RU2524276C1 - Multifunctional heavy transport helicopter of day-and-night operation, on-board radioelectronic equipment complex used in given helicopter - Google Patents

Abstract

FIELD: transport.

SUBSTANCE: multifunctional heavy transport helicopter of day-and-night operation includes body with power plant, common helicopter equipment, helicopter mechanisation means, operational controls. Cabin is divided by partition-wall with door into two parts - crew cockpit for two crew members in the front part of which there is panel for radioelectronic equipment installation and in the rear part - additional folding seat, and cabin for attendants. In-cabin partition wall is made as rack with structural access doors in which rack instrumentation units are placed. On-board radioelectronic equipment complex includes navigation-flight instrumentation complex, helicopter and power plant control system, complex of radiocommunication facilities, state identification facilities, switching unit, on-board defence complex, on-board meteo-radar station, land approach early warning system, on-board TV unit, on-board control system, backup devices system, five multifunctional indicators, multifunctional instrument panel, external memory unit and on-board computing system.

EFFECT: lowering operating costs and substantial helicopter functionality enhancement.

3 cl, 1 dwg

Description

The invention relates to the field of aircraft building and aircraft instrumentation, in particular to heavy transport helicopters for multipurpose use, performing transport, search and rescue, fire fighting, evacuation and emergency airborne transport functions, and avionics equipment complexes that equip helicopters to provide navigation and perform the above functions at any time of the day in simple and difficult weather conditions both singly and as part of a group.

Of the well-known modern heavy transport helicopters: CH-47f Chinook (manufactured by Boeing companies), Mi-26, Mi-26T (developed by the ML Mil Mill), the closest analogue is described in book [1] B. R. Mikheev. “The cost center named after M.L. Milya, LLC IIG POLIGON-PRESS, 2008, pp. 231, 232, 237, 238, Mi-26T helicopter. This helicopter contains a fuselage with a power plant, including two gas turbine turboshaft engines, with an air start from an onboard auxiliary power plant, general helicopter equipment, helicopter mechanization equipment, including the main and tail rotors, a three-wheeled chassis, and operational controls. The fuselage consists of a bow and a central part, an end beam. The nose of the fuselage includes a crew cabin of four people, a cabin accompanying the cargo. The central part of the fuselage, connected inseparably with the end beam, includes a cargo floor, with fastening assemblies for the front and main landing gear mounted on it and fuel tanks located inside the floor; side panels with front, left, right and rear doors and windows. At the rear is a cargo hatch consisting of cargo doors, a ramp and two folding ramps.

The disadvantages of the closest analogue include:

- overestimated operating costs due to the large number of crew members (4 people);

- design features of the helicopter, not allowing to place additional electronic equipment.

Of the well-known modern avionics systems: the Mi-28 avionics system, the Mi-28N avionics complex, the Chinook avionics complex CH-47f, the closest analogue is the Mi-28N avionics system described in the book [1 ], p. 261, 264, 265, 268. The complex of on-board electronic equipment Mi-28N includes connected components with inputs and outputs to the channel of communications, connections and information exchange control and surveillance equipment, navigation and flight control equipment, helicopter and power plant control system, radio communication system, weapon and countermeasure control system, electronic identification and counteraction system, television signal generation unit, information interface and conversion unit, television camera review, on-board video recorder, system for monitoring and recording parameters, the first and second multifunction indicators le Chika, pilot indicator on the windshield, the first and second multifunctional operator indicators, a multifunctional operator console, an external storage device and an on-board computer system, including computer-logical modules of a combined database interconnected by inputs and outputs on the highway of computer-information exchange, the formation of navigation and flight parameters, the formation of sighting and flight parameters and commands for the use of means of destruction and counteraction, the formation of selection information, input-output and information exchange management, a combined overview of the surrounding space and target designation, the formation of low-altitude flight parameters, the formation of group helicopter parameters, the coordinated management of a group of helicopters, the other input-output of which is the input-output of the on-board computer system.

The disadvantages of the closest analogue include:

- lack of information about the weather and radar situation;

- limited ability to determine the risk of collision with ground and air obstacles.

The objective of the invention is to reduce operating costs by reducing the number of crew members, as well as expanding the functionality of a multifunctional heavy transport helicopter and the complex of avionics used on it and, as a result, increasing its functional and operational capabilities.

This result is achieved by the fact that in a multifunctional heavy-duty transport helicopter of round-the-clock action, containing the interconnected outputs and inputs through the channel of connections, connections and information exchange, the fuselage with a power plant, including two gas turbine turboprop engines, with an air launch from an onboard auxiliary power plant, helicopter equipment, helicopter mechanization equipment, including the main and tail rotors, a three-wheeled landing gear, operational controls, and the fusel g consists of a bow part, including a cabin, a central part, including a cargo floor, with fastening assemblies for the front and main chassis supports and fuel tanks located inside the floor, side panels with front, left, right and rear doors and windows and an end beam transport and landing sanitary-rescue equipment, depending on the tasks assigned to the helicopter, including: racks for placing and fastening a stretcher, a set of safety belts for fixing the wounded on a stretcher, equipped with that of medical personnel, a sanitary unit, airborne seats for placing and transporting paratroopers, additional fuel tanks, the cabin is made by a divided partition with a door into two parts - the crew cabin, designed for two crew members (commander and second navigator pilot), in front of which is located a panel for the installation of electronic equipment, and in the back there is an additional folding chair, and a cabin for the attendants, and the cabin compartment is made in the form of a closed whatnot with technological hatches, in A number of blocks of instrumentation equipment are located.

A complex of on-board electronic equipment, including a complex of navigation and aeronautical means connected to the channel of communications, connections and information exchange, a control system for a helicopter and a power plant, a complex of radio communication equipment, state recognition equipment, a switching unit, an on-board defense complex, four multifunction indicators, multifunctional remote control, external storage device and on-board computer system, including interconnected inputs and outputs along the line of computational-informational exchange, the logical units of the integrated database, the formation of navigation and aerobatic parameters, the formation of aerobatic parameters and counter commands, the formation of displayed information, the formation of low-altitude flight parameters, the formation of group helicopter navigation parameters, input-output and information exchange control, another the input-output of which is the input-output of the on-board computer system, is additionally equipped with connected inputs odes-outputs, respectively, to the channel of communications, connections and information exchange of the airborne weather radar station, the system of early warning of proximity to the earth, the airborne television installation, the airborne monitoring system, the backup instrument system, the fifth multifunction indicator, and also introduced into the airborne computer system, connected by inputs the outputs, respectively, to the highway of computer-information exchange by the computer-logical module for the formation of the navigational flight plan.

A multifunctional heavy transport helicopter of round-the-clock action in interaction via a communications channel, connections and information exchange with a complex of avionics, a ground-based complex for planning combat operations and preparing flight missions, ground and air command posts and members of the helicopter’s crew additionally form an interactive complex that provides round-the-clock and all-weather coordinated in space and time cargo, search and rescue, vakuatsionnye, fire, landing-transport functions in individual and group use, including during training and combat tactical operations of ground forces.

Figure 1 shows a block diagram of a multifunctional heavy transport helicopter with round-the-clock operation and the complex of avionics used on it, where it is indicated: 1 - fuselage with a power plant FSU, 2 - mechanization tool SMV helicopter, 3 - general helicopter equipment OBO, 4 - operational OOU control, 5 - ground-based complex of operations planning and preparation of flight tasks of the NKPZ, 6 - ground and air points of command control of PKU, 7 - ground control and verification equipment and NKPA, 8 - transport and landing sanitary and rescue equipment TDSSO, 9 - communication channel, connections and information exchange KSIO, 10 - a complex of avionics electronic equipment KBREO, 11 - a complex of navigation and flight equipment KNPS, 12 - control system for a helicopter and a power plant SUVS, 13 - a complex of radio communications KSS, 14 - radio identification equipment of the state recognition of the Russian Geographical Society, 15 - an early warning system of proximity to land SRPBZ, 16 - weather radar station MRLS, 17 - on-board television installation BTU, 18 - block com Utilities BK, 19 - external storage device VZU, 20 - airborne control system BSK, 21 - airborne defense system BKO, 22 - system of backup devices SRP, 23 - the first multifunctional indicator PMFI, 24 - the second multifunctional indicator VMFI, 25 - the third multifunctional indicator TMPI, 26 - the fourth multifunctional indicator of the ChMPI, 27 - the fifth multifunctional indicator of the PTMFI, 28 - the multifunctional MFP, 29 - the on-board computer system BVS, 30 - the computational logic module (VLM) of the integrated database OBD, 31 - VLM f of the navigation and flight control parameters FNPP, 32 - VLM input-output and information exchange control of the VVUO, 33 - VLM formation of flight parameters and counter commands FPPP, 34 - VLM of the formation of the displayed information FOI, 35 - VLM of the formation of the parameters of group helicopter driving FPGVV, 36 - VLM formation of low-altitude flight FMVP, 37 - VLM formation of the navigational flight plan FSHPP, 38 - highway computing and information exchange MVIO.

The interconnections of the helicopter design segments and the information interconnections of the on-board equipment are carried out according to KSIO 9, which includes natural, mechanical, electromechanical, electrical and electromagnetic communications.

Information communication on the transfer of data between the inputs and outputs of the VLM BVS 29 is carried out according to MVIO 38 ([2] Presnukhin LN, Nesterov PV "Digital Computers", Moscow, VSh, 1981, p. 29, p. .474), while VLM VVUO 32 ([2], p. 478) implements an exchange order between VLM BVS 29, data reception and transmission via one input-output to MVIO 38, information exchange with airborne equipment interconnected by ISIS 9 , receiving and transmitting data through another input-output through the input-output of the BVS 298 on the ISMS 9.

Examples of technical performance of the FSU 1, SMV 2, OVO 3, OOU 4, TDSSO 8 are given in the type certificate No. 81-25 TS from 09/26/1895

Examples of technical performance of KSIO 9, KNPS 11, SUVS 12, KSS 13, RGO 14, BK 18, PMFI 23, VMPI 24, TMPI 25, ChMPI 26, PTMFI 27, MFP 28 are given in the RF patent for invention No. 2102531 of 11.25.02 d. "Multifunctional double combat helicopter", p. 8-11, designs are given in the book [1], p. 231, p. 232.

An example of the technical implementation of SRPBZ 15 is given in the specification of RShPI.461534.004-05.

An example of the technical implementation of the radar 16 is given in the specification AB1.000.169-55.

An example of the technical execution of BTU 17 is given in the specification FRAE.468157.055.

An example of the technical implementation of BSK 20 is given in the specification KIVSh.461264.045.

An example of the technical implementation of the PSA 22 is given in the specification ISMYA.392122.008.

An example of the technical implementation of BVS 29 based on computational logic modules (VLM) is given in [2], pp. 27-32.

VLM FNPP 31, VVUO 32, FPPP 33, FOI 34, FPGVV 35, FMVP 36, FShPP 37 are implemented according to standard computational schemes based on a processor (including graphic for FOI 34) and a storage device with an input to MVOI 38 ([2] , p. 30), OBD 30 and VZU 19 are implemented on the basis of a reprogrammable non-volatile memory ([2], p. 288).

FSU 1 includes a helicopter fuselage structure containing an end beam, a nose of the fuselage in which the cockpit is located, a central part of the fuselage including a cargo floor with fastening assemblies for the front and main landing gear mounts and fuel tanks located inside the floor, side panels with doors and windows. The power plant includes two gas turbine engines, an auxiliary power plant, as well as units and systems that ensure their uninterrupted operation. Engines are located above the ceiling panel of the power plant, engine compartments are closed by hoods on hinges.

SMV 2 includes an eight-blade screw mounted on a sleeve equipped with a swash plate; a five-blade tail rotor mounted on a keel beam and a stabilizer; three-axle chassis with a nose wheel; hoists and winches installed in the central part of the fuselage for unloading and loading cargo.

OVO 3 includes a fuel system, an electrical supply system, a fire protection system, an anti-icing system, a hydraulic system, lighting equipment for lighting the inside of the cabin, the outdoor take-off and landing surface and signal lighting.

OOU 4 includes intra-cabin means of operational control of the helicopter by the commander, co-pilot and navigator (pedals and control sticks of the helicopter, power plant, if necessary, external suspension).

TDSSO 8 is designed for the transport of goods both inside the cargo compartment and on external sling. Depending on the tasks assigned to the helicopter, it may include: racks for accommodating and securing sixty stretchers, a set of safety belts for fixing the wounded on a stretcher, equipped places for three paramedics, a sanitary unit; airborne seats for accommodating and transporting eighty-two paratroopers; additional fuel tanks. The control of loading and unloading and cargo transportation is carried out by the flight engineer using OOU 4 according to KSIO 9.

FSU 1, OVO 3, OOU 4 in conjunction with ISIS 9 form directly an aircraft - a helicopter, which ensures its piloting by the crew by acting on OOU 4.

A complex of on-board electronic equipment KBREO 10 as part of KNPS 11, SUVS 12, KSS 13, RGO 14, SRPBZ 15, MRLS 16, BTU 17, BK 18, VZU 19, BSK 20, BKO 21, SRP 22, PMFI 23, VMFI 24, TMPI 25, ChMPI 26, PTMP 27, MFP 28 and BVS 29 interacts with each other and with the FSU 1, OBO 3, OOU 4, through the communication channel of connections and information exchange KSIO 9.

NKPZ 5 is ([3] GosNIIAS, STI "Aviation Systems", No. 4, 2000, pp. 22, 29) a ground-based complex for planning operations of helicopters, helicopter groups and helicopter groups in tactical exercises and combat operations as part of other ( in particular land forces. In accordance with the planned operation at the NKPZ 5, an oil refinery carrier for flight tasks (a device with programmable memory such as a flash card) is prepared containing a database for equipment and crew for the planned operation. The refinery for each helicopter with NKPZ 5 is transferred to the existing helicopter connection, either by conventional transportation, or with the possibility of transmission via radio communication via KSIO 9 to the input-output of KSS 13 and then through the harness connections of KSIO 9 with KSS 13 to interacting equipment (VZU 19 or OBDZO).

PKU 6 are ground (stationary or mobile) or air command posts for controlling a single helicopter, groups of helicopters as part of airborne units during training tactical interactions or combat operations, especially during the operational change of flight missions and strategic plans for combat operations. The interaction of PKU 6 with the crew is carried out mainly via radio communication channels through KSIO 9 through KSS 13 and audio and video receivers of information and indicating means of the helicopter. Processing of information received from PKU 6 on KSIO 9 through KSS 13 for conducting group operations in combat operations occurs in FPGVV 35 BVS29.

NKPA 7 is a stationary or mobile means of verification with the help of control and testing equipment of all helicopter units and components of the KBREO 10 complex in case of failures, routine and acceptance work, the results of the checks are recorded on the relevant storage media and through KSIO 9, KSS 13 via radio engineering channels communications can be transferred to the technical and operational units of the formations and to the NKPZ 5 to form groups of helicopters involved in training and combat operations.

KNPS 11 includes physically dissimilar (air, inertial, gyroscopic, satellite, radio) sensors and systems of state parameters of the helicopter and the surrounding air, forming and issuing from the input-output of KNPS 11 on KSIO 9 to the interacting coordinate system of the location of the helicopter relative to the Earth, which constitute the track and airspeed, components of accelerations and overloads, heading, roll, pitch, attack and slip angles.

SUVS 12 according to the signals received by KSIO 9 from the interacting equipment (angles of attack, slip, course, roll and pitch, components of air and ground speed, altitude, longitudinal and lateral deviation from the given parameters of the state of the helicopter), in manual, semi-automatic and automatic modes controls forms and from its input-output on KSIO 9 transmits commands to the actuators control helicopter and power plant. At the same time, control signals and their information components have parametric restrictions to prevent the helicopter from reaching critical modes, for example, overloads, angle of attack and slip.

KSS 13 includes radio engineering devices that provide two-way radiotelephone communication between crew members and ground personnel in preparation for departure and debugging, listening to a voice informant, receiving guidance commands, tactical environment and interaction from ground command control points, searchless radio communication and data interchange between the group’s helicopters and other ground and air controls interacting in a combat operation. All types of exchange are carried out through the input-output of KCC 13 according to KSIO 9.

RGO 14 includes identification radio equipment and means for fixing factors of possible helicopter detection by radar and laser means (enemy ground and air stations), commands are sent to BVS 29 for the use of passive countermeasures from BKO 21. The RGO 14 interacts with the helicopter equipment through the input-output OGS 14 according to CSIS 9.

SRPBZ 15, being a newly introduced device, generates and transmits through its input-output via KSIO 9 information about the nature of the terrain, the presence of artificial obstacles and the degree of their danger in the direction of helicopter flight, as well as additional information regarding warning and alarm systems. The information received from SRPBZ 15 on KSIO 9 to the inputs and outputs of the PMFI 23, VMPI 24, TMPI 25, ChMPI 26, PTMFI 27, allows the crew to assess the presence of potentially dangerous obstacles, the location of the obstacle relative to the helicopter (distance to the obstacle and course angle to the obstacle, exceeding the obstacle relative to the current height of the helicopter).

MRLS 16 is a newly introduced device. MRLS 16 generates information about the weather and radar situation, as well as warning messages, such as “DANGEROUS METEO”, “DANGEROUS TURBULENCE”. MRLS 16 transmits information through its input-output according to KSIO 9, VVOU 32 to the input-output of the FOI 34, for subsequent transmission to the input-output of the PMFI 23, VMFI 24, TMFI 25, ChMPI 26, PTMP 27.

BTU 17 is a newly introduced device and includes three cameras that capture the image of the cockpit space, cargo compartment. The television signal from the input-output of BTU 17 through KSIO 9 is fed to the inputs and outputs of the BC 18 for outputting the image on the PMPI 23, VMPI 24, TMPI 25, ChMPI 26, PTMPI 27. Using the controls PMFI 23, VMFI 24, TMFI 25, ChMPI 26, PTMFI 27 (multifunction buttons and manipulators) control BTU 17 video cameras (camera selection, adjustment of the line of sight, magnification adjustment). The interaction of the BTU 17 with the equipment of the helicopter is carried out through the input-output of the BTU 17 according to KSIO 9.

BK 18 at its input-output receives television signals from KBREO 10 devices equipped with television outputs, commutation of television signals and their output from the input-output through KSIO 9 to the input-outputs of the PMFI 23, VMPI 24, TMFI 25, ChMPI 26, PTMPI 27.

VZU 19 is a device for long-term non-volatile storage of data on the theater of operations, cartographic information, digital data on the terrain, helicopter state models, the environment, goals and landmarks needed in preparing combat and training flights, and data on a variety of possible flight tasks allowing to carry out many combat and flight missions without preliminary pre-flight input of initial data. The interaction of the VZU 19 with the equipment of the helicopter is carried out through the input-output of the VZU 19 according to KSI 09.

BSK 20 is a newly introduced device that measures, calculates and converts input signals from helicopter sensors and outputs them from BSK 20 input-output through KSIO 9 to PMFI 23, VMFI 24, TMFI 25, CMFI 26, PTMP 27. BSK 20 informs crew about the state of helicopter systems.

BKO 21 includes means of passive counteraction - false thermal, light, radar targets. Signals for the use of funds are received at the input-output of the BKO

21 according to KSIO 9, VVOU 32 from FPPP 33 interaction of BKO 21 with other units of the helicopter is carried out according to KSIO 9.

PSA 22 is a newly introduced device designed to form, display and issue a gyromagnetic course, true heading, target heading, roll and pitch angles, altitude and speed parameters, lateral sliding, latitude, longitude. PSA 22 is a backup system introduced in KBREO 10 to improve flight safety in the event of a failure of the main systems. The interaction of the PSA 22 with other units of the helicopter is carried out according to KSIO 9.

PFMP 23, VMPI 24, TMPI 25, ChMPI 26, PTMFI 27 are multifunction indicators (MFIs) with color liquid crystal screens (LCD), which display color and monochrome signographic, television, cartographic and mixed information display modes of complex displays, operating modes helicopter and all interacting equipment. The multifunctional buttons-keys framing the LCD indicate the display modes and are used to manually select sub-modes for various purposes. MFIs operate in the same or different basic display modes: NVG - “navigation information indicator”, PMT - “aerobatic information indicator”, IOS - “survey systems indicator”, for example, weather and radar situation received from MRLS 16 according to KSIO 9, RTS - “indicator radio engineering of communication means ”, OVO -“ indicator of general helicopter equipment ”, etc. The main operating modes of MFIs: PMFI 23 - PLT, VMFI 24 - NVG, TMFI 25 - IOS, ChMPI 26 - RTS, PTMFI 27 - OBO.

The MFP 28 contains an information display made on the basis of the LCD, framed by nameless multi-function buttons on the right and left, corresponding to the modes (sub-modes) of the helicopter and equipment operation, fixed by the function buttons located at the top of the panel, setting the modes (PDG - preparation, NVG - navigation and other). Below the information panel there are engraved buttons-keys of digital symbols for entering the initial data on the ground during on-line training and in flight and of executive commands (VVD - input, CST - control, etc.). The upper part of the information panel is occupied by a panel of prompts with information output to the navigator by mode (“preparation”, etc.) and action prompts (“choose a mode”, etc.). MFP 28 is an operational display and control tool, supplementing PMFI 23, VMFI 24, TMFI 25, ChMPI 26, PTMPI 27 and allowing for immediate changes in the given motion and guidance parameters to be carried out without disrupting their current information frames and to carry out operational monitoring and control.

BVS 29 contains, for duplication, two high-speed (priority system-based) on-board digital computers (BTsVM), including computational logic modules (VLM) - OBD 30, FNPP 31, VVUO 32, FPPP 33, FOI 34, FPGVV 35, FMVP 36 interconnected according to MVIO 38, which receive, convert the received signals, carry out computational and logical operations, convert and issue 9 signals to consumers in real time in accordance with KSIO.

OBD 30 provides long-term non-volatile storage of source data of flight routes, data of aeronautical maps of the area of operation, data of graphic and alphanumeric characters and digital data of the terrain. Addition and change of data in OBD 30 is carried out by interconnection from the OBD 30 input-output via MVOI 38 to one input-output of VVUO 32 and from the other input-output of VVUO 32 through BVS 29 input-output on KSIO 9 to VZU 19 and other interacting equipment .

FNPP 31 carries out complex, including correlation-extreme processing of flight and navigation information received from KNPS 11, SRPBZ 15, SPSV 16, MRLS 16 with the initial data from OBD 30, generates flight and navigation parameters of the flight from preparation to landing and stop helicopter in various flight modes; the generated parameters from the input-output of FPPP 33 through MVOI 38 go to interacting VLM BVS 29, respectively, through VVUO 32 through KSIO 9 go to the interacting equipment of the helicopter, in particular to SUVS 12 for controlling the helicopter and the power plant in manual, semi-automatic and automatic control modes .

VVUO 32 carries out one input-output through the input-output of the BVS 29 receiving, converting and transmitting data via ISIS 9, and the other input-output of the VVUO 32 is connected to the MVIO 38, providing computational and information exchange between all VLM BVS 29.

FPPP 33 carries out complex processing of data received from RGO 14, data on the used countermeasures received from BKO 21, characteristics of the applied funds received from HBS 30; the parameters formed in FPPP 33 for the use of on-board funds from BKO 21, for controlling a helicopter, which from the input-output of FPPP 33 through MVOI 38 enter into the interaction of VLM BVS 29 and through VVUO 32 through KSIO 9 into the interacting equipment of KBREO 10, in particular SUVS 12 for controlling a helicopter, and in BKO 21 for the preparation and use of countermeasures.

In FOI 34, according to the data obtained by MVIO 38 from OBD 30, FNPP 31, FPPP 33 and from the KBREO 10 interacting equipment through KSIO 9, VVUO 32, generalized mnemo frames are formed with a functional, alphanumeric, television, if necessary combined with an aeronautical map of the flight area information that from the entrance and exit of FOI 34 through MVOI 38, VVUO 32, KSIO 9 is received by the UMPI 23, VMPI 24, TMPI 25, ChMPI 26, PTMFI 27, MFP 28 for presentation to crew members for the purpose of making a decision on helicopter driving.

In FPGVV 35 through MVIO 38, WSIS 32, KSIO 9, KSS 13 from PKU 6 data are received on the remaining fuel, the current location of each group helicopter. The navigator of the helicopter of the group commander, through the MFP 28, assigns a new group formation (distances, excesses, intervals, speed). According to the received data, operational flight tasks are formed for each helicopter of the group - a place in the ranks, the order of group helicopter driving, the procedure for returning to places of possible post-flight basing. The generated data from the FPGVV 35 input and output via MVOI 38 is fed to the input and output of the FOI 34 to form generalized mnemo frames of the given and current flight situation of the group on the screens of the UMPI 23, VMPI 24, TMPI 25, ChMPI 26, PTMFI 27 and through VVUO 32, KSIO 9, KSS 13 in the interacting aircraft of the group and in PKU 5 for coordination of operations.

In FMVP 36, according to the helicopter location data obtained from KNPS 11 and the digital terrain map data obtained from OBD 30 (or from VZU 19), a spatio-temporal curve is formed - a given flight path (STP) with the flight of the terrain and bypass fixed obstacles, discrete values of the calculated STP from the FMVP 36 input-output through MVOI 38 are transferred to the FNPP 31 for formation and transmission to the SUVS 12, where the parameters of manual, semi-automatic and automatic control of the helicopter through the OOU 4 are formed.

In the additionally introduced FSPP 37, the helicopter is controlled by radio equipment (RTS): automatic control of the radio compass, control of the radio navigation system and landing. FSHPP 37 allows you to change the parameters of existing ones, as well as quickly add new RTS. Data on RTS is stored in OBD 30. Exchange FSPP 37 with OBD 30 is carried out through MVIO 38, WSIS 32.

The installation of a new modernized cockpit in conjunction with the new avionics complex allowed to reduce the number of crew members, thus, the tasks set for the invention: reducing operating costs, as well as expanding functionality, were solved.

Information sources

1. V.R. Mikheev. “The cost center named after M.L. Milya, LLC IIG POLIGON-PRESS, 2007.

2. Presnukhin L.N., Nesterov P.V. "Digital Computers", Moscow, VS, 1981

3. GosNIIAS, NTI "Aviation Systems", No. 4, 2000

Claims (3)

1. A multifunctional heavy-duty transport helicopter of round-the-clock operation, containing the fuselage interconnected by the outputs and entrances through the channel of communications, connections and information exchange with the power plant, which includes two gas turbine turbo-engines, with an air launch from the onboard auxiliary power plant, general helicopter equipment, helicopter mechanization equipment, including main and tail rotors, three-wheeled chassis, operational controls, and the fuselage consists of a bow, including cable inu, the central part, including the cargo floor, with fastening assemblies for the front and main landing gear mounts and fuel tanks located inside the floor, side panels with front, left, right and rear doors and windows and an end beam, airborne sanitary and rescue equipment, depending on the tasks assigned to the helicopter, including: racks for placing and attaching a stretcher, a set of safety belts for fixing the wounded on a stretcher, equipped places for paramedics, a sanitary unit, landing seats for accommodating and transporting paratroopers, additional fuel tanks, characterized in that the cabin is divided by a partition with a door into two parts - the crew cabin, designed for two crew members (commander and second navigator pilot), in front of which there is a panel for installation of electronic equipment, and in the back - an additional folding chair, and an accompanying cabin, and the cabin compartment is made in the form of a closed whatnot with technological hatches, in which there is a number of instrumentation units. 2. A complex of on-board electronic equipment, including a complex of navigation and aeronautical means connected to the channel of communications, connections and information exchange, a control system for a helicopter and a power plant, a complex of radio communication equipment, state identification equipment, a switching unit, an on-board defense complex, four multifunctional indicator, multifunctional remote control, external storage device and on-board computer system, including interconnected input-output and along the line of computational-informational exchange, the logic modules of the integrated database, the formation of navigation and aerobatic parameters, the formation of aerobatic parameters and counter commands, the formation of displayed information, the formation of low-altitude flight parameters, the formation of group helicopter navigation parameters, input-output and information exchange control, another input-output of which is the input-output of the on-board computer system, characterized in that it is additional equipped with connected inputs and outputs, respectively, to the communication channel, connections and information exchange of the airborne weather radar station, an early warning system for the proximity of the earth, an airborne television installation, an airborne monitoring system, a backup instrument system, a fifth multifunction indicator, and also included in the airborne computing system, connected by inputs and outputs, respectively, to the highway of the computational-informational exchange by the computational-logical module for generating Turman flight plan. 3. The multi-functional round-the-clock heavy transport helicopter according to claim 1, interacting via a communications channel, connections and information exchange with a complex of avionics, a ground-based complex for planning combat operations and preparing flight missions, ground and air command posts and helicopter crew members forming an interactive complex, carrying out round-the-clock and all-weather freight and space-time coordinated search and rescue tion, evacuation, fire, landing-transport functions in individual and group use, including during training and combat tactical operations of ground forces.