CN216925326U

CN216925326U - Fusion type cruise bomb device suitable for remote emission

Info

Publication number: CN216925326U
Application number: CN202122375067.1U
Authority: CN
Inventors: 陈其盛; 黄江涛; 陈宪; 刘刚; 单恩光; 钟世东; 陈诚; 陈立立; 余龙舟; 雷鹏轩
Original assignee: Institute of Aerospace Technology of China Aerodynamics Research and Development Center
Current assignee: Institute of Aerospace Technology of China Aerodynamics Research and Development Center
Priority date: 2021-09-29
Filing date: 2021-09-29
Publication date: 2022-07-08
Anticipated expiration: 2031-09-29

Abstract

The utility model discloses a fusion type cruise bomb device suitable for remote emission, and particularly relates to the field of overall design of aircrafts. The utility model provides a fusion formula is patrolled and is navigated bullet device suitable for long-range transmission, including many pieces of cruise bullet and flying wing formula oil tank device, be connected with the mechanical clamp between cruise bullet and the flying wing formula oil tank device, be equipped with the connecting tube in the mechanical clamp, every piece of cruise bullet all is equipped with the guided missile oil tank, be connected with the oil inlet pipeline with the connecting tube intercommunication on the guided missile oil tank, be equipped with the wing oil tank in the flying wing formula oil tank device, be equipped with many output oil pipe on the wing oil tank, all be equipped with the oil pump on every output oil pipe, be equipped with quick docking mechanism between every mechanical clamp and the oil inlet pipeline that corresponds, quick docking mechanism is used for advancing the intercommunication of oil pipe and connecting tube. By adopting the technical scheme, the problem that the cruise missile needs to carry the aircraft to go deep into a high-risk area in the task execution process is solved, the cruise range of the cruise missile in the task execution process can be enlarged, and the safety of the cruise missile carrier is improved.

Description

Fusion type cruise bomb device suitable for remote emission

Technical Field

The utility model relates to the field of general design of aircrafts, in particular to a fusion type cruise missile device suitable for remote emission.

Background

The cruise bomb is a main object for intercepting enemy, and is commonly used for striking important measures such as enemy airports, ports and transportation hubs. Because the ground air defense system is increasingly perfect at present, the flight of the cruise missile is greatly hindered. In order to successfully complete the attack task of the enemy, the cruise missile must adopt an effective protection means to escape the attack of the enemy missile. The currently adopted method mainly comprises the following steps: stealth technology, ultra-low-altitude flight, bait throwing, maneuvering orbital transfer and the like, however, even if the technologies are adopted, the probability of escaping from the cruise missile and being attacked by the missile is still low.

Because the cruise bomb has a short range, the cruise bomb is generally transported by a high-value manned machine or a large unmanned machine to a designated area and then released to execute a task at present. This also results in the carrier penetrating into high-risk areas, thereby increasing the risk of damage to the aircraft.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide a fusion type cruise bomb device suitable for remote launching, and solves the problem that a cruise bomb needs to be carried deeply into a high-risk area in a task execution process.

In order to achieve the purpose, the technical scheme of the utility model is as follows: the utility model provides a fusion formula is patrolled and is navigated bullet device suitable for long-range transmission, includes many pieces of cruise bullet and flying wing formula oil tank device, many pieces of it is connected with mechanical clamp to patrol between bullet and the flying wing formula oil tank device, be equipped with the connecting tube in the mechanical clamp, every piece all be equipped with the guided missile oil tank in patrolling the bullet, be connected with the oil inlet pipeline with the connecting tube intercommunication on the guided missile oil tank, be equipped with the wing oil tank in the flying wing formula oil tank device, be equipped with many output oil pipe on the wing oil tank, every all be equipped with the oil pump on the output oil pipe, every be equipped with quick docking mechanism between mechanical clamp and the oil inlet pipeline that corresponds, quick docking mechanism is used for advancing the intercommunication of oil pipeline and connecting tube.

Further, two magnetism of quick docking mechanism inhale subassembly, pressure sensor and two solenoid valves of being connected with the pressure sensor electricity, two inhale the subassembly and install respectively on the mechanical clamp and advance the cruise bullet of oil pipe way, pressure sensor sets up on the magnetism of mechanical clamp department inhales the subassembly, two the solenoid valve is installed respectively on connecting line and oil pipe way.

Compared with the prior art, the beneficial effect of this scheme:

the scheme enhances the remote attack capability of the cruise bomb; the scheme has the characteristic of high elasticity, so that when the scheme is close to a target area, the number of directional targets is suddenly increased by multiple times, an enemy air defense system cannot react in time, and saturated attack on enemies is realized.

Drawings

FIG. 1 is a top plan view of a fusion type cruise apparatus suitable for remote launching according to the present invention in a converged state;

FIG. 2 is a left side view of a fusion type cruise missile device suitable for remote launching in a polymerization state according to the utility model;

FIG. 3 is a front view of a fusion type cruise apparatus suitable for remote launching according to the present invention in a separated state;

fig. 4 is a schematic view of the structure of the mechanical clamp in this embodiment.

Detailed Description

The present invention will be described in further detail below by way of specific embodiments:

reference numerals in the drawings of the specification include: the device comprises a cruise missile 1, a flying wing type oil tank device 2, a mechanical clamp 3, a missile oil tank 4, a wing oil tank 5, an oil inlet pipeline 6, an output oil pipe 7 and an oil pump 8.

Examples

As shown in figures 1-4: the utility model provides a fusion formula device of patrolling and voyage suitable for long-range transmission, including many pieces of bullet of patrolling and voyage 1 and all be connected with mechanical clamp 3 between every piece of bullet of cruising 1 and the wing-type oil tank device 2 of flying, be equipped with the connecting line in the

mechanical clamp

3, 3 fixed lower surfaces that set up at wing-type oil tank device 2 are pressed from both sides to machinery, mechanical clamp 3 comprises two blocks of snap-on boards and the connecting plate of connection between two blocks of snap-on boards, two blocks of snap-on boards and 1 joint of bullet of patrolling and voyage, it has the through-hole to open on the connecting plate, still the fixed connecting line that is provided with in every through-hole. Each cruise bomb 1 is internally provided with a missile oil tank 4, and the missile oil tank 4 is connected with an oil inlet pipeline 6 communicated with a connecting pipeline. The wing type fuel tank device is characterized in that a wing fuel tank 5 is arranged in the wing type fuel tank device 2, a control system is arranged in the wing type fuel tank device 2, a power device is not arranged, a plurality of output fuel pipes 7 are arranged on the wing fuel tank 5, an oil pump 8 electrically connected with the control system of the wing type fuel tank device 2 is arranged on each output fuel pipe 7, a quick butt joint mechanism is arranged between each output fuel pipe 7 and a corresponding connecting pipeline of the mechanical clamp 3, and the quick butt joint mechanism is used for communicating the connecting pipeline with the output fuel pipes 7.

The quick butt joint mechanism comprises two magnetic suction components, a pressure sensor and two electromagnetic valves electrically connected with the pressure sensor, wherein the two magnetic suction components are respectively arranged at a connecting pipeline of a mechanical clamp 3 and on a cruise bomb 1 of an oil inlet pipeline 6, the magnetic suction components are conventional equipment, the magnetic suction components are not improved in the embodiment, and the quick connection of the mechanical clamp 3 and the oil inlet pipeline 6 can be realized by means of the magnetic suction components; pressure sensor sets up on the subassembly is inhaled to magnetism of mechanical clamp 3 department, and two solenoid valves are installed respectively on connecting line and oil inlet pipe way 6.

The operation method of the fusion type cruise bomb 1 device comprises the following steps: when the cruise missile 1 and the flying wing type oil tank device 2 are combined, the cruise missile 1 and the flying wing type oil tank device 2 fly as a whole, at the moment, the oil inlet pipeline 6 and the connecting pipeline are communicated with the oil outlet pipe 7, the oil pump 8 is used for enabling the wing oil tank 5 to continuously supply oil to the missile oil tank 4, the missile oil tank 4 is always kept full of oil, and therefore the center of gravity of the whole is not greatly changed. Meanwhile, an engine in the cruise bomb 1 provides thrust for the whole body, the tail wing of the cruise bomb 1 provides control torque, and the whole body has speed after the cruise bomb 1 provides the thrust, so that the lift force is generated by the aid of the flying wing type oil tank device 2, and the whole take-off is realized. When the cruise missile 1 is separated from the flying wing type oil tank device 2, the cruise missile 1 is in a separated state and flies by using fuel oil carried in a missile oil tank 4 in the cruise missile.

The foregoing are merely examples of the present invention and common general knowledge of known specific structures and/or features of the schemes has not been described herein in any greater detail. It should be noted that, for those skilled in the art, without departing from the structure of the present invention, several changes and modifications can be made, which should also be regarded as the protection scope of the present invention, and these will not affect the effect of the implementation of the present invention and the practicability of the patent. The scope of the claims of the present application shall be determined by the contents of the claims, and the description of the embodiments and the like in the specification shall be used to explain the contents of the claims.

Claims

1. The utility model provides a fusion formula patrols boat bullet device suitable for long-range transmission which characterized in that: the flying-wing type aircraft missile comprises a plurality of traveling missiles and flying-wing type oil tank devices, wherein a plurality of mechanical clamps are connected between the traveling missiles and the flying-wing type oil tank devices, connecting pipelines are arranged in the mechanical clamps, each traveling missile is internally provided with a missile oil tank, the missile oil tanks are connected with oil inlet pipelines communicated with the connecting pipelines, wing oil tanks are arranged in the flying-wing type oil tank devices, a plurality of output oil pipes are arranged on the wing oil tanks, each output oil pipe is provided with an oil pump, a quick butt joint mechanism is arranged between each mechanical clamp and the corresponding oil inlet pipeline, and the quick butt joint mechanisms are used for communicating the oil inlet pipelines with the connecting pipelines.

2. A fusion type cruise device suitable for remote launching according to claim 1, characterized in that: two magnetism of quick docking mechanism inhale subassembly, pressure sensor and two solenoid valves of being connected with the pressure sensor electricity, two inhale the subassembly and install respectively on the mechanical clamp with advance the cruise bullet of oil pipe way, pressure sensor sets up on the magnetism of mechanical clamp department inhales the subassembly, two the solenoid valve is installed respectively on connecting line and oil pipe way.