RU2731296C1 - Automated missile loading system into self-propelled launcher of mobile coastal missile system - Google Patents

Abstract

FIELD: military equipment.

SUBSTANCE: automated missile loading system into self-propelled launcher of mobile coastal missile system comprises self-propelled launcher (SPL) with transport module fixed on chassis power frame, with opening rear flaps, lodgments for placement of transport-launching containers (TLC) with missiles and transloader (TL), including transport module fixed on chassis power frame, with opening rear flaps, motor-reducer and chain drive. TL comprises positioning platform arranged on hydraulic supports on chassis power frame, on which unlocked lodgments interconnected by means of guides are rigidly fixed. Lodgments accommodate cylindrical rollers, as well as TLC with missile movement mechanism. On the SPL there is a starting device including a guide boom with movable carriages installed on it. Except for rear flaps, SPL and TL contain upper flaps to provide crane loading TLC, and lodgments for SPL are made open with possibility of unloading empty TLC in vertical position. On standard assemblies of chassis bumper attachment there is a beam for docking and leveling SPL with TL.

EFFECT: broader operational capabilities of the system and shorter recharging of the ammunition.

1 cl, 7 dwg

Description

The invention relates to military equipment, in particular to the field of supply and loading of ammunition, and describes an automated system for loading and changing the ammunition of missiles in transport-launch cups (TPS) in a self-propelled launcher (SPU) using a transport-loading machine (TZM) as part of a mobile coastal missile complex (PBRK).

The closest analogue to the claimed invention in terms of a set of essential features is a method for automatically loading missiles using a chain drive and rail guides [Patent RU 2578917, IPC F41A 9/04, “Automatic system for loading missiles into a self-propelled launcher, publ. 03/27/2016], containing chain conveyors and rail guides, placed on the basis of containers TZM and SPU.

The closest analogue has the following disadvantages:

- the lack of the ability to load missiles into the TPS in the TZM from the ammunition storage;

- the need to use 2 TPM (empty and loaded) to recharge, which increases the time of its recharge;

- the high cost of implementing this scheme for loading missiles.

The technical problem of the present invention is to reduce the time for reloading the ammunition and expand the operational capabilities of the PBRK.

The technical problem posed is achieved due to the fact that the proposed automated system for loading missiles into a self-propelled launcher of a mobile coastal missile complex contains an SPU with a transport module fixed on the chassis power frame, with opening rear flaps, cradles for placing a TPM with missiles and TPM, including a transport a module fixed on the chassis power frame, with opening rear doors, a geared motor and a chain drive, and differs in that the TPM contains a positionable platform located on hydraulic supports on the chassis power frame, on which the disconnectable cradles are rigidly fixed to each other by means of guides, in which cylindrical rollers are installed to reduce the frictional force when moving the TPS with a rocket, as well as a mechanism for moving the TPS with a rocket, made in the form of a pusher, driven by a chain drive and a gear motor, while a starting device is installed on the SPU, including A guide boom with movable carriages mounted on it, in the rear of which a holding device with a mechanical latch is installed, in which a groove is made for hitting a pin located on the bottom spacer, for fastening and orientation along the roll of the TPS with a rocket in the SPU. Moreover, the SPU and TZM, in addition to the rear flaps, contain upper flaps to ensure crane loading of the TPS, and the cradles on the TPS are made openable with the possibility of unloading empty TPSs in a vertical position, and a beam for docking and alignment along the course of the TPS with TZM is installed on the standard chassis bumper attachment points. The essence of the invention is illustrated in the following figures:

Figure 1 - TPM design;

Figure 2 - SPU design;

Figure 3 - principle of operation of the missile loading system;

Figure 4 - the principle of unloading empty pipes;

Figure 5 - pusher design;

Figure 6 - the structure of the positioned platform;

Figure 7 - design of the holding device, where

1 - transport module TZM;

2 - positioned platform;

3 - detachable TZM cradles;

4 - cylindrical rollers of TZM cradles;

5 - TPN with missiles;

6 - pusher:

7 - gear motor;

8 - detachable SPU cradles;

9 - directing boom;

10 - cylindrical rollers of SPU cradles;

11 - holding device;

12 - mechanical latch;

13 - beam;

14 - carriage;

15 - pin of the bottom spacer;

16 - front lodgment SPU;

17 - hydraulic supports;

18 - supports;

Referring to FIG. 1 shows the design of the TPM from the composition of the PBRK with the design of the upper and rear doors of the transport module (1), each consisting of two sections. In the transport module (1) of the TPM, on a positioned platform (2), placed by hydraulic supports, disconnectable cradles (3) with cylindrical rollers (4), connected to each other by means of guides, are installed, on which the TPM with missiles (5) are located. Moving the TPM with missiles from the TPM to the SPU is carried out using a movement mechanism made in the form of a pusher (6), driven by a chain drive and a gear motor (7).

FIG. 2 shows the design of the SPU from the composition of the PBRK with the design of the upper and rear doors of the transport module, each consisting of two sections. Cylindrical rollers (10) and a holding device (11) with a mechanical latch are installed in the design of the openable cradles (8) of the boom guide (9).

FIG. 3 shows the principle of operation of the missile loading system in the SPU PBRK. TZM and SPU are interlocked using a beam (13) and standard hooks installed on standard attachment points for the rear bumpers of the chassis. After that, the TZM pulls the RV to ensure the parallelism of the axes of the RV and TZM cradles and align the two moving parts of the complex relative to each other along the course angle. The positioned platform (2) adjusts the openable cradles (3) from the RTS to the TPM so that the axes of the centers of the cradles are above the axes of the centers of the cradles (8) on the SPU. Next, the mechanism for moving the TPS with the rocket is activated as follows: a gear motor is turned on from the TZM cabin and transfers the force to the chain drive, which drives the pusher (6), which is pre-docked on the standard attachment points of the TPS with the rocket located in the TZM. On the SPU, detachable cradles (8) are preliminarily unfastened and in a horizontal position the carriage (14) of the boom guide (9) is extended backward, while the holding device (11) is split open. TPS with a rocket moves until the pin (15) of the bottom spacer enters the groove of the holding device. Then the holding device (11) is locked, and the carriage moves forward, moving the front part of the TPS with the rocket to the front cradle of the SPU (16). The missiles are loaded from the ammunition storage using lifting devices through the upper doors of the SPU and TZM.

FIG. 4 shows the principle of unloading empty TPS, which is carried out in the vertical position of the boom guide (9) of the SPU when opening the upper and rear flaps by opening the cradles (8) and the holding device (11). After that, the guide boom (9) of the SPU is transferred to a horizontal position.

FIG. 5 shows the pusher (6), which is docked on the standard attachment points of the TPS with the rocket. After loading, the pusher returns to its original position using a chain drive.

FIG. 6 shows a positioned platform (2) of the TPM, which, with the help of hydraulic supports (17) placed on the load-bearing frame of the chassis, aligns the TPM with a missile on the TPM in the pitch plane with respect to the steering boom of the SPU. In the stowed position, the positioned platform (2) is placed on the supports (18). On the positioned platform (2) of the TZM, detachable cradles (3) are installed, in which cylindrical rollers (4) are installed in order to reduce friction when moving the TPS with the rocket.

FIG. 7 shows a holding device (11) located in the rear part of the carriage (14) of the boom guide (9) of the RVC. The holding device (11) is provided with a mechanical latch (12) and contains a groove for the pin (15) of the bottom spacer to enter. The mechanical latch (12) for free movement of the pin (15) of the bottom spacer is moved to the open position, and to hold the TPS on the boom of the SPU is moved to the closed position.

The technical result of the present invention is to expand the operational capabilities of the complex, including the possibility of undocking the empty TPM immediately after the missile launch, as well as, due to the absence of additional TPM, reducing the time for reloading ammunition with the minimum possible modifications to the existing elements of the PBRK.

Claims (1)

An automated system for loading missiles into a self-propelled launcher of a mobile coastal missile system, containing a transport module of a self-propelled launcher (SPU), mounted on a chassis power frame, with opening rear flaps, cradles for placing transport and launching glasses (TPS) with missiles, a transport module for a transport - a charging machine (TZM) with opening rear doors and fixed on the chassis power frame, a geared motor and a chain drive, characterized in that it contains a positionable TZM platform located on hydraulic supports on the chassis frame, on which the chassis are rigidly connected to each other with the help of guides openable cradles, in which cylindrical rollers are installed to reduce the frictional force when moving the TPS with a rocket, as well as a mechanism for moving the TPS with a rocket, made in the form of a pusher, driven by a chain drive and a gear motor, while the SPU starting device includes guides boom with movable carriages installed on it, in the rear part of which a holding device with a mechanical latch is installed, in which a groove is made for a pin located on the bottom spacer to enter and orientate along the roll of the TPS with a rocket in the SPU, while the upper flaps of the SPU and TZM provide crane loading of the RTS, and the cradles on the SPU are made to be disconnected with the ability to unload empty RVs in a vertical position, and a beam is installed on the standard attachment points for the chassis bumpers for docking and alignment along the course of the SPU with the TPM.

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