CN201761643U - Integrated cabinet of hardware devices on power patrol inspection helicopter - Google Patents

Integrated cabinet of hardware devices on power patrol inspection helicopter Download PDF

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Publication number
CN201761643U
CN201761643U CN2010201550909U CN201020155090U CN201761643U CN 201761643 U CN201761643 U CN 201761643U CN 2010201550909 U CN2010201550909 U CN 2010201550909U CN 201020155090 U CN201020155090 U CN 201020155090U CN 201761643 U CN201761643 U CN 201761643U
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CN
China
Prior art keywords
unit
rack
integrated
layer
helicopter
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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.)
Expired - Lifetime
Application number
CN2010201550909U
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Chinese (zh)
Inventor
袁杰
吴奇文
吕永新
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GUANGZHOU KEYI PHOTO-ELECTRIC TECHNOLOGY Co Ltd
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GUANGZHOU KEYI PHOTO-ELECTRIC TECHNOLOGY Co Ltd
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Priority to CN2010201550909U priority Critical patent/CN201761643U/en
Application granted granted Critical
Publication of CN201761643U publication Critical patent/CN201761643U/en
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Abstract

The utility model discloses an integrated cabinet of hardware devices on a power patrol inspection helicopter. The cabinet is integrated a control unit, a communication unit, a memory unit and a server unit; the units are in different layers of the cabinet and are connected electrically, a plurality of peripheral equipment interfaces are arranged on the cabinet and are respectively connected with a patrol inspection instrument nacelle, a patrol inspection auxiliary antenna and a user operating platform. The cabinet is also integrated with a power supply unit for supplying electric power for the units in the cabinet and the patrol inspection equipment connected with the peripheral equipment interfaces. In the utility model, the unordered hardware devices of the power patrol inspection helicopter are integrated together, so that the hardware devices can operate more stably and are convenient to be maintained; besides, the internal space of the helicopter is saved.

Description

The integrated rack of the hardware device on a kind of electric inspection process helicopter
Technical field
The utility model relates to helicopter and patrols and examines technology, relates to a kind of rack that is used for integrated hardware equipment that is installed on the electric inspection process helicopter specifically.
Background technology
Helicopter is patrolled and examined technology and has been used in a lot of fields, and it is not influenced by the locus, and polling period is short, and the numerous advantages such as digital assay processing means that adopt high confidence level, will replace traditional open-air manual inspection mode gradually.Especially electric inspection process, its cycle of operations is long, and the most work that need carry out in the open air, adopts helicopter as health check tool, has become one of important goal of Future Development.The electric inspection process of helicopter is more and more used at present, but be subjected to the restriction in space in the machine, airborne hardware device can not be installed too much excessive, its work mainly still is images acquired, simply think analysis, confidence level and timely processing capacity are all not enough, and in the helicopter flight process, also lack the necessary security auxiliary antenna.
Realize safety, comprehensively, real-time electric power helicopter is patrolled and examined, the hardware device that inspecting helicopter must be equipped with has more much than inspecting helicopter in the past, except navigationsystem and data acquisition unit, data analysis unit, large-capacity data memory cell and be equipped with the airborne service platform of the giant-screen equipment that all is absolutely necessary, usually all parts all are scattered being installed on the helicopter, this mode has a significant impact for the stability of equipment itself, plurality of transmission lines between each equipment makes the interior original little space of machine seem narrower and small, more in disorder, increased the danger of work, and circuit is made mistakes easily also when mounted.For service personnel, the work that in disorder equipment is put to them has also brought great inconvenience.So how to handle the installation question of airborne hardware device, become one of key factor that influences the helicopter in electric inspection process technology.
The utility model content
The purpose of this utility model is to be convenient to the electric inspection process helicopter and to carry in order to provide, and can be to the integrated integrated rack of hardware device of airborne hardware device height.
Technological means: the utility model is the integrated rack of the hardware device on a kind of electric inspection process helicopter, described integrated rack is integrated control unit, communication unit, memory cell and server unit and each unit layering are located in the rack, wherein server unit comprises removable data storage server and data analytics server, link together by integrated rack in-to-in circuit between each unit, on rack, be provided with some external apparatus interfaces, wherein there are two external apparatus interfaces to connect user's service platform, it is the antenna entrance hole that an external apparatus interface is arranged, there are two external apparatus interfaces to connect and patrol and examine the instrument pod, have an external apparatus interface to connect the panorama visualizer.
This integrated rack is also integrated power subsystem unit, power subsystem unit provides power supply for each unit that is integrated in the rack, and power subsystem unit also provides power supply for patrolling and examining the instrument gondola, described rack branch has six layers, from bottom to top, ground floor is a power subsystem unit, comprises the airborne power supply case and patrols and examines the power devices case; The second layer is a control unit, comprises hardware device general controller, video distributor and the network switch; The 3rd layer is communication unit, patrols and examines auxiliary antenna equipment with the communication unit bonded assembly and comprises flight attitude detector, GPS fixing aid, airborne data radio station, radio-frequency (RF) Reader and Big Dipper airborne version subscriber computer; The 4th layer is memory cell, comprises solid state hard disc array and navigation embedded PC; Layer 5 and layer 6 are respectively two parts of server unit, and wherein layer 5 is the removable data storage server, and layer 6 is a data analytics server, and described interfaces for external devices is arranged on the rack bottom.
Perhaps described integrated rack is divided into four layers, from bottom to top, data analytics server is fixed on ground floor, memory cell is fixed on the second layer, control unit and communication unit are fixed on the 3rd layer and Unit two and interconnect by fixed block, the 4th layer is fixed with the removable data storage server, is provided with described external equipment socket in the upper side of described integrated rack.
The bottom and the rear portion of described integrated rack are equipped with mounting bracket.
Beneficial effect: the utility model volume is little, generally can make: six layers of long 800mm * wide 550mm * high 888mm(, can satisfy the high standard configuration of patrolling and examining requirement), or: four layers of long 780mm * wide 550mm * high 530mm(, can satisfy the basic configuration of patrolling and examining requirement), it is little to take up room, and attractive in appearance; This integrated rack is installed in the rack a plurality of airborne hardware device height are integrated, connect by the internal circuit that lays in advance each other, be not prone to interface and come off or become flexible phenomenon, and saved space in the machine, the connection between the hardware also simply is difficult for makeing mistakes; Rack is inner to adopt the layering form, and is connected with external device by external apparatus interface, and such design can make things convenient for the user to dispose flexibly, adapts to the different work of patrolling and examining that require; Hardware device is concentrated and is put, and also helps maintenance and the maintenance of maintainer to equipment.
Description of drawings
Fig. 1 is one of block construction distribution schematic diagram of the present utility model;
Fig. 2 is two of a block construction distribution schematic diagram of the present utility model.
Wherein: 1 is integrated rack, and 2 is the external device interface, and 3 is power subsystem unit, and 4 is control unit, and 5 is communication unit, 6 memory cell, and 7 is data storage server, 8 is data analytics server.
The specific embodiment
Embodiment 1:
As shown in Figure 1, integrated rack 1 is divided into six layers, and from bottom to top, ground floor is a power subsystem unit 3, comprises the airborne power supply case and patrols and examines the power devices case; The second layer is a control unit 4, comprises hardware device general controller, video distributor and the network switch; The 3rd layer is communication unit 5, also comprises flight attitude detector, GPS fixing aid, airborne data radio station, radio-frequency (RF) Reader and Big Dipper airborne version subscriber computer with communication unit bonded assembly inspection device; The 4th layer is memory cell 6, comprises solid state hard disc array and navigation embedded PC; Layer 5 is a data storage server 7; Layer 6 is a data analytics server 8.Wherein data storage server 7 and data analytics server 8 constitute server units jointly.Also be provided with six external apparatus interfaces on the rack, wherein have an end of two external apparatus interfaces to connect user's service platform, the other end connects control unit; It is entrance hole that an external apparatus interface is arranged, be used to connect auxiliary antenna equipment and communication unit, these auxiliary antennas comprise flight attitude detector, GPS fixing aid, airborne data radio station, radio-frequency (RF) Reader and Big Dipper airborne version subscriber computer, and the user can be equipped with one or more auxiliary antenna equipment voluntarily according to the needs of oneself; There are two external apparatus interfaces to be connected and installed with the pod of patrolling and examining instrument; There is an external apparatus interface to connect the panorama visualizer.
Can be installed in each unit in the rack in advance during use, each parts of each unit of power subsystem unit and all the other are connected by lead, all the other each unit are connected by signal transmssion line according to functions of modules, rack is installed in the inspecting helicopter cabin again, all the other matching components is connected to the relevant position by external apparatus interface.
Embodiment 2:
As shown in Figure 2, integrated rack 1 is divided into four layers, and from bottom to top, ground floor is an Analysis server 8; The second layer is a memory cell 6; The 3rd layer is control unit 4 and communication unit 5, links together by fixed block between these two unit; The 4th layer is storage server 7.The corresponding assembly in all unit or unit is all captiveed joint with its place layer, makes whole rack become as a whole, and interfaces for external devices is arranged on the upper end of integrated rack.Be connected by signal transmssion line between each unit and the unit block, the distribution of interfaces for external devices is identical with embodiment one with effect.
Present embodiment does not have the integrated power supply unit, and such advantage is the volume that can further reduce integrated rack, and power supply can directly be provided by the helicopter power supply.
Integrated level height of the present utility model, the rack volume is little, can save space in the machine in a large number, and can actv. prevents the vibrations that produce in the aircraft flight process influence to the stability of instrument work; Rack is divided into multilayer, and the user can be according to the different hardware of needs configuration of oneself, alerting ability height; Hardware device is installed concentratedly, also helps maintenance and the maintenance of maintainer to equipment.Above-mentioned two embodiment are two kinds of configuration occupation modes the most practical of the present utility model, and should not be construed as restriction of the present utility model.

Claims (5)

1. the integrated rack of the hardware device on the electric inspection process helicopter, it is characterized in that: described integrated rack is integrated control unit, communication unit, memory cell and server unit and each unit layering are fixed in the rack, wherein server unit comprises data analytics server and removable data storage server, on rack, be provided with some external apparatus interfaces, wherein there are two external apparatus interfaces to connect user's service platform, it is the antenna entrance hole that an external apparatus interface is arranged, there are two external apparatus interfaces to connect and patrol and examine the instrument gondola, have an external apparatus interface to connect the panorama visualizer.
2. the integrated rack of the hardware device on the electric inspection process helicopter according to claim 1, it is characterized in that: described integrated rack is also integrated power subsystem unit, power subsystem unit provides power supply for each unit that is integrated in the rack, and power subsystem unit also provides power supply for patrolling and examining the instrument pod.
3. the integrated rack of the hardware device on the electric inspection process helicopter according to claim 2 is characterized in that: described rack branch has six layers, and ground floor is a power subsystem unit from bottom to top, comprises the airborne power supply case and patrols and examines the power devices case; The second layer is a control unit, comprises hardware device general controller, video distributor and the network switch; The 3rd layer is communication unit, patrols and examines auxiliary antenna equipment with the communication unit bonded assembly and comprises flight attitude detector, GPS fixing aid, airborne data radio station, radio-frequency (RF) Reader and Big Dipper airborne version subscriber computer; The 4th layer is memory cell, comprises solid state hard disc array and navigation embedded PC; Layer 5 and layer 6 are respectively two parts of server unit, and wherein layer 5 is the removable data storage server, and layer 6 is a data analytics server, and described interfaces for external devices is arranged on the rack bottom.
4. the integrated rack of the hardware device on the electric inspection process helicopter according to claim 1, it is characterized in that: described integrated rack is divided into four layers, from bottom to top, data analytics server is fixed on ground floor, memory cell is fixed on the second layer, control unit and communication unit are fixed on the 3rd layer and Unit two and interconnect by fixed block, and the 4th layer is fixed with the removable data storage server, are provided with described external equipment socket in the upper side of described integrated rack.
5. according to the integrated rack of the hardware device on the arbitrary described electric inspection process helicopter of claim 1 ~ 4, it is characterized in that: the bottom and the rear portion of described integrated rack are equipped with mounting bracket.
CN2010201550909U 2010-04-12 2010-04-12 Integrated cabinet of hardware devices on power patrol inspection helicopter Expired - Lifetime CN201761643U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010201550909U CN201761643U (en) 2010-04-12 2010-04-12 Integrated cabinet of hardware devices on power patrol inspection helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010201550909U CN201761643U (en) 2010-04-12 2010-04-12 Integrated cabinet of hardware devices on power patrol inspection helicopter

Publications (1)

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CN201761643U true CN201761643U (en) 2011-03-16

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103841472A (en) * 2014-02-28 2014-06-04 国家电网公司 Case
CN109992073A (en) * 2019-04-15 2019-07-09 中国南方电网有限责任公司超高压输电公司检修试验中心 Storage management system based on helicopter routing inspection mass data

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103841472A (en) * 2014-02-28 2014-06-04 国家电网公司 Case
CN103841472B (en) * 2014-02-28 2018-05-29 国家电网公司 Cabinet
CN109992073A (en) * 2019-04-15 2019-07-09 中国南方电网有限责任公司超高压输电公司检修试验中心 Storage management system based on helicopter routing inspection mass data

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Granted publication date: 20110316

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