200M 400M 200M
RNG: 2.4 KM
BRG: 047°
ALT: 3,200 FT
SPD: 480 KTS
HDG: 012° N
TGT: ALPHA-7
MODE: SEARCH
PWR: NOMINAL
FREQ: X-BAND
STATUS: LOCK
NAVTGTWPNDEFRDRCOM
MIL-STD-1553IFF: ACTIVELINK-16: SYNC
SECTOR: ALPHA
THREAT: CLEAR
RADAR: ACTIVE
TRACK: 6 TGT
LAT 28.6213°N LON 77.3873°E
NX
Neometrix Target Acquired
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Rotor‑Bearing‑Support Systems / Indian Aero‑Engine R&D Programme / MIL‑E‑23699/7808 · EN 1063:1999 · ISO 1940 / Noida · India 2026 · Product Page
RDTF · UP TO 52,000 RPM

Rotor‑bearing dynamics, characterised to 52,000 rpm.

A cutting-edge test facility for evaluating Rotor-Bearing-Support systems across simply-supported, overhung, and twin-rotor configurations. Critical speed, unbalance response, misalignment and damping — measured on rotors up to 90 kg with real-time PLC-SCADA data acquisition.

Representative render — rotor dynamics test facility: twin-motor drive lines with step-up gearboxes on a T-slotted cast bed, instrumented pedestals carrying a multi-disc test rotor, and a polycarbonate safety enclosure
Fig · 01 Twin-drive rotor test bench · instrumented pedestals P1/P2 · polycarbonate safety enclosure (representative render)
Qualification testing supported to:
DEF STAN STANAG MIL-SPEC DO-160
Max.Speed
52K RPM
Rotor Mass
90kg
Shaft Dia.
15–70mm
Drive Power
200kW
Axial Load
20kN
01
Overview

Rotor dynamics is not a simulation problem.

Rotors are the critical, high-consequence component in aircraft engines, turbines, compressors, and generators — and their dynamic behaviour under real running conditions cannot be fully predicted on paper. Vibration, critical speed, unbalance, and misalignment have to be measured on hardware, at speed, under load.

Representative render — instrumented rotor pedestals with bearing housings carrying a multi-disc test rotor on a T-slotted bed, proximity-probe cabling and safety enclosure behind
Fig · 02 Test section · instrumented pedestals and disc-pack rotor on the T-slot bed (representative render)

The Rotor Dynamics Test Facility (RDTF) is an advanced engineering system built by Neometrix for an Indian aero-engine research & development centre, to evaluate the functional and operating characteristics of Rotor-Bearing-Support systems. It enables detailed analysis of critical speeds, vibrations, unbalance, misalignment, and damping across simply-supported, overhung (single and double-sided), and twin-rotor configurations with inter-shaft bearings.

The facility supports rotors up to 90 kg with shaft diameters from 15 to 70 mm and disc diameters up to 750 mm, running at speeds up to 52,000 rpm. Two variable-speed AC drive systems, step-up gearboxes, precision lubrication, axial and lateral loading, and a protective safety enclosure round out a complete test-bench package.

Real-world validation of rotor behaviour, beyond what simulation alone can provide — reducing failure risk before a rotor ever reaches service.

Real-time data acquisition through PLC-SCADA integration gives operators automated control, safety interlocks, alarms, and detailed logging — with dual operator PCs for test configuration and monitoring inside the control console.

02
Architecture

Six subsystems, one test bench.

The facility is built around a generic Rotor-Bearing-Support test set-up, covering both-sides overhung, simply-supported, and one-side-overhung arrangements. Every subsystem below is designed, integrated, and controlled from a single console.

Sub · 01

Control of Operation

Dual AC drive systems up to 200 kW with encoder feedback, regenerative braking, and acceleration up to 100 rpm/s. Step-up gearboxes take output speed to 41,000 and 52,000 rpm with 5% overspeed margin.

Sub · 02

Data Acquisition

PLC-SCADA integration with accelerometers, proximity probes, RTDs, and high-speed tachometers. Optional FFT analysis: frequency/order spectra, waterfall and Bode plots, orbits, and shaft centreline tracking.

Sub · 03

Rotor Dynamics Test Measurement

Four instrumented pedestals support simply-supported, overhung, and twin-rotor configurations with inter-shaft bearings, squeeze-film and elastomeric damping options.

Sub · 04

Oil / Heating / Cooling System

Up to 20 L/min at 15 bar, compatible with aerospace-grade MIL-E-23699/7808 oils. Water-cooled heat exchangers hold oil temperature between 15°C and 150°C.

Sub · 05

Axial Loading

Double-acting hydraulic actuator applies thrust loads up to 20 kN, with integrated load cells and remote control from the SCADA interface.

Sub · 06

Test Enclosure

Industrial-grade laminated safety glass enclosure to EN 1063:1999, containing high-energy failures while preserving operator visibility of the running rotor.

03
Test Configurations

Three rotor layouts, fully instrumented.

The bench adapts to real rotor-support arrangements rather than forcing a single generic layout — with rigid and flexible support options and damping mechanisms for each.

CFG · 01

Simply Supported

Classic two-bearing arrangement for baseline critical-speed and unbalance-response measurement, with rigid or flexible (squeeze-film / elastomeric damper) support options.

Baseline Vibration · Critical Speed
CFG · 02

Overhung (Single / Double-Sided)

Cantilevered disc arrangements replicating overhung turbine and compressor stages, up to 750 mm disc diameter and 1 kgm² polar inertia.

Cantilever Bearing Analysis
CFG · 03

Twin-Rotor with Inter-Shaft Bearing

Dual-rotor systems sharing an inter-shaft bearing, for aero-engine-representative dynamics — two independent drive lines feeding a shared coupling span.

Aero-Engine Representative
Rotor Dynamics Test Facility engineering drawing — pillow block unit, shaft, rotor disc, ball bearing, spacer and circlip labelled components
Fig · 04 Rotor-support component detail · pillow-block bearing unit, test shaft, rotor disc and locating hardware

Instrumented pedestals & bearing hardware

Four instrumented pedestals carry the test rotor on precision pillow-block bearing units with deep-groove ball bearings, located by spacers and circlips on the test shaft. Rotor discs are mounted between the pedestals, with the coupling span sized to the configuration under test.

Low-speed and high-speed couplings connect each drive line into the test shaft while minimising misalignment and vibration transmission back into the motor and gearbox. Two step-up gearboxes with dedicated lubrication systems bring drive speed up to the required test speed for each rotor mass and shaft diameter combination.

04
Test Capabilities

Five protocols. Complete rotor characterisation.

From critical-speed identification through high-speed balancing — the facility runs structured test sequences with automatic data logging on every channel via the PLC-SCADA system.

T · 01

Critical Speed Validation

Identifies resonance points via whirl maps and resonance-frequency analysis across the full speed range (0–55,000 rpm), to optimise rotor design before service.

Whirl Maps · Resonance Frequency
T · 02

Unbalance Response Testing

Analyses the rotor's reaction to residual and excessive unbalance per ISO 1940 G2.5, capturing vibration amplitude and phase response across the speed sweep.

ISO 1940 G2.5
T · 03

Misalignment Testing

Simulates angular and offset misalignment between coupling stages to quantify its impact on vibration, load, and bearing response.

Angular & Offset Misalignment
T · 04

High-Speed Balancing

Verifies rotors can operate at speeds up to 42,000 rpm without introducing vibration-related failures, supporting production balancing sign-off.

Up to 42,000 RPM
T · 05

Damping Analysis

Evaluates the effectiveness of squeeze-film and elastomeric dampers under dynamic conditions, validating damping design choices experimentally rather than analytically.

Squeeze-Film · Elastomeric Dampers
05
General Arrangement

Top, front, side, isometric.

The exact twin-drive arrangement Neometrix ships — two AC motors, step-up drive line, instrumented coupling span, and polycarbonate safety enclosure on a common T-slot base.

Rotor Dynamics Test Facility general arrangement drawing — top view, isometric view, front view and side view of twin-motor test bench
Fig · 05 GA drawing · top / isometric / front / side views · twin-motor rotor test bench on T-slot base
07
Downloads

Drawings & catalog.

General arrangement drawings and capability sheet for the Rotor Dynamics Test Facility, available as PDF.

08
Specifications

Full technical parameters.

Key system parameters for the standard Rotor Dynamics Test Facility configuration, as delivered to an Indian aero-engine research & development centre.

System TypeRotor Dynamics Test Facility (Rotor-Bearing-Support Test System)
Maximum SpeedUp to 52,000 rpm  ·  Speed variation range 0–55,000 rpm
Rotor MassUp to 90 kg  ·  Polar inertia up to 1 kgm²
Shaft Diameter15 mm to 70 mm
Disc SizeUp to 750 mm diameter
Support ConfigurationsSimply supported · Overhung (single & double-sided) · Twin-rotor with inter-shaft bearing
Damping OptionsRigid supports · Squeeze-film dampers · Elastomeric dampers
Drive SystemTwo variable-speed AC drives — 60 kW and 200 kW · Encoder feedback within 0.1% of nominal speed
AccelerationUp to 100 rpm/s · Regenerative dynamic braking
Step-Up GearboxesTwo gearboxes — output to 41,000 rpm and 52,000 rpm · 5% over-speed margin
CouplingsLow-speed and high-speed couplings, sized to minimise misalignment and vibration
PedestalsFour instrumented pedestals · precision pillow-block bearing units · deep-groove ball bearings
InstrumentationAccelerometers · Proximity probes · RTD temperature sensors · High-speed tachometers
Vibration AnalysisOptional FFT analyzer — frequency/order spectra, waterfall & Bode plots, polar plots, orbits, shaft centreline tracking, transient capture
Control SystemPLC-SCADA integration · Automated & manual operation · Safety interlocks, alarms, data logging
Lubrication SystemUp to 20 L/min at 15 bar · Compatible with MIL-E-23699 / MIL-E-7808 aerospace oils
Oil Temperature Range15°C to 150°C · Water-cooled heat exchangers
Axial LoadingUp to 20 kN · Double-acting hydraulic actuator · Integrated load cells · SCADA remote control
Safety EnclosureIndustrial-grade laminated safety glass · Compliant to EN 1063:1999
Control ConsoleDual operator PCs · Emergency stop · Automated fault detection
Reference StandardsISO 1940 G2.5 (unbalance) · MIL-STD · IS · EN 1063:1999 (enclosures)
WarrantyStandard 12-month warranty · Extended support available up to 3 years
09
Applications

Where it runs.

Aerospace and defence rotor-bearing qualification, turbomachinery R&D, and industrial rotating-equipment reliability programmes.

A · 01Aircraft rotor system testing — speed variation from 0 to 55,000 rpm
A · 02Critical speed validation and resonance identification for new rotor designs
A · 03Unbalance response testing to ISO 1940 G2.5, including excessive-unbalance excitation
A · 04Misalignment response testing — angular and offset misalignment simulation
A · 05Experimental validation of squeeze-film and elastomeric damping
A · 06High-speed rotor balancing up to 42,000 rpm
A · 07Turbomachinery, turbine, compressor and generator rotor R&D
A · 08Defence and aerospace rotor qualification programmes
A · 09Automotive and railway rotating-machinery vibration studies
A · 10Power generation and oil & gas high-speed rotating equipment testing
10
In Depth

The complete technical read.

Engineering narrative for rotor-dynamics engineers, procurement teams, and QA managers who want the full picture before committing to a test programme.

Why rotor dynamics testing matters

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 an Indian aero-engine research & development centre, 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. The facility includes comprehensive features such as drive systems, measurement and control systems, lubrication units, and axial loading systems, and supports multiple rotor configurations for simulating real-world operating conditions.

1. Versatile test configurations

The facility supports a wide range of testing set-ups, 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 via encoder feedback for precise speed regulation within 0.1% of nominal speed, dynamic braking through regenerative braking for enhanced safety and energy efficiency, and high acceleration at a maximum 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 frequency and order spectrum analysis, waterfall plots, Bode plots, polar plots, and orbits, plus shaft centreline 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 litres per minute at 15 bar pressure. Compatible with aerospace-grade oils such as MIL-E-23699 / MIL-E-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, and is 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, plus emergency stop mechanisms and fault detection systems for enhanced safety.

Applications

The Rotor Dynamics Test Facility supports various critical testing scenarios, including:

  • Critical speed validation: Identifying resonance points to optimize rotor design.
  • Unbalance response testing: Analyzing the rotor's reaction to both residual and excessive unbalance as per ISO 1940 G2.5 standards.
  • Misalignment testing: Simulating angular and offset misalignments to understand their impact on performance.
  • High-speed balancing: Ensures rotors can operate at speeds up to 42,000 rpm without introducing vibration-related failures.
  • Damping analysis: Evaluates the effectiveness of dampers under dynamic conditions.

Technical specifications

Maximum SpeedUp to 52,000 rpm
Rotor Diameter15 mm to 70 mm
Rotor MassUp to 90 kg
Power200 kW (maximum)
Oil Flow20 L/min at 15 bar pressure
Temperature Range15°C to 150°C
Safety StandardsEN 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 customer’s 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.

11
FAQ

Common questions.

Plain-language answers from the engineering team.

Q · 01 What is a Rotor Dynamics Test Facility?
A Rotor Dynamics Test Facility (RDTF) is an advanced test system used to analyze the dynamic behavior of rotating shafts. It enables engineers to study vibration, stability, and critical speeds under controlled high-speed conditions, ensuring reliable rotor performance in aerospace and industrial applications.
Q · 02 What rotor speeds does the RDTF support?
Up to 52,000 rpm with precision bearing assemblies. This capability allows accurate simulation of real operating conditions for turbines, compressors, and aerospace rotors while maintaining high measurement accuracy and repeatability.
Q · 03 What bearing configurations can the RDTF test?
Simply supported, overhung, and twin-rotor set-ups. These configurations enable comprehensive evaluation of different rotor layouts and support validation of real-world mechanical arrangements.
Q · 04 How does the RDTF measure critical speed?
Via whirl maps and resonance frequency analysis. The system captures vibration amplitude and phase response across speed ranges to accurately identify instability zones and critical speeds.
Q · 05 What industries use rotor dynamics test facilities?
Rotor dynamics systems are widely used in aerospace, defence, power generation, and oil & gas sectors for testing turbines, compressors, and high-speed rotating equipment.
Q · 06 What parameters are measured during testing?
The system measures vibration, displacement, speed, temperature, and bearing response. These parameters provide insights into rotor stability, imbalance, and operational performance.
Q · 07 Can the RDTF simulate real operating conditions?
Yes, the facility replicates real-world speeds, loads, and boundary conditions, allowing accurate performance validation and reducing design risks before deployment.
Q · 08 Is the system fully automated?
Modern RDTF systems use PLC/SCADA-based automation with real-time monitoring, data acquisition, and safety interlocks for consistent and repeatable testing.
Q · 09 How does the RDTF improve rotor design?
By identifying critical speeds and instability, the system helps optimize rotor geometry, bearing design, and alignment, improving efficiency and service life.
Q · 10 What safety features are included?
The facility includes overspeed protection, vibration limits, emergency shutdown systems, and interlocks to ensure safe operation at high rotational speeds.
Q · 11 Can custom test configurations be supported?
Yes, the system can be configured for different rotor sizes, weights, and applications, making it suitable for both standard and specialized testing requirements.
Q · 12 Why is rotor dynamics testing important?
Rotor dynamics testing ensures safe operation, minimizes vibration, and improves reliability. It provides real-world validation beyond simulation, reducing failure risks.
Get a proposal

Tell us your rotor sizes
and test requirements.

We size the drive line, configure the pedestal layout, and walk through the test programme with your engineering team before you commit.

Request proposal +91 7777 876 876

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Engineered To Standards Used In UK, NATO & U.S. Defence Procurement
DEF STAN (UK MoD)
NATO STANAG
RTCA/EUROCAE DO-160
MIL-SPEC / MIL-STD
Address
E-148, Sector-63, Noida, Delhi-NCR, India
Phone
Email
Working Hours
8:30 AM – 5:30 PM  ·  Mon – Sat
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