CN209027800U - A kind of engine testsand - Google Patents
A kind of engine testsand Download PDFInfo
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- CN209027800U CN209027800U CN201821618634.3U CN201821618634U CN209027800U CN 209027800 U CN209027800 U CN 209027800U CN 201821618634 U CN201821618634 U CN 201821618634U CN 209027800 U CN209027800 U CN 209027800U
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Abstract
A kind of engine testsand, including supply source, temperature simulation unit, boiler-plate and exhaust injector；Supply source includes fuel delivery source, oxygen supply source, engine charge supply source, alcohol supply source and injector active flow supply source；Temperature simulation unit includes tube body and shell, and it is first medium channel in tube body, the space between the outer wall of tube body and the inner wall of shell forms second medium channel that tube body, which is located at enclosure interior,；It is located in boiler-plate by spreadsheet engine；Fuel delivery source is connected to by pipeline with by spreadsheet engine, oxygen supply source and engine charge supply source pass through pipeline respectively and are connected to the entrance in second medium channel, the outlet in second medium channel is connected to by pipeline with by the air inlet of spreadsheet engine, alcohol supply source is connected to by pipeline with the entrance in first medium channel after igniter, injector active flow supply source is connected to by pipeline with exhaust injector, and exhaust injector passes through boiler-plate close to by the exhaust pipe of spreadsheet engine.
Description
Technical field
The utility model relates to test measurement technical field, especially a kind of engine testsand.
Background technique
Aero-engine need to do altitude simulation test on ground before being taken a flight test, when engine test, it is desirable that one group of ginseng
Number, including inlet total pressure, Induction air flow, air inlet oxygen content, inlet total temperature, engine oil oil mass, air environment pressure,
Referred to as state point, at the same reach setting value and stablize after, record its performance and parameter or examine its performance, available engine examination
Ride technology, for engine charge simulation, flight environment of vehicle pressure simulation there is no mature technology, simultaneously for emulation mode when
Reach stable state also without accurate theoretical determination method, causes test simulation effect poor, the test period is long, at high cost, resource
It is serious to waste situation.
Summary of the invention
The technology of the utility model solves the problems, such as: overcoming the deficiencies of the prior art and provide a kind of engine testsand.
The technical solution of the utility model is: a kind of engine testsand, including supply source, temperature simulation unit,
Boiler-plate and exhaust injector；Supply source includes fuel delivery source, oxygen supply source, engine charge supply source, alcohol supply
Source and injector active flow supply source；Temperature simulation unit includes tube body and shell, and tube body is located at enclosure interior, is in tube body
First medium channel, the space between the outer wall of tube body and the inner wall of shell form second medium channel；It is located at by spreadsheet engine
In boiler-plate；Fuel delivery source is connected to by pipeline with by spreadsheet engine, oxygen supply source and engine charge supply source difference
It is connected to by pipeline with the entrance in second medium channel, the outlet in second medium channel passes through pipeline and the air inlet by spreadsheet engine
Mouth connection, alcohol supply source are connected to by pipeline with the entrance in first medium channel after igniter, injector active flow
Supply source is connected to by pipeline with exhaust injector, and exhaust injector passes through boiler-plate close to by the exhaust pipe of spreadsheet engine.
Further, it is connected to fuel delivery source and is provided with engine fuel supply flow rate tune on the pipeline of spreadsheet engine
It saves valve and engine fuel supplies shut-off valve.
Further, oxygen supply flow tune is provided on the pipeline of connection oxygen supply source and the entrance in second medium channel
Save valve and oxygen supply shut-off valve.
Further, engine is provided on the pipeline of connection engine charge supply source and the entrance in second medium channel
Air inlet supply pressure regulating valve.
Further, alcohol supply flow rate is provided on the pipeline of connection alcohol supply source and the entrance in first medium channel
Regulating valve and with alcohol supply shut-off valve, the outlet in first medium channel is in communication with the outside.
Further, it is connected on the pipeline of injector active flow supply source and exhaust injector and is provided with injector actively
Air-flow supply pressure regulating valve.
The utility model compared with prior art the advantages of be:
1, the engine testsand of the utility model, will be by spreadsheet engine as in boiler-plate, and boiler-plate uses seal shape
State is evacuated by exhaust injector, and simulated engine is in the environmental pressure of different flying heights, passes through injector active flow
Supply source provides injection air-flow for exhaust injector, and structure is simple；The fuel feeding to engine is realized by fuel delivery source.
2, the engine testsand of the utility model, by engine charge supply source simulated engine charge flow rate, into
Gas stagnation pressure, meanwhile, it is that engine charge carries out oxygenating and by temperature simulation unit simulation engine by oxygen supply source
Intake air temperature realizes the real simulation of engine charge, and structure is simple, and simulation precision is high.
3, alcohol supply source is arranged in the engine testsand of the utility model, and alcohol is lighted generation heat by igniter
Amount exchanges heat in temperature simulation unit with engine charge, realizes the adjusting of Engine Inlet Temperature.
4, the engine testsand of the utility model realizes the flow and pressure in joint supply source by the way that various valves are arranged
Power is adjustable, and then realizes the simulation of multimode point.
Detailed description of the invention
Fig. 1 is the engine testsand structure principle chart of the utility model.
Fig. 2 is the partial structural diagram of the temperature simulation unit of the engine testsand of the utility model.
Fig. 3 is the application method flow chart of the engine testsand of the utility model.
Specific embodiment
In the description of the present invention, it should be understood that term " center ", " longitudinal direction ", " transverse direction ", " length ", " width
Degree ", " thickness ", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom" "inner", "outside", " suitable
The orientation or positional relationship of the instructions such as hour hands ", " counterclockwise ", " axial direction ", " radial direction ", " circumferential direction " is orientation based on the figure
Or positional relationship, be merely for convenience of describing the present invention and simplifying the description, rather than the device of indication or suggestion meaning or
Element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as the limit to the utility model
System.In addition, defining " first ", the feature of " second " can explicitly or implicitly include one or more of the features.
In the description of the present invention, unless otherwise indicated, the meaning of " plurality " is two or more.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified
Dress ", " connected ", " connection ", " abutting " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection,
Or it is integrally connected；It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, intermediary can also be passed through
It is indirectly connected, can be the connection inside two elements.For the ordinary skill in the art, it can be managed with concrete condition
Solve the concrete meaning of above-mentioned term in the present invention.
A kind of engine testsand is used for engine high-altitude multimode point simulation test, the parameter packet of the state point
Include engine charge stagnation pressure, Induction air flow, air inlet oxygen ingredient, inlet total temperature, engine oil oil mass, air environment pressure
Power；The engine testsand includes supply source, temperature simulation unit 200, boiler-plate 300 and exhaust injector 600；Supply source
Including fuel delivery source 110, oxygen supply source 120, engine charge supply source 130, alcohol supply source 140 and injector are actively
Air-flow supply source 150；The temperature simulation unit includes tube body 210 and shell 220, and the tube body 210 is located at the shell 220
Inside, the interior tube body 210 is first medium channel, the sky between the outer wall of the tube body 210 and the inner wall of the shell 220
Between formed second medium channel；When the temperature simulation unit 200 works, first medium circulates in first medium channel, the
Second medium circulates in second medium channel, and first medium temperature is higher than second medium, and the first medium and second medium are logical
The tube wall for crossing the tube body 210 realizes heat exchange；It is located in the boiler-plate 300 by spreadsheet engine 400；The fuel delivery source
110 are connected to described by spreadsheet engine 400 by pipeline, the oxygen supply source 120 and the engine charge supply source 130
It is connected to respectively by pipeline with the entrance in second medium channel, the outlet in second medium channel is started by pipeline and the subject
The air inlet of machine 400 is connected to, to provide the engine intake airflow of simulation, inlet total pressure and oxygen content by spreadsheet engine 400；
The alcohol supply source 140 is connected to by pipeline with the entrance in first medium channel after igniter, first medium channel
Outlet is in communication with the outside, and alcohol is lighted burning and generates heat in the temperature simulation unit 200 and second medium by igniter
Second medium in channel exchanges heat to adjust the temperature of the second medium in second medium channel, to realize engine inlet temperature
The engine charge simulation of degree simulation, the utility model is true, and precision is high, and structure is simple.
The injector active flow supply source 150 is connected to by pipeline with the exhaust injector 600, and the exhaust is drawn
Emitter 600 passes through the boiler-plate 300 close to the exhaust pipe by spreadsheet engine 400；It is preferred that the exhaust injector 600
Entrance section with it is described by a distance from 400 exhaust outlet section of spreadsheet engine for by 400 exhaust outlet of spreadsheet engine cut
The half of radius surface sets performance to improve drawing for injector；The exhaust injector 600 draws the gas set in the boiler-plate 300
And the exhaust by spreadsheet engine 4000, the environmental pressure of different flying heights, the injection are in simulated engine
Device active flow supply source 150 is that the exhaust injector 600 provides injection air-flow；The structure of exhaust injector 600 is existing
Technology, referring specifically to applicant identified patent applications CN201610786167.4, CN201610786117.6,
CN201610790335.7, CN201610764543.X, CN201610764549.7 etc..Be connected to the fuel delivery source 110 with
It is described that engine fuel supply flow rate regulating valve 510 is provided on the pipeline of spreadsheet engine 400, it is connected to the oxygen supply source
120 be provided with oxygen supply flow control valve 530 on the pipeline of the entrance in the second medium channel, be connected to the engine into
It is provided with engine charge supply pressure regulating valve 550 on the pipeline of gas supply source 130 and the entrance in second medium channel, is connected to
It is provided with alcohol supply flow rate regulating valve 560 on the alcohol supply source 140 and the pipeline of the entrance in first medium channel, is connected to
The confession of injector active flow is provided on the injector active flow supply source 150 and the pipeline of the exhaust injector 600
Meet the simulation of multimode point to pressure-regulating valve 580 to realize the parameter regulation of each supply source.
Preferably, the engine testsand includes engine fuel supply shut-off valve 520,540 He of oxygen supply shut-off valve
Alcohol supplies shut-off valve 570, and engine fuel supply shut-off valve 520 setting is being connected to the fuel delivery source 110 and institute
It states by the pipeline of spreadsheet engine 400；The oxygen supply shut-off valve 540 setting be connected to the oxygen supply source 120 with it is described
On the pipeline of the entrance in second medium channel；Alcohol supply shut-off valve 570 setting be connected to the alcohol supply source 140 with
On the pipeline of the entrance in first medium channel.In the use process of engine testsand, the engine fuel supply stream is opened
The engine fuel supply shut-off valve 520 is opened before adjustable valve 510, is opened before opening the oxygen supply flow control valve 530
Oxygen supply shut-off valve 540 is opened, opens the alcohol supply shut-off valve 570 before opening the alcohol supply flow rate regulating valve 560；It closes
The engine fuel supply shut-off valve 520 is closed after closing the engine fuel supply flow rate regulating valve 510, closes the oxygen
Oxygen supply shut-off valve 540 is closed after supply flow rate regulating valve 530, closes institute after closing the alcohol supply flow rate regulating valve 560
Alcohol supply shut-off valve 570 is stated, to guarantee safety of the test bay under non-experimental state.
The application method of the engine testsand, includes the following steps:
S100), simulation storehouse pressure is adjusted
Injector active flow supply pressure is adjusted according to the environmental pressure of the engine flight height of the first emulation mode point
Force regulating valve keeps the pressure in boiler-plate identical as the environmental pressure of engine flight height of the first emulation mode point.
S200), engine charge stagnation pressure and oxygen content are adjusted
Engine charge supply pressure regulating valve and oxygen are adjusted according to the inlet total pressure of the first emulation mode point and oxygen content
Supply flow rate regulating valve makes the stagnation pressure and oxygen content and the first emulation mode point of the second medium by second medium channel outlet
The inlet total pressure of engine is identical with oxygen content.
S300), engine charge total temperature is adjusted
Alcohol supply flow rate regulating valve and initial igniter are adjusted according to the inlet total temperature of the first emulation mode point, lights wine
Essence makes alcohol burn, and the alcohol of burning exchanges heat in the second medium in first medium channel and second medium channel, makes by second
The total temperature of the second medium of medium channel outlet is identical as the inlet total temperature of the first emulation mode point engine；
S310), alcohol supply flow rate regulating valve, starting are adjusted according to the highest operating condition value that temperature simulation unit can bear
Igniter, lighting alcohol makes alcohol burn, and the alcohol of burning changes in first medium channel and the second medium in second medium channel
Heat；
S320), state to the temperature simulation unit of step S310 is kept to enter steady-working state；
S330), according in the first emulation mode point, the second medium total temperature of second medium channel outlet, second medium leads to
The quality of second medium in road, the specific heat at constant pressure of second medium, inboard wall of tube body convection transfer rate, the inner wall of entire tube body
It is long-pending, the quality of first medium in first medium channel, the specific heat at constant pressure of first medium, tube wall convection transfer rate, entirely
The outer wall area of tube body and the second medium total temperature of second medium feeder connection, determine the supplying temperature of first medium；
S340), alcohol supply flow rate regulating valve is adjusted, by the first medium state in first medium channel by with temperature mould
The highest operating condition value supply that quasi-simple member can bear is adjusted to the predetermined value supply according to the first simulation test state point；
S350), keep the first medium in first medium channel according to the predetermined value of the first simulation test state point of experiment
Supply state to temperature simulation unit enters steady-working state, at this point, the second medium by second medium channel outlet
Total temperature is identical as the inlet total temperature of the first emulation mode point engine.
S400), engine charge stagnation pressure is adjusted
Engine charge supply pressure regulating valve is adjusted according to the inlet total pressure of the first emulation mode point, makes to be situated between by second
The stagnation pressure of the second medium of matter channel outlet is identical as the inlet total pressure of the first emulation mode point engine.
S500), engine ignition
Engine fuel supply flow rate regulating valve is adjusted according to the fuel demand amount of engine the first emulation mode point, makes to fire
The fuel oil of oily supply source supply is identical as the fuel demand amount of engine the first emulation mode point, and engine ignition carries out first
The simulation test of emulation mode point to the state point simulation test terminates.
S600), the simulation test of N emulation mode point
Injector active flow supply pressure regulating valve is adjusted respectively, adjusts oxygen supply flow control valve, engine charge
Supply pressure regulating valve, alcohol supply flow rate regulating valve and engine fuel supply flow rate regulating valve, make the pressure in boiler-plate
It is identical as the environmental pressure of engine flight height of N emulation mode point, the second medium of second medium channel outlet it is total
Pressure, total temperature and oxygen content are identical as the inlet total pressure of N emulation mode point engine, total temperature and oxygen content, and fuel delivery source supplies
The fuel oil given is identical as the fuel demand of N emulation mode point engine；Wherein, N >=2 start the simulation of engine nth state point
Test to the state point simulation test terminates.
S610), injector active flow is adjusted according to the environmental pressure of the engine flight height of N emulation mode point to supply
To pressure-regulating valve, keep the pressure in boiler-plate identical as the environmental pressure of engine flight height of N emulation mode point；
S620), oxygen supply flow control valve is adjusted, the oxygen content and N of the second medium of second medium channel outlet are made
The oxygen content of emulation mode point engine is identical；
S630), according in N emulation mode point, the second medium total temperature of second medium channel outlet, second medium channel
The quality of interior second medium, the specific heat at constant pressure of second medium, inboard wall of tube body convection transfer rate, the inner wall area of entire tube body,
The quality of first medium in first medium channel, the specific heat at constant pressure of first medium, tube wall convection transfer rate, entire tube body
Outer wall area and second medium feeder connection second medium total temperature, determine the supplying temperature of first medium；
S640), alcohol supply flow rate regulating valve is adjusted, by the first medium state in first medium channel by the first simulation
The predetermined value supply of trystate point is adjusted to the predetermined value supply according to N simulation test state point；
S650), the first medium in first medium channel is kept to supply according to the predetermined value of experiment N simulation test state point
Enter steady-working state to state to temperature simulation unit, at this point, the second medium by second medium channel outlet is total
The inlet total temperature of Wen Yu N emulation mode point engine is identical；
S660), according to the inlet total pressure of N emulation mode point adjust engine charge supply pressure regulating valve, make by
The stagnation pressure of the second medium of second medium channel outlet is identical as the inlet total pressure of N emulation mode point engine；
S670), engine fuel supply flow rate is adjusted according to the fuel demand amount of engine N emulation mode point to adjust
Valve, the fuel oil for supplying fuel delivery source is identical as the fuel demand amount of engine N emulation mode point, starts engine N
State point simulation test to the state point simulation test terminates.
S700), step S600 is repeated until after all emulation mode experimental tests, engine misses close engine
Fuel delivery flow control valve, oxygen supply flow control valve, engine charge supply pressure regulating valve and alcohol supply flow rate tune
After saving valve, injector active flow supply pressure regulating valve is closed.
Preferably, the highest operating condition value that temperature simulation unit can bear is first Jie that temperature simulation unit can bear
Maximum pressure, maximum temperature and the maximum flow of matter；The parameter of the predetermined value of simulation test state point includes medium inlet and goes out
The pressure of mouth, the flow of medium and the temperature of medium.
Preferably, in step S320, state to the temperature simulation unit of step S310 is kept to enter steady-working state, institute
The time needed is T1；Keep the first medium in first medium channel according to the first simulation test state point of experiment in step S350
Predetermined value supply state to temperature simulation unit enter steady-working state, the required time is T2；It is kept in step S650
First medium in first medium channel is according to the predetermined value supply state of experiment N simulation test state point to temperature simulation list
Member enters steady-working state, and the required time is TN；
T1, T2And TNEnter steady-working state calculation formula according to temperature simulation unit to determine；Temperature simulation unit into
Enter steady-working state calculation formula are as follows:
In formula: TxEnter the time of steady-working state, unit s for temperature simulation unit；M is the matter of entire tube body
Amount, unit kg are known quantity；cmpFor the specific heat at constant pressure of tube body, unit J/kgK is known quantity；hhFor inboard wall of tube body pair
The coefficient of heat transfer is flowed, unit is W/ (m2It K), is known quantity；AsiFor the inner wall area of entire tube body, unit m2, it is known quantity；
mhFor the quality of the first medium in first medium channel, unit kg is known quantity；cphFor the level pressure ratio of first medium
Heat, unit J/kgK are known quantity；hcFor tube wall convection transfer rate, unit is W/ (m2It K), is known quantity；
AseFor the outer wall area of entire tube body, unit m2, it is known quantity；mcFor the matter of the second medium in second medium channel
Amount, unit kg are known quantity；cpcFor the specific heat at constant pressure of second medium, unit J/kgK is known quantity.
Preferably, step S330 is according in the first emulation mode point, the second medium total temperature of second medium channel outlet, and
The quality of second medium in second medium channel, the specific heat at constant pressure of second medium, inboard wall of tube body convection transfer rate, entire tube body
Inner wall area, the quality of first medium, the specific heat at constant pressure of first medium, tube wall heat convection system in first medium channel
Number, the outer wall area of entire tube body and the second medium total temperature of second medium feeder connection, determine the supplying temperature of first medium,
At this point, the supplying temperature of first medium is Thi1；
In step S630, according in N emulation mode point, the second medium total temperature of second medium channel outlet, second is situated between
The quality of second medium in matter channel, the specific heat at constant pressure of second medium, inboard wall of tube body convection transfer rate, the inner wall of entire tube body
Area, the quality of first medium, the specific heat at constant pressure of first medium, tube wall convection transfer rate are whole in first medium channel
The outer wall area of a tube body and the second medium total temperature of second medium feeder connection, determine the supplying temperature of first medium, at this point,
The supplying temperature of first medium is ThiN；
Thi1And ThiNDetermined according to temperature simulation unit hot-fluid input temp formula；Temperature simulation unit hot-fluid input temperature
Spend formula are as follows:
In formula:
ThixFor the supplying temperature of first medium, unit K；TcoIt is single for the second medium total temperature of second medium channel outlet
Position is K, is known quantity；mcFor the quality of second medium in second medium channel, unit kg is known quantity；cpcFor second medium
Specific heat at constant pressure, unit J/kgK, be known quantity；hhFor inboard wall of tube body convection transfer rate, unit is W/ (m2K), it is
Known quantity；AsiFor the inner wall area of entire tube body, unit m2, it is known quantity；mhFor first medium in first medium channel
Quality, unit kg are known quantity；cphFor the specific heat at constant pressure of first medium, unit J/kgK is known quantity；hcFor tube body
Outer wall convection transfer rate, unit are W/ (m2It K), is known quantity；AseFor the outer wall area of entire tube body, unit m2, it is
Known quantity；TciFor the second medium total temperature of second medium feeder connection, unit K is known quantity.
For the engine testsand of the utility model, in addition to the advantageous effects mentioned before, application method has
Following advantageous effects:
1, using the pressure of first adjusting boiler-plate, then inlet total pressure and oxygen content are adjusted, then adjusts inlet total temperature, finally
After accurate adjustment inlet total pressure, the mode of fuel feeding igniting, adjustment speed is fast, saves the simulation of test bay engine charge and flying height
The regulating time of environmental pressure simulation, reduces experimentation cost, avoids energy waste.
2, in the use process of temperature simulation unit, it is creative on startup, can first be held using temperature simulation unit
The highest operating condition value received inputs thermal current to heat exchanger, so that the inner tube of temperature simulation unit is operated at full capacity, with most fast speed
It warms up, it is fast that tube body temperature promotes speed, uniformity of temperature profile, then is adjusted to test predetermined value by full load condition, into steady
Determine the working condition time and substantially shortens.
3, in the use process of temperature simulation unit, pass through the quasi- to data and curves of a large amount of test data and creativeness
It closes, it is determined that the temperature simulation unit of high accuracy enters steady-working state calculation formula, being capable of accurate temperature simulation
Unit enters the time of steady-working state, substantially shortens test period, reduces experimentation cost, avoids energy waste.
4, in the use process of temperature simulation unit, pass through the quasi- to data and curves of a large amount of test data and creativeness
It closes, it is determined that the temperature simulation unit hot-fluid of high accuracy inputs calculation formula, the temperature simulation unit heat that can accurately determine
Input temp is flowed, substantially shortens test period, reduces experimentation cost, avoid energy waste.
In the description of this specification, reference term " one embodiment ", " some embodiments ", " illustrative examples ",
The description of " example ", " specific example " or " some examples " etc. means specific features described in conjunction with this embodiment or example, knot
Structure, material or feature are contained at least one embodiment or example of the utility model.In the present specification, to above-mentioned art
The schematic representation of language may not refer to the same embodiment or example.Moreover, description specific features, structure, material or
Person's feature can be combined in any suitable manner in any one or more of the embodiments or examples.
While there has been shown and described that the embodiments of the present invention, it will be understood by those skilled in the art that:
These embodiments can be carried out with a variety of variations, modification, replacement in the case where not departing from the principles of the present invention and objective
And modification, the scope of the utility model are defined by the claims and their equivalents.
Claims (6)
1. a kind of engine testsand, which is characterized in that including supply source, temperature simulation unit, boiler-plate and exhaust injector；
Supply source includes fuel delivery source, oxygen supply source, engine charge supply source, alcohol supply source and injector active gas
Flow supply source；
Temperature simulation unit includes tube body and shell, and tube body is located at enclosure interior, is first medium channel in tube body, tube body it is outer
Space between wall and the inner wall of shell forms second medium channel；
It is located in boiler-plate by spreadsheet engine；
Fuel delivery source is connected to by pipeline with by spreadsheet engine, and oxygen supply source and engine charge supply source pass through pipe respectively
Road is connected to the entrance in second medium channel, and the outlet in second medium channel is connected by pipeline with by the air inlet of spreadsheet engine
Logical, alcohol supply source is connected to by pipeline with the entrance in first medium channel after igniter, the supply of injector active flow
Source is connected to by pipeline with exhaust injector, and exhaust injector passes through boiler-plate close to by the exhaust pipe of spreadsheet engine.
2. engine testsand according to claim 1, it is characterised in that: be connected to fuel delivery source and by spreadsheet engine
Engine fuel supply flow rate regulating valve and engine fuel supply shut-off valve are provided on pipeline.
3. engine testsand according to claim 1, it is characterised in that: connection oxygen supply source and second medium channel
Entrance pipeline on be provided with oxygen supply flow control valve and oxygen supply shut-off valve.
4. engine testsand according to claim 1, it is characterised in that: connection engine charge supply source and second is situated between
Engine charge supply pressure regulating valve is provided on the pipeline of the entrance in matter channel.
5. engine testsand according to claim 1, it is characterised in that: connection alcohol supply source and first medium channel
Entrance pipeline on be provided with alcohol supply flow rate regulating valve and alcohol supply shut-off valve, the outlet in first medium channel and outer
Boundary's connection.
6. engine testsand according to claim 1, it is characterised in that: connection injector active flow supply source and row
Injector active flow supply pressure regulating valve is provided on the pipeline of gas injection device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821618634.3U CN209027800U (en) | 2018-10-05 | 2018-10-05 | A kind of engine testsand |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821618634.3U CN209027800U (en) | 2018-10-05 | 2018-10-05 | A kind of engine testsand |
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| Publication Number | Publication Date |
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| CN209027800U true CN209027800U (en) | 2019-06-25 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201821618634.3U Active CN209027800U (en) | 2018-10-05 | 2018-10-05 | A kind of engine testsand |
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| CN (1) | CN209027800U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109141906A (en) * | 2018-10-05 | 2019-01-04 | 北京航天三发高科技有限公司 | A kind of engine testsand |
| RU2770072C2 (en) * | 2021-06-09 | 2022-04-14 | Валентин Павлович Рылов | Test bench for the pumping system for powdered metal supply to the combustion chamber of a rocket engine |
-
2018
- 2018-10-05 CN CN201821618634.3U patent/CN209027800U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109141906A (en) * | 2018-10-05 | 2019-01-04 | 北京航天三发高科技有限公司 | A kind of engine testsand |
| RU2770072C2 (en) * | 2021-06-09 | 2022-04-14 | Валентин Павлович Рылов | Test bench for the pumping system for powdered metal supply to the combustion chamber of a rocket engine |
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