转换装置中的棱镜进行聚光,聚光后的激光在空气中传输到光电探测器13,光电探测器13将接收到的光信号转换为电信号后传输给数据处理装置12,数据处理装置12对发射回的激光信号和激光发射装置发射的激光信号进行分析,得出被测气体组成和含量。 Since the absorption wavelength of methane gas is 1653.7nm, during detection, the laser emission wavelength of the laser emitting device 11 is first adjusted around 1653.7nm, and then the flight position of the drone is adjusted so that the laser emitted by the laser in the first positioning system can When the laser is shot on the photosensitive plate at the lower end of the UAV, the laser light diverted by the optical path conversion device can be received by the photoelectric detector, and the UAV stops at this position, and then the laser emitting device emits laser light to the detected area, and the laser emitted by the laser The laser beam is irradiated horizontally to the area to be detected, and the laser light is reflected by the gas to be measured, and the reflected and absorbed laser light is condensed by the prism in the optical path conversion device, and the condensed laser light is transmitted to the photodetector 13 in the air, and the photoelectric detection The device 13 converts the received optical signal into an electrical signal and transmits it to the data processing device 12. The data processing device 12 analyzes the laser signal emitted back and the laser signal emitted by the laser emitting device to obtain the composition and content of the gas to be measured.

综上,由于发明实施例将重量较重的激光发射装置和光谱数据处理装置设置在地面上,而只是将重量较轻的光路转换装置通过飞行装置携带到空中,这势必大大地减轻飞行装置的负担,增大飞行装置的续驶里程,可以一次完成较大区域的气体检测。 In summary, because the embodiment of the invention arranges the heavier laser emitting device and the spectral data processing device on the ground, but only carries the lighter optical path conversion device into the air through the flying device, this will greatly reduce the weight of the flying device. burden, increase the mileage of the flight device, and can complete the gas detection of a large area at one time.

显然,本领域的技术人员可以对本发明进行各种改动和变型而不脱离本发明的精神和范围。这样,倘若本发明的这些修改和变型属于本发明权利要求及其等同技术的范围之内,则本发明也意图包含这些改动和变型在内。 Obviously, those skilled in the art can make various changes and modifications to the present invention without departing from the spirit and scope of the present invention. Thus, if these modifications and variations of the present invention fall within the scope of the claims of the present invention and equivalent technologies thereof, the present invention also intends to include these modifications and variations.

Claims (10)

1.一种气体检测系统,其特征在于,包括:地面系统(1)和飞行系统(2);其中, 1. A gas detection system, characterized in that it comprises: a ground system (1) and a flight system (2); wherein, 所述地面系统(1)包括光电探测器(13)和数据处理装置(12);所述飞行系统(2)包括飞行装置(21)及设置于所述飞行装置(21)的激光发射装置(23)和光路转换装置(22); The ground system (1) includes a photoelectric detector (13) and a data processing device (12); the flight system (2) includes a flight device (21) and a laser emitting device ( 23) and optical path conversion device (22); 所述激光发射装置(11)用于向被检测区域发射激光;所述光路转换装置(22)用于接收所述被检测区域反射回的激光并转向至光电探测器(13); The laser emitting device (11) is used to emit laser light to the detected area; the optical path conversion device (22) is used to receive the laser light reflected back from the detected area and turn it to the photodetector (13); 所述光电探测器(13)用于接收所述反射回的激光并转换成反射激光参数电信号; The photodetector (13) is used to receive the reflected laser light and convert it into an electrical signal of reflected laser light parameters; 所述数据处理装置(12)与所述光电探测器(13)相连接,用于接收所述反射激光参数电信号,并根据所述反射激光参数电信号和预先存储的所述激光发射装置(1)的发射激光参数电信号确定被检测区域的气体成分和/或含量。 The data processing device (12) is connected with the photodetector (13), and is used for receiving the reflected laser parameter electric signal, and according to the reflected laser parameter electric signal and the pre-stored laser emitting device ( 1) The emitted laser parameter electric signal determines the gas composition and/or content of the detected area. 2.根据权利要求1所述的气体检测系统,其特征在于,所述激光发射装置(11)为单波长激光发射装置。 2. The gas detection system according to claim 1, characterized in that the laser emitting device (11) is a single-wavelength laser emitting device. 3.根据权利要求1所述的气体检测系统,其特征在于, 3. The gas detection system according to claim 1, characterized in that, 所述激光发射装置(11)发射的激光通过空气或光纤传播至所述光路转换装置(22)。 The laser light emitted by the laser emitting device (11) propagates to the optical path conversion device (22) through air or optical fiber. 4.根据权利要求1所述的气体检测系统,其特征在于, 4. The gas detection system according to claim 1, characterized in that, 所述光路转换装置(22)接收的所述被检测区域反射回的激光通过空气或光纤传播至所述光电探测器(13)。 The laser light received by the optical path conversion device (22) and reflected back by the detected area is transmitted to the photodetector (13) through air or optical fiber. 5.根据权利要求1所述的气体检测系统,其特征在于,还包括: 5. The gas detection system according to claim 1, further comprising: 地面车载,所述光电探测器(13)和数据处理装置(12)均设置于所述地面车载。 The ground vehicle, the photoelectric detector (13) and the data processing device (12) are both arranged on the ground vehicle. 6.根据权利要求1至5中任一项所述的气体检测系统,其特征在于,还包括: 6. The gas detection system according to any one of claims 1 to 5, further comprising: 第一定位系统,用于确定所述飞行装置(21)置于所述地面系统(1)上方的预设范围内,以使光电探测器(13)接收所述激光发射装置(11)转向的反射激光。 The first positioning system is used to determine that the flying device (21) is placed within a preset range above the ground system (1), so that the photodetector (13) receives the steering direction of the laser emitting device (11) Reflect the laser. 7.根据权利要求6所述的气体检测系统,其特征在于,所述第一定位系统包括: 7. The gas detection system according to claim 6, wherein the first positioning system comprises: 激光器,设置于所述地面系统(1),用于向所述飞行装置(11)发射激光; a laser device, arranged on the ground system (1), for emitting laser light to the flying device (11); 感光板,设置于所述飞行装置(21)的底部,用于接收所述激光器发射的激光,并返回感光电信号; A photosensitive plate, arranged at the bottom of the flying device (21), is used to receive the laser light emitted by the laser and return a photosensitive signal; 接收装置,设置于地面系统(1),用于接收返回的所述感光电信号并根据返回的所述感光电信号确定所述飞行装置(21)是否处于所述地面系统(1)上方的预设范围内。 The receiving device is arranged on the ground system (1), and is used for receiving the returned photosensitive signal and determining whether the flying device (21) is above the ground system (1) according to the returned photosensitive signal. within the set range. 8.根据权利要求6所述的气体检测系统,其特征在于,所述第一定位系统包括:第一GPS系统、第二GPS系统和控制装置;其中, 8. The gas detection system according to claim 6, wherein the first positioning system comprises: a first GPS system, a second GPS system and a control device; wherein, 所述第一GPS系统设置于地面系统(1),用于定位地面系统(1)的位置; The first GPS system is set on the ground system (1), and is used for locating the position of the ground system (1); 所述第二GPS系统设置于飞行系统(2),用于定位飞行系统(2)的位置; The second GPS system is set in the flight system (2), and is used for locating the position of the flight system (2); 控制装置,与所述第一GPS系统和所述第二GPS系统电连接,用于接收所述地面系统(1)和所述飞行系统(2)的位置,以及控制所述飞行系统(2)以使所述飞行系统(2)置于所述地面系统(1)上方的预设范围内。 A control device, electrically connected to the first GPS system and the second GPS system, for receiving the positions of the ground system (1) and the flight system (2), and controlling the flight system (2) so that the flight system (2) is placed within a preset range above the ground system (1). 9.根据权利要求1至5中任一项所述的气体检测系统,其特征在于,还包括: 9. The gas detection system according to any one of claims 1 to 5, further comprising: 第二定位系统,设置于所述飞行装置(21),用于保证所述飞行装置(21)与被检测区域之间的距离在预设距离范围内。 The second positioning system is arranged on the flying device (21), and is used to ensure that the distance between the flying device (21) and the detected area is within a preset distance range. 10.根据权利要求9所述的气体检测系统,其特征在于, 10. The gas detection system according to claim 9, characterized in that, 所述第二定位系统还用于在反射距离小于预设距离时发出检测异常报警信号;所述反射距离为所述光路转换装置(22)与被检测区域内的激光反射点之间的距离。 The second positioning system is also used to send out a detection abnormality alarm signal when the reflection distance is less than a preset distance; the reflection distance is the distance between the optical path conversion device (22) and the laser reflection point in the detected area.
CN201510771433.1A 2015-11-12 2015-11-12 Gas detection system Pending CN105300890A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510771433.1A CN105300890A (en) 2015-11-12 2015-11-12 Gas detection system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510771433.1A CN105300890A (en) 2015-11-12 2015-11-12 Gas detection system

Publications (1)

Publication Number Publication Date
CN105300890A true CN105300890A (en) 2016-02-03

Family

ID=55198402

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510771433.1A Pending CN105300890A (en) 2015-11-12 2015-11-12 Gas detection system

Country Status (1)

Country Link
CN (1) CN105300890A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105938087A (en) * 2016-06-29 2016-09-14 华南理工大学 Laser-ultrasonic detection system and method based on multi-axis aircraft
CN108072498A (en) * 2016-11-16 2018-05-25 中国石油天然气集团公司 Cryogenic gas leak detection systems
CN109668853A (en) * 2017-10-13 2019-04-23 中国石油化工股份有限公司 A kind of atmosphere pollution monitoring system
CN114965335A (en) * 2021-02-23 2022-08-30 北京迪特锐科技有限公司 Remote laser optical fiber gas detection system and method thereof

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040263852A1 (en) * 2003-06-03 2004-12-30 Lasen, Inc. Aerial leak detector
CN202372174U (en) * 2011-12-30 2012-08-08 中国测绘科学研究院 Miniaturized low-altitude airborne remote sensing system
US8269971B1 (en) * 2009-11-12 2012-09-18 Exelis, Inc. System and method for simultaneous detection of a gas using a mode-locked based transmitter
CN102980977A (en) * 2012-12-10 2013-03-20 环境保护部卫星环境应用中心 Unmanned pollution gas monitoring system
CN204008404U (en) * 2014-07-28 2014-12-10 南京信息工程大学 A kind of PM2.5 pick-up unit
CN104950708A (en) * 2015-06-02 2015-09-30 大连市环境监测中心 Aerial environment monitoring terminal and environmental emergency monitoring and deploying system
CN105021567A (en) * 2015-05-04 2015-11-04 南京大学 Non-contact remote laser atmospheric environment monitoring system and method

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040263852A1 (en) * 2003-06-03 2004-12-30 Lasen, Inc. Aerial leak detector
US8269971B1 (en) * 2009-11-12 2012-09-18 Exelis, Inc. System and method for simultaneous detection of a gas using a mode-locked based transmitter
CN202372174U (en) * 2011-12-30 2012-08-08 中国测绘科学研究院 Miniaturized low-altitude airborne remote sensing system
CN102980977A (en) * 2012-12-10 2013-03-20 环境保护部卫星环境应用中心 Unmanned pollution gas monitoring system
CN204008404U (en) * 2014-07-28 2014-12-10 南京信息工程大学 A kind of PM2.5 pick-up unit
CN105021567A (en) * 2015-05-04 2015-11-04 南京大学 Non-contact remote laser atmospheric environment monitoring system and method
CN104950708A (en) * 2015-06-02 2015-09-30 大连市环境监测中心 Aerial environment monitoring terminal and environmental emergency monitoring and deploying system

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105938087A (en) * 2016-06-29 2016-09-14 华南理工大学 Laser-ultrasonic detection system and method based on multi-axis aircraft
CN105938087B (en) * 2016-06-29 2018-10-30 华南理工大学 A kind of laser ultrasonic detection system and method based on Multi-axis aircraft
CN108072498A (en) * 2016-11-16 2018-05-25 中国石油天然气集团公司 Cryogenic gas leak detection systems
CN109668853A (en) * 2017-10-13 2019-04-23 中国石油化工股份有限公司 A kind of atmosphere pollution monitoring system
CN109668853B (en) * 2017-10-13 2022-02-08 中国石油化工股份有限公司 Atmospheric pollutant monitoring system
CN114965335A (en) * 2021-02-23 2022-08-30 北京迪特锐科技有限公司 Remote laser optical fiber gas detection system and method thereof

Similar Documents

Publication Publication Date Title
EP3186605B1 (en) Apparatus and method for detecting a gas using an unmanned aerial vehicle
CN105300925A (en) Gas detection system
CN105300890A (en) Gas detection system
KR101731884B1 (en) Integrated multi-wavelength remote visibility monitor
CN105319173B (en) Gas remote sensing device and method
RU2693509C2 (en) Control system of headlight or lamp translucent cap, especially aircraft external head lamp
RU2008103708A (en) METHOD AND SYSTEM FOR IDENTIFICATION OF A MOVING OBJECT AND METHOD AND SYSTEM FOR CHECKING A MOVING OBJECT BY RADIATION IMAGE FORMATION
CN103091266B (en) Gas telemetering method with alarm function
JP7201003B2 (en) Fire detection system and fire detection method
CN112611730A (en) Unmanned aerial vehicle gas detection method, system and storage medium
CN104062268A (en) Non-contact type road surface meteorological state sensor and application method thereof
WO2008036468A3 (en) System and method for built-in testing of a fiber optic transceiver
JPWO2019116725A1 (en) In-tunnel fire control system
CN105388134A (en) Fluorescence signal enhanced distance-self-adaptation oil spilling monitoring method
CN104614334A (en) Distributed optical fiber gas sensor
WO2020026589A1 (en) Receiver, fire detection system, and fire detection method
JP2014238307A (en) Gas detection device
CN105334187A (en) Gas detection system
CN102253013A (en) Transmission method visibility detection device and method applied in field of transportation
CN105223177A (en) A kind of distance self-adaptation marine oil spill monitoring equipment and method
CN104374747B (en) Double-base-line transmissometer for atmospheric visibility
CN105444970A (en) Gas detection system
CN105445206A (en) Gas detection system
CN114270176A (en) Moisture sensing device
CN105203485A (en) Detection device and method for indoor gas

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20160203