RU2413156C1 - Controlled independent universal positional underwater anti-aircraft (anti-ship) complex ("spider") and method of its implementation - Google Patents

Abstract

FIELD: weapons and ammunition.

SUBSTANCE: proposed complex consists of floating-up container with surface-to-air missiles, which is separated into floating segments supported on the sea surface with external capacities filled with gas. The above-water part of the main segment has radar receiving-radiating device, and underwater part has the disturbance stabilisation device. Missile segments are connected to the main segment by hinge-rod mechanisms with one degree of freedom in vertical plane. Standard mine anchor and coil of mooring cable with mechanism of installation to the specified depth are fixed by means of explosive bolt to lower part of transport-startup container. The proposed method involves attacking of air or sea objects with self-directing missiles starting in above-water position from floating-up transport-startup container initially located at the specified depth in positional underwater position. Container is kept at the specified depth with mooring cable attached to anchor and changes the modes of its activity as per the commands received via radio channel and/or hydroacoustic communication channel.

EFFECT: group of inventions allows enlarging tactical capabilities of tactical employment of the complex as sea mine intended for attacking air or sea objects.

2 cl, 6 dwg

Description

The invention relates to naval technology, in particular to marine underwater air defense systems, and is an improvement of the invention described in application No. 2008105175 (incoming 005621 from 02/11/2008).

Known anti-aircraft autonomous universal complex of self-defense of submarines ("PAUK" WITH PL) and the method of its application.

The specified device and method of its use have a narrow tactical orientation and disadvantages:

1. "SPIDER" WITH PL is intended for use only with submarines;

2. "SPIDER" WITH PL is used only for self-defense;

3. The "SPIDER" WITH the submarine after use unmasks the location of the submarine;

4. "SPIDER" WITH A submarine arbitrarily changes its location under the influence of wind and currents (the result is an artificial limitation of the time spent in combat).

The main objective to which the invention is directed is to expand the tactical capabilities of the combat use of an anti-aircraft autonomous universal complex, like a sea mine, designed to destroy air or sea targets.

To accomplish this task, an air-defense autonomous universal positional underwater controlled complex (PAUK-PPU) is proposed, consisting of a pop-up container with anti-aircraft missiles, divided into floating segments supported on the sea surface by external containers filled with gas, while the main segment has a radar receiving-emitting radar in the surface part device, in the underwater part - stabilization device on a wave, and rocket segments are connected to the main segment of the hinge rods Vym mechanisms with one degree of freedom in a vertical plane, characterized in that instead of the reactive accelerator is attached to a container with standard mine anchor coil minrepa and setting mechanism by a predetermined recess. The complex contains systems that ensure its functioning:

- a system of initiation and setting for a given recess;

- a control system and ascent activation, characterized in that an electro-acoustic transducer and (or) a pop-up radio receiver are used to receive control commands and classification signs of targets;

- deployment system;

- a system of stabilization and accounting of roll angles in waves;

- system of search and localization of goals;

- target destruction system;

- self-destruction system.

This design of an autonomous missile system allows for the implementation of important operational and tactical capabilities:

- have a long-term combat and psychological impact on air or naval forces in areas where the enemy has absolute superiority;

- block intercontinental and island air or sea communications;

- carry out missile defense of the coast from sea directions;

- carry out anti-landing defense of the coast from sea directions;

- carry out air defense of routes and areas of action of submarines;

- to protect marine mine anti-ship barriers from trawling by helicopters;

- in the anti-ship version, the complex has a significantly larger radius of destruction than known sea mines.

The placement of devices and mechanisms that make up the complex’s systems is illustrated by drawings, where FIG. 1 shows “PAUK-PPU” in a sectional (undisclosed) position, FIG. 2 shows PAUK-PPU in a positional underwater position, in figure 3 the principle of separation from the anchor and the ascent to the surface is shown, figure 4 shows the principle of disclosure of segments, figure 5 shows the "SPID" in the open position, figure 6 shows a pop-up receiver of control signals in section.

The complex consists of: a transport and launch container (Fig. 1, pos. 1), divided into floating segments supported on the sea surface by external containers filled with gas (Figs. 1, 4, 5, pos. 2, 3), while the main segment ( 1, 4, 5 pos. 4) has a radar receiving-emitting device in the surface part (Figs. 1, 4, 5 pos. 5), in the underwater part there is a wave stabilization device (1, 4, 5 pos. 6 ), and the rocket segments (Figs. 1, 4, 5, pos. 7) are connected to the main segment by articulated-rod mechanisms with one degree of freedom (Figs. 1, 4, 5, pos. 8) in the vertical oh plane. To the aft end of the transport and launch container, pyro-bolts are attached with a mine anchor (Figs. 1, 2, 3, pos. 11) and a minrepa coil (Figs. 1, 3, pos. 12) with a mounting mechanism for a given recess (Fig. 1, pos. 12a). The complex contains systems that ensure its functioning:

1. The system of initiation and installation on a given recess, consisting of:

- a standard electric contact device (Fig. 1, pos. 9), compatible with an electric contact device of a torpedo tube, designed to initiate complex mechanisms in a launcher from a control panel (operator);

- a standard mechanical contact device (Fig. 1, pos. 10), designed to record the moment the complex leaves the launcher and transmits a signal to the on-board computer;

- a standard mine anchor (Fig. 1, pos. 11) with a minrepa coil (Figs. 1, 2, 3, pos. 12) and a mounting mechanism for a given recess (Fig. 1, pos. 12a), designed to hold the complex at a position in the underwater position before receiving a command to ascend to the surface.

2. The control system and the activation of the ascent, consisting of:

- a pop-up radio receiver (FIGS. 1, 2, 3, 6, pos. 21) having significant positive buoyancy, comprising a retractable antenna (FIG. 6, pos. 22), a spring or electromechanical device for extending the antenna (FIG. 6, pos. 23) , a self-unwinding cable-cable wound externally on the receiver body (Fig.6 pos. 24), a spring device for compensating jerk loads on the cable-cable (Fig.6 pos.25), an electronic unit (Fig.6 pos.26). In the initial position, the receiver is in an unsecured state in the anchor niche, the cable is attached to the connector located on the bed of the minrepa coil, and docked with the connector of the transport-launch container. The pop-up radio signal receiver is intended for receiving control radio commands and (or) detecting and transmitting radio signals to the on-board computer, which are characteristic classification features of the affected objects;

- two or more electro-acoustic devices (FIGS. 1, 3, pos. 21a), intended for receiving control sonar commands and (or) detecting and transmitting on-board computer sonar signals, which are characteristic classification signs of the affected objects;

- the external gas tank of the main segment (Figs. 1, 3, 4, 5, pos. 2), designed to give the complex positive buoyancy at the ascent, as well as create confident buoyancy of the main segment of the complex on the surface. In the unopened position, the gas containers are packed in external niches of the body and covered with self-opening shields (Fig. 1, pos. 13);

- cylinder high pressure gas (high pressure gas) or gas generator (figure 1, position 14), designed to fill the external gas tank with gas;

- an on-board power source of the battery type (Fig. 1, pos. 15), designed to provide power to the systems and mechanisms of the complex;

- a control unit (on-board computer with actuators) (Fig. 1, pos. 16), designed to control the interaction of systems and mechanisms of the complex according to a given program;

- a block of hydrostatic sensors (Fig.1 pos.17), designed to transmit signals to the control unit to achieve a certain depth of ascent.

3. Deployment system, consisting of:

- pyro-bolts of the compartment intended for separating the anchor (Fig. 1, pos. 18), the minrepa coil (Fig. 1, 3, pos. 18a) and missile segments (Fig. 1, pos. 19) from the main segment of the container;

- articulated-rod mechanisms with one degree of freedom (Fig.1, 4, 5 pos.8), connecting missile segments with the main. In the unopened position, the rods are recessed into the niches of the transport launch container body;

- external gas tanks of the rocket segments (FIGS. 1, 4, 5, pos. 3), designed to give stable buoyancy to the rocket segments;

- cylinders GVD or gas generators of the rocket segments (Fig.1 pos.20), designed to fill the gas of the external gas tanks of the rocket segments.

4. The system of stabilization and accounting of roll angles in waves, consisting of:

- retractable stabilization mechanism on the wave type "floating anchor" (Fig.1, 4, 5 pos.6), designed to reduce the swing of the complex on the wave;

- a unit for accounting roll angles (gyroscopic instruments of the main segment) located in the control unit (Fig. 1, pos. 27), designed to determine and transmit to the control unit the instantaneous roll values of the complex on a wave.

5. The system of search and localization of goals, consisting of:

- receiving-emitting device (PIE) (figure 1, 4, 5 pos.5), designed to transmit and receive radar signals;

- electronic radar unit (Fig.1 pos.28), designed to generate radar pulses and process received signals;

- logical device radar (computer radar), which is part of the electronic radar unit (Fig.1 pos.29), designed to control the emission and reception of signals, as well as the classification of received signals according to specified criteria.

6. Target destruction system, consisting of:

- homing missiles (Fig. 1 pos. 30), located in the missile segments (Figs. 1, 4, 5, pos. 7), designed to directly hit targets;

- power supply and control cables (Fig. 1, pos. 31), placed in hollow swivel-rod mechanisms connecting the main and rocket segments (Figs. 1, 4, 5, pos. 8), designed to supply power and control signals to the rocket mechanisms segments, the installation mechanism for a given recess, electro-acoustic devices and a pop-up radio.

7. Self-destruction system, consisting of:

- explosive charge with an electric detonator located in the main segment (Fig. 1, pos. 32), designed to undermine the equipment and the external gas tank of the main segment;

- explosive charges of missiles located in the missile segments (Fig.1 pos.33), designed to undermine missiles and external gas tanks of missile segments;

- electronic command device of self-destruction (structurally included in the control unit) (Fig. 1, pos. 15), designed to send a command for self-destruction of the complex according to specified signs;

- atmospheric pressure hydrostat located in the lower part of the main segment (Fig. 1 pos. 34), designed to send a signal to the electronic self-destruction command device to remove the complex from the water (one of the signs of self-destruction).

Device operation

A method of hitting air or sea targets with homing missiles starting in the above-water position from a pop-up transport and launch container, initially located at a predetermined recess in a positional underwater position, characterized by controllability and durability of combat action, while the systems and mechanisms of the complex independently carry out the following operations:

1. Department of the anchor and the installation of the container on a given recess. Hold the container attached by the minrep to the anchor in a certain position.

2. Surfacing to the surface of the radio receiver connected to the container with a cable.

3. Receiving through a radio receiver or (and) electro-acoustic device control commands and (or) signals that are characteristic features of the affected objects.

4. Ascent of the container to the surface under the influence of positive buoyancy of the external gas tank.

5. Separation of the container into segments while maintaining power supply, control and a single coordinate system for all segments.

6. Giving the segments significant positive buoyancy due to their own external floating gas tanks.

7. Involvement of a mechanical stabilization system and an electronic system for recording sea waves.

8. The search for air (sea) targets by radiolocation of the air hemisphere (surface horizon).

9. The implementation of the classification of goals according to specified criteria.

10. The issuance of target designation data (flight paths) to homing missiles.

11. Launching rockets.

12. Repeat paragraph 8-11, if necessary.

13. Self-destruction of the complex for a given sign.

In the case when the carrier of the PAUK-PPU complex is a submarine, its method of use is described as follows.

The complex is located in the launcher (torpedo tube), their electrical contact devices are docked. By order of application, the operator of the launcher control panel supplies power to the system, fills the launcher (launcher) with water and opens its front cover. Power is supplied through a standard electrical contact device (Fig. 1, pos. 9) to the on-board power supply (Fig. 1, pos. 15), initiating it, then to the control unit (Fig. 1, pos. 16), where the onboard is heated and turned on computer, to the unit accounting roll angles (gyroscopic instruments of the main segment) located in the control unit (Fig.1 pos.16), where the absolute values of the vertical and horizontal are fixed. By the time the front cover TA is opened, the power supply of the complex mechanisms is transferred to the on-board power supply (Fig. 1, item 15). The Pauka-PPU is ejected from the PU by the standard method (high pressure gas or water), and there is a loss of hard contact of the standard mechanical contact device (Fig.1 pos.10) with the launcher track, which is transmitted to the control unit ( Fig.1 pos.16).

After the complex leaves the launcher and soaks a predetermined time interval from the control unit (Fig. 1, pos. 16), a signal is supplied to undermine the pyro-bolts of the armature compartment (Fig. 1, pos. 18). The anchor (Fig. 1, 2, 3 pos. 11) is separated and, under the influence of gravity, rushes to the bottom, the transport-launch container (TPK) (Figs. 1, 2, 3, pos. 1) with a minrepa coil fixed on it ( figure 1, 2, 3 pos.12) under the influence of positive buoyancy rushes to the surface, while minrep (figure 2, 3, 6 pos.24) is freely unwound. When the TPK (Figs. 1, 2, 3, pos. 1) reaches the upper limit of the specified range of setting depth, the signal from the block of hydrostatic sensors (Fig. 1, pos. 17) enters the control unit (Fig. 1, pos. 16), and from there to the installation device for a given recess (Fig. 1 pos. 12a), which fixes the minrepack coil (Figs. 1, 2, 3, pos. 12) and stops its unwinding. TPK (Fig. 1, 2, 3 pos. 1) under the influence of the gravity of the anchor (Fig. 1, 2, 3 pos. 11) sinks until it reaches the lower limit of the specified range of recesses. In this case, the signal from the unit of hydrostatic sensors (Fig. 1 pos. 17) enters the control unit (Fig. 1 pos. 16), and from there to the installation device at a predetermined recess (Fig. 1 pos. 12a), which stops fixing the minrepa coil (figure 1, 2, 3 pos.12) and resumes its unwinding. Free unwinding minrep (Fig.2, 3, 6 pos.24) allows TPK to emerge, and the anchor to sink.

This cyclic process continues until the anchor sinks to the bottom, and the TPK does not occupy a position at a given depth near the surface. The specified recess should be minimally sufficient to ensure the safety of the complex in stormy conditions.

Simultaneously with the separation of the anchor (Fig. 1, 2, 3, item 11), the radio receiver (Fig. 1, 2, 3, 6, item 21) is released and it emerges under the influence of its own buoyancy. In this case, the cable cable is unwound (Fig.6 pos.24), protected from breaking by a spring device for compensation of jerk loads on the cable cable (Fig.6 pos.25).

Upon completion of installation on a given recess, the complex is in the position shown in figure 2.

To control the state of the complex, two channels can be used: radio communication and sonar communication.

Control commands allow you to transfer the complex to one of four modes programmed in the control unit (Fig. 1, pos. 16):

- "positional mode" - KTP in the underwater position at anchor, the radio receiver on the surface (Fig.1, 2, 3, 6 pos.21) and electro-acoustic device (Fig.1, 3 pos.21a) under water accept only control commands .

From the "positional" mode, command translation into the "search", "combat", and "self-destruction" modes is possible;

- "search mode" - KTP in the underwater position at anchor, the radio receiver (Fig. 1, 2, 3, 6 pos. 21) on the surface and the electro-acoustic device (Fig. 1, 3 pos. 21a) under water receive control commands and (or) external signals in specified frequency ranges. Received signals are classified in the control unit to identify the characteristic features of the affected objects. If the signal is classified as a sign of an object of destruction, the complex switches to the “combat” mode.

From the “search” mode, command translation into the “positional”, “combat”, and “self-destruction” modes is possible;

- "combat mode" - the control unit (Fig. 1, pos. 16) gives a command to detonate the pyro-bolts of the minrepa coil compartment (Fig. 1, 3, pos. 18a). After resetting the minrepa coil (Fig. 1, 2, 3, pos. 12), the control unit (Fig. 1, pos. 16) gives a command to open the shut-off valve of the cylinder of the high pressure water supply (Fig. 1, pos. 14), from where the gas enters the external gas tank the main segment (Fig. 1, 2, 3, 4, 5, pos. 2), while the internal pressure drops flaps (Fig. 1, pos. 13) and the container opens. Ascent of the launch container occurs due to the positive buoyancy of the external gas tank of the main segment. The transition to the "combat" mode is shown in Fig.3.

When the surface is reached, the hydrostatic sensor unit (FIG. 1, pos. 17) sends a signal to the control unit (FIG. 1, pos. 16), the control unit (FIG. 1, pos. 16) gives a command to detonate the pyro-bolts of the missile segment compartment (FIG. 1 pos.19), to open the locking valves of the cylinders of the GVD of the rocket segments (Fig.1 pos.20) and supply gas to the external gas tanks of the rocket segments (Fig.1, 4, 5 pos.3), as well as the commands for the cylinder locking valve GVD of the main segment and gas supply to the extension of the stabilization mechanism on a wave (Fig.1, 2, 3, 4 pos.6).

Missile segments (Figs. 1, 2, 3, pos. 7) held by articulated-rod mechanisms (Figs. 1, 2, 3, pos. 8) unfold and circulate to the surface position under the influence of positive buoyancy of gas tanks.

Power supply for heating the equipment and initiating the electronic radar unit (Fig. 1 pos. 28) and the logical device of the radar (computer radar) (Fig. 1 pos. 29), as well as the arrest of gyro gyroscopes, is supplied simultaneously with the start of the ascent of the complex. After the stabilization mechanism is disclosed (Figs. 1, 2, 3, 4, pos. 6) and the rocket segments emerge (Figs. 1, 2, 3, and pos. 7) through a set time delay designed to stabilize the complex on the surface, the control unit (Figs. .1 pos. 16) sends a command to the logical device of the radar (Fig. 1 pos. 29) at the beginning of the search for targets. The logical device of the radar (Fig. 1 pos. 29) for a given program controls the generation, emission and reception of signals generated by the equipment of the electronic radar unit (Fig. 1 pos. 28), emitted and received by the radar receiving-emitting device (Figs. 1, 2, 3 item 5). The classification of targets is carried out in the logical device of the radar (Fig. 1, pos. 29) by comparing, according to a given program, the signs of received signals with embedded reference values. If the received signals are classified as a target of combat action, then its current coordinates are transmitted to the control unit (Fig. 1, pos. 16), where they are adjusted by the correction received from the roll angle meter (gyroscopic devices of the main segment) (Fig. 1, pos. 27) . Further, the on-board computer of the control unit according to a given program determines the flight path of the missiles and transmits data to the inertial control system of the SD. After that, the control unit (Fig.1 pos.16) gives a command to launch missiles. At the time of launch, the first rocket drops the plastic cover of the rocket segment, which protects against water ingress, rises vertically to a predetermined height, carries out a programmed turn to the combat course and scans the space of its own seeker during the flight. This sequence of operations is carried out relative to each of the targets classified as an object of attack. After the maximum missile flight time has elapsed, the complex again searches for and classifies targets and, if any, finds them, shells them again until the ammunition is fully used up.

If during the initial search, targets classified as an object of attack were not found, by the command of the radar logic device (Fig. 1, pos. 29), the electronic radar unit (Fig. 1, pos. 28) goes into passive mode, searching for signals of radio-emitting devices inherent objects of attack, in given frequency ranges. If such signals are detected, or after a predetermined time, the complex again enters the active search mode.

From the "combat" mode, the complex is transferred only to the "self-destruction" mode on its own;

- "self-destruction mode" - the self-destruction of the complex is carried out by the command of the electronic command device of self-destruction (structurally included in the control unit) (Fig. 1 pos. 15) by detonating the explosive charge with an electric detonator located in the main segment (Fig. 1 pos. 32) , as well as explosive charges of missiles located in the missile segments (Fig.1 pos.33) according to the following criteria:

- upon receipt of a management team;

- with full use of ammunition of the UR;

- when the energy reserves of the on-board power supply are used up by more than 90%;

- after a predetermined time of the complex, set in the timer of the control unit;

- by a signal from a hydrostat of atmospheric pressure located in the lower part of the main segment (Fig. 1, pos. 34), during unauthorized removal of the complex from water.

From the "self-destruction" mode, transfer to other modes is impossible.

Information sources

1. Application for invention No. 2008105175 (incoming 005621 dated 02/11/2008) “Anti-aircraft autonomous universal complex of self-defense of submarines (PAUK SO PL)”.

Claims (2)

1. An anti-aircraft (anti-ship) autonomous universal position-controlled underwater complex, consisting of a pop-up container with missiles, divided into floating segments supported on the sea surface by external containers filled with gas, the main segment having a radar receiving-emitting device in the surface part, in the underwater part - wave stabilization device, and rocket segments are connected to the main segment by articulated-rod mechanisms with one degree of freedom in a vertical plane, characterized in that instead of a jet accelerator, a standard mine anchor and a minrepa coil with a mechanism for installing on a given recess are attached to the container, containing systems that ensure its functioning: a system for initiating and setting to a given recess; an ascent control and activation system using an electro-acoustic transducer and / or a pop-up radio receiver to receive control commands and classification features of targets; deployment system; a system of stabilization and accounting for roll angles in waves; target search and localization system; target destruction system; self-destruction system. 2. A method of hitting aerial or marine objects with homing missiles starting in the above-water position from a pop-up transport and launch container, initially located in a position underwater, held at a predetermined recess by a minrep, attached to the anchor, and changing its modes of activity according to the instructions of the commands received by a radio channel and / or a hydroacoustic communication channel, while the systems and mechanisms of the complex autonomously carry out the following operations: separate the anchor and set the container p to a predetermined recess in a certain position, they ascend to the surface of a radio receiver connected to a cable-cable container, receive control commands and / or signals that are characteristic features of the affected objects through a radio receiver and / or electro-acoustic device, initiate separation from the minrep and surfacing the container to the surface under the influence of the positive buoyancy of the external gas tank, carry out the separation of the container into segments, while maintaining power supply, control and a single coordinate system for all segments, give segments significant positive buoyancy due to their own external floating gas tanks, use a mechanical stabilization system and an electronic system for recording sea waves, search for air or sea targets by radiolocation of the air hemisphere or surface horizon, classify targets according to specified criteria, give target designation data (flight paths) to homing missiles, launch missiles, repeat search, classification of targets and missile launch operations, if necessary, self-destruct complex on a given basis.

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