Two Shaft Gas Turbines Manufacturer,Supplier and Exporter in India

Two Shaft Gas Turbines

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.

 

   

Office Address

Works: #975 Malleshwaram,
Bengaluru, Karnataka 560003

[email protected]

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