阅读说明：本技术 流体中运动体的减阻和快速散热方法 (Drag reduction and rapid heat dissipation method for moving body in fluid ) 是由 李新亚 于 2019-10-28 设计创作，主要内容包括：本发明涉及一种流体中运动体的减阻和快速散热方法,其为流体中运动体(1)前端部(2)的内部,有人字形导流管(3)和多个弯曲导流管(4)。使得前端部(2)在运动时所受阻力减小,运动体(1)的航程和速度都将大大增加；使得前端部(2)散热快,前端部(2)的动态平衡温度较低,对前端部(2)材料的耐温要求较低,从而制造成本显著降低。本申请为减阻和散热另辟蹊径闯了一条新路。(The invention relates to a drag reduction and rapid heat dissipation method for a moving body in fluid, which is characterized in that a herringbone flow guide pipe (3) and a plurality of bent flow guide pipes (4) are arranged in the front end part (2) of the moving body (1) in the fluid. The resistance borne by the front end part (2) during movement is reduced, and the range and the speed of the moving body (1) are greatly increased; the heat dissipation of the front end part (2) is fast, the dynamic balance temperature of the front end part (2) is low, the temperature resistance requirement on the material of the front end part (2) is low, and the manufacturing cost is obviously reduced. The application develops a new path for drag reduction and heat dissipation.)

1. A drag reduction and rapid heat dissipation method for a moving body in fluid comprises the moving body (1); the moving body (1) comprises all objects moving in the air or in the water, such as missiles, airplane fuselages, shells, high-speed rail locomotives, torpedoes, submarines, ships and the like;

the method is characterized in that:

the front end of the moving body (1) is a front end part (2); the front end portion (2) being either originally present or newly installed; the front end part (2) is in a semi-sphere shape with a vertex right in front, a streamline shape or other shapes;

a herringbone flow guide pipe (3) and a plurality of bent flow guide pipes (4) are arranged inside the front end part (2), the axes of the herringbone flow guide pipe (3) and the plurality of bent flow guide pipes (4) are positioned on the same horizontal plane, and the axis of the moving body (1) is positioned on the horizontal plane;

the cross section of the herringbone flow guide pipe (3) or the bent flow guide pipe (4) is round, flat or in other shapes;

the front port of the herringbone flow guide pipe (3) or the bent flow guide pipe (4) is positioned on the front end surface of the front end part (2) and is opened forwards; the rear port of the herringbone flow guide pipe (3) or the bent flow guide pipe (4) is open to the side rear of the front end part (2);

the center point of the front port of the herringbone flow guide pipe (3) is positioned at the vertex of the front end part (2);

the plurality of bent draft tubes (4) are respectively arranged at two sides of the herringbone draft tube (3), and the bent draft tubes (4) at the two sides are axially symmetrical with each other.

Technical Field

The invention relates to a method for reducing resistance and quickly dissipating heat of a moving body in fluid, in particular to a method for reducing resistance borne by the moving body in fluid and quickly dissipating heat of the moving body in fluid.

Background

When a moving body in the fluid moves, particularly moves at a high speed, the resistance of the fluid to the moving body is very large, so that the speed is limited, the energy consumption is high, and the voyage is shortened; due to the frictional heat generation, the front end of the moving body is heated sharply, and the front end of the moving body is melted or sublimated or even disintegrated when being heavy, and the performance of the material is obviously reduced when being light.

The current method for overcoming air resistance is to adopt a high-power engine, and the speed of a moving body reaches dozens of times of sound velocity, such as hypersonic missile; the current method for overcoming the water resistance is to use a high-power engine and to use a 'cavitation' technology, and the speed of the 'storm' torpedo reaches 100m/s (about 200 knots); the current approach to overcome the rapid temperature rise is to develop high temperature resistant materials, which have been developed to have unchanged performance at high temperatures of more than 3 thousand degrees celsius.

The above methods all have disadvantages. The high-power engine and the cavitation generator have high energy consumption, and the range of the moving body is limited; the production process of the high-temperature resistant material is complex, and the manufacturing cost is very high.

Except for the above method, can not reduce the energy consumption, increase the range and speed by reducing the resistance of the moving body? Can the exercise body not adopt a new structure to rapidly cool the exercise body, so as to reduce the temperature resistance requirement on the material and reduce the manufacturing cost?

In order to rapidly change the China from the large manufacturing country to the strong manufacturing country and greatly improve the military strength of China, science and technology workers need to make a new way for the technology.

Disclosure of Invention

The technical problem to be solved by the invention is to provide a method for reducing resistance and quickly dissipating heat of a moving body in fluid, so that the resistance of the moving body in the fluid is reduced, and the moving body in the fluid can be quickly dissipated.

In order to solve the technical problems, the technical scheme of the invention is as follows:

a drag reduction and rapid heat dissipation method for a moving body in fluid comprises the moving body; the moving body comprises all objects moving in the air or in the water, such as missiles, airplane bodies, shells, high-speed rail locomotives, torpedoes, submarines, ships and the like.

The front end of the moving body is a front end part; the front end portion either originally existing or newly installed; the front end portion may be a hemispherical shape with its apex right in front, a streamline shape, or other shapes.

The front end has inside one V-shaped guide pipe and several bent guide pipes, and the V-shaped guide pipe and the bent guide pipes have their axes in the same horizontal plane.

The cross section of the herringbone flow guide pipe or the bent flow guide pipe is round, flat or in other shapes.

The front port of the herringbone flow guide pipe or the bent flow guide pipe is positioned on the front end surface of the front end part and is opened forwards; the rear port of the herringbone flow guide pipe or the bent flow guide pipe is opened to the side rear of the front end part.

The center point of the front port of the herringbone flow guide pipe is positioned at the peak of the front end part.

The plurality of bent draft tubes are arranged on two sides of the herringbone draft tube, and the bent draft tubes on the two sides are axially symmetrical with each other.

There are both attractive and repulsive forces between the molecules, which are balanced when the distance between the molecules is equal to r. When the distance between molecules is less than r, both the attractive force and the repulsive force increase as the distance decreases, but the repulsive force increases significantly faster than the attractive force, so that the repulsive force is greater than the attractive force, and thus the molecular force (the resultant force of the attractive force and the repulsive force) appears as the repulsive force. When the moving body in the air moves forwards at a high speed, the air in front of the front end part of the moving body is compressed, so that the distance between air molecules is smaller than r, and the moving body collides with an air wall under the action of strong molecular force, so that the resistance is large. And because the specific heat capacity of air is small, the temperature of the front end part is increased quickly due to frictional heat generation. After adopting such structure, this application provides the passageway that flows backward for the air in locomotorium front end portion the place ahead because chevron shape honeycomb duct and a plurality of crooked honeycomb duct, and the density of locomotorium front end portion place ahead air reduces, that is to say the distance between the molecule increases, and the air is to the resistance of locomotorium front end portion reduction, and the frictional heating is less. On the other hand, in the process that the air flows through the herringbone flow guide pipe and the plurality of bent flow guide pipes at the front end part, the interior of the front end part is continuously cooled, so that the dynamic balance temperature of the front end part is low, and the air can be used even if a material with low temperature resistance is adopted. The reduction of the resistance of the moving body in water can be explained just by the fact that the herringbone flow guide pipe and the plurality of bent flow guide pipes mainly play a role in reducing the resistance due to the large specific heat capacity of water, and the heat dissipation and temperature reduction also exist but do not play a great role.

After the structure is adopted, because the resistance borne by the front end part of the moving body is reduced, the range and the speed of the moving body are greatly increased under the condition of an engine with the same power according to the law of conservation of energy.

After adopting such structure, because the internal surface and the inside of the front end of the moving body are all radiated, the radiation is fast, the temperature-resistant requirement on the front end material is reduced, thereby the manufacturing cost is obviously reduced.

By adopting the structure, the structure probably plays a role in improving the manufacturing and military force of China.

After adopting such structure, a new way is opened for drag reduction and heat dissipation.

Drawings

The following describes embodiments of the present invention in further detail with reference to the accompanying drawings.

Fig. 1 is a schematic horizontal section of a moving body in a fluid, the axis of the moving body lying on the section.

Detailed Description

As shown in fig. 1.

A drag reduction and rapid heat dissipation method for a moving body in fluid comprises a moving body 1; the moving body 1 includes all objects moving in the air or in the water, such as missiles, airplane bodies, shells, high-speed rail locomotives, torpedoes, submarines, ships and the like.

The front end of the moving body 1 is a front end part 2; the tip portion 2 may be either originally present or newly installed. The front end 2 may be formed in a hemispherical shape with its apex right in front, a streamline shape, or other shapes.

The front end 2 has a herringbone flow guide tube 3 and a plurality of curved flow guide tubes 4 inside, the axis of the herringbone flow guide tube 3 and the axis of the plurality of curved flow guide tubes 4 are located on the same horizontal plane, and the axis of the moving body 1 is located on the horizontal plane.

The herringbone draft tube 3 or the bent draft tube 4 has a cross section which is either circular, flat or other shapes.

The forward end of the chevron flow guide tube 3 or the curved flow guide tube 4 is located on the forward end face of the forward end portion 2 and is open forward. The rear end of the chevron flow guide tube 3 or the curved flow guide tube 4 is open to the side and rear of the front end 2.

The center point of the front end of the herringbone flow guide pipe 3 is located at the vertex of the front end part 2.

The plurality of curved draft tubes 4 are arranged on both sides of the herringbone draft tube 3, and the curved draft tubes 4 on both sides are axisymmetric to each other.

The embodiments of the present invention are described in detail above with reference to the accompanying drawings. The present invention is not limited to the above-described embodiments, and various changes may be made without departing from the spirit of the present invention within the scope of knowledge of those skilled in the art, for example, in order to reduce the difficulty of manufacturing, the curved flow guide tube 4 is changed to a straight tube; for another example, when the vertical height of the front end portion 2 is greater than the lateral width, the curved draft tube 4 is added to the inside of the upper or lower portion of the front end portion 2. Variations that do not depart from the gist of the invention are intended to be within the scope of the invention.