RU61678U1 - INFORMATION AND MANAGEMENT SYSTEM FOR MAINTENANCE AND OPERATION OF AERONAUTICAL ENGINEERING - Google Patents

Abstract

Information management system for maintenance and operation of aircraft, containing a database, computational and logical modules, information exchange channels and peripherals. According to the utility model, it contains a logistic database as a database, including blocks of reference data and operational data. In addition, it contains a control unit for technical maintenance and material and technical support for the operation of aircraft, connected with the logistics database, at least one device for information support of the operation of the aircraft, made with the possibility of communication with the logistics database. In this case, the reference data block is made with the possibility of communication via information exchange channels with suppliers and consumers of aircraft, and the operational data block with consumers of aircraft.

Description

A utility model relates to systems (devices) for providing maintenance and operation of aircraft.

Known (Russian Patent N2177897) information management system for aircraft, providing control of fighter and tactical aircraft in close air combat. The system is located in an aircraft and contains a set of weapons and countermeasures, a system of parameters for the movement of the aircraft, a system of air parameters, a system of survey and aiming parameters, an indication-control system and an on-board computer system with computational and logical modules of a unified database, display of synthesized information, navigation and integrated information processing, stabilization and control of aircraft and propulsion, the use of weapons and input-output-control info exchange interaction, formation of air parameters when performing super-maneuvers, and controlling an airplane and a propulsion system when performing super-maneuvers. Systems are connected by a channel of information exchange of systems, and modules in an on-board computer system are connected by a channel of internal information exchange. Thanks to the presence of this system, the aircraft has expanded functional capabilities, since it provides the restoration of air parameters when they are unreliable, as well as the formation of control signals for super-maneuvers and the use of weapons and countermeasures when performing super-maneuvers.

However, such a system has only the limited capabilities listed above for providing control of aircraft directly in flight, but does not, for example, provide the possibility of high-quality technical maintenance of aviation equipment between flights, as well as monitoring by suppliers of equipment for its behavior in flight.

Known (Russian Patent N2147141) information management system for maintenance and operation of aircraft, containing a database,

computational and logical modules, information exchange channels and peripherals. The system is used in the planning and preparation of flight missions of a tactical group of aircraft and is intended for use as part of ground-based combat planning systems for strike aircraft. The technical result consists in expanding the functionality and is achieved due to the fact that the system comprises a keyboard, a manipulator, a digital graphic indicator, a recorder for recording flight tasks and a device for printing flight documents connected to the electronic unit of the system. The latter includes the computational and logical modules of the integrated database interconnected through the channel of mutual information exchange, planning the route flight of a group of aircraft, planning the actions of a group of aircraft in the target area, displaying information and synthesizing images, and input-output-control information exchange. In addition, computer-logical modules for planning refueling of group aircraft, planning for collecting group aircraft in predetermined battle formations when they take off from different aerodromes, planning for the dissolution of the battle order of group planes for organizing their landing at different aerodromes were introduced.

Such a system, like the previous one, has only limited capabilities for providing control of aircraft directly in flight, but does not provide the possibility of high-quality technical maintenance of aircraft between flights, as well as control by suppliers of equipment for its behavior in flight.

Closest to the proposed one is an information management system for servicing and operating aviation equipment, containing a logistics database including reference data and operational data blocks, a control unit connected to the logistics database, information exchange channels and peripherals (Kudritsky et al. “Control automation electronic equipment ”, M., Soviet Radio, 1977, pp. 44-47).

This system allows for the monitoring of electronic equipment of the aircraft, both in the parking lot and in flight, including sending messages about the results of control to the ground.

At the same time, this system is designed to control only electronic equipment; if necessary, use it to control other systems due to the complexity of the problem, the reliability of the device arises. In some difficult situations, it becomes necessary to access extended databases of suppliers and consumers of aircraft, which in a known system can lead to system overload and its failure. In addition, the known system did not provide for the possibility of communication with extended databases of suppliers and consumers of aircraft.

The task was to develop such a system to ensure maintenance and operation of aviation equipment, which would have advanced capabilities, would enable quality technical maintenance of aviation equipment between flights, as well as broad control by suppliers of equipment, would provide communication with suppliers and consumers of aircraft , and also would have increased reliability.

The problem was solved by a real utility model. An information management system for servicing and operating aviation equipment, comprising a logistics database including reference data and operational data blocks, a control unit associated with the logistics database, information exchange channels and peripherals, according to the invention, comprises a maintenance control unit as a control unit and logistical support for the operation of aircraft, containing a Central processor, at least one device information sub Operational support of the aircraft, made with the possibility of communication with the logistic database, while the reference data block is made with the possibility of communication via information exchange channels with the terminals of suppliers and consumers of aircraft, and the operational data block with the terminals of consumers of aircraft.

The logistics database preferably contains data on maintenance, logistics, storage, packaging, transportation, personnel management, analysis of reliability, availability, manufacturability of products, cost analysis of information and logistics support.

The reference data block preferably contains interactive technical manuals, a catalog of supplies, reference data on the type of aircraft product.

The reference data in the reference data block is preferably divided into the following groups: product structure and cross-references between tables, requirements for operation and maintenance, results of reliability, availability, manufacturability analysis, maintenance tasks, analysis and requirements for support and personnel, requirements for auxiliary equipment , description of the tested products, data on material means or objects of support for maintenance, operation, data on professional skills of personnel, requirements logistics, analysis of transportation processes, requirements for packaging, storage and transportation of goods.

The operational data in the operational data block is preferably divided into groups: the equipment of each instance of the aircraft, operational data on operating hours and movement in the operating system, operational data on maintenance and repair, operational data for engineering and aviation support of flight tasks, operational data on the aerodrome and means of aerodrome-technical support, on objects of engineering and aviation services at the airfield, on the stocks of material and technical resources, perativnye data for planning resource requirements.

The aircraft information support device preferably comprises a radio unit.

Moreover, the logistics database preferably contains a radio unit for communication with the radio unit of the information support device of the aircraft.

The information input / output device may have sensors and / or diagnostic units configured to connect to systems, components, and parts of an aircraft.

The aircraft information support device is preferably located in the aircraft and comprises an information input / output device.

The device information support of the aircraft preferably contains a processor and sensors, and diagnostic blocks associated with systems and blocks of the aircraft.

When performing this invention, the following technical effect is achieved: improving the reliability of the device and the possibility of its communication and exchange of information with suppliers and consumers of aircraft.

The creation of the proposed device allows for integrated logistics support not only during the operation of aircraft, but also in the process of its maintenance and repair, significantly expand the range of automatically performed operations at all stages of the life cycle of aircraft.

The creation of such a system actually means the electronic support of the after-sales service system. At the same time, paper documentation is converted into electronic form, a single information field for after-sales service participants is created, and a single electronic after-sales service management system is created. When creating such an electronic system, a reference database is created for each type of aircraft, an automated after-sales service process control system is created, and an operational database is created for specific aircraft aircraft numbers. When the automated control system for after-sales service processes is carried out

maintenance and restoration of aircraft, supply of spare parts and materials, distance training of personnel, as well as warehouse operations and transportation.

The availability of a logistics database allows providing consumers with reference and operational information for integrated management of the following tasks of integrated logistics support: maintenance, logistics, storage, packaging, transportation, personnel management, reliability analysis, availability, manufacturability of products, cost analysis of integrated logistics support.

In figure 1. The general scheme of the system is shown.

Figure 2 shows a preferred embodiment of a control unit for maintenance and logistics of the operation of aircraft.

Figure 3 shows a preferred embodiment of an information support device for an aircraft.

The information management system for servicing and operating aviation equipment contains a logistics database 1. Database 1 contains a block 2 of reference data and a block of 3 operational data. A control unit 4 for technical maintenance and material and technical support for the operation of aircraft is connected with the logistics database 1. The logistics database contains a radio unit 5 for communication with a radio unit 6 of the aircraft 7 information support device. The reference data block is connected via channels 8 and 9 of information exchange with terminals 10 and 11 located respectively at suppliers and consumers of aircraft, spare parts and consumables. Block 3 operational data is connected via channels 12 of information exchange with terminals 13 located at consumers of aircraft.

The control unit 4 maintenance and logistical support of the operation of aircraft (figure 2) contains a device for input-output information (keyboard 14, the display of the video monitor 15

and a printer 16 associated with the central processor 17, sensors 18 and diagnostic units 19, configured to connect to the systems, components and parts of the aircraft.

The aircraft information support device (FIG. 3) comprises a keyboard 20, a video monitor 21 display connected to the processor 22. Also connected to the processor 22 are sensors 23 and diagnostic units 24 associated with the systems and units of the aircraft.

As a logistic database, a conventional information storage device having an appropriate capacity, for example, a hard disk or a hard disk system, can be used. A device for storing information has the usual means of accessing information, for example, computer, widely known to specialists and allowing you to read information from a device for storing it and enter it into this device. The presence in the database of blocks of reference data and operational data can be performed by known methods. For example, if the database contains one hard disk, these blocks are performed by allocating two logical disks in this hard disk, one of which will contain a block of reference data, and the other - a block of operational data. If the database contains two or more hard drives, each of the two blocks mentioned is located on a separate drive (or drives). The control unit for maintenance and logistical support of the operation of aircraft can be performed, for example, containing an information input / output device having a keyboard and a video monitor in the simplest version, and also containing a central processor interconnected as is well known to specialists in this technical field. In addition, the information input / output device may have sensors or diagnostic units configured to connect to aircraft systems, components, and parts. Many such sensors and diagnostic units are known to those skilled in the art, and it is also known how to organize communication between them and the aforementioned control unit.

The information support device 7 of the aircraft is located in the aircraft and can in the simplest embodiment, an information input / output device, and in a more complex embodiment, also a processor and sensors, and diagnostic units. All of these devices are connected to aircraft systems and units.

The information support device 7 and the logistic database are interconnected via radio blocks, which allows communication between them if the aircraft is in flight.

As the terminals 10, 11 and 13, in the simplest embodiment, terminals containing information input-output devices, for example, a keyboard, and a video monitor can be used. In addition, the terminal may comprise a printer, a memory unit, a control processor, and other components well known to those skilled in the art. The connection of these components in the terminal with each other is well known to specialists.

As channels 8, 9 and 12 of information exchange, you can use any channels commonly used for this purpose, including, for example, electric cables, optical, radio, infrared interfaces.

The above sections of information in the database are stored as separate files.

As an electronic-hardware implementation of the functional elements of the information-control system for maintenance and operation of aircraft as of state (Fig. 1), for example, the following solutions can be proposed:

1. Due to the fact that any modern database is a product (result) of software development, various storage devices, including solid state disks (Solid State Disk, SSD), can currently be carriers of this product.

2. As an SSD in the considered circuit microcircuits (modules) of flash disks can be applied:

- Advantech firms: PCD-1230A, a flash drive module with a standard IDE and PCD-100 interface, a flash drive module that is fully compatible with

IDE and others. The memory volumes of these modules are, respectively, in the intervals: up to 4-16 MB and up to 4-40 MB, operating temperature range: 0 ° С ÷ + 60 ° С. More complete technical characteristics of the proposed storage devices are presented, for example, in the "Advantech" product catalog. Volume 91. 1999 p. 7-6;

- M-Systems firms: DiskOnChip 2000 type module (memory capacity up to 1024 MB in DIP32 package; operating temperature range -40 ° С ÷ + 85 ° С according to X.Extended version) 2.5 / 3.5 "format module with IDE / UltraATA interface (memory capacity up to 90,112 MB, operating temperature range -40 ° С ÷ + 85 ° С) of the FFD-IDE Plus / Ultra ATA type in the 44-pin IDE package. For more complete technical specifications of the proposed data storage devices, see, for example, “PROSOFOT , short product catalog ”No. 10 of 2004, pp. 157-158.

- SanDisk companies: modules in the PC Card standard (PCMCIA ATA) of the SDP3 series (memory capacity up to 4096 MB, operating temperature range -40 ° С ÷ + 85 ° С) in the PCMCIA card construct or (from the same company) - in standard 2, 5 "SD25 series, structurally fully compatible with standard 2.5" HDDs. More complete technical characteristics of the proposed data storage devices are presented, for example, in “PROSOFOT, a short catalog of products” No. 10 2004, pp. 208-209.

3. As boards that ensure the installation of flash drives and organize a storage device that meets the requirements of the architecture of the information management system, special electronic boards from Advantech, storage device controllers, such as:

- RSM-3835, standard size RS / 104, supporting one RSM-1230A module and one RSM-100 and emulating two HDDs at the same time; can be used for electronic installation of an FFD-IDE Plus / Ultra ATA type module in a 44-pin IDE package (see "Advantech", product catalog. Volume 91. 1999, pp. 7-6);

- PCD-894A, supports PCMCIA storage device modules and is a PC / AT compatible plug-in card with one slot for installing PCMCIA modules (see "Advantech" product catalog. Volume 91. 1999, pp. 7-9 );

- PCD-897 is intended for use in computers with ISA bus and has three DIP32 sockets for electronic installation of DiskOnChip 2000 (see "Advantech", product catalog. Volume 91. 1999, pp. 7-10);

- PCM-3840 has three DIP32 sockets for installing DiskOnChip 2000, is made in the standard size PC / 104 (see "Advantech", product catalog. Volume 91. 1999, pp. 7-10).

Thus, the logistic database (item 1, figure 1) can be implemented, depending on the required amount of data storage, on the controllers of the types listed above, for example, on controllers of the type PCM-3835, with an electronically installed flash drive FFD-IDE Plus / Ultra ATA (type FFD-25-UATA). The number of such controllers should be combined with the information volumes of data storage devices in pos.2 - a block of reference data and pos.3 - a block of operational data.

The control unit 4 maintenance and logistics of the operation of aircraft can be implemented on the basis of single-board computers. Schemes of single-board computers are shown, for example, in Russian patent 2215329, Cl. G08B 25/08, published. 2003. It is preferable to use commercially available single-board computers, for example, types PCM-5864 / 5864L, which are highly integrated multimedia processor devices that include: a Pentium MMX processor, a 32-bit SVGA audio controller on the PCI bus, input and output for video signal, 24-bit LVSD interface, Ethernet controller on the PCI bus and one PCI expansion slot. PCM-5864 / 5864L with a Pentium MMX processor provides all the functions specific to a single-board industrial computer. Single-board computers (RSA-6176, PCN-6351 / L, PCM-5864 / 5864L and other types) are presented in the Advantech catalog, volume 91, for 1999, pp. 4-2 ÷ 4-20, pp. 5-2 ÷ 5-20.

As terminals (10, 11, 13), both office computers having standard configurations (system unit, monitor, keyboard, mouse, printer) and specialized operator stations of types IPC-510-SYS1-1, IPC-510 can be used -SYS1-2, IPC-510-SYS2 and other models of the Advantech SYS line of products (see "PROSOFOT, a short product catalog" No. 10.0 2004 p. 8-9), also with the ability to connect a monitor, keyboard, mouse and printer .

As channels of information exchange (8, 9, 12), wired interfaces such as RS-485 or / and Ethernet can be used.

As a radio unit (5, 6), 2.4 GHz radio modems of the ADAM-4550 type can be used (see "Advantech", product catalog. Volume 91. 1999, pp. 12-11).

In this way:

1. Position 1, figure 1 can be implemented on the basis of a flash chip FFD-IDE Plus / Ultra ATA (for example, type FFD-25-UATA, 90 GB), and in the field pos.2 figure 1, as in field pos.3 figure 1, you can enter the designation, for example, "Controller PCM-3835".

2. Position 4, figure 1 can be implemented on the basis of a single-board computer, one of the types PCM-5864 / 5864L and in the field pos.4 of figure 1, you can enter the designation, for example, "PCM-5862E / L".

3. Positions 5 and 6, FIG. 1 can be implemented on the basis of an ADAM-4550 radio modem and, accordingly, the designation “ADAM-4550” can be entered in the fields of these positions.

4. Position 7, FIG. 1 can be implemented on the basis of a single-board industrial computer for mobile applications of the OCTAGON SYSTEMS type PC-510 model and expansion cards (see "PROSOFOT, short product catalog" No. 10, 2004, p. .166-175), providing real-time, real-time collection of information from airborne sensors of the technical state of airborne equipment. Therefore, in the field of pos.7, figure 1 can be entered somewhat conditional

designation “On-board technological controller based on Octagon Systems processor boards” - “BTK OS”.

5. Positions 8, 9, 12, FIG. 1 can be implemented on the basis of wired interfaces such as RS-485 or / and Ethernet.

6. Positions 10, 11, 13, FIG. 1 can be implemented on the basis of specialized stations of the Advantech SYS line operator and, for example, the designation “IPC-510-SYS1-1” can be entered in the field of pos. 10 of FIG. ; in the field of item 11 of figure 2, the designation "IPC-510-SYS1-2" may be entered; in the field pos.13 of figure 1, the designation "IPC-510-SYS2" may be entered.

Single-board computers (PCM-5864 / 5864L) include ports (connectors) for connecting input-output devices: keyboard (14), video monitor display (15), and printer (16) as part of their circuit configuration.

As one of the many examples of existing industrial keyboards (14), IKEY's universal, secure keyboard in the DT / PM-2000 / IS / NI stainless steel case can be proposed (see "PROSOFOT, a short product catalog" No. 10, 2004 ., p. 134).

As an example of a video monitor display (15), a 17 "LiteM LD1745 liquid crystal display company of LiteMax can be proposed (see" PROSOFOT, a short product catalog "No. 10, 2004, p. 149).

As an example of a printer (16), any known A4 printer (e.g., Canon LASER SHOT LBP-11200, Epson FX-800), A3 and a number of plotters can be offered.

As examples of sensors (18), sensors can be used to measure various physical parameters of such well-known companies as Omron, Pepperl + Fuchs, Siemens, and others (see PROSOFOT, a short product catalog No. 10,2004 g p. 176-180, p. 182-188, p. 224-235).

To ensure the connection of sensors (18) to the PCM-5864 / 5864L, ADC cards can be used, for example, PCI-1713, which are 32-channel analog input cards with a PCI bus equipped with a 12-bit ADC with

sampling frequency up to 100 kHz and providing galvanic isolation of digital and analog parts (isolation voltage 2500 V DC).

Scopes of ADC boards:

- multichannel measurement of direct voltage;

- reception and measurement of sensor signals;

- control systems;

- systems with galvanic isolation of signals.

The PCI-1710 / 1710HG, PCI-1713 boards are presented in the Advantech catalog, Volume 91, 1999, pp. 10-2 ÷ 10-48.

As an example of diagnostic blocks (19), high-performance measuring devices (interface modules such as TP5008, TE6100, AD128, etc., external measuring devices such as Hahdyprobe HP2, HahdyScope 3, etc., as well as logic analyzers of the type “ Annie 200p "," Logic-3p "and others. Firms" TiePie "(" PROSOFOT, No. 10, 2004, pp. 238-239). All of the listed devices that can be assigned to diagnostic units have interfaces that provide them direct connection to computers, industrial single-board computers, etc. Depending on the specific technological requirements of the diagnosed process, various types of analyzers or measuring devices can be entered in field pos.19. Therefore, in this particular case, it is proposed to enter the name TiePie in the field pos.19 as a synonym for devices that can be perceived as diagnostic blocks.

In this way:

1. Position 14 can be implemented on the basis of the keyboard in a stainless steel case and in the field pos.14 of figure 2, you can enter the designation, for example, "DT / PM-2000 / IS / NI".

2. Position 15 can be implemented on the basis of the 17 "display and in the field pos.15 of figure 2, you can enter the designation, for example," LD1745 ".

3. Position 16, figure 2 can be implemented on the basis of an A4 printer and in the field pos.16 figure 2, you can enter the designation, for example, "Canon LASER SHOT LBP-11200".

4. Position 17, figure 2 can be implemented on the basis of a single-board computer, one of the types PCM-5864 / 5864L and in the field pos.17 of figure 2, you can enter the designation, for example, "PCM-5862E / L".

5. Position 18, figure 2 can be implemented on the basis of a variety of parametric sensors for various purposes and different manufacturers, therefore, in the field pos.18 figure 2, you can enter the designation, for example, "Sensors".

6. Position 19, figure 2 can be implemented on the basis of a variety of high-performance measuring devices, so in the field pos.18 figure 2, you can enter the designation, for example, "TiePie".

Aircraft information support device, item 7, can be implemented on the basis of a single-board industrial computer for mobile applications of the OCTAGON SYSTEMS type PC-510 model and expansion cards (see "PROSOFOT, short product catalog" No. 10 of 2004 p. 166-175), providing prompt, real-time, collection of information from on-board sensors of the technical condition parameters of on-board equipment. As expansion cards, microcontrollers of the 60 × 0 series can be used and can form airborne data acquisition and processing complexes, including providing tasks of taking and primary processing of technological information from sensors (pos. 23, Fig. 3) and connecting measurement (diagnostic) equipment (item 24, figure 3).

On the basis of single-board industrial computers, microcontrollers, and expansion cards offered by Octagon Systems, as well as using the Octagon Systems crate, an on-board process controller based on Octagon Systems processor boards, BTK OS, can be developed

As a keyboard (20), small-sized industrial keyboards with short-stroke keys of the TKS-030 and TKS-042 series by IKEY (see "Prosofot, No. 10,2004, p. 138) can be used.

As the on-board display (pos. 21, Fig. 3), 10.4 "-15" liquid crystal displays of the type LD1041, LD1548 from LiteMax can be used

(see "PROSOFOT, a short catalog of products" No. 10 of 2004, p. 149) and similar companies of other companies. In this way:

1. Position 20, figure 3 can be implemented on the basis of a small industrial keyboard with a short stroke of keys and in the field pos.20 figure 3, you can enter the designation, for example, "TKS-030".

2. Position 21, figure 3 can be implemented on the basis of liquid crystal 10.4 "-15" displays and in the field pos.21 figure 3, you can enter the designation, for example, "LD1041".

3. Position 22, figure 3 can be implemented on the basis of a single-board industrial computer and expansion cards (microcontrollers) of the company "OCTAGON SYSTEMS" and in the field pos.16 figure 2, you can enter the designation, for example, "BTK OS".

4. Position 23, figure 3 can be implemented on the basis of a variety of parametric sensors for various purposes and different manufacturers, therefore, in the field of pos.23 of figure 2, you can enter the designation, for example, "Sensors".

Position 24, figure 3 can be implemented on the basis of a variety of high-performance (built-in) measuring devices, therefore, in the field pos.24 figure 4, you can enter the designation, for example, "TiePie".

The device in one of the options for its implementation works as follows.

Bringing the system into working condition provides for the supply of power to its blocks and nodes, the launch of software, where necessary. When the system is turned on and operational, the tested and passed necessary maintenance aircraft with information support device 7 is lifted into the air. In this case, the processor of the information support device 7, through sensors and diagnostic blocks, receives information about the state of the nodes and systems of the aircraft, which enters the operational information block and is compared with the reference information stored in the reference information block of this information by processor commands

devices. If the received information coincides with the reference, no commands are sent to the input / output device. An inscription may appear on the monitor, indicating that all aircraft systems are normal. By means of the radio unit 6, information on the state of the systems and components of the aircraft can be supplied to the logistic database 1 and recorded in the online data unit 3 or recorded in the operational information unit of the device 7. If there are deviations received from the sensors and diagnostic blocks from the reference information from the reference, by processor command preliminary analysis of such a deviation, and relevant information and recommendations to the crew are submitted to the monitor. At the same time, through the radio unit 6, information about the detected deviations is supplied to the logistic database 1 and recorded in the operational data unit 3. If, as a result of a preliminary analysis of deviation at 7, it is revealed that additional data and analysis are necessary for the crew to submit recommendations, the corresponding command is sent by device 7 via radio blocks 6 and 5 to the logistics database 1. The processor of control unit 4 analyzes this information using unit 3 operational data and, if necessary, 2 reference data. Recommendations to the crew to device 7 are provided through radio blocks 5 and 6. If the information contained in block 2 of the reference data is not enough, the processor of block 4 sends a request to terminal 10 to aircraft suppliers or through terminal 13 to their consumers.

After the aircraft lands in accordance with the regulations, the aircraft is serviced and repaired. Since during this work the aircraft is located on a specially equipped site or in a hangar, the connection between the device 7 and the logistic database 1 by means of radio units 5 and 6 can be replaced by a wired connection via the corresponding stationary connectors 7 and 1.

In accordance with the regulations, the condition and performance of parts, assemblies and units of the aircraft are checked. Status information received from sensors and diagnostic blocks of device 7

systems, components and parts of the aircraft is fed into the logistics database 1 and is recorded in block 3 operational data. To obtain information about the state of the systems, components and parts of the aircraft, a control unit for maintenance and logistical support of aircraft operation may also be used, containing sensors and / or diagnostic units configured to connect to systems, components and parts of the aircraft. Information about the status of systems, components and parts that are checked manually is entered by an authorized person of the operating personnel through the information input-output device of unit 4. The processor of unit 4 compares the received information with standard information contained in operational data block 3 and, if necessary, in the block 2 reference data, and displays a conclusion on the status of the system on the display of the video monitor 15. This conclusion lists the components, assemblies and blocks of the aircraft to be replaced, as well as to be repaired or serviced. The calculation of the cost of repair and maintenance. Through the terminal 11, located at the consumer of the aircraft, a request for spare parts and materials to the consumer’s warehouse. If the request has revealed the absence of any spare parts or materials, an application is submitted through terminal 10 for their supply. If there is not enough data to draw a conclusion, the necessary additional data can be requested through terminals 10 or 11.

Claims (6)

1. An information management system for servicing and operating aviation equipment, comprising a logistics database including reference data and operational data blocks, a control unit associated with the logistics database, information exchange channels and peripherals, characterized in that it contains a block as a control unit maintenance management and logistics of the operation of aircraft, containing a Central processor, at least one information device under aircraft operation support, made with the possibility of communication with the logistic database, while the reference data block is made with the possibility of communication via information exchange channels with the terminals of suppliers and consumers of aircraft, and the operational data block with terminals of consumers of aircraft. 2. The information management system according to claim 1, characterized in that the information support device of the aircraft contains a radio unit. 3. The information management system according to claim 1, characterized in that the logistics database contains a radio unit for communication with the radio unit of the information support device of the aircraft. 4. The information-control system according to claim 1, characterized in that the information input-output device has sensors and / or diagnostic units configured to connect to systems, components and parts of the aircraft. 5. The information management system according to claim 1, characterized in that the information support device of the aircraft is located in the aircraft and comprises an information input-output device. 6. The information-control system according to claim 5, characterized in that the information support device of the aircraft contains a processor, sensors and diagnostic blocks associated with the systems and blocks of the aircraft.