Two Shaft Gas Turbines Manufacturer,Supplier and Exporter in India
Product Code : SCL-CELE-13929
This experimental Biogas Plant is a sophisticated,
laboratory-scale system designed to demonstrate and investigate the complete
process of anaerobic degradation and biogas generation. Its two-stage
configuration and integrated PLC control allow for comprehensive
study of the parameters influencing biogas yield and quality.
The plant simulates an industrial biogas process using a
two-stage (dual stage) method for optimized control over the degradation
phases. It supports both continuous and discontinuous (batch) operation
modes.
|
Stage |
Reactor |
Substrate Process |
Key Control Parameters |
Capacity |
|
Stage 1 |
Stirred Tank Reactor 1 |
Hydrolysis and Acidification
(Conversion of long-chain organic substances into short-chain organic
substances). |
Temperature and pH value are
individually controlled. |
Approx. 20L |
|
Stage 2 |
Stirred Tank Reactor 2 |
Methane Formation (Last step of anaerobic
degradation; generation of biogas, primarily methane and carbon dioxide). |
Temperature and pH value are
individually controlled. |
Approx. 70L |
- Substrate
Supply: A separate supply unit includes a 25L substrate tank
with a stirring machine (maximum 200 revolutions per minute) and peristaltic
feed pumps (maximum 25 L per hour flow rate).
- Digestate
Collection: A 25L digestate tank collects the final
product.
- pH
Regulation: Two metering pumps (maximum 2.1 L per
hour each) are provided for precise addition of acid and caustic to
control the pH in both reactors.
- Temperature
Control: A dedicated heating water circuit (with a tank,
heater, temperature controller, and pump - maximum 480 L per hour
flow rate) manages the thermal environment of the reactors.
Instrumentation and Data Analysis
The plant is fully instrumented for extensive biogas and process
analysis, with a central control system for operation and data logging.
Control and Monitoring
- System
Control: Controlled by a PLC (Programmable Logic
Controller).
- Operation: Via a
touch screen interface.
- Data
Acquisition: Measured values are transmitted to a PC via USB
(Optional software for Windows 7, 8.1, 10).
Biogas Analysis Specifications
|
Parameter |
Sensor Type |
Measuring Range |
|
Biogas Quality |
Sensors |
Methane content: 0 to 100 percent |
|
Carbon dioxide content: 0 to 100 percent |
||
|
Biogas Flow |
Flow Meter |
0 to 30 NL per hour (Normal Liters per hour) |
|
Biogas Treatment |
Drying Column |
Biogas is dried with silica gel to measure Humidity
(0 to 100 percent range). |
|
Process Control |
Sensors |
pH value: 2x 1 to 14 (in each reactor) |
|
Temperature (reactors and biogas): 3x 0 to 100 deg C |
Core Experiment Capabilities
The system allows students to conduct practical experiments
on process optimization and performance evaluation of biogas technology:
- Operating
State Stability: Achieving and maintaining a stable operating
state in both single-stage and dual-stage configurations.
- Parameter
Influence Studies: Investigating how key factors impact biogas
generation:
- Temperature
- Substrate type
(e.g., maize, potatoes)
- Volumetric
loading
- pH
value
- Operation
Mode Comparison: Analyzing the influence of different modes on biogas
yield:
- Single
stage versus dual stage
- With
and without post-fermentation (by utilizing the digestate
tank)
- Continuous
versus discontinuous (batch) operation
- Performance
Determination: Quantifying key output parameters based on
operating conditions:
- Biogas
yield
- Biogas
flow rate
- Biogas
quality (Methane and Carbon Dioxide content)
The system's core is a gas generator connected to a power
turbine on a separate shaft, enabling the study of two-shaft performance
characteristic of vehicle, ship, or generator drives.
1. Gas Generator (High Pressure Turbine)
- Components:
Radial compressor, tubular combustion chamber, and a radial turbine
mounted on a single shaft (Turbine 1).
- Speed
Range: 70,000 to 90,000 revolutions per minute (Maximum
speed limit is 92,500 revolutions per minute).
- Fuel: Propane
gas, with a maximum consumption of 20 kg per hour.
- Performance:
Maximum compression ratio of 2:1.
- Starting: A
computer-controlled start-up fan is used for starting and gas
sweep.
2. Operation Modes (Two-Shaft vs. Jet Engine)
|
Mode |
Arrangement |
Energy Conversion |
Key Measurement |
|
Power Turbine |
Two-shaft arrangement |
Exhaust gas energy is converted into mechanical energy by
the free-running power turbine (Turbine 2). |
Electrical power output (0 to 200 Watts) from the
asynchronous generator/motor. |
|
Jet Engine |
Single-shaft arrangement |
Exhaust gas is accelerated and transformed into thrust
via a propelling nozzle. |
Thrust measurement (force sensor) from 0 to 50 N. |
3. Power Generation & Load
- Power
Turbine Speed: 15,000 to 25,000 revolutions per minute
(Maximum 42,600 rev per minute
- Generator:
Asynchronous motor with a frequency converter acts as a generator.
- Load:
Generated electrical energy is converted into heat using four 600W
braking resistors.2
Sensors and Instrumentation
The system is extensively instrumented with sensors
and a PLC (Programmable Logic Controller) for precise, real-time data
acquisition via USB and the optional 'Sci-Cal' software.3
|
Parameter |
Type/Quantity |
Measurement Range |
|
Temperature |
8 “K” type sensors (0.1 deg C resolution) |
0 to 1100 deg C (Gas path and oil circuit) |
|
Speed |
2 sensors (for each turbine shaft) |
0 to 200,000 revolutions per minute |
|
Pressure |
5 Pressure sensors 02 |
Measures fuel, combustion chamber, compressor inlet/outlet,
and turbine outlet. |
|
Air/Gas Flow |
2 Flow sensors |
Inlet/Outlet Air/Gases: 0 to 3000 cubic meters per hour |
|
Thrust Force |
Load cell/Force sensor |
0 to 50 N (Newtons) |
|
Lubrication System |
Gear pump, filtration, heat exchangers |
Comprehensive monitoring of the essential oil cooling and
filtration loop. |
Core Experiment Capabilities
The laboratory unit facilitates critical experiments for
understanding thermal machines and propulsion:
- System
Performance: Investigation of the function and typical
behavior during operation of a gas turbine in both power turbine and
jet engine modes.
- Efficiency
Analysis: Determining thermal, isentropic, and mechanical
efficiencies across the components.
- Key
Metrics: Determining effective power, thrust
measurement, specific fuel consumption, and pressure losses
and ratios across the compressor and turbine.
- Characteristic
Recording: Recording the characteristic curves (e.g., speed
vs. power) of the power turbine.
- Exhaust
Emissions Analysis: Measuring key emission components in the exhaust
gas, including CO2, CO, NO, NO2 (NOx), and SO2.
