CN209838521U - Water-cooling radiator for ground-effect air cushion composite wing ship engine - Google Patents

Abstract

The utility model discloses a water-cooled radiator of a ground effect air cushion composite wing ship engine, which comprises an engine, a first threaded rod, a second threaded rod, a third threaded rod, a fixing ring, a duct and a radiating box, wherein the engine is sleeved with a radiating shell, the inside of the radiating shell is provided with a cavity, the radiating shell is sleeved with a fixing shell, the right side wall of the fixing shell is contacted with the left side wall of the engine, a first internal threaded pipe is uniformly penetrated and arranged on the radiating shell, a first threaded hole is arranged on the fixing shell corresponding to the first internal threaded pipe, each first threaded hole is in threaded connection with a first threaded rod, the lower end of the first threaded rod is in threaded connection with the first internal threaded pipe, the left side wall of the engine is provided with a second internal threaded pipe, and the engine simultaneously cools the radiating pipe when driving an internal screw to rotate, thereby ensuring better water-cooling effect, and the utility model discloses simple to operate dismantles simply, the user maintenance of being convenient for.

Description

Water-cooling radiator for ground-effect air cushion composite wing ship engine

Technical Field

The utility model relates to an engine radiator technical field, specific field is ground effect air cushion composite wing ship engine water-cooling radiator.

Background

WIG craft utilizes the ground effect principle to make a vessel. The WIG craft can be divided into two types, namely an impulse wing craft and an air wing craft, wherein the impulse wing craft consists of a hull for providing buoyancy and wings with a certain aspect ratio. The surface effect is generated by the influence of the surface on the airflow when the wings move close to the surface, so that the lift-drag ratio of the wings is increased, the propelling power can be reduced, and the sailing away from the ground can be kept. The ground effect craft needs the support of the engine when working normally, and the engine can produce a large amount of heat when working, so need special heat-dissipating equipment to dispel the heat to the engine.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a ground is imitated compound wing ship engine water-cooling radiator to solve the problem that proposes among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: the water-cooled radiator for the engine of the ground effect air cushion composite wing ship comprises an engine, a first threaded rod, a second threaded rod, a third threaded rod, a fixing ring, a duct and a radiating box, wherein a radiating shell is sleeved on the engine, a cavity is arranged in the radiating shell, a fixing shell is sleeved on the radiating shell, the right side wall of the fixing shell is in contact with the left side wall of the engine, a first internal threaded pipe uniformly penetrates through the radiating shell, a first threaded hole is formed in the fixing shell corresponding to the first internal threaded pipe, a first threaded rod is in threaded connection with each first threaded hole, the lower end of the first threaded rod is in threaded connection with the first internal threaded pipe, a second internal threaded pipe is arranged on the left side wall of the engine, a third internal threaded pipe is integrally formed in the left side wall of the fixing shell corresponding to the second internal threaded pipe, and the third internal threaded pipe is communicated with the second internal threaded pipe, the second threaded rod is in threaded connection with a third internal threaded pipe and a second internal threaded pipe simultaneously, fourth internal threaded pipes are symmetrically arranged on the right side wall of the engine, the right ends of the two fourth internal threaded pipes are in contact with the left side wall of the fixing ring, the third threaded rod penetrates through the fixing ring and is in threaded connection with the fourth internal threaded pipes, fixing rods are arranged on the upper side wall and the lower side wall of the fixing shell respectively, the upper fixing rods are connected with the inner upper side wall of the duct, the lower fixing rods are connected with the inner lower side wall of the duct, one end of a first water outlet pipe is connected onto the upper side wall of the radiating shell, the first water outlet pipe is communicated with the cavity, one end of a first water inlet pipe is connected onto the lower side wall of the radiating shell, the first water inlet pipe is communicated with the cavity, the other end of the first water outlet pipe penetrates through the radiating box and is connected with the second water inlet pipe, and the other end of the, the cooling water pipe is characterized in that a plurality of cooling pipes are connected between the second water inlet pipe and the second water outlet pipe, cooling fins are arranged on the cooling pipes, the rotating end of the engine is connected with an inner spiral propeller through a connecting rod, and the outer side wall of the inner spiral propeller is connected with the duct.

Preferably, a gasket is arranged between the first threaded rod and the fixed shell.

Preferably, the heat dissipation shell is a copper heat dissipation shell, the heat dissipation pipe is a copper heat dissipation pipe, and the cooling fins are copper cooling fins.

Preferably, the second water inlet pipe and the second water outlet pipe are connected with the heat dissipation box through small-sized connecting blocks.

Compared with the prior art, the beneficial effects of the utility model are that: ground effect air cushion composite wing ship engine water-cooling radiator, the engine is driven interior propeller and is cooled down for the cooling tube simultaneously when rotating to make the water-cooling effect better, and the utility model discloses simple to operate dismantles simply, the user's maintenance of being convenient for.

Drawings

FIG. 1 is a schematic front view of the structure of the present invention;

fig. 2 is a schematic sectional view of the structure of the fixing shell of the present invention;

fig. 3 is a left side view of the structure of the heat dissipation box of the present invention.

In the figure: 1-an engine, 2-a heat dissipation shell, 3-a cavity, 4-a fixed shell, 5-a first internal threaded pipe, 6-a first threaded rod, 7-a second internal threaded pipe, 8-a third internal threaded pipe, 9-a second threaded rod, 10-a fourth internal threaded pipe, 11-a third threaded rod, 12-a fixed ring, 13-a fixed rod, 14-a duct, 15-a first water outlet pipe, 16-a first water inlet pipe, 17-a heat dissipation box, 18-a second water inlet pipe, 19-a second water outlet pipe, 20-a heat dissipation pipe, 21-a heat dissipation plate, 22-a connecting rod and 23-an internal screw.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-3, the present invention provides a technical solution: the water-cooled radiator for the engine of the ground-effect air cushion composite wing ship comprises an engine 1, a first threaded rod 6, a second threaded rod 9, a third threaded rod 11, a fixing ring 12, a duct 14 and a radiating box 17, wherein a radiating shell is sleeved on the engine, a cavity 3 is arranged inside the radiating shell, the radiating shell is filled with radiating liquid when the water-cooled radiator is used, the radiating shell is tightly attached to the engine, so that the radiating shell can radiate the heat of the engine through the radiating liquid in the cavity, a fixing shell 4 is sleeved on the radiating shell 2, the right side wall of the fixing shell is contacted with the left side wall of the engine, a first internal threaded pipe 5 is uniformly arranged on the radiating shell in a penetrating way, first threaded holes are respectively arranged on the fixing shell corresponding to the first internal threaded pipes, a first threaded rod is in threaded connection with each first threaded hole, and the lower end of the first threaded rod is in threaded connection with the first internal threaded, the heat dissipation shell can be connected with the fixed shell through the first threaded rod, so that the engine can be wrapped, the engine, the heat dissipation shell and the fixed shell are fixed with each other, the engine can be kept stable during operation, the left side wall of the engine is provided with the second internal threaded pipe 7, the left side wall of the fixed shell is integrally formed with the third internal threaded pipe 8 corresponding to the second internal threaded pipe, the third internal threaded pipe is communicated with the second internal threaded pipe, the second threaded rod is simultaneously in threaded connection with the third internal threaded pipe and the second internal threaded pipe, the fixed shell and the engine can be fixed through the second threaded rod, so that the engine cannot move in the heat dissipation shell, the right side wall of the engine is symmetrically provided with the fourth internal threaded pipes 10, the right ends of the two fourth internal threaded pipes are in contact with the left side wall of the fixed ring, and the third threaded rod penetrates through the fixed ring and is in threaded connection with the fourth internal threaded pipes, the possibility of the engine to move in the radiating shell is further reduced through a fixing ring, fixing rods are arranged on the upper side wall and the lower side wall of the fixing shell, the fixing rods 13 on the upper portion are connected with the inner upper side wall of the duct, the engine can be installed in the duct through the fixing rods, the fixing rods on the lower portion are connected with the inner lower side wall of the duct, one end of a first water outlet pipe 15 is connected onto the upper side wall of the radiating shell, the first water outlet pipe is communicated with the cavity, one end of a first water inlet pipe 16 is connected onto the lower side wall of the radiating shell, the first water inlet pipe is communicated with the cavity, the other end of the first water outlet pipe penetrates through the radiating box and is connected with a second water inlet pipe 18, the other end of the first water inlet pipe penetrates through the radiating box and is connected with a second water outlet pipe 19, a plurality of radiating pipes 20 are connected between the second water inlet pipe and, the rotation end of engine is connected with interior screw 23 through connecting rod 22, the lateral wall of interior screw is connected with the duct, can upwards float after the radiating fluid heat absorption intensifies in the cavity, thereby flow out from first outlet pipe, the radiating fluid after the outflow flows into to the second inlet tube, because be linked together through the cooling tube between second inlet tube and the second outlet pipe, so the lower radiating fluid of temperature flows into to first inlet tube from the lower part, thereby the circulation of radiating fluid has been realized, cooling rate can be accelerated through the fin on the cooling tube, because ground effect hovercraft is at the during operation motor drive interior screw rotation, the air current that interior screw produced cools down the cooling tube, make cooling tube cooling rate accelerate, it is to be the utility model discloses a radiating effect is better.

Specifically, a gasket is arranged between the first threaded rod and the fixed shell.

Particularly, the heat dissipation shell is copper heat dissipation shell, the cooling tube is copper cooling tube, the fin is copper fin, and copper heat conductivility is strong, and intensity is higher, is applicable to the utility model discloses in.

Particularly, the second inlet pipe and the second outlet pipe are connected with the heat dissipation box through small-sized connecting blocks.

The working principle is as follows: the utility model discloses, the intracavity is filled with the cooling fluid when the utility model is used, because the cooling shell is clung to the engine, the cooling shell can cool the engine through the cooling fluid in the intracavity, the cooling shell can be connected with the fixed shell through the first threaded rod, so that the engine can be wrapped, the engine, the cooling shell and the fixed shell can be kept fixed with each other when in operation, the engine can be kept stable when in operation, the fixed shell can be fixed with the engine through the second threaded rod, so that the engine can not move in the cooling shell any more, the possibility of the engine moving in the cooling shell is further reduced through the fixed ring, the engine can be arranged in the bypass through the fixed rod, the cooling fluid in the intracavity can float upwards after absorbing heat and increasing temperature, thereby the cooling fluid flows out from the first water outlet pipe, and the cooling fluid after flowing out flows into the second water inlet pipe, because be linked together through the cooling tube between second inlet tube and the second outlet pipe, so the lower radiating fluid of temperature flows in to first inlet tube from the lower part to realized the circulation of radiating fluid, can accelerate cooling rate through the fin on the cooling tube, because ground effect air cushion wing ship drives interior propeller rotation at the during operation motor, the air current that interior propeller produced cools down the cooling tube, makes cooling tube cooling rate accelerate, is the utility model discloses a radiating effect is better.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (4)

1. Ground effect air cushion composite wing ship engine water-cooling radiator includes engine (1), first threaded rod (6), second threaded rod (9), third threaded rod (11), solid fixed ring (12), duct (14) and heat dissipation case (17), its characterized in that: the engine is characterized in that a heat dissipation shell (2) is sleeved on the engine (1), a cavity (3) is arranged inside the heat dissipation shell (2), a fixing shell (4) is sleeved on the heat dissipation shell (2), the right side wall of the fixing shell (4) is in contact with the left side wall of the engine (1), first internal thread pipes (5) uniformly penetrate through the heat dissipation shell (2), first threaded holes are formed in the positions, corresponding to the first internal thread pipes (5), of the fixing shell (4), a first threaded rod (6) is in threaded connection with each first threaded hole, the lower end of each first threaded rod (6) is in threaded connection with each first internal thread pipe (5), a second internal thread pipe (7) is arranged on the left side wall of the engine (1), and a third internal thread pipe (8) is integrally formed on the left side wall of the fixing shell (4) corresponding to the second internal thread pipes (7), the heat dissipation shell is characterized in that the third internal thread pipe (8) is communicated with the second internal thread pipe (7), the second threaded rod (9) is simultaneously in threaded connection with the third internal thread pipe (8) and the second internal thread pipe (7), the right side wall of the engine (1) is symmetrically provided with fourth internal thread pipes (10), the right ends of the two fourth internal thread pipes (10) are in contact with the left side wall of the fixing ring (12), the third threaded rod (11) penetrates through the fixing ring (12) to be in threaded connection with the fourth internal thread pipes (10), the upper side wall and the lower side wall of the fixing shell (4) are respectively provided with a fixing rod (13), the upper fixing rod (13) is connected with the inner upper side wall of the duct (14), the lower fixing rod (13) is connected with the inner lower side wall of the duct (14), the upper side wall of the heat dissipation shell (2) is connected with one end of a first water outlet pipe (15), first outlet pipe (15) are linked together with cavity (3), be connected with the one end of first inlet tube (16) on the lower lateral wall of heat dissipation shell (2), first inlet tube (16) are linked together with cavity (3), the other end of first outlet pipe (15) runs through heat dissipation case (17) and links to each other with second inlet tube (18), the other end of first inlet tube (16) runs through heat dissipation case (17) and links to each other with second outlet tube (19), be connected with a plurality of cooling tubes (20) between second inlet tube (18) and second outlet tube (19), be equipped with fin (21) on cooling tube (20), the rotation end of engine (1) is connected with interior screw (23) through connecting rod (22), the lateral wall of interior screw (23) is connected with duct (14).

2. The water-cooled radiator of the ground effect air cushion composite wing ship engine as claimed in claim 1, wherein: and a gasket is arranged between the first threaded rod (6) and the fixed shell (4).

3. The water-cooled radiator of the ground effect air cushion composite wing ship engine as claimed in claim 1, wherein: the heat dissipation shell (2) is a copper heat dissipation shell, the heat dissipation pipe (20) is a copper heat dissipation pipe, and the heat dissipation fins (21) are copper heat dissipation fins.

4. The water-cooled radiator of the ground effect air cushion composite wing ship engine as claimed in claim 1, wherein: and the second water inlet pipe (18) and the second water outlet pipe (19) are connected with the heat dissipation box (17) through a small connecting block.