RU2336199C1 - Strategic helicopter - Google Patents

Abstract

FIELD: transportation.

SUBSTANCE: strategic helicopter contains vertical cylindrical fuselage (1) and bearing coaxial propellers (2). Fuselage is implemented according to scheme "tube inside tube", and all helicopter units are located in space formed between external tube walls and internal through tube for installation inside of through fuselage chamber the missile with ability of its launching.

EFFECT: invention improves helicopter maneuverability.

2 cl, 1 dwg

Description

The invention relates to aircraft used for basing and launching medium-range missiles, in particular, to the design of special missile-carrying helicopters.

Known design launchers equipped with medium-range missiles mounted on automobile chassis.

The disadvantage of such missile systems is limited patency when used in highly rugged terrain, which reduces maneuverability and increases the vulnerability of the systems.

The purpose of the invention is to develop a missile system designed for transportation, basing and launching medium-range ballistic missiles, capable of operating effectively in mountainous and other conditions of rugged terrain.

This goal is achieved by developing the design of a special helicopter with a vertical fuselage, made according to the scheme "pipe in pipe". A rocket is located in the inner through pipe on the guides.

All components and assemblies of such a helicopter are located either in the space formed between the walls of the external and internal pipes, or are hung from the outside.

In the upper part of the fuselage, the hubs of one or more pairs of coaxial screws, which are located one above the other, are pivotally hinged. The hubs are hung with the possibility of deflecting the screws in any direction for the translational flight of the helicopter in all directions without a turn.

The drawing shows a helicopter with one pair of coaxial rotors.

The rocket is launched from the ground position of the helicopter, the fuselage of which in this case serves as a launcher. Before starting, the fuselage is lifted by means of telescopic legs, previously fixed on the supporting surface, and the propeller blades are lowered.

Analogs of the present invention are not known to the author.

The drawing schematically depicts a strategic helicopter of the proposed design with a missile.

This helicopter contains a tubular fuselage 1, coaxial screws 2 and telescopic legs 3. For greater reliability, the helicopter should be equipped with two engines if possible combat maneuvering on one of them.

The use of a vertical cylindrical fuselage 1 in the design of the helicopter and the possibility of deflecting the screws 2 to either side provides the helicopter with the high maneuverability necessary when flying at a minimum height and in tight mountain conditions. Adjustable telescopic legs 3 provide a strictly vertical position of the fuselage 1 before launching the rocket.

The thermal effect of the gases generated during the launch of the rocket on the walls of the inner tube of the fuselage 1 will be short-lived. However, the walls must be covered with insulating material, and it is possible to provide for air cooling.

The proposed strategic helicopter operates as follows.

With an increase in the level of combat readiness, helicopters are equipped with missiles, and at the command “readiness number one” they take off, disperse, occupying the intended launching positions, and are brought into a state of complete readiness for launching missiles.

At the “start” command, the missiles go to the set targets, and the helicopters alternately fly to the base, where they are recharged by the missiles and again dispersed to other coordinates, reducing their vulnerability.

Possessing high operational maneuverability, the ability to quickly disperse and conceal basing in mountainous folds, the ability to suddenly approach enemy territory and launch missiles, strategic helicopters maneuvering along the borders of the alleged aggressor and armed with missiles with powerful warheads will become a sufficient deterrent.

We must not threaten, but we must be afraid!

The author has developed a variant of launching a ballistic missile from a helicopter hovering mode, which may be the subject of a separate invention.

Claims (2)

1. A strategic helicopter containing a vertical cylindrical fuselage and coaxial rotors, the fuselage made according to the “pipe in pipe” scheme, and all helicopter assemblies are placed in the space formed between the walls of the outer pipe and the inner through pipe for installation inside the through cavity of the fuselage of the rocket with the possibility of its launch. 2. The strategic helicopter according to claim 1, containing a vertical cylindrical fuselage and bearing coaxial screws, and several pairs of coaxial screws are hung on the outer fuselage tube one above the other.