CN104121827B - A kind of stealthy bombing guided missile of repeatable utilization - Google Patents

Abstract

A reusable stealth bombing missile comprises a missile body, the missile body includes a warhead part, a weapon part, a body part and a propulsion part, a guidance system is arranged in the warhead part, the body part is a regular hexagonal prism structure, and the missile body There is also a layer of wave-absorbing polymer composite material layer on the top, and a magazine that can hold multiple warheads is provided inside the weapon part; a wing assembly is provided on the outer circumference of the projectile body, and the wing assembly consists of a main wing, a folding wing and an empennage. Composed, and the two sides of the missile body are symmetrically equipped with a wing recovery compartment, and a hatch is provided on the wing recovery compartment; there is also a folding landing gear at the bottom of the missile body, and a storage compartment for accommodating the folding landing gear is provided on the missile body; The invention can be used repeatedly, carrying multiple warheads to attack multiple targets one by one at a time. It has good stealth, can fly to the target at high altitude without being detected by radar, has a high cruising speed, and is not easy to be intercepted by fighter jets.

Description

A Reusable Stealth Bombing Missile

technical field

The invention relates to a stealth bombing missile, in particular to a reusable stealth bombing missile.

Background technique

At present, ballistic missiles such as medium and long-range missiles and intercontinental missiles are used once, which is a waste of cost; they basically do not have stealth performance, and the method of avoiding enemy radar and anti-ballistic missiles is to dive from high altitude and high speed when attacking, and use the tail to fine-tune the ballistic and use separate guides The former has limited ability to change the trajectory, while the latter can make the enemy tired of dealing with it, but it is obviously a waste of cost to use multiple warheads to strike a target. Carrying several warheads also increases weight and reduces maneuverability. Cruise missiles have good maneuverability at the end, and after launch, the altitude of the cruise missile is 7 to 15 meters (7 to 15 meters on the sea surface, less than 50 meters on flat land, and less than 100 meters on mountainous and hilly areas), and can avoid enemy radars, but the speed Slow, ordinary small arms can shoot it down, and it is not reusable either.

Contents of the invention

In order to solve the above technical problems, the present invention provides a reusable stealth bombing missile. The missile is reusable and carries multiple warheads to attack multiple targets one by one. It has good stealth and can fly to the target at high altitude without being detected by radar. It has a high cruising speed and is not easy to be intercepted by fighter jets.

The technical solution adopted in the present invention: a reusable stealth bombing missile, comprising a missile body, the missile body including a warhead part, a weapon part, a missile body part and a propulsion part, wherein a guidance system is arranged in the warhead part, its The head is pyramid-shaped, and the projectile body is a regular hexagonal prism structure. There is also a layer of wave-absorbing polymer composite material layer on the missile body, and a magazine that can hold multiple warheads is provided inside the weapon part; The outer circumference of the projectile part is provided with a wing assembly, which is composed of a main wing, a folding wing and an adjustable empennage, and the two sides of the projectile part are symmetrically provided with wing recovery bins for accommodating the folding wings. Each wing recovery compartment is provided with a hatch that can be opened automatically; the bottom of the missile body is also provided with a folding landing gear for easy landing, and the missile body is provided with a storage compartment for accommodating the folding landing gear.

The folding wing is composed of an inner wing, a middle wing and an outer wing, wherein the folding of the folding wing is realized through a four-link folding mechanism between the inner wing and the middle wing and between the middle wing and the outer wing.

The propulsion part adopts a rocket motor.

Beneficial effects of the present invention:

(1) The present invention has a main wing, a folding wing and an adjustable tail. After the missile is launched, the folding wing can be opened to perform cruising flight like an airplane. When entering the attack state, the folding wing can be folded away, and can be opened after the bomb is dropped to determine the target to be eliminated. Fold the wings and fly to the next target;

(2) The projectile body part of the present invention is a regular hexagonal prism, and is coated with a wave-absorbing polymer composite material, which can reflect and absorb radar waves to achieve a stealth effect, so that it can cruise at high altitude without relying on terrain to be invisible and being hit by light air defense weapons on the ground ;

(3) The present invention is equipped with folding landing gear. After the folding wings are unfolded, the lift and gravity generated by the folding wings are balanced, so that it can land smoothly on the runway, and the mission can be performed again after reloading and refueling;

(4) The present invention carries multiple warheads and can deliver warheads like a bomber.

Description of drawings

Fig. 1 is a structural representation of the present invention;

Fig. 2 is a side view of the present invention;

Marks in the figure: 1. Missile body, 2. Warhead part, 3. Weapon part, 4. Projectile body part, 5. Propulsion part, 6. Wing assembly, 7. Main wing, 8. Folding wing, 9. Empennage, 10 11. Folding landing gear, 12. inner wing, 13. middle wing, 14. outer wing.

detailed description

As shown in the figure, a reusable stealth bombing missile includes a missile body 1, and the missile body 1 includes a warhead part 2, a weapon part 3, a body part 4 and a propulsion part 5, wherein the warhead part 2 is provided with The guidance system has a pyramid-shaped head, and the body part 4 is a regular hexagonal prism structure. The propulsion part 5 adopts a rocket motor, and the missile body 1 is also provided with a layer of wave-absorbing polymer composite material. In that: the inside of the weapon part 3 is provided with a magazine that can hold a plurality of bullets; And the adjustable empennage 9 is made up of, and folding wing 8 is made up of inner wing 12, middle wing 13 and outer wing 14, wherein between inner wing 12 and middle wing 13 and between middle wing 13 and outer wing 14, through four-link folding mechanism The folding of the folding wing 8 is realized, and the wing recovery compartment 10 for accommodating the folding wing 8 is symmetrically provided on both sides of the body part 4, and each wing recovery compartment 10 is provided with a hatch that can be opened automatically; The bottom of the missile body 1 is also provided with a folding landing gear 11 for easy landing, and the missile body 1 is provided with a storage compartment for accommodating the folding landing gear 11 .

In the working process of the present invention, the folded wings can be opened to carry out cruising flight like an airplane, and fly at the edge of the atmosphere, waiting for fighter planes. When entering the attack state, the folded wings are retracted, and the speed is very fast due to the conversion of gravitational potential energy into kinetic energy. When flying over the target, drop the bomb to determine the target, then open the folding wings, fly back to the base, open the folding landing gear, land on the airport like an airplane, and then reuse it. The magazine can carry multiple warheads to attack multiple targets; after the warheads are delivered, the folding wings can be unfolded to land on the runway, and the mission can be carried out again after reloading and fueling.

Claims (1)

1. the stealthy bombing guided missile of a repeatable utilization, including guided missile body (1), described guided missile body (1) includes warhead section (2), weapon part (3), body part (4) and propulsive units (5), wherein it is provided with guidance system in warhead section (2), its head is pyramid-shaped, body part (4) is regular hexagon prism structure, it is additionally provided with one layer on described guided missile body (1) and inhales wave height molecular composite material layer, it is characterized in that: described propulsive units (5) uses rocket engine, described weapon part (3) is internal is provided with the magazine that can hold multiple bullet；The excircle of described body part (4) is provided with wing components (6), this wing components (6) is made up of main wing (7), folding wings (8) and adjustable empennage (9), and body part (4) is symmetrically arranged on two with the wing recovery bin (10) for receiving folding wings (8), each wing recovery bin (10) is equipped with the hatch door that can automatically open up；Described guided missile body (1) bottom is additionally provided with the folding undercarriage (11) of convenient landing, and guided missile body (1) is provided with for accommodating the place position folding undercarriage (11), described folding wings (8) is by inner wing (12), wing centre section (13) and outer wing (14) composition, the folding of folding wings (8) is wherein realized between inner wing (12) and wing centre section (13) and wing centre section (13) and outer wing (14) by double leval jib fold mechanism, cruising flight can be carried out as aircraft when making folding wings (8) open, and fly in atmosphere edge, wait opportunity of combat, folding wings is packed up when entering attack state, dive rapidly.