RU2341758C1 - Self-propelled command control and communication centre - Google Patents

Abstract

FIELD: arms.

SUBSTANCE: invention concerns mobile systems of arms of coastal basing and can be used at creation mobile coastal antiship missile systems. The self-propelled command control and communication centre contains the self-propelled chassis and the command post located on it (CP). In CP the workplaces of operators of staff, radar station (RS), control system allocation of targets and start-up of rockets, communication facility and information interchange, navigating complex, monitors by an electric equipment and the aerial are placed. The CP is executed in the form of a van and it is divided into three compartments.

EFFECT: increase of reliability of the device of lifting of aerial radar installations, protection of aerial radar installations and the elevating mechanism from influence of climatic factors and influences influences, an exception of possibility of influence of microvawe radiation on staff.

4 dwg

Description

The invention relates to coastal-based mobile weapon systems and can be used to create mobile coastal mobile anti-ship missile systems.

Self-propelled command and control command post (SKPUS) is designed to detect surface targets, generate target designation data and control the complex when firing at designated targets.

Known coastal mobile anti-ship complex "Rubezh" (Russia), (Armament of the Navy. Encyclopedia of the XXI century. Arms and technologies of Russia, volume III, p. 129. Moscow: Publishing house "Arms and technologies, 2001), consisting from self-propelled missile launchers, including a radar target designation system.

Self-propelled launcher (SPU) of the Rubezh complex is made on a self-propelled wheeled chassis, has a combat control post (BPU) located in front of the wheeled chassis and a launcher located at the rear of the wheeled chassis.

The control room is made in the form of a sealed van, which houses the commander, equipment operators, radar equipment, fire control systems, power supply unit, communications, personnel support equipment.

A radar antenna with an electromechanical device for lifting it from the traveling position to the working one is installed on the front wall of the control room.

The disadvantages of this design are:

- the complexity and lack of reliability of the electromechanical device for lifting the mast of the radar antenna;

- the radar antenna, mast and its lifting device are not protected from external climatic and mechanical influences, which reduces the reliability and service life of the antenna device;

- radar devices are located in the control room, therefore, during their operation, the possibility of a negative impact of microwave radiation on the crew is not ruled out;

The objective of the present invention is to increase the reliability of the device for lifting the mast of the radar antenna, protecting the antenna of the radar station and radar from the effects of climatic factors and mechanical stresses, eliminating the possibility of exposure to microwave radiation on personnel.

The technical result of the present invention is achieved by the fact that in a self-propelled command and control post containing a self-propelled chassis and located on it a combat control post (BPU), made in the form of a van, which houses the workplaces of operators of personnel, radar station, missile targeting and launch control systems, communication and information exchange facilities, a navigation complex, electrical equipment control devices and a radar antenna with a device for its lifting, and an autonomous source of electronic catering, and the van is divided into three compartments, in the front of which are the radar operator’s devices, missile targeting and launch control systems, communication and information exchange systems, a navigation complex and electrical equipment control devices, in the middle compartment, which is made radio-sealed and connected to the front radio-sealed door , non-operational maintenance radar devices are placed, including devices operating in the microwave range, and the rear compartment is equipped with front and rear covers pivotally mounted respectively Naturally, on the roof of the control unit and the rear wall of the compartment, and there is a mast with a radar antenna and a lifting device made in the form of a hinged parallelogram and a hydraulic cylinder, while the hinged parallelogram is formed by the antenna mast, the lower double arms and the upper arm, one ends of which are pivotally attached to the antenna mast, while others are pivotally mounted on the front wall of the rear compartment, the hydraulic cylinder rod is pivotally mounted on the front wall of the rear compartment of the control unit, and its body is pivotally mounted on the lower double levers of the pairs an allelogram lifting device, on the upper arm of which a lever is mounted pivotally connected to the front cover of the compartment, and a trunnion is mounted on the antenna mast, which, when the antenna is lowered, is engaged with a hook connected with a torsion bar and a lever system connected to the rear cover of the rear compartment.

Figure 1 and figure 2 shows a General view of the SKPS in the stowed and working position, respectively.

SKPUS contains a self-propelled chassis 1, on which a combat control post 2 and an autonomous power supply (AIP) 3 are installed.

BPU is made in the form of a van, divided into three compartments. Front 6 and middle 7 compartments are airtight. In the rear non-pressurized compartment 4 there is a radar antenna 5 with a hydraulic device 10 for lifting it from the traveling position to the working one.

In the front compartment are the personnel of the SKPUS, the radar operator’s devices, the control systems for targeting and launching missiles from the SPU, the electrical control devices, the complex of communication and information exchange with the SPU, a navigation complex, and life support equipment.

In the middle radio-sealed compartment connected to the front compartment of the sealed door, there are non-operational maintenance radar devices, including devices operating in the microwave range.

Figure 3 and figure 4 shows the rear compartment of the control unit with a device for lifting the radar antenna in the stowed and working position, respectively.

A hydraulic cylinder 11 is mounted on the front wall of the rear compartment, pivotally connected to a pair of lower levers 12 of the parallelogram lifting device, which are also pivotally connected to the mast 13 of the radar antenna 5, with the mast 13 the upper lever 14 of the parallelogram lifting device is pivotally connected, the second ends of the levers 12 and 14 are pivotally mounted on the front wall of the rear compartment.

On the front and rear walls of the rear compartment, covers 8 and 9 are hingedly mounted.

On the upper lever 14 of the lifting device, a lever 15 is pivotally mounted pivotally connected to the cover 8 of the rear compartment.

The cover 9 is connected to the torsion bar 16 and the lever system 17, on which the hook 19 is fixed. A pin 18 is mounted on the mast 13 of the antenna 5.

Work SKPUS in combat position is as follows.

After the chassis is stopped, the AIP is launched, from the electrical equipment control devices, power is supplied to all systems involved in the combat work. A signal is sent to raise the radar mast, the radar devices are turned on. After raising the radar antenna and completing the radar test control, it turns on the radiation and begins to search for targets, the data of which are transmitted to the target distribution and missile launch control system. The latter automatically transmits firing tasks to SPU via communication channels.

The radar antenna lift device operates as follows.

When a signal is sent to raise the antenna, the hydraulic system for lifting the antenna starts to work, and the rod of hydraulic cylinder 11 extends, which acts on the lower arms 12 and rotates them relative to the mounting axis “a” on the wall of the control unit, as a result, the antenna mast 13 and the upper lever are driven 14. Due to the fact that the points “a”, “b” of the attachment of the levers to the body and “c”, “d” to the mast form a parallelogram, the mast with the antenna 5 mounted on it makes plane-parallel movement. The rise of the antenna is completed when the hydraulic cylinder rod is fully out.

When the lever 14 moves, the lever 15 connected to it opens the cover 8. When the mast moves, the pin 18 disengages from the lever system 17 and the torsion bar 16 opens the cover 9.

When lowering the antenna 5, reverse processes are carried out. The lever 15 closes the lid 8, and the pin 18, engaging with the hook 19 of the lever system 17, closes the lid 9, while cocking the torsion bar 16.

Claims (1)

A self-propelled command and control command post containing a self-propelled chassis and a combat control post (BPU) located on it, made in the form of a van, which houses the workplaces of personnel personnel, a radar station, missile targeting and launch control systems, and communications and information exchange, a navigation complex, electrical control devices and a radar antenna with a device for lifting it, and an autonomous power source, characterized in that the van is divided into three compartments, in in the afternoon of which the radar operator’s devices, missile targeting and launch control systems, communication and information exchange systems, a navigation complex and electrical equipment control devices are located, in the middle compartment, made radio-sealed and connected to the front radio-sealed door, non-operational maintenance radars are placed, including devices operating in the microwave range, and the rear compartment is equipped with front and rear covers pivotally mounted respectively on the roof of the control unit and the rear wall of the compartment, and in it a mast with a radar antenna and a lifting device made in the form of a hinged parallelogram and a hydraulic cylinder are placed, while the hinged parallelogram is formed by the antenna mast, the lower double arms and the upper lever, some ends of which are pivotally attached to the antenna mast and the other are pivotally mounted on the front wall of the rear compartment, the hydraulic cylinder rod is pivotally mounted on the front wall of the rear compartment of the control unit, and its body is pivotally mounted on the lower double levers of the parallelogram lifting device, on the upper lever where the lever is fixed pivotally connected to the front cover of the compartment, and a trunnion is mounted on the antenna mast, which, when the antenna is lowered, is engaged with a hook connected to the torsion bar and a system of levers connected to the rear cover of the rear compartment.

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