CN217978991U - Main unit for pneumatic heat energy heating - Google Patents
Main unit for pneumatic heat energy heating Download PDFInfo
- Publication number
- CN217978991U CN217978991U CN202222340071.9U CN202222340071U CN217978991U CN 217978991 U CN217978991 U CN 217978991U CN 202222340071 U CN202222340071 U CN 202222340071U CN 217978991 U CN217978991 U CN 217978991U
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- Prior art keywords
- turbofan
- air
- speed
- pneumatic
- rotor shaft
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- 238000010438 heat treatment Methods 0.000 title claims abstract description 12
- 230000003068 static effect Effects 0.000 claims abstract description 17
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 6
- 238000001816 cooling Methods 0.000 abstract description 2
- 230000000694 effects Effects 0.000 abstract 2
- 238000011161 development Methods 0.000 abstract 1
- 230000018109 developmental process Effects 0.000 abstract 1
- 230000002349 favourable effect Effects 0.000 abstract 1
- 108010066057 cabin-1 Proteins 0.000 description 11
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a main machine for supplying heat by pneumatic heat energy, wherein a single rotor shaft in a motor is respectively connected with a dynamic high-speed turbofan and a static diversion turbofan after extending out of the motor; the high-speed turbofan of developments is arranged in the inside pneumatic entry of turbine compressor short storehouse left end, and the right-hand member of single rotor shaft runs through static water conservancy diversion turbofan and is connected with the fairing cone that is arranged in high-speed pneumatic jet outlet, the utility model discloses when the air enters into to the short storehouse of turbine compressor via pneumatic entry, under the effect of first frustum shape air guide cover, the air accelerates the velocity of flow, enters into to the short storehouse right-hand member of turbine compressor via the gap of reserving between motor and the short storehouse of turbine compressor, and the air takes the rotation of dynamic and static water conservancy diversion turbofan this moment, again can rise slightly at the speed of air under the effect of fairing cone, and the air can more evenly ground gets into to the cooling tube via high-speed pneumatic jet outlet, improves the circulation rate of air, is favorable to improving the heating efficiency of hot-air.
Description
Technical Field
The utility model relates to a heat supply technical field specifically is a host computer is used in pneumatic heat energy heating.
Background
The equipment in traditional heat supply field all uses water as the heat medium, and the extravagant water resource of the very high while of energy consumption, the proportion that the pipe network dropped into in earlier stage is higher, and the maintenance cost is higher to the phenomenon of "running out and leaking" of the oxidation corrosion of pipeline and system can appear, lead to the whole life-span of system to be shorter.
Based on the relevant principles of fluid dynamics and air thermodynamics, air is used as a heat-conducting medium, and the specific enthalpy of the air is very low, so that the electric energy utilization rate is greatly improved, the power consumption of a heating system is greatly reduced, and a large amount of expenses are saved for enterprises and units needing heat supply in winter.
However, when hot air is circulated after the air is heated, the hot air is blocked, the flow rate is reduced, the heat loss of the hot air is caused, the circulation speed of the hot air is low, and the heat supply efficiency is low.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a pneumatic heat can for heat supply host computer 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: a main machine for supplying heat by pneumatic heat energy comprises a short cabin of a turbine compressor, wherein a motor is installed in the short cabin of the turbine compressor, and a single rotor shaft in the motor is connected with a dynamic high-speed turbofan and a static diversion turbofan after extending out of the motor;
the dynamic high-speed turbofan is positioned in a pneumatic inlet inside the left end of the short cabin of the turbine compressor, the static flow guide turbofan is positioned in a high-speed pneumatic ejection port inside the right end of the short cabin of the turbine compressor, and the right end of the single rotor shaft penetrates through the static flow guide turbofan and is connected with a rectifying cone positioned in the high-speed pneumatic ejection port;
the left end of motor is fixed with first frustum shape air guide cover through first screw, and the left end of single rotor shaft stretches out via the round hole in first frustum shape air guide cover middle part, the right-hand member of motor is fixed with second frustum shape air guide cover through the second screw, and the right-hand member of single rotor shaft stretches out via the round hole in second frustum shape air guide cover middle part.
Compared with the prior art, the beneficial effects of the utility model are that: the utility model discloses the motor work, drives dynamic high-speed turbofan rotation through single rotor shaft and forms suction, inhales the air to turbine compressor short storehouse via pneumatic entry, and the air finally gets into the cooling tube via high-speed pneumatic jet orifice, and then gets into in the auxiliary heating device, heats through the heating rod in the auxiliary heating device, finally gets into turbine compressor short storehouse again via pneumatic entry;
when air enters the short cabin of the turbine compressor through the pneumatic inlet, the air accelerates the flow speed under the action of the first frustum-shaped air guide cover, enters the right end of the short cabin of the turbine compressor through a gap reserved between the motor and the short cabin of the turbine compressor, at the moment, the air drives the dynamic and static flow guide turbofan to rotate, the speed of the air slightly rises under the action of the rectifying cone, the air can uniformly enter the radiating pipe through the high-speed pneumatic jet outlet, the circulation speed of the air is improved, and the heat supply efficiency of hot air is improved.
Drawings
Fig. 1 is a schematic view of the overall cross-sectional structure of the present invention.
In the figure: 1. a short cabin of a turbine compressor; 2. a motor; 3. a first screw; 4. a dynamic high-speed turbofan; 5. a first bolt; 6. a first flange; 7. a single rotor shaft; 8. a first frustum-shaped air guide hood; 9. a second screw; 10. a second frustum-shaped air guide cover; 11. a static flow guide turbofan; 12. a rectifying cone; 13. a second flange; 14. a second bolt; 15. a high-speed pneumatic ejection port; 16. a pneumatic inlet.
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 efforts all belong to the protection scope of the present invention.
Referring to fig. 1, the present invention provides a technical solution: a main machine for supplying heat by pneumatic heat energy comprises a short cabin 1 of a turbine compressor, wherein a motor 2 is installed in the short cabin 1 of the turbine compressor, and a single rotor shaft 7 in the motor 2 is connected with a dynamic high-speed turbofan 4 and a static flow guide turbofan 11 respectively after extending out of the motor 2;
the dynamic high-speed turbofan 4 is positioned in a pneumatic inlet 16 in the left end of the short cabin 1 of the turbine compressor, the static flow guide turbofan 11 is positioned in a high-speed pneumatic ejection port 15 in the right end of the short cabin 1 of the turbine compressor, and the right end of the single rotor shaft 7 is connected with a rectifying cone 12 positioned in the high-speed pneumatic ejection port 15 after penetrating through the static flow guide turbofan 11;
the left end of the motor 2 is fixed with a first frustum-shaped air guide cover 8 through a first screw 3, the left end of the single rotor shaft 7 extends out through a round hole in the middle of the first frustum-shaped air guide cover 8, the right end of the motor 2 is fixed with a second frustum-shaped air guide cover 10 through a second screw 9, and the right end of the single rotor shaft 7 extends out through a round hole in the middle of the second frustum-shaped air guide cover 10.
The outer side of the left end of the short cabin 1 of the turbine compressor is connected with a first flange 6, and the outer side of the right end of the short cabin 1 of the turbine compressor is connected with a second flange 13.
The middle part of the dynamic high-speed turbofan 4 is sleeved on the outer side of the left end of the single rotor shaft 7 and is fixed with the single rotor shaft 7 through a first bolt 5.
Static water conservancy diversion turbofan 11 cup joints in the right-hand member outside of single rotor shaft 7 to fix fairing cone 12 on single rotor shaft 7 through second bolt 14.
Specifically, when the device is used, the motor 2 works, the single rotor shaft 7 drives the dynamic high-speed turbofan 4 to rotate to form suction, air is sucked into the short cabin 1 of the turbine compressor through the pneumatic inlet 16, the air finally enters the radiating pipe through the high-speed pneumatic jet 15, then enters the auxiliary heating device, is heated through the heating rod in the auxiliary heating device, and finally enters the short cabin 1 of the turbine compressor again through the pneumatic inlet 16;
when air enters the short cabin 1 of the turbine compressor through the pneumatic inlet 16, the air accelerates the flow rate under the action of the first frustum-shaped air guide cover 8, enters the right end of the short cabin 1 of the turbine compressor through a gap reserved between the motor 2 and the short cabin 1 of the turbine compressor, at the moment, the air drives the dynamic and static flow guide turbofan 11 to rotate, the speed of the air slightly rises under the action of the rectifying cone 12, the pressure and the temperature slightly decrease, and the air can uniformly enter the radiating pipe through the high-speed pneumatic ejection port 15.
Through the setting of first frustum shape air guide cover 8, when air gets into in the short storehouse of turbine compressor 1 with first frustum shape air guide cover 8 contact, reduce the contact of air and motor 2 left end, reduce the resistance to the air, when the gap that reserves between air admission motor 2 and the short storehouse of turbine compressor 1, improve the velocity of flow of air.
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. The utility model provides a host computer for pneumatic heat energy heating, includes turbocompressor short storehouse (1), its characterized in that: a motor (2) is installed in the short cabin (1) of the turbine compressor, and a single rotor shaft (7) in the motor (2) extends out of the motor (2) and is connected with a dynamic high-speed turbofan (4) and a static diversion turbofan (11) respectively;
the dynamic high-speed turbofan (4) is positioned in a pneumatic inlet (16) in the left end of the short cabin (1) of the turbine compressor, the static flow guide turbofan (11) is positioned in a high-speed pneumatic ejection port (15) in the right end of the short cabin (1) of the turbine compressor, and the right end of the single rotor shaft (7) penetrates through the static flow guide turbofan (11) and is connected with a rectifying cone (12) in the high-speed pneumatic ejection port (15);
the left end of motor (2) is fixed with first frustum shape air guide cover (8) through first screw (3), and the left end of single rotor shaft (7) stretches out via the round hole at first frustum shape air guide cover (8) middle part, the right-hand member of motor (2) is fixed with second frustum shape air guide cover (10) through second screw (9), and the right-hand member of single rotor shaft (7) stretches out via the round hole at second frustum shape air guide cover (10) middle part.
2. A pneumatic heat and power host as claimed in claim 1, wherein: the outer side of the left end of the short cabin (1) of the turbine compressor is connected with a first flange (6), and the outer side of the right end of the short cabin (1) of the turbine compressor is connected with a second flange (13).
3. A pneumatic heat and power host as claimed in claim 1, wherein: the middle part of the dynamic high-speed turbofan (4) is sleeved on the outer side of the left end of the single rotor shaft (7) and is fixed with the single rotor shaft (7) through a first bolt (5).
4. A pneumatic heat and power host as claimed in claim 1, wherein: static water conservancy diversion turbofan (11) cup joints in the right-hand member outside of single rotor shaft (7) to fix fairing cone (12) on single rotor shaft (7) through second bolt (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222340071.9U CN217978991U (en) | 2022-09-03 | 2022-09-03 | Main unit for pneumatic heat energy heating |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222340071.9U CN217978991U (en) | 2022-09-03 | 2022-09-03 | Main unit for pneumatic heat energy heating |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217978991U true CN217978991U (en) | 2022-12-06 |
Family
ID=84261750
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222340071.9U Expired - Fee Related CN217978991U (en) | 2022-09-03 | 2022-09-03 | Main unit for pneumatic heat energy heating |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217978991U (en) |
-
2022
- 2022-09-03 CN CN202222340071.9U patent/CN217978991U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20221206 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |