CN218235270U - Miniature gas turbine housing applying injection principle - Google Patents
Miniature gas turbine housing applying injection principle Download PDFInfo
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- CN218235270U CN218235270U CN202123121421.4U CN202123121421U CN218235270U CN 218235270 U CN218235270 U CN 218235270U CN 202123121421 U CN202123121421 U CN 202123121421U CN 218235270 U CN218235270 U CN 218235270U
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- combustion engine
- air inlet
- exhaust system
- gas turbine
- ejector
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Abstract
The utility model discloses an use miniature combustion engine housing of drawing and penetrate principle, include combustion engine chassis, combustion engine box and be located the air inlet system of this combustion engine box inside, exhaust system and exhaust system interconnect constitute the ejector. The air inlet system comprises air inlet shutters of the combustion engine. The air inlet system also comprises a combustion engine air inlet filter positioned behind the combustion engine air inlet shutter. The air inlet system comprises a combustion engine air inlet silencer positioned behind the combustion engine air inlet filter. The utility model discloses the volume of reducible little housing has reduced material cost and weight, and convenient transportation and hoist and mount have reduced the design degree of difficulty, have improved the rate of utilization of miniature combustion engine.
Description
Technical Field
The utility model relates to a gas turbine housing especially relates to a miniature gas turbine housing of injection principle is drawn in application.
Background
The existing gas turbine cover generally comprises an air inlet system, an air exhaust system and an exhaust system. The air inlet system is used for allowing air to pass through and enter the housing for the use of the combustion engine; the exhaust system is used for exhausting high-temperature gas in the housing, so that airflow in the housing flows, the ambient temperature of the gas turbine is reduced, and the gas turbine can normally run without being too high in temperature; the exhaust system is used for exhausting high-temperature tail gas when the combustion engine burns. Because of the existence of the air inlet system, the air exhaust system and the air exhaust system, the whole volume of the housing is large, the weight is large and the installation and the transportation are inconvenient.
Particularly for a micro-combustion engine, if the exhaust system and the exhaust system are adopted as a large combustion engine, the volume of the housing is increased, and the cost is increased. In order to solve the problem, the sizes of an air inlet system, an air exhaust system and an exhaust system need to be changed, so that the utilization of the internal space of the whole housing is particularly critical, and great difficulty is brought to the design work.
Disclosure of Invention
The technical problem to prior art not enough, the utility model provides an use miniature combustion engine housing of penetrating the principle is provided, it has reduced the volume of whole combustion engine housing and has reduced the cost.
The utility model discloses an ejector uses the stealthy principle of penetrating, replaces original exhaust system and exhaust system, structurally can practice thrift the space like this, reduces the design degree of difficulty, makes the combustion engine housing size diminish.
The technical scheme of the utility model is that: a miniature gas turbine housing applying an injection principle comprises a gas turbine chassis, a gas turbine box body, an air inlet system, an air exhaust system and an air exhaust system, wherein the air inlet system, the air exhaust system and the air exhaust system are positioned in the gas turbine box body, and the air exhaust system are connected with each other to form an injector.
The air inlet system comprises air inlet shutters of the combustion engine.
The air inlet system also comprises a combustion engine air inlet filter positioned behind the combustion engine air inlet shutter.
The air inlet system comprises a combustion engine air inlet silencer positioned behind the combustion engine air inlet filter.
The ejector comprises an upper assembly consisting of an outer plate, a pore plate and sound absorption materials between the outer plate and the pore plate, a lower assembly and an exhaust funnel for exhausting high-temperature gas, wherein the upper assembly is hinged with the lower assembly and is provided with an inclined contact surface.
The engine box also comprises a sound insulation door positioned on the engine box body.
The technical effects of the utility model are that:
1. the utility model discloses an integrate into a system exhaust system and exhaust system, form the ejector, the ejector plays simultaneously and airs exhaust and carminative purpose, under the prerequisite that the function satisfies, reduces the volume of little housing.
2. The utility model discloses reduced material cost and weight, convenient transportation and hoist and mount.
3. The utility model discloses reduce the design degree of difficulty, improved the rate of utilization of miniature combustion engine.
Drawings
FIG. 1 is a front view of a housing of a micro gas turbine according to the present invention;
FIG. 2 is a top view of the micro gas turbine housing of the present invention;
FIG. 3 is a cross-sectional view of a micro gas turbine housing of the present invention;
FIG. 4 is a front view of a micro gas turbine housing of the present invention;
FIG. 5 is a rear view of the micro gas turbine housing of the present invention;
fig. 6 is a perspective view of the ejector of the present invention;
fig. 7 is a side view of the eductor of the present invention;
fig. 8 is a sectional view of fig. 7.
Detailed Description
The present invention will now be described in further detail with reference to the accompanying drawings and examples.
Referring to fig. 1 to 5, the micro housing of the present invention comprises: the internal combustion engine comprises an internal combustion engine box body 1, an internal combustion engine chassis 2, an internal combustion engine air inlet shutter 3, an internal combustion engine air inlet filter 4, an internal combustion engine air inlet silencer 5, an ejector 6 and a soundproof door 7, wherein the internal combustion engine box body 1 has the main function of isolating noise, and the external noise of a housing meets the use requirement when an engine operates. The main function of the gas turbine chassis 2 is to ensure the integral strength, and the gas turbine chassis can be integrally hoisted during hoisting. The air inlet shutter 3 of the combustion engine mainly has the function of preventing rainwater from entering. The air inlet filter 4 of the gas turbine mainly has the function of ensuring that gas required by combustion of the gas turbine meets the requirement of cleanliness. The air inlet silencer 5 of the combustion engine mainly has the function of reducing the noise of an air inlet. The ejector 6 has the main function of exhausting high-temperature gas and exhausting air in the box body at the same time, so that the air in the box body flows circularly. The soundproof door 7 is mainly used for maintenance and repair of the engine.
Referring to fig. 6 to 7, the ejector 6 of the present invention is composed of an ejector upper assembly 8, an ejector lower assembly 9, and an exhaust funnel 10. Ejector upper portion subassembly 8 mainly include: an upper assembly outer plate 11, an upper assembly orifice plate 12 and an upper assembly sound absorbing material 13. The upper component outer plate 11 mainly functions as a lower injection system supporting plate to play a role in fixing and reinforcing. The upper assembly micro-perforated plate 12 functions primarily to dampen sound and reduce noise. The main function of the upper assembly sound absorption material 13 is sound absorption and sound insulation.
Exhaust draw and penetrate system lower part subassembly 9, mainly include: a lower assembly outer plate 14, a lower assembly orifice plate 15, and a lower assembly sound absorbing material 16. The upper component outer plate 14 mainly functions as a lower injection system support plate to play a role in fixing and reinforcing. The upper assembly micro-perforated plate 15 mainly functions to eliminate noise. The upper assembly sound absorbing material 16 serves the primary function of sound absorption and sound isolation.
The engine exhaust funnel is connected with the exhaust funnel of the ejector, and the main effect is that when high-temperature gas is exhausted, the ejector drives normal-temperature green gas in the housing to be exhausted, so that air in the housing flows, the gas in the box body can form a flowing state, and the exhaust ejector system is an exhaust ejector system and can play the roles of an exhaust system and a fan. The hot air in the box body can be ejected and discharged without using an independent air exhaust system with a fan, the same function as the air exhaust system is achieved, the temperature in the box body is reduced, and the temperature in the box body is controlled within a reasonable range. The upper component 8 of the ejector mainly has the function of noise elimination, and can be conveniently disassembled, so that the inspection is very convenient. Can produce very big noise when high-speed air current discharges, add sound absorbing material through inside and play the effect of sound absorption, the inner wall is laid the micropunch plate and can be reduced the impact of air current to sound absorbing material, can play fine noise elimination effect simultaneously.
When the ejector is designed, mainly the ejection parameters and the ejection distance are difficult to determine, and the proper parameters can be determined through repeated tests and multiple tests, so that the miniature gas turbine housing with the ejector is not widely applied. The ejector is less applied to the cover of the micro gas turbine. It is also contemplated that more advanced technology and well-established concepts may serve the same purpose or be substituted.
Although the present invention has been described with reference to the preferred embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the present invention.
Claims (5)
1. The utility model provides an use miniature combustion engine housing of drawing penetrating principle, includes combustion engine chassis, combustion engine box and is located the air inlet system, exhaust system and the exhaust system of this combustion engine box inside, characterized by: the air exhaust system and the exhaust system are connected with each other to form the ejector, the ejector comprises an upper component and a lower component which are composed of an outer plate, a pore plate and sound absorption materials between the outer plate and the pore plate, and an exhaust funnel used for exhausting high-temperature gas, and the upper component is hinged with the lower component and provided with an inclined contact surface.
2. The micro-combustion engine cover applying the ejection principle according to claim 1, wherein: the air inlet system comprises a gas turbine air inlet shutter.
3. The micro internal combustion engine cover applying the ejection principle according to claim 2, wherein: the air inlet system also comprises a combustion engine air inlet filter positioned behind the combustion engine air inlet shutter.
4. The micro internal combustion engine cover using the injection principle according to claim 3, wherein: the air inlet system comprises a combustion engine air inlet silencer positioned behind the combustion engine air inlet filter.
5. The micro internal combustion engine cover applying the ejection principle according to claim 4, wherein: the engine box also comprises a sound insulation door positioned on the engine box body.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202123121421.4U CN218235270U (en) | 2021-12-10 | 2021-12-10 | Miniature gas turbine housing applying injection principle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202123121421.4U CN218235270U (en) | 2021-12-10 | 2021-12-10 | Miniature gas turbine housing applying injection principle |
Publications (1)
Publication Number | Publication Date |
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CN218235270U true CN218235270U (en) | 2023-01-06 |
Family
ID=84662834
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202123121421.4U Active CN218235270U (en) | 2021-12-10 | 2021-12-10 | Miniature gas turbine housing applying injection principle |
Country Status (1)
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CN (1) | CN218235270U (en) |
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2021
- 2021-12-10 CN CN202123121421.4U patent/CN218235270U/en active Active
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