Rotor Dynamics Test Facility

About

The Rotor Dynamics Test Facility (RDTF) is a cutting-edge system designed for evaluating the performance and behavior of Rotor-Bearing-Support systems under various configurations such as simply supported, overhung, and twin-rotor setups. It enables detailed analysis of critical speeds, vibrations, unbalance, misalignment, and damping, with advanced features like high-speed drive systems, precision lubrication, axial loading mechanisms, and real-time data acquisition through PLC-SCADA integration. Supporting rotors up to 90 kg and speeds up to 52,000 rpm, the facility provides robust safety measures, including protective enclosures and automated fault detection.
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Technical Details

  • Test Bench supporting structure
  • Two drive Systems
  • Two step up Gear Boxes with lubrication system
  • Two low speed couplings and two high speed couplings
  • Four instrumented pedestals
  • Oil system to supply/scavenging oil to/ from Test rotor Bearings
  • Measurement, control and safety system
  • Control console
  • Axial and Lateral loading system
  • Safety enclosure

To test the behaviour of Aircraft Rotor System by varrying the different test parameter like Speed variation (0 to 55000 RPM), Unbalance response to excessive unbalance, The response due to misalignment, Experimental validation of damping etc.

Key Features

  • To Test the different type of Aircraft Rotor
  • To Test the behaviour of Rotor due to Axial Loading System
  • To Test the behaviour of Rotor due to Lateral Misalignment System
  • To Test the behaviour of Rotor due to change in pressure and flow of bearing lubrications system
  • Critical speed validation of Rotor System at different operating speed

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Details


The Rotor Dynamics Test Facility (RDTF) is an advanced engineering system meticulously designed to evaluate the functional and operational characteristics of Rotor-Bearing-Support systems. Developed for AERDC, HAL Bangalore, this facility enables in-depth testing of rotor dynamics—an essential branch of mechanical engineering focused on understanding and analyzing the behavior of rotating machinery. Rotors are critical components in applications such as aircraft engines, turbines, compressors, and generators, where their performance significantly impacts efficiency, safety, and reliability.

Rotor Dynamics encompasses the study of vibrations, critical speeds, unbalance, stability, and misalignment in rotating systems. By testing these factors under controlled conditions, the RDTF provides invaluable insights into the performance, durability, and dynamic stability of rotors and their supporting systems.

This facility includes comprehensive features such as drive systems, measurement and control systems, lubrication units, and axial loading systems. It supports multiple rotor configurations, enabling users to simulate and analyze real-world operating conditions.

Key Features and Capabilities

1. Versatile Test Configurations
The facility supports a wide range of testing setups, accommodating varying rotor geometries, sizes, and operating conditions:
- Shaft Diameters: Supports rotors with diameters ranging from 15 mm to 70 mm.
- Rotor Mass: Capable of testing rotor weights up to 90 kg with polar inertia of up to 1 kgm².
- Disc Sizes: Accommodates rotors with disc diameters of up to 750 mm.
- Support Types: Adapts to both rigid and flexible support systems, with options for damping mechanisms such as squeeze film dampers and elastomeric dampers.
- Configurations: Includes simply supported, overhung (single and double sides), and twin-rotor systems with inter-shaft bearings.

2. Comprehensive Testing Infrastructure
- Test Bench Base Structure: 
  The mechanical structure is optimized to minimize vibrations and external excitations, ensuring stable operation. 
  Designed for efficient use of space, the bench incorporates advanced instrumentation for vibration monitoring.
- Drive System: 
  The facility features two variable-speed AC drive systems rated at 60 kW and 200 kW, offering:
- Speed Control: Encoder feedback for precise speed regulation within 0.1% of nominal speed.
- Dynamic Braking: Regenerative braking for enhanced safety and energy efficiency.
- High Acceleration: Maximum acceleration rate of 100 rpm/s to replicate real-world conditions.
- Step-Up Gearboxes: 
  Two step-up gearboxes increase the rotor speed to 41,000 rpm and 52,000 rpm, with 5% over-speed margins, ensuring compatibility with high-performance applications.
- Couplings: 
  The facility includes low-speed and high-speed couplings designed for seamless power transmission while minimizing misalignment and vibration.

3. Integrated Measurement and Control Systems
The facility employs advanced instrumentation for real-time monitoring and analysis:
 - Sensors and Signal Conditioning: Includes accelerometers, proximity probes, RTD temperature sensors, and high-speed tachometers for comprehensive data acquisition.
 - Vibration Analysis: Equipped with optional FFT analyzers, offering capabilities such as:
 - Frequency and order spectrum analysis.
 - Waterfall plots, Bode plots, polar plots, and orbits.
 - Shaft centerline tracking and transient capture.
 - PLC-SCADA Integration: Allows for automated and manual control of test operations, with safety interlocks, alarms, and data logging. 
   Operators can configure tests through a user-friendly interface.

4. High-Performance Oil and Axial Loading Systems
- Lubrication System: 
- Delivers up to 20 liters per minute at 15 bar pressure.
- Compatible with aerospace-grade oils such as MIL-E-23699/7808.
- Features water-cooled heat exchangers for maintaining oil temperatures within a range of 15°C to 150°C.
- Axial Loading System: 
- Applies thrust loads of up to 20 kN using a double-acting hydraulic actuator.
- Ensures precise load application through integrated load cells and remote control via the SCADA interface.

5. Safety and Ergonomics
- Protective Enclosure: 
- Industrial-grade laminated safety glass provides robust protection against debris while ensuring operator visibility.
- Designed to contain high-energy failures, ensuring personnel safety during high-speed tests.
- Control Console: 
- Includes dual operator PCs for data acquisition and test configuration.
- Emergency stop mechanisms and fault detection systems for enhanced safety.

Applications
The Rotor Dynamics Test Facility supports various critical testing scenarios, including:
1. Critical Speed Validation: Identifying resonance points to optimize rotor design.
2. Unbalance Response Testing: Analyzing the rotor's reaction to both residual and excessive unbalance as per ISO 1940 G2.5 standards.
3. Misalignment Testing: Simulating angular and offset misalignments to understand their impact on performance.
4. High-Speed Balancing: Ensures rotors can operate at speeds up to 42,000 rpm without introducing vibration-related failures.
5. Damping Analysis: Evaluates the effectiveness of dampers under dynamic conditions.

Technical Specifications

Maximum Speed :       Up to 52,000 rpm 
Rotor Diameter :      15 mm to 70 mm 
Rotor Mass :          Up to 90 kg  
Power :               200 kW (maximum) 
Oil Flow :            20 L/min at 15 bar pressure
Temperature Range :    15°C to 150°C  
Safety Standards :      EN 1063:1999 for enclosures 

Delivery and Support

- Design and Documentation: Comprehensive design reports, operating manuals, and schematics.
- Training: Operator training on system usage, safety protocols, and data analysis.
- Warranty and Maintenance: A standard 12-month warranty with options for extended support for up to 3 years.
- Commissioning: Full installation and testing of the facility at the HAL premises, ensuring operational readiness.

Conclusion

The Rotor Dynamics Test Facility sets a new benchmark in the field of rotor dynamics analysis. Its advanced capabilities, versatile configurations, and robust safety measures make it an indispensable asset for industries and research institutions involved in the design and development of high-performance rotating machinery.

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