CN209559502U - Turbogenerator dynamic experiment platform - Google Patents
Turbogenerator dynamic experiment platform Download PDFInfo
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- CN209559502U CN209559502U CN201920136765.6U CN201920136765U CN209559502U CN 209559502 U CN209559502 U CN 209559502U CN 201920136765 U CN201920136765 U CN 201920136765U CN 209559502 U CN209559502 U CN 209559502U
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- turbine
- front housing
- wall
- turbogenerator
- side outer
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Abstract
The utility model provides turbogenerator dynamic experiment platform, including air intake duct, front housing, combustion chamber, turbine rear casing and fixed plate, air intake duct is located at the side outer wall of front housing, the side outer wall of front housing has been bolted compressor casing, one end of compressor casing is provided with delivery conduit, the side outer wall of front housing and the side outer wall of turbine rear casing weld, combustion chamber is located at the inside of front housing, turbine rear casing is internally provided with turbine, the utility model can be good at allowing user clearly to observe flowing through the gas of engine from the overall process for being compressed to ejection, the compressor casing or turbo blade for preventing personnel's finger to be rotating well in the case where device normally moves squeeze wound, improve the observability and safety when use;By tinting to combustion chamber, turbine and tail spirt row, can be good at display device, each occupy-place temperature is different in actual work in engine, and the integration and analysis of data are carried out convenient for user.
Description
Technical field
The utility model relates to turbogenerator technical fields, and in particular to turbogenerator dynamic experiment platform.
Background technique
Turbogenerator is a kind of parts of utilization rotation from the engine type for drawing kinetic energy in its fluid is passed through, and is
One kind of internal combustion engine.It is commonly used for the engine of aircraft and large-scale ship or vehicle, all turbogenerators all have compression
Machine, combustion chamber, turbine three are most.Compressor is usually also divided into low pressure compressor (low pressure stage) and high pressure compressor (high pressure
Section), low pressure stage also has both the effect that supply fan increases air inflow sometimes, and the air-flow of entrance is compressed into highly dense in compressor
Degree, high pressure, low speed air-flow, to increase the efficiency of engine.After air-flow enters combustion chamber, fuel is ejected by fuel nozzle,
Combining combustion is mixed with air-flow in the combustion chamber.The high hot waste gas generated after burning, then will push turbine makes its rotation, then
It with remaining energy, is discharged via nozzle or exhaust pipe, is used to push turbine as the energy how many is understood, then regards turbine
Depending on the type and design of engine, turbine and compressor is the same is divided into high pressure section and low pressure stage.
Although turbogenerator is possible there are many different operation principles, simplest turbogenerator can only include
One " rotor ", such as a flabellum with central axis, this flabellum is placed in a fluid (such as air or water), fluid is logical
The out-of-date strength applied to flabellum will drive entire rotor and start turning, so be able to from central axis output shaft to torsion.Wind
Vehicle and this kind of device of waterwheel, it may be said that be the turbogenerator prototype that the mankind invent earliest.
Turbogenerator experimental provision in the prior art cannot observe each occupy-place in the inside of turbogenerator well
The motion conditions of (component), while temperature when each occupy-place work cannot be observed well.
Therefore, design turbogenerator dynamic experiment platform is needed to solve the above problems.
Utility model content
In view of the deficienciess of the prior art, the purpose of this utility model is to provide turbogenerator dynamic experiment platform,
It especially can be good at observing the motion conditions of internal part and the temperature of each occupy-place.
To achieve the goals above, the utility model provides the following technical solutions: turbogenerator dynamic experiment platform, including
Air intake duct, front housing, combustion chamber, turbine rear casing and fixed plate, the air intake duct is located at the side outer wall of front housing, before described
The side outer wall of casing has been bolted compressor casing, the side outer wall of the front housing and the side of turbine rear casing
Outer wall welding, the combustion chamber are located at the inside of front housing, and the turbine rear casing is internally provided with turbine, the turbine
Outside is provided with the turbine leaf equidistantly distributed, and one end of the turbine is provided with rotor, and the inlet port of the air intake duct is set
It is equipped with aerosol producer, the side outer wall of the turbine rear casing is provided with tail spray, and the side outer wall of the tail spray is provided with out
The a quarter part of air flue, the turbine rear casing and front housing is splitted by cutter, and turbine rear casing and preceding machine
The section of air intake duct and compressor casing is painted with blue in casket, and the section of the combustion chamber is painted with red, the turbine and tail spray
Section be painted with yellow or purple.
Further, the top exterior walls of the turbine rear casing are provided with oil pipe pedestal, the inside card of the oil pipe pedestal
It is connected to oil pipe, one end of the oil pipe is located at the inside of combustion chamber.
Further, the top exterior walls of the turbine rear casing are provided with heat sink, and the top exterior walls of the heat sink are set
It is equipped with filter screen.
Further, the section of the combustion chamber, air intake duct, compressor casing and tail spray is provided with transparent acrylic
Plate.
Further, the blue is low temperature, and the red is high temperature, and the yellow or purple are higher temperatures.
Further, the bottom outer wall of the fixed plate is bolted there are four annulus is supported, and four branch are held round
Ring is located at four corners of fixed plate bottom outer wall.
Further, turbine rear casing and front housing are bolted on the top exterior walls of fixed plate.
Compared with prior art, the utility model has the beneficial effects that
1, by the transparent acrylic of setting, can be good at that user is allowed clearly to observe the gas for flowing through engine
Body is from the overall process for being compressed to ejection, the compressor machine for preventing personnel's finger to be rotating well in the case where device normally moves
Casket or turbo blade squeeze wound, improve the observability and safety when use.
2, by tinting to combustion chamber, turbine and tail spirt row, it can be good at display device in engine real work
When each occupy-place temperature it is different, the integration and analysis of data are carried out convenient for user, improves each occupy-place temperature when device uses
Observability.
3, by the heat sink of setting and filter screen, heat sink can be good at the thermal energy generated when discharger work,
The service life of each component is improved, while filter screen can be good at preventing the external biggish particle of volume from entering device
It is internal.
Detailed description of the invention
Fig. 1 be the utility model proposes turbogenerator dynamic experiment platform schematic cross-sectional view.
Main element symbol description: 1- air intake duct;2- compressor casing;3- gas off-take;4- rotor;5- filter screen;6- combustion
Burn room;7- supports annulus;8- turbine leaf;9- front housing;10- fixed plate;11- turbine rear casing;The spray of 12- tail;13- smog occurs
Device;14- heat sink;15- oil pipe.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
It should be noted that it can be directly on another component when component is referred to as " being fixed on " another component
Or there may also be components placed in the middle.When a component is considered as " connection " another component, it, which can be, is directly connected to
To another component or it may be simultaneously present component placed in the middle.When a component is considered as " being set to " another component, it
It can be and be set up directly on another component or may be simultaneously present component placed in the middle.Term as used herein is " vertical
", " horizontal ", "left", "right" and similar statement for illustrative purposes only.
Unless otherwise defined, all technical and scientific terms used herein are led with the technology for belonging to the utility model
The normally understood meaning of the technical staff in domain is identical.Terminology used in the description of the utility model herein only be
The purpose of description specific embodiment, it is not intended that in limitation the utility model.Term " and or " used herein includes
Any and all combinations of one or more related listed items.
Please referring also to Fig. 1, after turbogenerator dynamic experiment platform, including air intake duct 1, front housing 9, combustion chamber 6, turbine
Casing 11 and fixed plate 10, air intake duct 1 are located at the side outer wall of front housing 9, and the side outer wall of front housing 9 has been bolted
Compressor casing 2, the side outer wall of front housing 9 and the side outer wall of turbine rear casing 11 weld, and combustion chamber 6 is located at front housing 9
Inside, turbine rear casing 11 is internally provided with turbine, and the outside of turbine is provided with the turbine leaf 8 equidistantly distributed, turbine
One end be provided with rotor 4, the inlet port of the air intake duct 1 is provided with aerosol producer 13, and aerosol producer 13 can be very
Good converts air to atomization little particle, and the side outer wall of turbine rear casing 11 is provided with tail spray 12, and tail sprays outside 12 side
Wall is provided with gas off-take 3, and turbine rear casing 11 and a quarter part of front housing 9 are splitted by cutter, and after turbine
The section of air intake duct 1 and compressor casing 2 is painted with blue in casing 11 and front housing 9, and the section of combustion chamber 6 is painted with red, whirlpool
The section of wheel and tail spray 12 is painted with yellow or purple.
Further, the top exterior walls of turbine rear casing 11 are provided with oil pipe pedestal, and the inside of oil pipe pedestal is connected with oil
Pipe 15, one end of oil pipe 15 are located at the inside of combustion chamber 6, and oil pipe 15 can be good at being supplied for the burning of engine interior
Oil provides raw material for the power of engine.
Further, the top exterior walls of turbine rear casing 11 are provided with heat sink 14, the top exterior walls setting of heat sink 14
There is filter screen 5, radiate, 14 can be good at the thermal energy generated when discharger work, improve the service life of each component, simultaneously
Filter screen 5 can be good at the inside for preventing the external biggish particle of volume from entering device.
Further, the section of combustion chamber 6, air intake duct 1, compressor casing 2 and tail spray 12 is provided with transparent acrylic
Plate, transparent acrylic can be good at allowing user clearly to observe flowing through the gas of engine from being compressed to the complete of ejection
Process, the compressor casing 2 for preventing personnel's finger to be rotating well in the case where device normally moves or turbine leaf 8 squeeze wound,
Improve the observability and safety when use.
Further, blue is low temperature, and red is high temperature, and yellow or purple are higher temperatures, combustion chamber 6, air intake duct 1, pressure
Mechanism of qi casing 2 and tail spray 12, combustion chamber 6 are high temperature, and tail sprays 12 higher temperatures, and air intake duct 1 and compressor casing 2 are low temperature.
Further, the bottom outer wall of fixed plate 10 is bolted that there are four support annulus 7, and four support annulus
7 are located at four corners of 10 bottom outer wall of fixed plate, by supporting the setting of annulus 7, can be good at being easy to use
Mounting plate 10 is fixed in person, and fixed plate 10 and device is made to be in a stable position, convenient for user in experiment
Observation.
Further, turbine rear casing 11 and front housing 9 are bolted on the top exterior walls of fixed plate 10.
Working principle: in use, starter first, oil pipe 15 passes through oil inside offering of the external oil pump to combustion chamber 6, combustion
Oil burns in the inside of combustion chamber 6, while starting compressor casing 2, after gas compression is discharged into turbine by compressor casing 2
Casing 11 pushes the turbine rotation being located in turbine rear casing 11, drives while turbine rotation and is located in turbine rear casing 11
Coaxial turbine leaf 8 rotates, and turbine leaf 8 is compressed by 2 bring fresh air of compressor casing, so that rotor 4 is rotated,
The compression degree of compressor casing 2 increases, and the air inflow of engine is correspondingly increased, and the velocity of rotation of turbine faster, is burnt
Fuel burning in room 6 is more abundant, and power output is just higher.
During use, it by the transparent acrylic of setting, can be good at that user is allowed clearly to observe stream
Through the gas of engine after the processing of aerosol producer 13 is converted into atomization little particle state from the overall process for being compressed to ejection, In
The compressor casing 2 or turbine leaf 8 that device prevents personnel's finger to be rotating well under normally moving squeeze wound;By to combustion
It burns room 6, turbine and tail spray 12 to tint, can be good at display device, each occupy-place temperature is not in actual work in engine
Together, the integration and analysis of data are carried out convenient for user.
Above description is the detailed description for the preferable possible embodiments of the utility model, but embodiment is not limited to
The patent claim of the utility model, the same changes or modifications completed under technical spirit suggested by all the utility model
Change, should belong to the covered the scope of the patents of the utility model.
Claims (7)
1. turbogenerator dynamic experiment platform, which is characterized in that including air intake duct (1), front housing (9), combustion chamber (6), turbine
Rear housing (11) and fixed plate (10), the air intake duct (1) are located at the side outer wall of front housing (9), and the one of the front housing (9)
Side outer wall has been bolted compressor casing (2), and the one of the side outer wall of the front housing (9) and turbine rear casing (11)
The welding of side outer wall, the combustion chamber (6) are located at the inside of front housing (9), and the turbine rear casing (11) is internally provided with whirlpool
Wheel, the outside of the turbine are provided with the turbine leaf (8) equidistantly distributed, and one end of the turbine is provided with rotor (4), described
The inlet port of air intake duct (1) is provided with aerosol producer (13), and the side outer wall of the turbine rear casing (11) is provided with tail
It sprays (12), the side outer wall of the tail spray (12) is provided with gas off-take (3), the turbine rear casing (11) and front housing (9)
A quarter part is splitted by cutter, and turbine rear casing (11) and front housing (9) interior air intake duct (1) and compressor machine
The section of casket (2) is painted with blue, and the section of the combustion chamber (6) is painted with red, and the section that the turbine and tail spray (12) is painted with
Yellow or purple.
2. turbogenerator dynamic experiment platform according to claim 1, which is characterized in that the turbine rear casing (11)
Top exterior walls are provided with oil pipe pedestal, and the inside of the oil pipe pedestal is connected with oil pipe (15), one end position of the oil pipe (15)
In the inside of combustion chamber (6).
3. turbogenerator dynamic experiment platform according to claim 1, which is characterized in that the turbine rear casing (11)
Top exterior walls are provided with heat sink (14), and the top exterior walls of the heat sink (14) are provided with filter screen (5).
4. turbogenerator dynamic experiment platform according to claim 1, which is characterized in that the combustion chamber (6), air intake duct
(1), the section of compressor casing (2) and tail spray (12) is provided with transparent acrylic.
5. turbogenerator dynamic experiment platform according to claim 1, which is characterized in that the blue is low temperature, described
Red is high temperature, and the yellow or purple are higher temperatures.
6. turbogenerator dynamic experiment platform according to claim 1, which is characterized in that the bottom of the fixed plate (10)
Outer wall supports annulus (7) there are four being bolted, and four support annulus (7) are located at fixed plate (10) bottom outer wall
Four corners.
7. turbogenerator dynamic experiment platform according to claim 1, which is characterized in that turbine rear casing (11) and preceding machine
Casket (9) is bolted on the top exterior walls of fixed plate (10).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201920136765.6U CN209559502U (en) | 2019-01-25 | 2019-01-25 | Turbogenerator dynamic experiment platform |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201920136765.6U CN209559502U (en) | 2019-01-25 | 2019-01-25 | Turbogenerator dynamic experiment platform |
Publications (1)
Publication Number | Publication Date |
---|---|
CN209559502U true CN209559502U (en) | 2019-10-29 |
Family
ID=68308997
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201920136765.6U Expired - Fee Related CN209559502U (en) | 2019-01-25 | 2019-01-25 | Turbogenerator dynamic experiment platform |
Country Status (1)
Country | Link |
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CN (1) | CN209559502U (en) |
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2019
- 2019-01-25 CN CN201920136765.6U patent/CN209559502U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191029 Termination date: 20220125 |
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CF01 | Termination of patent right due to non-payment of annual fee |