RU23970U1 - WINGED ROCKET WITH ADDITIONAL DISCHARGED OUTBOARD BATTLE BOX AND FUEL TANK (OPTIONS) - Google Patents

Description

WINGED ROCKET WITH ADDITIONAL

RELEASED OUTDOOR BATTLE BLOCK

AND FUEL TANK (OPTIONS).

The utility model relates to the field of missile weapons and can be used both in the manufacture of new missiles and in the modernization of the existing fleet of missiles.

Known cruise missile (KR), utility model No. 19574 dated 05/29/2001, containing: a fuselage with a propulsion system, control system, aerodynamic surfaces, a warhead and at least one additional outboard warhead equipped with an engine, with the possibility of reset and flight of the war block along an independent trajectory.

The presence in the well-known KR of an additional suspended combat unit with the possibility of dropping and flying along an independent trajectory increases the likelihood of overcoming close air defense.

Moreover, the CR can be either newly made or upgraded from missiles that do not have an additional suspended combat unit, with a slight change in their design associated with the attachment of the combat unit.

To maintain the high flight speed of the known aircraft, especially at supersonic speeds, a large second fuel consumption is required, which limits the flight range, since the fuel supply of the aircraft is limited. An increase in the flight range by traditional methods will entail an increase in the diameter or length of the rocket, which will require almost the entire amount of development work to be carried out again, as well as worsen the maneuverability of the rocket.

Common features with the proposed technical solution are:

- according to option 1 - the presence of a fuselage with a propulsion system, control system, aerodynamic surfaces, and an additional suspended combat unit with the ability to reset and fly the combat unit along an independent trajectory;

- according to option 2 - the presence of a fuselage with a propulsion system, control system, aerodynamic surfaces, and an additional suspended combat unit equipped with a control system, with the ability to reset and fly the combat unit along an independent trajectory;

- according to option 3 - the presence of a fuselage with a propulsion system, control system, aerodynamic surfaces, and an additional outboard combat unit equipped with an engine, with

the ability to reset and fly the warhead along an independent trajectory.

The proposed technical solution solves the problem of increasing the flight range of a basic cruise missile without impairing its tactical and technical characteristics, with minimal expenses for experimental design work, manufacturing new ones or upgrading the existing fleet of missiles.

To achieve the specified technical result:

- according to option 1, a cruise missile containing a fuselage with a propulsion system, control system, aerodynamic surfaces and an additional resettable suspended warhead with the ability to reset and fly the warhead along an independent path, is equipped with at least one additional resettable suspended fuel tank connected to a missile docking and dumping unit and connected to the propulsion system of the rocket by the overflow line with a check valve;

- according to option 2, a cruise missile containing a fuselage with a propulsion system, control system, aerodynamic surfaces and an additional resettable suspended combat unit equipped with a control system, with the ability to reset and fly the combat unit along an independent path, is equipped with at least one additional resettable suspended a fuel tank connected to the missile by the docking and dumping unit and communicated with the rocket propulsion system by an overflow manifold with a check valve;

- according to option 3, a cruise missile containing a fuselage with a propulsion system, control system, aerodynamic surfaces and an additional resettable suspended combat unit equipped with an engine, with the ability to reset and fly the combat unit along an independent path, is equipped with at least one additional resettable suspended fuel a tank connected to the missile by a docking-discharge unit and connected to the rocket propulsion system by an overflow line with a check valve.

The distinctive features of the proposed design of a cruise missile with additional resettable mounted combat unit and at least one fuel tank from the above, known in options 1-3, is the presence of at least one additional resettable suspended fuel tank connected to the rocket assembly docking-discharge and communicated with the propulsion system rocket overflow line with check valve.

Due to the presence of the indicated distinctive features in combination with the known ones (indicated in the restrictive part of the formula), the following technical result is achieved - due to the presence of an additional amount of fuel in the outboard fuel tank, the flight range of the aircraft increases, moreover, due to the fact that they are reset as the outboard tanks are developed (in overflow lines

there are check valves), on the final, critical section, the rocket is not inferior to the base in its tactical and technical characteristics. In addition, the implementation of these technical solutions requires minimal changes in the design of the base missile, which minimizes the cost of development work, significantly reduces the development and manufacturing time, and also allows for the modernization of the existing fleet of missiles.

As a result of a search by sources of patent and scientific and technical information, the totality of features characterizing the proposed cruise missile with additional discharged suspended combat unit and fuel tank was not found. Thus, the proposed utility model meets the eligibility criterion new.

The proposed technical solution can find application in the design of cruise missiles. Thus, the proposed utility model meets the eligibility criterion of industrial applicability.

The utility model is illustrated by the attached figure.

The cruise missile shown in versions 1-3 contains a fuselage 1 with a propulsion system 2, a control system 3, a warhead 4, aerodynamic surfaces 5, an additional suspended warhead 6 with the ability to reset and fly along an independent trajectory, and at least one additional resettable suspended fuel tank 7 connected to the fuselage of the rocket 1 docking-discharge unit 8 and connected to the propulsion system 2 of the rocket, overflow line 9 with a check valve 10 located in the joints of the joint wki-reset 8.

In addition, according to option 2, the outboard combat unit 6 may have its own control system 11, and according to option 3, the outboard combat unit 6 may have its own engine 12.

The device according to options 1-3 works as follows. When flying KR to the target, an additional mounted fuel tank 7 is initially generated and discarded. When the CR approaches the target, its guidance system 3 guides the mounted combat unit 6, after which it is separated from the missile and the further path to the target passes independently. The rest - the cruise missile guides and flies to the same target according to the program laid down in it.

In addition, according to option 2, after the separation of the combat unit 6 from the rocket, it is provided to control it in autonomous flight with its own control system 11, for a more accurate hit on target.

In the device according to option 3, after the separation of the additional combat unit 6 from the fuselage of the rocket 1, the engine 12 of the combat unit 6 is activated, which allows the separation of the combat unit 6 at an earlier time, with an expanded air defense zone.

UJO 2 -W 9S

USEFUL MODEL FORMULA (OPTIONS)

1. WINGED ROCKET containing a fuselage with a propulsion system, control system, warhead, aerodynamic surfaces and an additional suspended combat unit with the ability to reset and fly along an independent path, characterized in that it is equipped with at least one additional resettable suspended fuel tank connected to the rocket by the docking-dumping unit and communicated with the rocket propulsion system by the overflow line with a check valve.

2. WINGED ROCKET containing a fuselage with a propulsion system, control system, warhead, aerodynamic surfaces and an additional suspended warhead equipped with a control system, with the ability to reset and fly the warhead along an independent path, characterized in that it is equipped with at least , with one additional resettable suspension fuel tank connected to the missile by the docking-discharge unit and connected to the rocket propulsion system by an overflow manifold with a non-return valve.

3. A WINGED ROCKET containing a fuselage with a propulsion system, control system, warhead, aerodynamic surfaces and an additional suspended warhead equipped with an engine, with the possibility of dropping and flying the warhead along an independent path, characterized in that it is equipped with at least one additional resettable suspended fuel tank connected to the missile by the docking-discharge unit and connected to the rocket propulsion system by an overflow manifold with a non-return valve.

Cruise missile with extra

discarded outboard combat

block and fuel tank (options).

Claims (3)

1. A cruise missile containing a fuselage with a propulsion system, control system, warhead, aerodynamic surfaces and an additional suspended combat unit with the ability to reset and fly along an independent path, characterized in that it is equipped with at least one additional resettable suspended fuel tank connected to the rocket by the docking-dumping unit and communicated with the rocket propulsion system by the overflow line with a check valve.  2. A cruise missile containing a fuselage with a propulsion system, control system, warhead, aerodynamic surfaces and an additional suspended warhead equipped with a control system, with the possibility of dropping and flying the warhead along an independent path, characterized in that it is equipped with at least , one additional resettable suspension fuel tank connected to the rocket by the docking-dumping unit and connected to the rocket propulsion system by an overflow manifold with a non-return valve. 3. A cruise missile containing a fuselage with a propulsion system, control system, warhead, aerodynamic surfaces and an additional suspended warhead equipped with an engine, with the possibility of dropping and flying the warhead along an independent path, characterized in that it is equipped with at least one additional discharged suspended fuel tank connected to the missile by the docking-discharge unit and connected to the rocket propulsion system by an overflow manifold with a non-return valve.