CN102900660A - Test method for testing terminal efficiency of integral reciprocating natural gas compressor unit - Google Patents
Test method for testing terminal efficiency of integral reciprocating natural gas compressor unit Download PDFInfo
- Publication number
- CN102900660A CN102900660A CN2012104150155A CN201210415015A CN102900660A CN 102900660 A CN102900660 A CN 102900660A CN 2012104150155 A CN2012104150155 A CN 2012104150155A CN 201210415015 A CN201210415015 A CN 201210415015A CN 102900660 A CN102900660 A CN 102900660A
- Authority
- CN
- China
- Prior art keywords
- compressor
- natural gas
- gas
- specific heat
- calculate
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Landscapes
- Control Of Positive-Displacement Pumps (AREA)
Abstract
The invention relates to a test method for testing the terminal efficiency of an integral reciprocating natural gas compressor unit, which can effectively test the terminal efficiency of the integral reciprocating natural gas compressor unit. The invention adopts the technical scheme that the method includes the steps of: taking an appropriate amount of compressed natural gas from an output end of a compressor for gas component analysis; reading the parameters of temperature, pressure and displacement on an instrument panel of the compressor unit, working out the polytropic exponents of all stages of natural gas according to the test data, and calculating the indicated power at all stages and the gross indicated power of the compressor unit; calculating the efficiency and the shaft power at jth stage of the reciprocating compressor unit, and working out the gross shaft power of the compressor from the shaft powers at all stages; and finally substituting the gross indicated power NP and the gross shaft power NI into a formula to calculate the terminal efficiency EtaT of the compressor unit. The test method is simple and convenient, and the calculation is simple. The test method can be applied to working condition evaluation of the reciprocating compressor and for providing reference for the assessment of energy saving and consumption reducing effects of the compressor.
Description
Technical field
The present invention relates to a kind of for gas engine and compressor are shared a fuselage, a bent axle, and the test method of the integrated reciprocating formula gas compressor set compression end efficient that is arranged symmetrically.
Background technique
In petroleum chemical enterprise produces, particularly in gas industry production and the conveying, Reciprocating Natural Gas Compressor is as a kind of supercharging commonly used and gas transmission equipment, the utilization of its compression end energy consumption and the efficiency of compression end, direct relation compressor whether energy-conservation, whether be in normal working, do not have a kind of specifically and accurately test method and evaluation criterion.Theoretically, isothermal compression situation lower compression machine power consumption is economized most, final temperature is minimum, and adiabatic compression situation lower compression machine power consumption is maximum, final temperature is the highest.But compressor is a changeable compression process between isothermal compression and adiabatic compression in compression process, and its by compression impact of the factors such as machine compressed media, working environment is larger.Computational methods and the integrated type compressor of existing compressor bank compression end efficient are not inconsistent, and can not truly reflect the status of energy consumption of integrated type natural gas compressor.Therefore a kind of test method of integrated reciprocating formula gas compressor set compression end efficient is provided, significant to the operating mode evaluation of petroleum chemical industry reciprocal compressor and energy-saving and cost-reducing judgement.
Summary of the invention
The purpose of this invention is to provide a kind of method of energy Validity Test integrated reciprocating formula natural gas compressor compression end efficient, refer to that mainly gas engine and compressor share a fuselage, a bent axle, be the Reciprocating Natural Gas Compressor group that symmetrical balance distributes.
Integrated reciprocating formula gas compressor set is by gas engine power to be input to bent axle, to have bent axle to drive the acting of compressor piston pressurized gas again.The air horsepower N of input compression end
IComprise compressor compresses gas indicated power N
P, mechanical wear wasted power, heat transfer and leakage loss power, compressor indicated power refers to the power of compressed natural gas in the compressor unit time, so the efficient of unit compression end is the indicated power N of compressor compresses gas
PWith compressor shaft power N
IThe ratio.Compressor bank field test data substitution formula (1) is calculated unit compression end efficient;
In the formula, η
T-unit compression end efficient, %; N
P-multistage compression indicated power sum, kW; N
I-compressor shaft power, kW; The method can be used for the measuring and calculation of multistage compressor compression end efficient.
The present invention adopts following technological scheme: a kind of test method of integrated reciprocating formula gas compressor set compression end efficient, it is characterized in that by compressed natural gas makings component in the test compression unit and compressor operating load, obtain unit compression indicated power at different levels and air horsepower, then obtained the efficient of compressor bank compression end by formula (1).
Test method of the present invention and step are:
(1) compressed natural gas makings is analyzed, and gets an amount of rock gas at compressor output end with seal container and carries out the component of natural gas analysis, obtains compressed natural gas makings analysis report.The makings analysis report mainly comprises compressed natural gas component molar percentage, compressibility factor Z, hydrogen sulfide content, carbon dioxide content, relative density S
G, critical temperature
Critical pressure
Air content and total sulfur content.
(3) compressor operating load test, test unit compression cylinder inlet temperature T at different levels
J1, delivery temperature T
J2, suction pressure p
J1, exhaust pressure p
J2And air displacement q
JV
What test instrumentation was arranged on the compressor bank instrument panel during test can directly read air inlet/delivery temperature, air inlet/exhaust pressure and compressor air-discharging amount; Unit instrument panel data read incomplete employing infrared radiation thermometer and directly measure air inlet/delivery temperatures at different levels, test air inlet/exhaust pressure at different levels at the preformed hole place, with ultrasonic flowmeter test compression gas discharge.
Test data substitution formula (2) is calculated rock gas polytropic index k at different levels
j
k
j=c
p/c
V (2)
In the formula, c
pThe specific heat at constant pressure kJ/ of-rock gas (kg ℃), c
VThe specific heat at constant volume kJ/ of-rock gas (kg ℃).Rock gas specific heat at constant pressure c wherein
p, rock gas specific heat at constant volume c
VCalculated by following formula;
In the formula,
The specific heat at constant pressure of-rock gas under reference pressure, kJ/ (kg ℃); Δ c
p, Δ c-real gas specific heat capacity corrected value, according to the equivalent reduced pressure
With the equivalent reduced temperature
Value is looked into from the real gas specific heat capacity correction chart of SY/T6637-2005 appendix B, C and is got.
The specific heat at constant pressure under the reference pressure wherein
Calculated by following formula:
In the formula, T
J2-Di j stage compressor rock gas delivery temperature, ℃; S
G-rock gas relative density.
In the formula,
-rock gas critical pressure, MPa; p
J2-Di j level compression cylinder exhaust pressure, MPa; T
J2-Di j level compression cylinder delivery temperature, K;
The critical temperature of-rock gas, K.The rock gas critical pressure
Critical temperature
Measured by the makings analysis report.
Test data substitution formula (3) is calculated unit indicated power at different levels,
In the formula, p
J1-Di j stage compressor rock gas suction pressure, MPa; q
Jv-inlet air conditions lower compression machine discharge capacity, m
3/ min; Z
J1/ Z
J2-being respectively the Gas Compression Factor under air inlet/exhaust conditions, computational methods can be with reference to GB/T17747; k
jThe rock gas polytropic index of-Di j level.
The total indicated power N of multistage compressor
PNamely indicated power N at different levels
PjAlgebraic addition, i.e. N
p=∑ N
Pj
Test data substitution formula (4), formula (5) are calculated compressor air horsepower at different levels and efficient:
In the formula, η
j-reciprocal compressor j stage efficiency, %; T
J1-Di j stage compressor rock gas intake temperature, K; The total air horsepower N of compressor
IAir horsepower N at different levels
IjAlgebraic addition, i.e. N
I=∑ N
Ij
And then calculate Reciprocating Natural Gas Compressor group compression end efficient by formula (1).
The invention has the beneficial effects as follows: easy, the safety of (1) test method of the present invention, calculate simply, when carrying out routine and patrol and examine inspection, compressor bank all can carry out; (2) test instrument is simple, easy to operate, economic and practical; (3) calculating of compression end energy consumption efficiency can be compressor management person and provides evaluation criterion to compressor operating, economic scene, for units consumption analysis and reducing energy consumption provide reference frame, also for gas industry is efficient, energy-saving run provides a kind of determination methods.
Embodiment
The below is described further test method of the present invention.
Before selected gas compressor set is tested, need carry out the collection of unit basic data, comprise size, the piston stroke of well station name, equipment model, unit rated power, rated speed, number of compression stages, compression cylinder cylinder diameter, single double-action of compression cylinder etc.
The tester is carried out safety education, and the personnel that take one's test should through training, take appointment with certificate; The major parameter such as each stage pressure, temperature, flow that should guarantee compressed natural gas in the test process carries out synchronism detection, and test parameter repeats to read more than three times, per 10 minutes readings once, the parameters that measures is calculated with arithmetic mean value.Reference temperature: 20 ℃; Reference pressure (absolute pressure): 101.3kPa.
The concrete testing procedure of test method of the present invention is as follows:
(1) compressed natural gas makings component analysis, get an amount of pressurized gas at compressor output end with seal container and carry out the natural gas quality component analysis, according to GB/T13610 " composition analysis-gas chromatography of rock gas " requirement, record the natural gas quality analysis report.Report content comprises presses gas component content: methane (mol%), ethane (mol%), propane (mol%), isobutane (mol%); Normal butane (mol%), isopentane (mol%), pentane (mol%), hexane above (mol%), carbon dioxide (mol%), nitrogen (mol%), helium (mol%), hydrogen (mol%); And heavy hydrocarbon total amount (%), compressibility factor, basic low heat value (MJ/m
3), hydrogen sulfide (g/m
3), relative density, critical temperature (K), critical pressure (MPa), air content (%), total sulfur content (mg/m
3) and water dew point (℃).
(2) compressor operating load test has compression cylinder inlet temperature T at different levels in the compressor operating load test
J1, delivery temperature T
J2, suction pressure p
J1, exhaust pressure p
J2And compressor displacement q
JVConcrete testing procedure is:
1) the unit time compressed natural gas measures examination
Unit time compressed natural gas amount should directly be enrolled the compressed natural gas tolerance of compressor measuring instrument indication.If compressor is not equipped with compressed natural gas tolerance measuring instrument, adopt the ultrasonic gas flowmeter test traffic, test position should be selected on the admission line straight length, and flow development length is no less than 30 times of calibers of institute's test tube line.Directly be attached on the pipeline straight length with ultrasonic flowmeter sensor during test, sensed flow meter reading behind the 15min reads a secondary data every 10min, averages as calculated data.
2) compression cylinder rock gas intake temperature/delivery temperatures at different levels, suction pressure/exhaust pressure test
Can directly read compression cylinder inlet/delivery temperatures at different levels, air inlet/exhaust pressure for what unit compression cylinder inlet/delivery temperatures at different levels, air inlet/exhaust pressure had a measuring instrument.Can be with infrared radiation thermometer to air inlets at different levels/delivery temperature test for the compressor bank that compression cylinder inlet/delivery temperature monitoring is incomplete.The position of temperature test and pressure test require:
1. compression cylinder inlet temperature at different levels position before the compression cylinder after knock out drum measures.
2. compression cylinder delivery temperatures at different levels position before the knock out drum after compression cylinder measures.
3. compression cylinder rock gas suction pressures at different levels are directly enrolled the field instrument designation data.
Begin test until the stable rear 15min of unit, with above-mentioned data every the 10min test once, test is averaged and is got off as data logging to be calculated more than three times, finishes whole testing process.
Test data substitution formula (2) is calculated rock gas polytropic index k at different levels
j
Test data substitution formula (3) is calculated unit indicated power N at different levels
PjThe total indicated power N of multistage compressor
PBe indicated power N at different levels
PjAlgebraic sum.
Test data substitution formula (4), formula (5) are calculated compressor air horsepower N at different levels
IjThe total air horsepower N of compressor
IBe air horsepower N at different levels
IjAlgebraic sum.
By test and the total air horsepower N of calculating compressor bank
IWith total indicated power N
PDraw Reciprocating Natural Gas Compressor group compression end efficiency eta by formula (1) afterwards
T
Embodiment: integrated reciprocating formula gas compressor set compression end efficiency test calculated examples
1 certain well station unit compression end efficiency test data
1.1 the test data of certain well station unit comprises the analysis of compressed natural gas matter: atmospheric pressure 95.6kPa; Gas component: methane 97.46mol%, ethane 1.23mol%, propane 0.16mol%, isobutane 0.031mol%; Normal butane 0.023mol%, isopentane 0.011mol%, pentane 0.007mol%, the above 0.02mol% of hexane, carbon dioxide 0.73mol%, nitrogen 0.27mol%, helium 0.011mol%, hydrogen 0.004mol%.Compressibility factor 0.998; Relative density: 0.571; Critical temperature 193.2K; Critical pressure 4.622Mpa; Air content 0.05%; Rock gas molal weight 18.926kg/kmol.
1.2 compressor operating load test data: this compressor bank is the one-level compression, and compressor is processed tolerance 9323m
3/ h(mark), 26 ℃ of Compressor Inlet Temperatures, 92 ℃ of outlet temperatures; Inlet pressure 1.18MPa, outlet pressure 2.59MPa.
2 integrated reciprocating formula gas compressor set compression end efficiency calculation
2.1 test data substitution formula (2) gets rock gas polytropic index k
j:
(1) the rock gas relative density is S
G=0.571.
(5) the specific heat at constant pressure value c of rock gas
p, specific heat at constant volume c
VThrough tabling look-up and calculating:
C
p=2.54(kJ/kg·K),C
v=1.95(kJ/kg·K)
(6) above test data and result of calculation substitution formula (2) are got rock gas polytropic index k:
k=c
p/c
V=1.30
2.2 the 1st grade of flow, air inlet/exhaust pressure test parameter substitution formula (3) are got the 1st grade of indicated power N of compressor
P1:
The indicated power N that compressor is total
PFor:
N
P=∑N
pj=247.07(kW)
2.3 the 1st grade of air inlet/delivery temperature, air inlet/exhaust pressure test data substitution formula (5) are got reciprocal compressor the 1st stage efficiency η
1:
2.4 calculate compressor j level air horsepower N by formula (4)
Ij:
The total air horsepower N of compressor
IFor:
N
I=∑N
ij=277.88(kW)
2.5 above test result substitution formula (1) is calculated compressor bank compression end efficiency eta
T:
Claims (2)
1. the test method of an integrated reciprocating formula gas compressor set compression end efficient, it is characterized in that: get an amount of compressed natural gas at compressor output end with seal container first and carry out the component of natural gas analysis, its component of natural gas analysis report comprises natural gas quality component molar percentage, compressibility factor Z, hydrogen sulfide content, carbon dioxide content, relative density S
G, critical temperature
Critical pressure
Air content and total sulfur content; Then read intake temperature T at different levels at the compressor bank instrument panel
J1, delivery temperature T
J2, suction pressure p
J1, exhaust pressure p
J2And compressor displacement q
JvAgain with test data substitution k
j=c
p/ c
VObtain rock gas polytropic index k at different levels
j, c in the formula
pBe the specific heat at constant pressure of rock gas, by
Calculate,
Be the specific heat at constant pressure of rock gas under reference pressure, by
Calculate Δ c
pBe real gas specific heat capacity corrected value, from real gas specific heat capacity correction chart, look into and get c
VFor the rock gas specific heat at constant volume, by c
V=c
p-Δ c calculates, and Δ c is real gas specific heat capacity corrected value, looks into from real gas specific heat capacity correction chart and gets; Again according to the k that records above
j, p
J1, p
J2, q
Jv, Z under the air inlet
J1, Z under the exhaust
J2Substitution
Calculate unit indicated power N at different levels
Pj, according to N
p=∑ N
PjCalculate the total indicated power N of multistage compression unit
PThen according to the T that records
J1, T
J2, p
J1, p
J2And k
j, substitution
Calculate reciprocal compressor j stage efficiency, again basis
Calculate compressor j level air horsepower N
Ij, by air horsepower N at different levels
IjAlgebraic sum is tried to achieve the total air horsepower N of compressor
I=∑ N
IjThe N that will try to achieve above at last
P, N
ISubstitution
Record Reciprocating Natural Gas Compressor group compression end efficiency eta
T
2. test method according to claim 1 is characterized in that: above-mentioned Δ c
p, Δ c real gas specific heat capacity corrected value is according to the equivalent reduced pressure
With the equivalent reduced temperature
Value is looked into from the real gas specific heat capacity correction chart of SY/T6637-2005 appendix B, C and is got; The equivalent reduced pressure
According to
Calculate the equivalent reduced temperature
According to
Calculate, wherein p
J1, p
J2,
For obtaining data in component of natural gas analysis report and the compressor bank instrument panel.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201210415015.5A CN102900660B (en) | 2012-10-26 | 2012-10-26 | Test method for testing terminal efficiency of integral reciprocating natural gas compressor unit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201210415015.5A CN102900660B (en) | 2012-10-26 | 2012-10-26 | Test method for testing terminal efficiency of integral reciprocating natural gas compressor unit |
Publications (2)
Publication Number | Publication Date |
---|---|
CN102900660A true CN102900660A (en) | 2013-01-30 |
CN102900660B CN102900660B (en) | 2014-12-10 |
Family
ID=47573082
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201210415015.5A Expired - Fee Related CN102900660B (en) | 2012-10-26 | 2012-10-26 | Test method for testing terminal efficiency of integral reciprocating natural gas compressor unit |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN102900660B (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103335682A (en) * | 2013-07-15 | 2013-10-02 | 成都千嘉科技有限公司 | Measuring method for gas flow of natural gas |
CN104895777A (en) * | 2015-05-11 | 2015-09-09 | 中国石油天然气集团公司 | Method and device for determining dynamic mechanical efficiency of compressor |
CN107882761A (en) * | 2016-09-30 | 2018-04-06 | 中国石油天然气股份有限公司 | Method for acquiring working condition parameters of natural gas long-distance pipeline centrifugal compressor |
CN112113617A (en) * | 2020-09-21 | 2020-12-22 | 江西资生科技有限公司 | Device and method for acquiring pressure and temperature in cylinder of reciprocating compressor in real time |
CN112459984A (en) * | 2020-11-13 | 2021-03-09 | 西安陕鼓动力股份有限公司 | Performance test calculation method for isothermal compressor |
CN116087613A (en) * | 2023-04-07 | 2023-05-09 | 沃德传动(天津)股份有限公司 | Reciprocating compressor energy efficiency calculation system |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030007873A1 (en) * | 2001-02-15 | 2003-01-09 | Toshiro Hattori | Screw compressor equipment for accommodating low compression ratio and pressure variation and the operation method thereof |
EP1774161B1 (en) * | 2004-08-05 | 2008-05-07 | VDO Automotive AG | Method and device for controlling an internal combustion engine |
CN101375044A (en) * | 2006-01-27 | 2009-02-25 | 里卡多英国有限公司 | A method of identifying engine gas composition |
CN101487466A (en) * | 2009-02-25 | 2009-07-22 | 华东理工大学 | On-line soft measuring method for compression ratio and polytropic efficiency of centrifugal compressor |
DE102008021102A1 (en) * | 2008-04-28 | 2009-10-29 | Siemens Aktiengesellschaft | Efficiency monitoring of a compressor |
-
2012
- 2012-10-26 CN CN201210415015.5A patent/CN102900660B/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030007873A1 (en) * | 2001-02-15 | 2003-01-09 | Toshiro Hattori | Screw compressor equipment for accommodating low compression ratio and pressure variation and the operation method thereof |
EP1774161B1 (en) * | 2004-08-05 | 2008-05-07 | VDO Automotive AG | Method and device for controlling an internal combustion engine |
CN101375044A (en) * | 2006-01-27 | 2009-02-25 | 里卡多英国有限公司 | A method of identifying engine gas composition |
DE102008021102A1 (en) * | 2008-04-28 | 2009-10-29 | Siemens Aktiengesellschaft | Efficiency monitoring of a compressor |
CN101487466A (en) * | 2009-02-25 | 2009-07-22 | 华东理工大学 | On-line soft measuring method for compression ratio and polytropic efficiency of centrifugal compressor |
Non-Patent Citations (2)
Title |
---|
张勇等: "天然气压缩机多变过程指数的研究", 《机械》, vol. 35, no. 1, 31 December 2008 (2008-12-31) * |
李宁等: "离心式压缩机多变指数的确定", 《油气储运》, vol. 28, no. 08, 31 December 2009 (2009-12-31) * |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103335682A (en) * | 2013-07-15 | 2013-10-02 | 成都千嘉科技有限公司 | Measuring method for gas flow of natural gas |
CN103335682B (en) * | 2013-07-15 | 2015-07-15 | 成都千嘉科技有限公司 | Measuring method for gas flow of natural gas |
CN104895777A (en) * | 2015-05-11 | 2015-09-09 | 中国石油天然气集团公司 | Method and device for determining dynamic mechanical efficiency of compressor |
CN104895777B (en) * | 2015-05-11 | 2017-03-22 | 中国石油天然气集团公司 | Method and device for determining dynamic mechanical efficiency of compressor |
CN107882761A (en) * | 2016-09-30 | 2018-04-06 | 中国石油天然气股份有限公司 | Method for acquiring working condition parameters of natural gas long-distance pipeline centrifugal compressor |
CN112113617A (en) * | 2020-09-21 | 2020-12-22 | 江西资生科技有限公司 | Device and method for acquiring pressure and temperature in cylinder of reciprocating compressor in real time |
CN112113617B (en) * | 2020-09-21 | 2021-07-23 | 中国石油化工股份有限公司 | Device and method for acquiring pressure and temperature in cylinder of reciprocating compressor in real time |
CN112459984A (en) * | 2020-11-13 | 2021-03-09 | 西安陕鼓动力股份有限公司 | Performance test calculation method for isothermal compressor |
CN112459984B (en) * | 2020-11-13 | 2022-05-03 | 西安陕鼓动力股份有限公司 | Performance test calculation method for isothermal compressor |
CN116087613A (en) * | 2023-04-07 | 2023-05-09 | 沃德传动(天津)股份有限公司 | Reciprocating compressor energy efficiency calculation system |
Also Published As
Publication number | Publication date |
---|---|
CN102900660B (en) | 2014-12-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN102900660B (en) | Test method for testing terminal efficiency of integral reciprocating natural gas compressor unit | |
CN102879201B (en) | Efficiency measuring method for gas engine for reciprocating natural-gas compressor unit | |
CN102937086B (en) | Method for testing system efficiency of integrated gas reciprocating natural gas compressor set | |
CN109611696A (en) | A kind of pipeline leakage testing and leak position positioning device and method | |
Serrano et al. | Importance of mechanical losses modeling in the performance prediction of radial turbochargers under pulsating flow conditions | |
CN111810395B (en) | Reciprocating compressor energy efficiency analysis system based on P-V graph test | |
CN110319982A (en) | Underground gas pipeline leak judgment method based on machine learning | |
CN206177542U (en) | Fatigue test device of engine blade | |
CN106404062A (en) | System for real-time monitoring and evaluating operation energy efficiency of industrial air compression station | |
Ren et al. | Effect of hydraulic oil compressibility on the volumetric efficiency of a diaphragm compressor for hydrogen refueling stations | |
CN111503025A (en) | Low-pressure-ratio axial flow compressor model level performance calculation method | |
CN103399227B (en) | The long-range equilibrium testing method of a kind of walking-beam pumping unit | |
CN203585824U (en) | Pipeline leakage test device | |
CN109441793B (en) | Method for obtaining p-V diagram of reciprocating compressor by measuring strain of piston rod | |
Huang et al. | Dynamic operating characteristics of a compressed CO2 energy storage system | |
Lei et al. | Investigation on performance of a compression-ignition engine with pressure-wave supercharger | |
CN204575162U (en) | A kind of measurement mechanism of automobile trunk volume | |
CN111222277B (en) | Vibration evaluation method for inlet and outlet pipelines of booster pump of gas transmission station | |
CN105466687A (en) | A usage life monitoring device used for a high and middle pressure cylinder of a frequently rapid start and stop combined cycle steam turbine | |
CN105388018A (en) | Total pressure difference airway tumble test apparatus for engine | |
CN107677482B (en) | A kind of test method of tandem pressure charging system gross efficiency | |
CN115064737B (en) | Method for monitoring hydrogen use accumulation amount of fuel cell | |
CN205670035U (en) | Filling machine device for on-site calibration | |
Dindorf | Study of the Energy Efficiency of Compressed Air Storage Tanks | |
CN106918451B (en) | System for testing oil-gas separation efficiency and test method thereof |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141210 Termination date: 20161026 |
|
CF01 | Termination of patent right due to non-payment of annual fee |