RU2819338C1 - Helicopter mooring and rigging device - Google Patents

Abstract

FIELD: aviation.

SUBSTANCE: invention relates to aircraft engineering, particularly, to handling equipment. Helicopter mooring and rigging device includes rigging equipment, which is intended for loading of wheelless cargoes, for equipment wheeling by electric winches (1) and mooring equipment required for reliable fastening of loads. Helicopter mooring and rigging device comprises two electric winches (1) installed on cargo floor (2) in front part of cargo compartment (3), two drive stations (4) installed on the left and right sides of the fuselage in the front part of cargo compartment (3). On the roof of cargo compartment (3), two crane beams (32) are installed, on each of which there is carriage (5), bracket (16) with mass meter (7) fixed on it, as well as bracket (84), on which two rollers (9, 10) are fixed. On each electric winch (1) one end of rope (31) is fixed.

EFFECT: higher safety and expanded operating performances of device.

5 cl, 23 dwg

Description

Field of technology to which the invention relates

The invention relates to the field of aviation, in particular to devices for carrying out loading and unloading operations and operations.

State of the art

A cargo helicopter with a cargo compartment is known, which is equipped with a set of cables for moving cargo through an opening in the hold (DE 102006019220 A1, B64C 27/04, published 10.25.2007), in the cargo compartment of which there is a guide in the inner part on the ceiling, on which Two cable winches are located at a given distance from each other. Cable winches have a coiled cable, on the underside of which there is a fastening device, such as a hook, by which loads are attached to the cables.

A device is known for loading cargo into the cargo compartment of an aircraft and unloading cargo from it, which is closest to the claimed technical solution (RU 2186002 C1, B64C 1/22, published July 27, 2002), which contains a winch with a rope installed in the front part of the cargo compartment. cabin, rollers of the bypass rope system with hooks for connection to the attachment points inside the cargo compartment and to the attachment point on the lower surface of the rear fuselage. To unload wheeled cargo, the fastenings of the rollers of the bypass rope system inside the cargo cabin are located with the possibility of passing the winch rope along the side of the cargo cabin, and the attachment point for the last of the rollers is located on top of the cargo opening of the cabin, and after it the winch rope passes to a roller installed on the lower surface of the tail section fuselage. The invention ensures the safety of the gripped end edges of products.

The disadvantage of the known devices is their limited application, since with their help only wheeled loads can be loaded into the cargo cabin of a helicopter.

A technical problem not solved in the known device, the solution of which is provided by the claimed invention, is to create a mooring and rigging device with which it is possible to load both wheeled and wheelless cargo into the cargo cabin of a helicopter.

The technical result achieved by the claimed invention is to increase the safety of use and expand the operational capabilities of using the device for loading.

To achieve the technical result, a helicopter mooring and rigging device is proposed, containing electric winches 1 with ropes 31 and loading blocks 17, 18, moreover, the device contains two electric winches 1 installed on the cargo floor 2 in the front part of the cargo compartment 3, two drive stations 4 installed on the left and right sides of the fuselage in the front part of the cargo compartment 3, on the ceiling of the cargo compartment 3, two crane beams 32 are installed, on each of which a carriage 5, a bracket 16 with a mass meter 7 mounted on it, as well as a bracket 84 on which the two rollers 9, 10, on each electric winch 1, one end is attached to a rope 31, which passes through a loading block 17 located on the cargo floor 2, a loading block 18 mounted on the ceiling of the cargo compartment 3, a roller 19 located on the carriage 5, a roller 77 movable block 6, roller 20 located on the carriage 5, the other end of the rope 31 is fixed to the mass meter 7, while a movable block 6 is installed on the rope 31,

the drive station 4 contains a housing 22, inside of which a drum 24 with a coupling 88 is installed on an axis 23, and an electric mechanism 25 with a gear 26 is installed on the side; a coupler 27 is installed in the side bosses of the housing 22, on which the levers 28 and the bushing 29 are located, and are fixed to the levers 28 two pressure rollers 30, on the outer surface of the drum 24 there is a helical groove for laying ropes 11 and 12 and two windows for attaching tips 33, 34 of ropes 11, 12, respectively, tips 33, 34 are pressed to the drum 24 with straps 35, 36, drum 24 with on one side it is closed by a cover 37, in the center of the cover 37 there is a hole into which a sleeve 38 is pressed into which the axis 23 of the drum 24 is installed, on the other side of the drum 24 a coupling 88 is installed inside on two pins 39, a gear 26 is installed on the shaft of the electric mechanism 25, which engages with the inner rim of the gear wheel 42 of the coupling 88, from the axial movement the gear 26 is fixed by the cup 49 and tightened by the nut 50,

At each drive station 4, ropes 11, 12 are attached, while rope 11 passes through roller 9 and is connected to carriage 5, rope 12 passes through roller 10 and is connected by means of a treadmill 13 to rope 14, which, bypassing carriage 5, passes through roller 15 , mounted on bracket 16, and connected to carriage 5 on the other side,

coupling 88 contains a flange 41 and a gear wheel 42, which during normal operation is fixed from rotation relative to the flange 41 by means of balls 43; balls 43, together with stops 44, springs 45, nuts 46, are installed in six cups 47, pressed into flange 41, balls 43 are included into engagement with the bushings 48 of the gear 42, which is mounted on bearings on the shank of the flange 41,

the pressure roller 30 contains a race 51, bearings 52 and an axis 53, a race 51 on bearings 52 is installed on an axis 53,

carriage 5 contains a body 54, four rollers 55 on which the carriage moves along the crane beam 32, two rollers 56 located in the front part of the carriage and two rollers 57 located in the rear part of the carriage 5, suspensions 58, 59, and two rollers 19 ,20, eye bolts 60, 61 are screwed into the housing 54 on both sides and brackets 62 are attached, two pendants 58, 59 are connected to each other by rods 74, spacer bushings 75 are installed in the central hole of the rollers 19, 20,

roller 55 contains a cage 63, inside of which two bearings 64 are installed, into which axles 65 are inserted, fixed in a housing 54, the fixation of the roller 55 on the axis 65 is ensured by a nut 66 and a bolt 67, rollers 56, 57 consist of cages 68, 69, inside which bearings 70, 71 are pressed in

movable block 6 contains two brackets 76, a roller 77 and a hook 78, the roller 77 rotates on a spacer sleeve 79, the brackets 76 are connected to each other by a bolt 80 and an axis 81, on which a hook 78 with a latch 82 is suspended, on both sides of the roller 77 on brackets 76 rods 83 installed.

Moreover, blocks of microswitches 96 are installed on the crane beams 32, which contain a bracket 92 on which microswitches 21 are fixed, a spring 93, a lever 94 with an adjustable screw.

In this case, control is carried out using a remote control 8, which is designed to remotely control the movement of carriages 5, lifting and lowering loads, to control the weight of the load being lifted, as well as control the weight falling on each carriage 5.

In addition, the mass meter 7 contains a cylinder 85, a pressure sensor 86 and a pressure alarm 87, the cylinder 85 of the mass meter 7 is fixed to the bracket 16 using a bolt 90, and a bracket 91 is attached to the bottom of the cylinder using screws 85, in which a pressure sensor 86 and an alarm are installed pressure 87.

The device contains mooring equipment, including mooring chains, mooring straps, mooring nets, mooring units, and devices for fastening cargo containers.

In this way, a technical result is achieved.

An increase in the safety of using a helicopter mooring and rigging device is achieved due to the presence of mass meters 7, which measure both the total mass of the cargo and the part of the mass falling on each carriage 5. If the limiting values exceed the specified values of the cargo mass, the operator stops lifting the cargo and lowers it on the cargo floor 2 or on the ground.

The safety of using the helicopter mooring and rigging device is also ensured by the presence of microswitches 21 and a safety clutch 88 in the drum of the drive station 4. In the event that the operator does not turn off the drive station 4 in time, when the carriages 5 approach the front or rear stops on the crane beams 32, microswitches 21 the power supply circuit of the drive stations 4 is opened and they stop. In addition, the presence of a clutch 88 in the drum of the drive station 4 provides protection against overload of the electric mechanism 25. It operates, i.e. slips at a certain torque on the drum axis and at the extreme positions of the carriages 5 in the event of a failure of the microswitches 21.

The safety of using the device is also ensured by the presence of fender rollers 56, 57 on the carriages 5, which prevent the lateral displacement of the carriage 5 from the crane beam 32, thereby preventing the carriages 5 from falling onto the cargo floor 2.

An expansion of the operational capabilities of using a helicopter mooring and rigging device is achieved in connection with the provision of the possibility of loading and unloading wheelless cargo without the use of ground equipment, as well as wheeled and tracked vehicles. In this case, loading and unloading is carried out through the rear cargo hatch using electric winches 1 and a loading unit 17 installed in the desired location on the cargo floor 2 of the cargo compartment 3 in the front part. To protect the cargo floor 2 of the cargo cabin 3 from damage when loading tracked vehicles, a rope floor is laid on the cargo floor 2 of the helicopter.

Brief description of drawings

The essence of the invention is illustrated by drawings:

fig. 1 - cargo compartment, starboard view, carriage in the rearmost position;

fig. 2 - cargo compartment, top view;

fig. 3 - view A in Fig. 2;

fig. 4 - cargo compartment, view of the left side, carriage in the extreme forward position;

fig. 5 - view B in FIG. 4;

fig. 6 - extension element B in Fig. 1;

fig. 7 - remote element G in Fig. 4;

fig. 8 - view D in FIG. 7;

fig. 9 - extension element E in FIG. 6;

fig. 10 - kinematic diagram of equipment for loading and unloading cargo;

fig. 11 - drive station, top view;

fig. 12 - section G-J in Fig. eleven;

fig. 13 - section I-I in Fig. eleven;

fig. 14 - section K-K in Fig. eleven;

fig. 15 - section L-L in Fig. eleven;

fig. 16 - carriage, general view;

fig. 17 - view M in FIG. 16;

fig. 18 - section H-H in Fig. 16;

fig. 19 - section P-P in Fig. 16;

fig. 20 - movable block, general view;

fig. 21 - section PP in Fig. 20;

fig. 22 - section C-C in Fig. 20;

fig. 23 - remote element T in Fig. 6, view of the mass meter.

Explanations for the drawings:

Carrying out the invention

The helicopter's mooring and rigging device includes rigging equipment, which is designed for loading wheelless cargo, for rolling up equipment with electric winches 1, and mooring equipment necessary for securely securing cargo.

The helicopter's mooring and rigging device contains two electric winches 1 located on the cargo floor 2 of the cargo cabin 3, two drive stations 4, two carriages 5, two moving blocks 6, two mass meters 7 and one remote control 8 for controlling loading and unloading operations and monitoring weight lifting load (Fig. 1, 2).

Electric winches 1 are installed on the cargo floor 2 in the front part of the cargo compartment 3 near the right and left sides of the helicopter (Fig. 1, 2). Drive stations 4 are installed on the left and right sides of the fuselage (Fig. 1, 2). Two crane beams 32 are installed on the ceiling of the cargo compartment near the right and left sides (Fig. 1, 2, 5). On the lower part of the crane beams 32, brackets 84 are installed, on each of which two rollers 9, 10 are attached to transfer the ropes of the drive station 4 into the plane of the crane beam 32 (Fig. 1, 2, 7). Two drive stations 4 ensure the movement of carriages 5 with cargo along crane beams 32 along the cargo compartment 3 (Fig. 1, 2, 10).

At each drive station 4, a rope 11 and a rope 12 with tips 33 and 34 are attached, respectively (Fig. 10, 12, 13, 14). Rope 11 passes through roller 9 mounted on bracket 84 and is connected to carriage 5 (Fig. 7, 10). The rope 12 passes through the roller 10 mounted on the bracket 84, and by means of a tandem 13 is connected to the rope 14, which, bypassing the carriage 5, passes through the roller 15 mounted on the bracket 16 and is connected to the carriage 5 on the other side (Fig. 6, 7, 10, 23). Bracket 16 is fixed to the lower edge of the crane beam 32 and a mass meter 7 is installed on it (Fig. 6). The storage of ropes 11, 12, 14 on the other side of the fuselage is similar (Fig. 10).

Adjustment of the tension of the ropes 11, 12, 14 is carried out using a turntable 13 at the stage of assembling the device on a helicopter and during seasonal maintenance (Fig. 10).

Rope 31 from the electric winch 1 passes through a loading block 17 located on the cargo floor 2, a loading block 18 mounted on the ceiling of the cargo compartment 3, a roller 19 located on the carriage 5, a roller 77 of the moving block 6, a roller 20 located on the carriage 5, and mounted on mass meter 7 (Fig. 2, 3, 4, 6, 10, 16, 20, 23).

Two front and two rear blocks of microswitches 96 are installed on the crane beams 32. The microswitch blocks 96 are attached to the top of the crane beam 32 (Fig. 6, 7). Each block of microswitches 96 contains a microswitch 21, a bracket 92, a spring 93, a lever 94 with an adjustable screw (Fig. 9). The microswitch blocks 96 are designed to turn off the drive stations 4 when the carriages 5 approach the front or rear stops (not shown) on the crane beams 32 (Fig. 6, 7).

Each drive station 4 contains a housing 22, inside of which a drum 24 with a coupling 88 is installed on an axis 23, and an electric mechanism 25 with a gear 26 is installed on the side (Fig. 11, 12, 15). A coupler 27 is installed in the side bosses of the housing 22, on which levers 28 and a sleeve 29 are located (Fig. 11, 12). Two pressure rollers 30 are attached to the levers 28 (Fig. 12).

On the outer surface of the drum 24 there is a helical groove for laying ropes 11, 12 and two windows for attaching tips 33, 34 of ropes 11, 12, respectively. The tips 33, 34 are pressed against the drum 24 by straps 35, 36 using screws (not shown) to prevent them from falling out of the windows (Fig. 12, 13, 14).

The drum 24 is closed on one side by a cover 37. In the center of the cover 37 there is a hole into which a sleeve 38 is pressed into which the axis 23 of the drum 24 is rotatably installed. On the other side of the drum 24, a coupling 88 is installed inside on two pins 39, secured with bolts 40 (Fig. 12, 15).

Clutch 88 is designed to protect the electric mechanism 25 from overload. It is activated (slips) at a certain torque on the axis 23 of the drum 24 and at the extreme positions of the carriages 5 in the event of a failure of the microswitches 21 (Fig. 6, 9, 11, 15).

The coupling 88 contains a flange 41 and a gear wheel 42, which during normal operation is fixed from rotation relative to the flange 41 by means of balls 43. Balls 43, together with stops 44, springs 45, nuts 46, are installed in six cups 47, pressed into the flange 41. Balls 43 are included into engagement with the bushings 48 of the gear 42, which is mounted on bearings on the shank of the flange 41. The pressing force of the balls 43 to the bushings 48 is adjusted by nuts 46 (Fig. 15).

The electric mechanism 25 rotates the drum 24. A gear 26 is installed on the shaft of the electric mechanism 25, which meshes with the inner rim of the gear wheel 42 of the coupling 88. The gear 26 is fixed by a cup 49 and tightened with a nut 50 to prevent axial movement (Fig. 15).

Each pressure roller 30 contains a race 51, bearings 52 and an axle 53. The race 51 on bearings 52 is mounted on an axis 53. A rubber mixture is vulcanized to the outer surface of the race 51 (Fig. 11, 12).

The carriage 5 is designed to move cargo along the crane beam 32 of the cargo compartment 3 (Fig. 1, 5).

The carriage 5 contains a body 54, four rollers 55 on which the carriage moves along the crane beam 32, two rollers 56 located in the front part of the carriage 5, and two rollers 57 located in the rear part of the carriage 5, two suspensions 58, 59 and two roller 19, 20 (Fig. 16, 17). On both sides, ear bolts 60, 61 are screwed into the housing 54 and brackets 62 are attached (Fig. 16, 17). Eye bolts 60, 61 are intended for connection with ropes 11 and 14 of the drive station 4 (Fig. 8). Brackets 62 are designed for contact with microswitches 21 (Fig. 6, 7).

The rollers 55 are designed to support and move the carriage 5 along the crane beam 32 along the cargo compartment 3 (Fig. 1, 5, 17). Roller 55 contains a cage 63, inside of which two bearings 64 are installed, into which axes 65 are inserted, fixed in the housing 54. The fixation of the roller 55 on the axis 65 is ensured by a nut 66 and a bolt 67 (Fig. 18). Rollers 56, 57 prevent lateral displacement of the carriage 5 from the crane beam 32, thereby holding it on the crane beam 32 (Fig. 17). Rollers 56, 57 consist of cages 68, 69, inside of which bearings 70, 71 are pressed, respectively. To prevent the carriage 5 from moving upward, collars 68, 69 are made of collars (not shown) (Fig. 17, 19).

Two suspensions 58, 59 are connected to each other by rods 74 and are designed to attach cargo rollers 19, 20 to the carriage 5 and serve as stops for the movable block 6 (Fig. 16). At the top of the suspensions 58, 59, stops 73 are screwed in to limit the swing of the suspension in the transverse direction. In the walls of the hangers 58, 59 there are holes for bolts 72 for attaching rods 74 and load rollers 19, 20, which are intended for installing the rope 31 of the electric winch 1. Spacer bushings 75 are installed in the central holes of the rollers 19, 20. Spacer bushings 75 are installed on the inner surface of the spacer bushings 75 and Anti-friction fabric is glued to the collars (Fig. 16, 18).

Movable blocks 6 are designed to lift and lower loads. Each of them contains two brackets 76, a roller 77 and a hook 78 (Fig. 20). Roller 77 rotates on spacer sleeve 79 (Fig. 21). The brackets 76 are connected to each other by a bolt 80 and an axis 81, on which a hook 78 with a latch 82 is suspended (Fig. 20). On both sides of the roller 77, rods 83 are installed on the brackets 76, protecting the rope 31 of the electric winch 1 from sliding off the roller 77 (Fig. 20, 22). Roller 77 is intended for installing rope 31 of winch 1 on it. Hook 78 is intended for hanging cargo. The suspension system of the hook 78 ensures its rotation in the plane of the roller 77 and its rotation around its own axis (Fig. 20).

Mass meters 7 are designed to measure the mass of the lifted load and transmit information to the remote control 8 (Fig. 1). Each mass meter 7 contains a cylinder 85, a pressure sensor 86 and a pressure alarm 87. The cylinder 85 of the mass meter 7 is fixed to the bracket 16 using a bolt 90. A bracket 91 is attached to the bottom of the cylinder 85 with screws (not shown), in which a pressure sensor 86 and an alarm are installed pressure 87 (Fig. 23).

The remote control 8 is designed to remotely control the movement of the carriages 5, lifting and lowering the load, as well as to control the weight of the load being lifted, as well as control the weight per carriage 5 (Fig. 1).

The operation of equipment for loading wheelless helicopter cargo is carried out as follows.

The movement of carriages 5, lifting and lowering of cargo is controlled by the operator using the remote control 8. The movement of cargo along the cargo compartment 3 is carried out using drive stations 4, and the lifting or lowering of cargo is carried out using electric winches 1 (Fig. 1, 2). For this, the ropes 31 of the electric winches 1 and the ropes 11, 12, 14 of the drive stations 4 are mounted in accordance with the kinematic diagram (Fig. 10).

A load beam 95 is installed on the hooks 78 of the movable blocks 6 (Fig. 5). Then the carriages 5 are removed from the stops (not shown) and moved from the stowed position to the position above the load. The carriages 5 are moved manually to avoid entanglement of each of the ropes 31. After the carriages 5 reach the location of the load and stop, the operator turns on the electric winches 1 to release the ropes 31. In this case, the cargo beam 95 begins to lower. After reaching the required height for picking up the load, electric winch 1 is turned off. The load is suspended from the cargo beam 95 using chains 89 (Fig. 5).

After this, the operator turns on the electric winches 1 to remove the ropes 31. While lifting the load, the operator measures and controls the permissible weight of the load. During the process of lifting the load, you can measure the mass falling separately on the left carriage 5 or the right carriage 5; this value should also not exceed the permissible value. To move the cargo inside the cargo compartment 3, the operator turns on the drive stations 4. The drive stations 4 are turned off when moving the load forward or backward by the operator or automatically after the microswitches 21 are activated when the carriages 5 reach the front or rear stops (not shown) on the crane beams 32. For When lowering the load, the operator turns on the electric winches 1 to release the ropes 31, and the load is lowered.

When the carriages 5 approach the front or rear stops (not shown), located on the crane beams 32, the bracket 62 of the carriage 5 presses the lever 94, which presses the rod of the microswitch 21. The microswitch 21 opens the power supply circuit of the drive stations 4, and they stop. After removing the carriages 5 from the stops, the lever 94, under the action of the spring 93, returns to its original position (Fig. 9).

The proposed device also allows for loading wheeled loads. To do this, use two electric winches 1, loading blocks 17, 18, guide bumpers, rope flooring, thrust blocks, a double hook, and a leveling cable (not shown).

Loading blocks 17, 18 are installed in the right places on the cargo floor 2 of the cargo compartment 3, depending on the pattern of rolling in and rolling out wheeled cargo. The guide bumpers are installed on the cargo floor 2 along the sides of the helicopter. The rope flooring is laid on the cargo floor 2 if necessary. Thrust blocks are placed under the wheels of wheeled weights. A double hook and a leveling cable are installed between the rope 31 of the electric winch 1 and the wheel load, depending on the pattern of rolling the wheel loads.

Depending on the weight of the wheel load, different seaming schemes are used: one or both electric winches 1 can be used, a double hook and a leveling cable can be used or not.

The wheeled load is placed in front of the helicopter ramp lowered to the ground. The rope 31 of the electric winch 1 is passed through the loading blocks 17, 18, fixed in the front part of the cargo compartment 3, and is attached to the front part of the wheeled load. If necessary, a double hook and a leveling cable are placed between the rope 31 and the load. The electric winch 1 is turned on to remove the rope 31, and the wheeled load begins to move along the ramp, and then along the cargo floor 2 of the cargo compartment 3. When the desired position of the load in the cargo compartment 3 is reached, the electric winch 1 is turned off.

In order to unload wheeled loads, loading blocks 17, 18 are installed in the rear part of the cargo compartment 3, and rope 31 is secured behind the wheeled load.

Tracked vehicles enter and exit cargo compartment 3 independently. In this case, a rope flooring is laid on the cargo floor 2 to protect it from damage.

After loading any type of cargo, it is necessary to securely secure wheeled and/or wheelless cargo to the cargo floor 2. For these purposes, the set of the proposed mooring and rigging device includes mooring chains, mooring straps, mooring nets, mooring units, devices for fastening cargo containers (not shown ).

The proposed mooring and rigging device has a number of features and advantages compared to the prototype:

- the possibility of carrying out loading and unloading operations and operations with wheelless cargo has been implemented, including on unprepared sites without the use of additional ground equipment;

- the required safety and ease of use of the equipment is ensured;

- the accuracy and reliability of using the equipment is ensured by the presence of a remote control 8, with which the operator lifts and lowers the load, moves it along the cargo compartment 3, while the weight of the load is reflected on the display of the remote control 8.

The helicopter's mooring and rigging device allows for loading and unloading operations with wheeled vehicles weighing up to 12,000 kg; with wheelless loads weighing up to 5000 kg both from the ground and from the vehicle. Electric winches 1 with a traction force of 1500 kg are installed, which provide a maximum load movement speed of 16 m/min. The ability to securely secure wheeled and/or wheelless loads with a total weight of up to 20,000 kg has been implemented.

Documentation for the proposed mooring and rigging device has been developed and approved. The design of the invention was tested, as a result of which the proposed technical solution has successfully proven itself in a prototype. Modern materials and technologies are used in production.

Claims (12)

1. Helicopter mooring and rigging device, containing electric winches (1) with ropes (31) and loading blocks (17, 18), characterized in that the device contains two electric winches (1) installed on the cargo floor (2) in the front part of the cargo compartment (3), two drive stations (4) installed on the left and right sides of the fuselage in the front part of the cargo compartment (3) , two crane beams (32) are installed on the ceiling of the cargo compartment (3), on each of which there is a carriage (5), a bracket (16) with a mass meter (7) attached to it, as well as a bracket (84) on which two rollers (9, 10), on each electric winch (1) a rope (31) is fixed at one end, which passes through a loading block (17) located on the cargo floor (2), a loading block (18) fixed on the ceiling of the cargo compartment (3), roller (19) located on the carriage (5), roller (77) of the moving block (6), roller (20) located on the carriage (5), the other end of the rope (31) is fixed to the mass meter (7) , while a movable block (6) is installed on the rope (31), the drive station (4) contains a housing (22), inside of which a drum (24) with a coupling (88) is installed on the axis (23), and an electric mechanism (25) with a gear (26) is installed on the side, in the side bosses of the housing (22) tie (27), on which the levers (28) and the bushing (29) are located, two pressure rollers (30) are attached to the levers (28), a helical groove is made on the outer surface of the drum (24) for laying ropes (11, 12) and two windows for fastening the tips (33, 34) of the ropes (11, 12), respectively, the tips (33, 34) are pressed against the drum (24) with straps (35, 36), the drum (24) is closed on one side with a lid (37), in the center of the cover (37) there is a hole into which a sleeve (38) is pressed into which the axis (23) of the drum (24) is installed; on the other side of the drum (24), a coupling (88) is installed inside on two pins (39), on a gear (26) is installed on the electromechanical shaft (25), which meshes with the inner rim of the gear (42) of the coupling (88), from axial movement the gear (26) is fixed by a cup (49) and tightened with a nut (50), At each drive station (4) ropes (11, 12) are fixed, while the rope (11) passes through the roller (9) and is connected to the carriage (5), the rope (12) passes through the roller (10) and through the treadmill (13 ) is connected to a rope (14), which, bypassing the carriage (5), passes through a roller (15) mounted on the bracket (16) and is connected to the carriage (5) on the other side, the coupling (88) contains a flange (41) and a gear wheel (42), which during normal operation is fixed from rotation relative to the flange (41) by means of balls (43), balls (43) together with stops (44), springs (45), nuts (46) are installed in six cups (47) pressed into the flange (41), balls (43) engage with bushings (48) of the gear wheel (42), which is mounted on bearings on the flange shank (41), pressure roller (30) contains a race (51), bearings (52) and an axle (53), a race (51) on bearings (52) is installed on the axle (53), the carriage (5) contains a body (54), four rollers (55) on which the carriage moves along the crane beam (32), two rollers (56) located in the front part of the carriage, and two rollers (57) located in the rear parts of the carriage (5), suspension (58, 59), and two rollers (19, 20), ear bolts (60, 61) are screwed into the body (54) on both sides and brackets (62), two suspensions (58, 59) are connected to each other by rods (74), spacer bushings (75) are installed in the central hole of the rollers (19, 20), the roller (55) contains a cage (63), inside of which two bearings (64) are installed, into which axes (65) are inserted, fixed in the housing (54), the roller (55) is fixed on the axle (65) by a nut (66) and bolt (67), rollers (56, 57) consist of cages (68, 69), inside of which bearings (70, 71) are pressed, the moving block (6) contains two brackets (76), a roller (77) and a hook (78), the roller (77) rotates on the spacer sleeve (79), the brackets (76) are connected to each other by a bolt (80) and an axle (81) , on which a hook (78) with a latch (82) is suspended, rods (83) are installed on both sides of the roller (77) on brackets (76). 2. The helicopter mooring and rigging device according to claim 1, characterized in that microswitch blocks (96) are installed on the crane beams (32), which contain a bracket (92) on which microswitches (21), a spring (93), lever (94) with adjustable screw. 3. Helicopter mooring and rigging device according to any one of paragraphs. 1 or 2, characterized in that the control is carried out using a remote control (8), which is designed to remotely control the movement of the carriages (5), lifting and lowering the load, to control the weight of the lifted load, as well as control the weight per each carriage (5). 4. Helicopter mooring and rigging device according to any one of paragraphs. 1-3, characterized in that the mass meter (7) contains a cylinder (85), a pressure sensor (86) and a pressure alarm (87), the cylinder (85) of the mass meter (7) is fixed to the bracket (16) using a bolt (90) , a bracket (91) is attached to the bottom of the cylinder using screws (85), in which a pressure sensor (86) and a pressure alarm (87) are installed. 5. Helicopter mooring and rigging device according to any one of paragraphs. 1-4, characterized in that the device contains mooring equipment, including mooring chains, mooring straps, mooring nets, mooring units, devices for fastening cargo containers.