CN109162892B - Air compressor machine aircraft nose - Google Patents
Air compressor machine aircraft nose Download PDFInfo
- Publication number
- CN109162892B CN109162892B CN201810968947.XA CN201810968947A CN109162892B CN 109162892 B CN109162892 B CN 109162892B CN 201810968947 A CN201810968947 A CN 201810968947A CN 109162892 B CN109162892 B CN 109162892B
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- Prior art keywords
- cooling
- air
- air compressor
- rod
- pipe
- Prior art date
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Links
- 238000001816 cooling Methods 0.000 claims abstract description 87
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 41
- 230000000712 assembly Effects 0.000 claims abstract description 9
- 238000000429 assembly Methods 0.000 claims abstract description 9
- 238000007664 blowing Methods 0.000 claims description 15
- 238000013016 damping Methods 0.000 claims description 9
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 5
- 229910052802 copper Inorganic materials 0.000 claims description 5
- 239000010949 copper Substances 0.000 claims description 5
- 230000000694 effects Effects 0.000 abstract description 25
- 230000017525 heat dissipation Effects 0.000 abstract description 11
- 230000005855 radiation Effects 0.000 abstract description 8
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 239000007789 gas Substances 0.000 description 8
- 229910052742 iron Inorganic materials 0.000 description 4
- 230000033001 locomotion Effects 0.000 description 3
- 239000002351 wastewater Substances 0.000 description 3
- 238000004891 communication Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000002912 waste gas Substances 0.000 description 2
- -1 and finally Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000191 radiation effect Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 230000003584 silencer Effects 0.000 description 1
- 210000003437 trachea Anatomy 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B35/00—Piston pumps specially adapted for elastic fluids and characterised by the driving means to their working members, or by combination with, or adaptation to, specific driving engines or motors, not otherwise provided for
- F04B35/04—Piston pumps specially adapted for elastic fluids and characterised by the driving means to their working members, or by combination with, or adaptation to, specific driving engines or motors, not otherwise provided for the means being electric
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/0027—Pulsation and noise damping means
- F04B39/0044—Pulsation and noise damping means with vibration damping supports
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/06—Cooling; Heating; Prevention of freezing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/06—Cooling; Heating; Prevention of freezing
- F04B39/064—Cooling by a cooling jacket in the pump casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/06—Cooling; Heating; Prevention of freezing
- F04B39/066—Cooling by ventilation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/12—Casings; Cylinders; Cylinder heads; Fluid connections
- F04B39/122—Cylinder block
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M7/00—Details of attaching or adjusting engine beds, frames, or supporting-legs on foundation or base; Attaching non-moving engine parts, e.g. cylinder blocks
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Compressor (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention discloses an air compressor head, and relates to the field of air compressors. The air compressor head comprises a motor, pump heads positioned at two ends of the motor and air cylinder assemblies arranged on the pump heads, a pair of air pipes are communicated between the two air cylinder assemblies, a plurality of radiating fins which are uniformly distributed are arranged at the top of the air cylinder assemblies, gaps are formed between every two adjacent radiating fins, cooling pipes are embedded in the gaps, one ends of the cooling pipes are mutually communicated and provided with a water inlet pipe, and the other ends of the cooling pipes are mutually communicated and provided with a water outlet pipe. The invention has the following advantages and effects: when the air compressor machine aircraft nose during operation, carry out cooling to the cylinder subassembly through radiating fin's heat radiation principle, carry out cooling to the cylinder subassembly jointly through the heat exchange principle of cooling tube simultaneously. The cooling efficiency and the cooling effect of the whole air compressor head are improved, so that the air compressor head achieves the effects of high cooling performance and high heat dissipation.
Description
Technical Field
The invention relates to the field of air compressors, in particular to an air compressor head.
Background
The air compressor is also called an air compressor, and is a device for compressing air, the air compressor is a main body in an air source device, the air compressor is a device for converting mechanical energy of a prime motor (usually a motor) into air pressure energy, and the air compressor is an air pressure generating device for compressing air.
The Chinese patent with the publication number of CN205207068U discloses an air compressor machine head, which comprises a frame, a motor is arranged in the frame, pump heads for compressing air are arranged at two ends of the frame, a cooling fan is arranged in the pump heads, the cooling fan sucks air into the pump heads and cools the pump heads, three groups of air cylinder assemblies for compressing air are arranged on the upper part of each pump head, the air cylinder assemblies are positioned between the cooling fan and the motor, an air inlet silencer is arranged on the side surface, close to the cooling fan, of each air cylinder assembly, and an air outlet is arranged on the side surface, far away from the cooling fan, of each air cylinder assembly.
When the air compressor works, the motor drives the air cylinder assembly to move, so that air is compressed. However, when the air compressor works, the air cylinder assembly generates a large amount of heat, and at the moment, the cooling fan radiates heat to cool, but the heat radiation effect of the method is poor, and the method needs to be improved.
Disclosure of Invention
The invention aims to provide an air compressor head, which has the effect of high heat dissipation.
The technical aim of the invention is realized by the following technical scheme: the utility model provides an air compressor machine aircraft nose, includes the motor, is located pump head at motor both ends and set up in cylinder subassembly on the pump head, two the intercommunication is provided with a pair of trachea between the cylinder subassembly, cylinder subassembly top is provided with a plurality of radiating fins of evenly arranging, adjacent two all be provided with the clearance between the radiating fin, the clearance is embedded to be equipped with the cooling tube, a plurality of the one end intercommunication of cooling tube is provided with the inlet tube each other, and the other end intercommunication is provided with the outlet pipe each other.
Through adopting above-mentioned technical scheme, when the air compressor machine aircraft nose during operation, the motor is started, and each component part in motor pump head and the cylinder subassembly is reciprocal to work, realizes the compression to the air. Meanwhile, when the air compressor machine head works, heat radiation principles of the radiating fins are used for radiating and cooling the air cylinder assembly, cold water is injected into the water inlet pipe, after the cold water in the water inlet pipe flows into the cooling pipes, the air cylinder assembly is cooled by the aid of the heat exchange principles of the water, and finally, waste water cooled by the air cylinder assembly is collected in the water outlet pipe and is discharged along the water outlet pipe. The cylinder assembly is cooled by the heat radiation principle of the radiating fins and the heat exchange principle of cold water, so that the cooling efficiency and the cooling effect of the cylinder assembly are improved, and the effects of high cooling performance and high heat dissipation are achieved.
The invention is further provided with: the cooling pipe is made of red copper.
Through adopting above-mentioned technical scheme, because red copper material has advantages such as corrosion resistance is strong, the thermal conductivity is good, with low costs, consequently only have the cooling tube of red copper material can increase substantially cooling efficiency and the cooling effect of cooling tube, and then further reached high cooling nature, high thermal diffusivity's effect.
The invention is further provided with: the bottom wall and the top wall of the cooling pipe are respectively provided with a plurality of baffle plates which are mutually staggered.
By adopting the technical scheme, the flow direction of the cold water is changed by arranging the baffle plates, the flow speed of the cold water in the cooling pipe is improved, the cold water is forced to transversely pass through the cooling pipe for a plurality of times according to a specified path, the turbulence degree of the cold water is enhanced, and the cooling efficiency and the cooling effect of the cooling pipe are improved.
The invention is further provided with: the outer wall cladding of motor has hollow cooling jacket, be provided with on the cooling jacket respectively in the inlet tube with the connecting pipe of outlet pipe.
Through adopting above-mentioned technical scheme, when the cold water is poured into in the inlet tube into, a portion of cold water in the inlet tube will flow into in the cooling jacket along the connecting pipe, and then utilize the heat exchange principle of water to cool down the motor. Finally, the wastewater after cooling the motor is collected in the water outlet pipe along the other connecting pipe and finally is discharged along the water outlet pipe, so that the whole air compressor head further achieves the effects of high cooling performance and high heat dissipation.
The invention is further provided with: the inside of pump head is provided with cooling fan, the pump head lateral wall is provided with a plurality of exhaust grooves.
Through adopting above-mentioned technical scheme, when the motor during operation, the motor drives cooling fan and rotates, and in this moment with external cold air suction pump head through cooling fan, utilize cold air to pump head cooling, further reached high cooling nature, high heat dissipation's effect. And meanwhile, the waste gas with heat is discharged along the exhaust groove, so that the influence of the air with heat on the normal operation of the cylinder assembly is avoided when the air with heat enters the cylinder assembly.
The invention is further provided with: the cooling fin is characterized in that a flow channel is arranged between the outer wall of the cooling tube and the side wall of the cooling fin, a gas blowing tube is arranged on the side wall of the pump head, and a plurality of gas blowing holes which are arranged towards the flow channel direction are formed in the gas blowing tube.
Through adopting above-mentioned technical scheme, when cooling fan rotates the during operation, the inspired part of fan cold air will flow into the gas blowing pipe, blow along the gas blowing hole again to the cooling pipe outer wall with the radiating fin in the runner that forms between the lateral wall, and then increased the air flow rate on radiating fin surface, further improved radiating fin's radiating effect, still further reached high cooling nature, high thermal diffusivity's effect.
The invention is further provided with: the outer wall of the lower end of the pump head is provided with a supporting seat, a supporting rod is connected to the supporting seat through threads, and a supporting pad is arranged on the lower end face of the supporting rod.
Through adopting above-mentioned technical scheme, when the ground that needs fixed air compressor machine aircraft nose is uneven, promote the supporting pad and drive the bracing piece and rotate, realized the upward or downward movement of supporting pad to until all supporting pads all stable conflict in ground after, be fixed in ground with the supporting pad, and then make whole air compressor machine aircraft nose during operation can be in the horizontality all the time, avoid the air compressor machine aircraft nose to take place to incline, improved the stability and the high reliability of air compressor machine aircraft nose during operation.
The invention is further provided with: the outer wall of the support pad is provided with a plurality of embedded grooves.
Through adopting above-mentioned technical scheme, when rotating the supporting pad, can insert the rigid tubular or the shaft-like driving piece in the embedded groove, utilize lever principle to promote the driving piece and drive the supporting pad rotation for the regulation of supporting pad is convenient and fast more, labour saving and time saving.
The invention is further provided with: the support rod comprises a first rod body and a second rod body, wherein the first rod body and the support pad are fixed with each other, the second rod body is in threaded connection with the support seat, the upper end face of the first rod body is provided with a sliding hole for the second rod body to be inserted and slide, and a damping spring is fixed between the lower end face of the second rod body and the bottom wall of the sliding hole.
Through adopting above-mentioned technical scheme, when the air compressor machine aircraft nose during operation, the motor will drive the pump head and rock from top to bottom, and the pump head drives the supporting seat motion this moment, and the pump head drives the second body of rod and slides from top to bottom along the sliding hole inner wall on the first body of rod, presses the damping spring compression simultaneously, and the pressure of the second body of rod is eliminated to the resilience force of damping spring self simultaneously, and then has played fine shock attenuation effect, has improved the stability of whole air compressor machine aircraft nose during operation, has further reached the effect of high stability, high reliability.
In summary, the invention has the following beneficial effects:
1. The cylinder assembly is cooled by the heat radiation principle of the radiating fins and the heat exchange principle of the cooling pipes, so that the cooling efficiency and the cooling effect of the whole air compressor head are improved, and the effects of high cooling performance and high heat dissipation are achieved;
2. The motor is cooled by arranging the cooling sleeve, and the pump head is cooled by the cooling fan, so that the whole air compressor head further achieves the effects of high cooling performance and high heat dissipation;
3. the air flow rate on the surface of the radiating fin is increased by arranging the air blowing pipe, so that the radiating efficiency and the radiating effect of the radiating fin are further improved;
4. Through setting up highly adjustable supporting pad and making above-mentioned air compressor machine aircraft nose can be applied to uneven ground, improved the stability of whole air compressor machine during operation through setting up the bracing piece that has shock-absorbing structure simultaneously, reached the effect of high stability, high reliability.
Drawings
FIG. 1 is a schematic structural view of an embodiment;
FIG. 2 is an enlarged view of a portion of FIG. 1 at A;
FIG. 3 is a schematic view of the structure of the support bar of the embodiment;
FIG. 4 is a schematic diagram of the connection relationship of the motor, pump body, and cylinder assembly of the embodiment;
Fig. 5 is a schematic view showing the internal structure of the cooling pipe of the embodiment.
Reference numerals: 1. a motor; 11. a cooling jacket; 12. a connecting pipe; 2. a pump head; 21. a cooling fan; 22. an exhaust groove; 23. an air blowing pipe; 24. a blow hole; 3. a cylinder assembly; 31. an air pipe; 32. a heat radiation fin; 33. a gap; 4. a support base; 5. a support rod; 51. a first rod body; 52. a second rod body; 53. a sliding hole; 54. a damping spring; 6. a support pad; 61. an embedding groove; 7. a cooling tube; 71. a baffle plate; 72. a water inlet pipe; 73. and a water outlet pipe.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
An air compressor head, as shown in fig. 1 and 2, comprises a motor 1, pump heads 2 positioned at two ends of the motor 1, and air cylinder assemblies 3 arranged on the pump heads 2, wherein a pair of air pipes 31 (see fig. 4) are communicated between the two air cylinder assemblies 3. The lower extreme outer wall of pump head 2 is provided with supporting seat 4, and threaded connection has bracing piece 5 on the supporting seat 4, and the lower terminal surface of bracing piece 5 is provided with supporting pad 6, and the outer wall of supporting pad 6 is provided with a plurality of embedded grooves 61.
When the air compressor head is used, the air compressor head is placed on the ground, then a rigid iron rod or iron pipe is inserted into the embedded groove 61, the iron rod or iron pipe is pushed to drive the support pad 6 to rotate, the support pad 6 drives the support rod 5 to rotate, and further upward or downward movement of the support pad 6 is achieved until all the support pads 6 stably abut against the ground, and then the support pad 6 is fixed on the ground.
When the air compressor head works, the motor 1 is started, the motor 1 drives a crankshaft (not shown in the figure) in the pump head 2 to rotate, and a piston (not shown in the figure) in the cylinder assembly 3 is driven to reciprocate through the crankshaft, so that air is compressed.
As shown in fig. 3, the support rod 5 includes a first rod 51 fixed to the support pad 6, and a second rod 52 screwed to the support base 4, where a sliding hole 53 for inserting and sliding the second rod 52 is provided on an upper end surface of the first rod 51, and a damping spring 54 is fixed between a lower end surface of the second rod 52 and a bottom wall of the sliding hole 53.
When the air compressor head works, the motor 1 (see fig. 1) will drive the pump head 2 (see fig. 1) to shake up and down, at this time, the pump head 2 drives the supporting seat 4 to move, the pump head 2 drives the second rod body 52 to slide up and down along the inner wall of the sliding hole 53 on the first rod body 51, meanwhile, the damping spring 54 is pressed to compress, and at the same time, the resilience force of the damping spring 54 eliminates the pressure of the second rod body 52, so that a good damping effect is achieved, the stability of the whole air compressor head during working is improved, and the effects of high stability and high reliability are achieved.
As shown in fig. 1 and 4, a plurality of heat dissipation fins 32 are uniformly arranged at the top of the air cylinder assembly 3, gaps 33 are formed between two adjacent heat dissipation fins 32, a red copper cooling tube 7 is embedded in the gaps 33, and a plurality of baffle plates 71 (see fig. 5) are arranged on the bottom wall and the top wall of the cooling tube 7 in a staggered manner. One end of the plurality of cooling pipes 7 is provided with a water inlet pipe 72 in mutual communication, and the other end is provided with a water outlet pipe 73 in mutual communication. The outer wall of the motor 1 is coated with a hollow cooling sleeve 11, and the cooling sleeve 11 is provided with a connecting pipe 12 respectively communicated with a water inlet pipe 72 and a water outlet pipe 73.
When the air cylinder assembly 3 works, the air cylinder assembly 3 is subjected to heat radiation and temperature reduction through the heat radiation principle of the heat radiation fins 32, meanwhile, cold water is introduced along the water inlet pipe 72, and after part of the cold water in the water inlet pipe 72 flows into the cooling pipes 7, the air cylinder assembly 3 is cooled by utilizing the heat exchange principle of the water. Meanwhile, the other part of cold water in the water inlet pipe 72 flows into the cooling sleeve 11 along the connecting pipe 12, and the motor 1 is cooled by utilizing the heat exchange principle of the water. Finally, the cooled air cylinder assembly 3 and the waste water of the motor 1 are collected in the water outlet pipe 73 and are discharged along the water outlet pipe 73, and then the effects of high cooling performance and high heat dissipation are achieved by water cooling.
As shown in fig. 1, a cooling fan 21 is arranged in the pump head 2, a plurality of exhaust grooves 22 are formed in the side wall of the pump head 2, a flow passage is formed between the outer wall of the cooling pipe 7 and the side wall of the radiating fin 32, a gas blowing pipe 23 is arranged on the side wall of the pump head 2, and a plurality of gas blowing holes 24 which are arranged towards the flow passage direction are formed in the gas blowing pipe 23.
When the motor 1 works, the motor 1 drives the cooling fan 21 to rotate, and at the moment, external cold air is sucked into the pump head 2 through the cooling fan 21, and meanwhile, waste gas with heat is discharged along the exhaust groove 22, so that the air with heat is prevented from entering the cylinder assembly 3 to influence the normal work of the cylinder assembly 3. Meanwhile, part of cold air sucked by the fan flows into the air blowing pipe 23 and then is blown into a flow passage formed between the outer wall of the cooling pipe 7 and the side wall of the radiating fin 32 along the air blowing hole 24, so that the air flow rate of the surface of the radiating fin 32 is increased, and the radiating effect of the radiating fin 32 is further improved.
Working principle: when the air compressor head is used, the motor 1 is started, the motor 1 drives the crankshaft in the pump head 2 to rotate, and then the crankshaft drives the piston in the cylinder assembly 3 to reciprocate, so that air is compressed. When the air compressor head works, the air cylinder assembly 3 and the motor 1 are cooled down through heat exchange of cold water, and the pump head 2 is cooled down through the cooling fan 21, so that the air compressor head achieves the effects of high cooling performance and high heat dissipation.
The present invention is not limited by the specific embodiments, and modifications can be made to the embodiments without creative contribution by those skilled in the art after reading the present specification, but are protected by patent laws within the scope of claims of the present invention.
Claims (4)
1. An air compressor machine aircraft nose, its characterized in that: the novel cooling device comprises a motor (1), pump heads (2) positioned at two ends of the motor (1) and air cylinder assemblies (3) arranged on the pump heads (2), wherein a pair of air pipes (31) are communicated between the two air cylinder assemblies (3), a plurality of uniformly arranged radiating fins (32) are arranged at the top of each air cylinder assembly (3), gaps (33) are formed between every two adjacent radiating fins (32), cooling pipes (7) are embedded in the gaps (33), one ends of the cooling pipes (7) are mutually communicated and provided with a water inlet pipe (72), and the other ends of the cooling pipes are mutually communicated and provided with a water outlet pipe (73);
The cooling pipe (7) is made of red copper;
The bottom wall and the top wall of the cooling pipe (7) are respectively provided with a plurality of baffle plates (71) which are arranged in a staggered way;
The outer wall of the motor (1) is coated with a hollow cooling sleeve (11), and the cooling sleeve (11) is provided with connecting pipes (12) respectively communicated with the water inlet pipe (72) and the water outlet pipe (73);
A cooling fan (21) is arranged in the pump head (2), and a plurality of exhaust grooves (22) are formed in the side wall of the pump head (2);
A flow passage is arranged between the outer wall of the cooling pipe (7) and the side wall of the radiating fin (32), an air blowing pipe (23) is arranged on the side wall of the pump head (2), and a plurality of air blowing holes (24) which are arranged towards the flow passage direction are formed in the air blowing pipe (23).
2. An air compressor head as set forth in claim 1, wherein: the outer wall of the lower end of the pump head (2) is provided with
The support seat (4) is arranged, the support seat (4) is connected with a support rod (5) in a threaded mode, and a support pad (6) is arranged on the lower end face of the support rod (5).
3. An air compressor head as set forth in claim 2, wherein: the outer wall of the supporting pad (6) is provided with
A plurality of embedded grooves (61).
4. An air compressor head as set forth in claim 3 wherein: the support rod (5) comprises a support rod and a support rod
The support pad (6) is fixed the first body of rod (51), threaded connection in the second body of rod (52) of supporting seat (4), the up end of first body of rod (51) is provided with confession second body of rod (52) grafting sliding hole (53), be fixed with damping spring (54) between the lower terminal surface of second body of rod (52) and the diapire of sliding hole (53).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810968947.XA CN109162892B (en) | 2018-08-23 | 2018-08-23 | Air compressor machine aircraft nose |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810968947.XA CN109162892B (en) | 2018-08-23 | 2018-08-23 | Air compressor machine aircraft nose |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109162892A CN109162892A (en) | 2019-01-08 |
| CN109162892B true CN109162892B (en) | 2024-05-24 |
Family
ID=64896539
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810968947.XA Active CN109162892B (en) | 2018-08-23 | 2018-08-23 | Air compressor machine aircraft nose |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109162892B (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110173418A (en) * | 2019-01-10 | 2019-08-27 | 苏州欧圣电气股份有限公司 | A kind of air pressure pump and air compressor machine |
| CN110486251A (en) * | 2019-09-27 | 2019-11-22 | 天津联科思创科技发展有限公司 | A kind of integrated exhaust is cooling and the oil-free air compressor of voltage stabilizing function |
| CN110878744B (en) * | 2019-10-24 | 2021-07-20 | 浙江藤井空压机有限公司 | Air compressor machine aircraft nose |
| CN112012921B (en) * | 2020-08-29 | 2022-04-12 | 芜湖西南机械有限公司 | Plunger pump that radiating effect is good |
| CN113738614B (en) * | 2021-09-10 | 2022-11-29 | 山东爱景节能科技有限公司 | Waste heat recycling mechanism of air compressor unit |
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| JP2007297981A (en) * | 2006-04-28 | 2007-11-15 | Hitachi Ltd | Reciprocating compressor |
| CN203655571U (en) * | 2013-12-28 | 2014-06-18 | 浙江美洲豹工贸有限公司 | Inflator |
| CN203892536U (en) * | 2014-06-12 | 2014-10-22 | 浙江升宏机械有限公司 | Durable type gear box |
| CN204239176U (en) * | 2014-10-20 | 2015-04-01 | 台州市伸顺电机制造有限公司 | Handpiece of air compressor |
| CN204320291U (en) * | 2014-11-27 | 2015-05-13 | 淄博坤瀚精细化工有限公司 | A kind of reactor with safe water sealing groove |
| CN205207068U (en) * | 2015-12-16 | 2016-05-04 | 台州市伸顺电机制造有限公司 | Miniature air compressor machine aircraft nose of multi -cylinder |
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| CN206376997U (en) * | 2016-12-23 | 2017-08-04 | 上海久信机电设备制造有限公司 | A kind of high efficiency and heat radiation formula vavuum pump |
| CN107143483A (en) * | 2017-06-24 | 2017-09-08 | 浙江永源机电制造有限公司 | A kind of oil-free twin-tub air compressor machine |
| CN208950791U (en) * | 2018-08-23 | 2019-06-07 | 浙江藤井空压机有限公司 | A kind of handpiece of air compressor |
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| CN203655571U (en) * | 2013-12-28 | 2014-06-18 | 浙江美洲豹工贸有限公司 | Inflator |
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| CN205207068U (en) * | 2015-12-16 | 2016-05-04 | 台州市伸顺电机制造有限公司 | Miniature air compressor machine aircraft nose of multi -cylinder |
| CN206175162U (en) * | 2016-11-02 | 2017-05-17 | 台州宝乾机电有限公司 | Air compressor machine easily dispels heat |
| CN206376997U (en) * | 2016-12-23 | 2017-08-04 | 上海久信机电设备制造有限公司 | A kind of high efficiency and heat radiation formula vavuum pump |
| CN107143483A (en) * | 2017-06-24 | 2017-09-08 | 浙江永源机电制造有限公司 | A kind of oil-free twin-tub air compressor machine |
| CN208950791U (en) * | 2018-08-23 | 2019-06-07 | 浙江藤井空压机有限公司 | A kind of handpiece of air compressor |
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| Publication number | Publication date |
|---|---|
| CN109162892A (en) | 2019-01-08 |
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