CN106027955A - Image collection system for assisting airplane inspection and remote fault diagnosis - Google Patents
Image collection system for assisting airplane inspection and remote fault diagnosis Download PDFInfo
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- CN106027955A CN106027955A CN201610270074.6A CN201610270074A CN106027955A CN 106027955 A CN106027955 A CN 106027955A CN 201610270074 A CN201610270074 A CN 201610270074A CN 106027955 A CN106027955 A CN 106027955A
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
- H04N7/183—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source
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Abstract
The invention provides an image collection system for assisting airplane inspection and remote fault diagnosis. The image collection system comprises an image collection device which is used for collecting images of an airplane, wherein the image collection device comprises an image collection module fixed on a mobile device, and an image generation sending module connected with the image collection module; a remote processing decision-making center which is used for storing the images and realizing airplane inspection and fault diagnosis through a special expert system; and a data communication network which is connected with the image collection device and the remote processing decision-making center and is used for sending the images collected by the image collection device to the remote processing decision-making center. Through adoption of the image collection system for assisting airplane inspection and remote fault diagnosis provided by the invention, the inconvenience of inspecting the airplane through adoption of an on-site manual mode in the prior art is solved, and the method for centrally processing inspection and fault diagnosis and establishing visual inspection records is provided.
Description
Technical field
The present invention relates to civil aviaton's sensor technical field, particularly relate to a kind of for second-mission aircraft inspection and remote fault diagnosis
Image capturing system.
Background technology
Owing to aircraft the most often generation part strains, bird is hit, and meets with thunderbolt or the invasion of runway foreign object causes damage etc.
Situation, in order to ensure flight safety, before flight, pilot or flight crew bear the responsibility guaranteeing that aircraft has airworthiness every time,
Need aircraft to carry out routine safety inspection to guarantee that aircraft can safe take-off.Safety inspection like this can relate to like flying
Machine structure and parts inspection etc., thus pinpoint the problems as early as possible and safeguard or keep in repair.Owing to bureau of civil aviation introduces minimum
Device requirement inventory (MEL), according to bureau of civil aviation's criterion, can allow aircraft to postpone the maintenance work of unnecessary equipment, the most just
It is to say that the flight with necessarily repairing state is allowed.Related personnel needs to record problem on time, and according to civil aviation mangement
The regulation of office, in conjunction with the abnormal state found before taking off to determine whether flight is cancelled, safeguards or let fly away.
From safety, cost, efficiency considers, anomaly in aircraft inspection, repairs or postpone maintenance it is critical that ring
Joint.Current flight check relies primarily on artificial mode to be carried out, and the condition at the scene of being subjected to an examination limits, pilot or engineering people
Member needs scene to determine the process decision-making after checking, this result of decision be often all highly dependent on on-the-spot be responsible for checking individual technical ability,
Knowledge, experience and by training degree etc., in addition, it is generally necessary to be pointed to the structure on fuselage roof and rudder,
Sensor and antenna on surface, and aircraft carry out routine inspection, and these parts are often all located at different height, to people
Work inspection brings inconvenience.Here once to use manual site to carry out the shortcoming of checking mode as follows for simplified summary: 1. owing to needing
Differing in aircraft components position to be observed, aircraft surfaces checks that the acquisition of situation needs to change according to altitudes, inspection personnel
Need by distinct device, the position of differing heights to be checked, to making troubles property of inspection；2. aircraft is carried out by inspection personnel
During inspection, there are certain requirements surface details situation, common camera collecting device is not suitable for adopting of airport environment image information
Collection, and in the case of light intensity difference, there is inexactness in inspection based on people's naked eyes；3. check the situation form with word
Carry out achieving the practical situation that cannot reflect aircraft inspection at that time visually；4. artificial field review cannot realize the surface of centralization
Check.
In consideration of it, be necessary that designing a kind of new image capturing system for second-mission aircraft inspection with remote fault diagnosis solves
The problems referred to above.
Summary of the invention
The shortcoming of prior art in view of the above, it is an object of the invention to provide one for second-mission aircraft inspection and remotely event
The image capturing system of barrier diagnosis, solves and checks aircraft with on-the-spot artificial mode in prior art and during fault diagnosis
The not convenient property existed and artificial detection record cannot reduce the problem of history truth.
For achieving the above object and other relevant purposes, the present invention provides a kind of for second-mission aircraft inspection and remote fault diagnosis
Image capturing system, described image capturing system includes:
Image collecting device, for gathering the image of aircraft, described image collecting device includes fixing image on the mobile apparatus
Acquisition module and the image being connected with described image capture module generate sending module；
Teleprocessing decision center, for described image is preserved, and by described image is carried out Display Realization aircraft inspection and
Fault diagnosis；
Data communication network, connects described image collecting device and teleprocessing decision center, is used for realizing described image collector
Put and the communication of described teleprocessing decision center.
Preferably, described image capture module includes: horizontal stand that vertical support frame is connected with described vertical support frame one end and
Described horizontal stand connect video camera, be positioned at the range sensor directly over camera lens and be positioned on described video camera
At least one anticollision sensor, the unexpected injury caused to avoid in inspection, aircraft being caused by collision.
Preferably, described vertical support frame and horizontal stand are telescoping shoring column, wherein, described vertical support frame include fixed part,
And and the cradle portion of fixed part connection.
Preferably, described video camera includes fixed mount and is positioned at the fuselage on described fixed mount, and described fuselage is can any direction
Rotate fuselage.
Preferably, the quantity of described anticollision sensor is 5.
Preferably, acquired image quality is judged by described image collecting device also by calculating image limit detail value.
Preferably, described image limit detail value includes minimum observable lateral dimension and minimum observable longitudinal size.
Preferably, described image generates sending module is computer.
Preferably, described teleprocessing decision center is computer.
Preferably, described data communication network is one or more of GPRS, CDMA, LTE, Wifi, Zigbee.
As it has been described above, a kind of image capturing system for second-mission aircraft inspection Yu remote fault diagnosis of the present invention, have following
Beneficial effect: 1. be capable of moving freely in horizontal or vertical direction due to the image collecting device of the present invention, examines to aircraft
Look into offering convenience property；2., by using with range sensor and the image capture module of anticollision sensor, the present invention not only may be used
With by calculate image limit detail value, and with quantify limit details reference standard compare, assist operators is preferably
Carry out image acquisition work, it is also possible to avoid the risk of collision of image capture device；3. in the present invention aircraft inspection result with image
Form preserve, it is possible to image, reflect the practical situation of aircraft inspection at that time exactly；4. by the long-range place of the present invention
Reason decision center can realize carrying out the image gathered the surface inspection of centralization.
Accompanying drawing explanation
Fig. 1 is shown as the system block diagram of the present invention.
Fig. 2 is shown as the structural representation of image capture module of the present invention.
Fig. 3 is shown as the top view of the video camera of belt sensor of the present invention.
Element numbers explanation
1 image collecting device
21 vertical support frames
211 fixed parts
212 cradle portion
22 horizontal stands
23 video cameras
231 fixed mounts
232 fuselages
24 range sensors
25 anticollision sensors
Detailed description of the invention
Below by way of specific instantiation, embodiments of the present invention being described, those skilled in the art can be by disclosed by this specification
Content understand other advantages and effect of the present invention easily.The present invention can also be added by the most different detailed description of the invention
To implement or application, the every details in this specification can also be based on different viewpoints and application, in the essence without departing from the present invention
Various modification or change is carried out under god.
Refer to Fig. 1 to Fig. 3.It should be noted that the diagram provided in the present embodiment illustrates the present invention the most in a schematic way
Basic conception, the most graphic in component count time only display with relevant assembly in the present invention rather than is implemented according to reality, shape
And size drafting, during its actual enforcement, the kenel of each assembly, quantity and ratio can be a kind of random change, and its assembly layout
Kenel is likely to increasingly complex.
As shown in Figure 1 to Figure 3, a kind of image capturing system for second-mission aircraft inspection Yu remote fault diagnosis, described image
Acquisition system includes:
Image collecting device, for gathering the image of aircraft, described image collecting device includes fixing image on the mobile apparatus
Acquisition module and the image being connected with described image capture module generate sending module；
Teleprocessing decision center, for described image is preserved, and by described image is carried out Display Realization aircraft inspection and
Fault diagnosis；
Data communication network, connects described image collecting device and teleprocessing decision center, is used for realizing described image collector
Put and the communication of described teleprocessing decision center.
It should be noted that in the present embodiment, described mobile device is automobile.
It should be noted that described image generates sending module at least includes control circuit, the display being connected with described control circuit
Circuit, telecommunication circuit, power circuit；Image of the present invention generates the circuit that sending module also includes realizing other function.
Preferably, in the present embodiment, described image generates sending module is computer.
Concrete, described image capture module includes: the level that vertical support frame 21 is connected with described vertical support frame 21 one end is propped up
Video camera 23 that frame 22 is connected with described horizontal stand 22, be positioned at the range sensor 24 directly over camera lens and
At least one the anticollision sensor 25 being positioned on described video camera 23.
Concrete, described vertical support frame 21 includes fixed part 211 and and the cradle portion 212 of fixed part 211 connection.
It should be noted that described fixed part 211 is for fixing described image capture module on the mobile apparatus, composition diagram picture
Harvester, realizes the image acquisition at each position of horizontal direction aircraft by the movement of mobile device.
Concrete, described vertical support frame 21 and horizontal stand 22 are telescoping shoring column.
It should be noted that by described vertical support frame 21 and horizontal stand 22 are set to telescoping shoring column, it is achieved described figure
As acquisition module regulation in height and regulation in the horizontal direction, it is simple to described image capture module is to aircraft differing heights
The position in position and varying level direction carries out image acquisition.
Concrete, described video camera 23 includes fixed mount 231 and is positioned at the fuselage 232 on described fixed mount 231, described machine
Body 232 is can to rotate fuselage by any direction.
During it should be noted that be arranged on fixed mount 231 by described fuselage 232, described fuselage 232 is can be towards any direction
Rotate, by being set to rotate towards any direction by described fuselage 232, it is achieved video camera 23 is from diverse location, different angle
Degree carries out image acquisition, more clearly captures the details of parts to be checked, improves the motility of video camera 23.
Concrete, the quantity of described anticollision sensor 25 is 5.
It should be noted that by installing described anticollision sensor 25, it is achieved remind the contingent low coverage of image acquisition personnel
From risk of collision；The range information of the object around described video camera 23 can be sent to image and adopt by described anticollision sensor 25
On the computer display of collection personnel, in order to image acquisition personnel collision free when lifting or mobile image acquisition module occurs.
It should be noted that the video camera owing to being used is different, the anticollision sensing installed on video camera of the present invention may be caused
The quantity of device 25 is different.Preferably, in the present embodiment, the quantity of described anticollision sensor 25 is 5.
It should be noted that described 5 anticollision sensors 25 lay respectively at described fuselage 232 front, rear, left and right and
Upper plane, it is achieved the preventing collision protection to 360 degree of fuselage.
Need further exist for explanation, be positioned at the anticollision sensor 25 before described fuselage 232 and be positioned at described camera lens
Top, other 4 anticollision sensors 25 then lay respectively on described fuselage 232, the central position of four planes rear, left and right
Put, the preventing collision protection of video camera 23 is better achieved.
Concrete, acquired image quality is judged by described image collecting device also by calculating image limit detail value,
Described image limit detail value includes minimum observable lateral dimension and minimum observable longitudinal size.
It should be noted that described image limit detail value captures the details quality of image for weighing sensor, but reality is schemed
Picture element amount may be affected by details such as light, causes picture quality deviation.
It should be noted that described minimum observable lateral dimension Wmin=2*hpixel* (D/f), described minimum observable longitudinal size
Hmin=2*Vpixel* (D/f), wherein, hpixelFor the wide size of pixel, V on video camera photosensitive partpixelFor video camera sense
The high size of pixel on light original paper, D is the inspected object distance to camera lens, and f is the focal length of video camera.
Need further exist for explanation, owing to aircraft routine inspection depends on the quality condition of gathered image, and different cameras
The details that the image captured under different distance, different focal can present is the most entirely different.The present invention is by institute
That states camera lens is arranged above range sensor 24, for measuring inspected object distance D to camera lens, and by taking the photograph
Wide and high size h of pixel on camera photosensitive partpixelAnd Vpixel, and the focal distance f of described video camera when gathering image,
Described image generates sending module and calculates current image limit detail value, and for image acquisition, personnel provide auxiliary reference, in order to
Image acquisition personnel understand the quality condition of gathered image, thus recalculate image by the adjustment position of video camera, focal length
Limit detail value, until the image limit detail value calculated according to current camera position, focal length meets routine inspection to image
The requirement of detail criteria, makes image acquisition personnel collect standard compliant image.
Concrete, described data communication network is one or more of GPRS, CDMA, LTE, Wifi, Zigbee.Preferably,
In the present embodiment, described wireless data communication network is Wifi.
Concrete, described teleprocessing decision center is computer.
It should be noted that in the present embodiment, realize the image of described image acquisition device is shown by computer
Show, file preservation, it is achieved aircraft inspection and fault diagnosis etc. operate.
Referring next to Fig. 1 to Fig. 3 to a kind of image acquisition for second-mission aircraft inspection Yu remote fault diagnosis of the present invention
The concrete operations of system illustrate.
When a certain airplane or certain several planes need to carry out safety inspection, described image collecting device is driven to be checked
By aircraft, by travelling mobile device or the vertical support frame of flexible described image capture module or horizontal stand, it is achieved to be checked
The image acquisition at position；Gather image time, described image acquisition personnel can according to anticollision sensor send return video camera with
Range information between aircraft components, it is to avoid video camera sends collision with aircraft components；Send according to range sensor simultaneously
Camera lens and parts to be checked between distance, described image generates sending module, and automatically calculate the image limit by formula thin
Joint value, described image acquisition personnel compare with image detail standard according to image limit detail value, if the image gathered is not inconsistent
Standardization, described image acquisition personnel adjust camera position and focal length Resurvey, till comparative result conformance with standard.
Standard compliant image is sent to teleprocessing decision center by wireless data communication network by described image acquisition personnel, described
Described image is carried out showing, filing preservation by teleprocessing decision center, and then realizes same veteran flight crew and can be
The aircraft of different location carries out malfunction elimination, also improves working performance while improving operation quality.
In sum, a kind of image capturing system for second-mission aircraft inspection Yu remote fault diagnosis of the present invention, have following
Beneficial effect: 1. be capable of moving freely in horizontal or vertical direction due to the image collecting device of the present invention, examines to aircraft
Look into offering convenience property；2., by using with range sensor and the image capture module of anticollision sensor, the present invention not only may be used
With by calculate image limit detail value, and with quantify limit details reference standard compare, assist operators is preferably
Carry out image acquisition work, it is also possible to avoid the risk of collision of image capture device；3. in the present invention aircraft inspection result with image
Form preserve, it is possible to image, reflect the practical situation of aircraft inspection at that time exactly；4. by the long-range place of the present invention
Reason decision center can realize carrying out the image gathered the surface inspection of centralization.
The principle of above-described embodiment only illustrative present invention and effect thereof, not for limiting the present invention.Any it is familiar with this skill
Above-described embodiment all can be modified under the spirit and the scope of the present invention or change by the personage of art.Therefore, such as
All that in art, tool usually intellectual is completed under without departing from disclosed spirit and technological thought etc.
Effect is modified or changes, and must be contained by the claim of the present invention.
Claims (10)
1. the image capturing system for second-mission aircraft inspection with remote fault diagnosis, it is characterised in that described image capturing system
Including:
Image collecting device, for gathering the image of aircraft, described image collecting device includes fixing image on the mobile apparatus
Acquisition module and the image being connected with described image capture module generate sending module；
Teleprocessing decision center, for described image is preserved, and by described image is carried out Display Realization aircraft inspection and
Fault diagnosis；
Data communication network, connects described image collecting device and teleprocessing decision center, is used for realizing described image collector
Put and the communication of described teleprocessing decision center.
Image capturing system for second-mission aircraft inspection Yu remote fault diagnosis the most according to claim 1, it is characterised in that
Described image capture module includes: the horizontal stand that vertical support frame is connected with described vertical support frame one end props up with described level
Frame connect video camera, be positioned at the range sensor directly over camera lens and be positioned at least on described video camera
Individual anticollision sensor.
Image capturing system for second-mission aircraft inspection Yu remote fault diagnosis the most according to claim 2, it is characterised in that
Described vertical support frame and horizontal stand are telescoping shoring column, and wherein, described vertical support frame includes fixed part and and fixes
The cradle portion that portion connects.
Image capturing system for second-mission aircraft inspection Yu remote fault diagnosis the most according to claim 2, it is characterised in that
Described video camera includes fixed mount and is positioned at the fuselage on described fixed mount, and described fuselage is can to rotate fuselage by any direction.
Image capturing system for second-mission aircraft inspection Yu remote fault diagnosis the most according to claim 2, it is characterised in that
The quantity of described anticollision sensor is 5.
Image capturing system for second-mission aircraft inspection Yu remote fault diagnosis the most according to claim 1, it is characterised in that
Acquired image quality is judged by described image collecting device also by calculating image limit detail value.
Image capturing system for second-mission aircraft inspection Yu remote fault diagnosis the most according to claim 6, it is characterised in that
Described image limit detail value includes minimum observable lateral dimension and minimum observable longitudinal size.
Image capturing system for second-mission aircraft inspection Yu remote fault diagnosis the most according to claim 1, it is characterised in that
It is computer that described image generates sending module.
Image capturing system for second-mission aircraft inspection Yu remote fault diagnosis the most according to claim 1, it is characterised in that
Described teleprocessing decision center is computer.
Image capturing system for second-mission aircraft inspection Yu remote fault diagnosis the most according to claim 1, its feature exists
In, described data communication network is one or more of GPRS, CDMA, LTE, Wifi, Zigbee.
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108454879A (en) * | 2016-12-12 | 2018-08-28 | 中国国际航空股份有限公司 | Airplane fault processing system and method and computer equipment |
| CN109782794A (en) * | 2018-12-24 | 2019-05-21 | 顺丰科技有限公司 | For detection device and unmanned vehicle before the boat of unmanned vehicle being independently arranged |
| CN110751819A (en) * | 2019-10-29 | 2020-02-04 | 中国航空工业集团公司沈阳飞机设计研究所 | Remote maintenance site information acquisition system for airplane |
| CN110823907A (en) * | 2019-11-21 | 2020-02-21 | 张红兵 | System and method for checking integrity condition of blades of aircraft engine |
| WO2022022181A1 (en) * | 2020-07-31 | 2022-02-03 | 中国民航大学 | Machine-vision-based vehicle for inspecting lightning stroke condition of outer surface of airplane in outdoor environment |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030089183A1 (en) * | 2001-11-13 | 2003-05-15 | Jacobsen Robert A. | Apparatus and method for non-destructive inspection of large structures |
| CN102355569A (en) * | 2011-05-30 | 2012-02-15 | 南京航空航天大学 | Aircraft skin structure monitoring method based on wireless machine vision |
| CN102439394A (en) * | 2009-05-14 | 2012-05-02 | 空中客车营运有限公司 | Method and system for the remote inspection of a structure |
| CN102686999A (en) * | 2009-10-29 | 2012-09-19 | 拉皮斯坎系统股份有限公司 | Mobile aircraft inspection system |
| CN104197855A (en) * | 2014-08-20 | 2014-12-10 | 云南师范大学 | Helicopter rotor cone measurement system and method based on image processing technology |
| WO2015059241A1 (en) * | 2013-10-24 | 2015-04-30 | Airbus Group Sas | Collaborative robot for visually inspecting an aircraft |
| CN104812304A (en) * | 2012-11-20 | 2015-07-29 | 卡尔斯特里姆保健公司 | Scan geometry corrections for tomosynthesis mobile radiographic apparatus |
| CN104937615A (en) * | 2013-01-22 | 2015-09-23 | 通用电气公司 | Self-directed inspection plan |
| US20160083117A1 (en) * | 2014-09-19 | 2016-03-24 | Raytheon Company | Dynamic testing of attitude determination and control systems, reaction wheel and torque rods using automotive robotic techniques |
-
2016
- 2016-04-27 CN CN201610270074.6A patent/CN106027955A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030089183A1 (en) * | 2001-11-13 | 2003-05-15 | Jacobsen Robert A. | Apparatus and method for non-destructive inspection of large structures |
| CN102439394A (en) * | 2009-05-14 | 2012-05-02 | 空中客车营运有限公司 | Method and system for the remote inspection of a structure |
| CN102686999A (en) * | 2009-10-29 | 2012-09-19 | 拉皮斯坎系统股份有限公司 | Mobile aircraft inspection system |
| CN102355569A (en) * | 2011-05-30 | 2012-02-15 | 南京航空航天大学 | Aircraft skin structure monitoring method based on wireless machine vision |
| CN104812304A (en) * | 2012-11-20 | 2015-07-29 | 卡尔斯特里姆保健公司 | Scan geometry corrections for tomosynthesis mobile radiographic apparatus |
| CN104937615A (en) * | 2013-01-22 | 2015-09-23 | 通用电气公司 | Self-directed inspection plan |
| WO2015059241A1 (en) * | 2013-10-24 | 2015-04-30 | Airbus Group Sas | Collaborative robot for visually inspecting an aircraft |
| CN104197855A (en) * | 2014-08-20 | 2014-12-10 | 云南师范大学 | Helicopter rotor cone measurement system and method based on image processing technology |
| US20160083117A1 (en) * | 2014-09-19 | 2016-03-24 | Raytheon Company | Dynamic testing of attitude determination and control systems, reaction wheel and torque rods using automotive robotic techniques |
Non-Patent Citations (1)
| Title |
|---|
| 刘正军: "大型无人机多传感器电力线路巡检总体技术设计", 《大型无人机电力线路巡检数据采集与处理技术》 * |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108454879A (en) * | 2016-12-12 | 2018-08-28 | 中国国际航空股份有限公司 | Airplane fault processing system and method and computer equipment |
| CN109782794A (en) * | 2018-12-24 | 2019-05-21 | 顺丰科技有限公司 | For detection device and unmanned vehicle before the boat of unmanned vehicle being independently arranged |
| CN109782794B (en) * | 2018-12-24 | 2022-10-11 | 丰翼科技(深圳)有限公司 | Independently-arranged pre-flight detection device for unmanned aerial vehicle and unmanned aerial vehicle |
| CN110751819A (en) * | 2019-10-29 | 2020-02-04 | 中国航空工业集团公司沈阳飞机设计研究所 | Remote maintenance site information acquisition system for airplane |
| CN110751819B (en) * | 2019-10-29 | 2021-05-28 | 中国航空工业集团公司沈阳飞机设计研究所 | Remote maintenance site information acquisition system for airplane |
| CN110823907A (en) * | 2019-11-21 | 2020-02-21 | 张红兵 | System and method for checking integrity condition of blades of aircraft engine |
| WO2022022181A1 (en) * | 2020-07-31 | 2022-02-03 | 中国民航大学 | Machine-vision-based vehicle for inspecting lightning stroke condition of outer surface of airplane in outdoor environment |
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Application publication date: 20161012 |