Dynomometer Test Rig

AP Racing is a leading manufacturer of performance brake and clutch systems for road and race cars. CCS has provided them with bespoke test rigs, calibrators, software upgrades and data acquisition systems since 2011.

Development of a control and acquisition system which could be built into a dynamometer, to create a bespoke regenerative braking simulator and test rig, implementing new methods of: track simulation, dynamic inertia simulation, and regenerative braking simulation. The objective of the test data includes information as to how the brake is wearing in order to determine how it could be improved.

Current Technological Uncertainities

 

Hardware-In-the-Loop (HIL) implementation and simulation in real time

  • Normally testing of the brakes of an F1 vehicle would be on a Dynamometer to measure torque and rotational speed of an engine, motor or other rotating prime mover so power can be calculated.
  • Starting with a Dynamometer, developing a replacement control system using HIL. The uncertainty is from doing this in real-time.
  • The system needs to update the test rig 2,000 times every second, which would require extremely fast processors and complex software if this is possible in real-time.

Accurate simulation of real inertia

Factors to consider in the simulation:

  • New Formula 1 vehicles have Kinetic Energy Recovery (KERS) System and regenerative breaking which will change the effect of the braking.
  • In F1 cars the driver will use both the brake and the accelerator at the same time in order to keep the vehicle stable in a turn, leading to a different patter of use.

In a normal scenario a dynamometer simulation is run to a set rpm and then the brakes are slammed on, we need to go further by:

  • Keeping the motor running at the same time as slamming the brake on.
  • Speeding the motor to achieve an even harder braking effort.
  • Create varying degrees of inertia to simulate changes in variables, eg. size of the vehicle, gradient the vehicle is moving at.

Baseline Technological Knowledge

This is a form of vehicle testing that did not previously exist and so we sort to develop a low-level electronics and software controlled systems to achieve a solution, and a limited number of companies have started to use dynos to achieve simulations of F1 vehicles, as opposed to consumer vehicles. The F1 marketplace is extremely competitive and so the methods and technologies are kept as closely guarded secrets, so independent research and development was required.

The knowledge developed here was not readily deducible due by our competent professionals as this uses a recent development of software and is a new application for it.

 

 

Results from the Actions Taken to Overcome the Uncertainities

  • Considerable brainstorming, conceptualisation, and experimentation on how the test rig would work.
  • Development and trademarking of a new system to test all the possible permutations of use of these new technologies without having to put a driver into a car on a track.

Hardware-In-the-Loop (HIL) implementation and simulation in real time

  • Worked out how to get the HIL code to work with this type of machine and application.
  • Development the front-end user interface to allow users to not only execute tests but to also create them.
  • Use of new hardware and development new types of electronics which has not been used for this type of application before.

Accurate simulation of real inertia

  • Integration of the mathematics involved in calculating inertia into software considering a variety of variables through a modified Davis Equation.
  • Adoption of an iterative process of trial and error for the creation of scenario algorithms, by testing each iteration on a test bed before it can be built up and added to the software of the main system.
  • Creation of a system to simulate different inertias with two ways of working:
    • Cyclic Testing to test, tune and retest.
    • Global F1 Track Tests to collect info from live track test and then trying to simulate them.

Future

  • Increasing the accuracy of the simulation of wear on the brakes and further tuning of the hardware so that the motors decelerate with exactly the required speed of reaction,
  • Advance in the field of Electrical and Mechanical Engineering particularly relating to regenerative braking and seeking to make an appreciable improvement over existing F1 test rigs.
  • Extension into worldwide transport development with electrification of vehicles and their huge impact in the area of braking and regenerative energy collection.

 

Similar Projects

  • Research and Development for a variety of industries, sectors, and organisations such as the Birmingham Centre for Railway Research and Education and Cranfield University.
  • Brake Test Rigs for brake cooling power units, friction testing, F1 Brake Dyno testing and other applications.
  • Automotive Projects including data acquisition and control systems, Autosport racing calliper test rig and battery monitoring systems.

Contact

Paul Riley

Certified LabView Architect

MD and Lead Software Developer at CCS

Tel: +44 (0)1926 485532

Email: paul@ccsln.com

Case studies

Aerospace

View all aerospace case studies

Automotive

View all automotive case studies

Energy

View all energy case studies

Transport

View all transport case studies

Brake Hose Capability Test Rig

A brake hose test rig with modular style, looking at the capabilities and fatigue of pressurised brake hoses under a variety of different parameters and simulations. Aiming for a modular approach for the overall system to allow for customisability and efficiency.

Jaguar Land Rover Automotive PLC are a British multinational automotive company, with its headquarters nearby in Whitley, Coventry. They are a leading technology company in the field, with two iconic British car brands and an international reputation. With over 15 years of experience working with JLR, CCS have been involved in countless projects, from calibration to impact testing, test rigs to measurement systems.

Requirements

  • Using a JLR built rig for pressure comprising of a 4.5kW Kolle Morgan motor via belt drive to ballscrew. Which provides approximately 100mm travel with the shaft pushing onto a brake cylinder, able to apply up to 350bar pressure. This also can vary conditions including displacement, gear ratio, motor power, extension speeds and pitch.
  • Transparent pass through for control and acquisition, handling safety, providing PT monitoring, calibration screen, manual control of all I/O.
  • Aim to incorporate the JLR programmed MTS to issue all test profiles and record demands for independent playback.

Design

Software

  • Testing Interface split into Pressure Cycle Control and Movement Cycle Control, Test Rig setup to lock/unlock guards and show system status, individual Cycle Counters to allow partial testing, Target and Completed counters, Movement Jogging and Pressure Increment control, Hose Movement and Brake Pressure plots.
  • Test Configuration Interface which can Create or Load Cycle Profile, Import Cycle Profile into controllers, enable controller to view profile and configure Manifold Pressure Trip Tolerance, Hose Pressure Drop Tolerance and Max Brake Displacement Change.
  • Rig Configuration Interface with a live status of Digital Inputs and Outputs to assist fault diagnosis, Analogue Inputs/Outputs Configuration and Data Logging Configuration.

Hardware

  • CCS bespoke mobile cabinet with an integrated monitor mount, separation of 240VAC circuits and ELV DC circuits, isolator, 32A Single Phase power supply, USB connectivity, Harting connectors for connection to test rig, PMA mechanical protection of cables, interlocked connectors, keyboard and mouse.

Safety

  • Prevention of motor and actuator movement if the guard is open and not in setup mode.
  • Setup mode to provide low pressure (70psi) brake fluid pressure to enable operator to bleed hoses and system.
  • Status indication beacon, E-Stop, Reset and No Access when pressurised, as standard and user-friendly safety features.

Results

The finished product for the initial stage was delivered to the site in January 2020, with supporting Software Instruction Manual and User presentation (including Rig Design and Wiring, Safety Overview, Software Overview, and Test Walk-Through).

Future

  • Customer Feedback collected after 3 weeks from sign off.
  • Software updates and reviews available to JLR for the future of the rig.
  • The Next Phase looking into incorporating the JLR programmed MTS.

Similar Projects

  • Brake Test Rigs for brake cooling power units, friction testing, F1 Brake Dyno testing and other applications.
  • Automotive Projects including data acquisition and control systems, autosport racing caliper test rig, battery monitoring system, among many

Contact

Ian Billingsley

Certified LabView Architect at CCS

Lead Software Developer on this Project

Tel: +44 (0)1926 485532

Email: ian@ccsln.com

 

Case studies

Aerospace

View all aerospace case studies

Automotive

View all automotive case studies

Energy

View all energy case studies

Transport

View all transport case studies

RVDT Portable Test Instrument

Collins Aerospace is anew unit of Raytheon Technologies Corporation, formed by the merger of UTC Aerospace Systems and Rockwell Collins in 2018. Collins Aerospace is one of the world’s largest suppliers of aerospace and defence products and have over 300 sites globally. CCS have been involved in multiple projects with their nearby UK Enterprise and Actuation Systems sites, and now internationally, with their Singapore section via Cranfield University. 

A Rotary Variable Differential Transformer (RVDT) Test box for PAT and fault-finding purposes.

Hardware Design

  • Controller and chassis: cRIO 9040 RT Controller and FPGA backplane.
  • Display: 5 in. touch screen Win CE LCD monitor with 680*400 screen resolution.
  • Analogue Input: 4 analogue inputs 16bit, independent ADC, Voltage Range Accuracy ±10V, and simultaneous sampling.
  • Analogue Output: 4 analogue output 16bit, Voltage Range Accuracy ±10V, Output amplifier with low pass filter Signal is 3012Hz (332ms), and frequency precision can be up to 0.003%

Field programmable gate array (FPGA)

FPGAs are semiconductor devices that are based around an array of configurable logic blocks and a hierarchy of reconfigurable interconnects. The logic blocks can be configured to perform as simple logic gates or to perform complex combinational functions. The first commercially viable FPGA was invented in 1985 and since then there has been a huge increase in market competition and applications, with significant improvements in prices and performance dynamics as of 2017 broadening the range of viable applications. Some notable applications have been for hardware acceleration of the Bing search algorithm, acceleration of artificial neural networks for machine learning, and even as full systems on chips (SoC).

CCS use an add-on for NI’s LabVIEW called LabVIEW FPGA to design complex systems efficiently and effectively, this includes an integrated development environment, various IP libraries and debugging features. Here we are using the FPGA to quickly calculate the required variables without the need to upload the test data before calculating so there it is instantaneously shown on the test rig.

      Software Design

        • Initial Start-Up & Graph Screen is the first screen on start-up, once the system has booted up it will begin plotting RVDT and Encoder positions onto the graph.
        • DPMS Screen displays the positions of the RVDTs in volts, the encoder position in revolutions, and the coil Vrms (root squared mean of voltage) from secondary coil measurements. Here you can also zero the position of the encoder with the “Reset Encoder” button.
        • Settings Screen enables the operator to modify the system parameters:
          • Volts the excitation voltage supplied to the RVDT (in Vrms)
          • Oscillatory Frequency the oscillation frequency supplied to the RVDT (in Hz)
          • Pulses per Revolutions the number of pulses per revolution of the encoder

        With options to “Save”, “Revert”, and “Demo”. To save new parameters, revert to the default values, and input random numbers into the DPMs to prove they are responding correctly.

        • About Screen displaying operating system details and contact information for CCS.

        Results

        The outcome is a RVDT Test Box housed in a 19” rack inclusive of the 2 and 4 metre harnesses, breakout box and encoder. This RVDT box is not strictly a one-off piece of equipment and multiples could be sold, either to multiple companies or within a company, as an adaptable PAT and fault-finding instrument.

         

        Similar Projects

        • Aerospace Projects including other test rigs, data acquisition systems and control interfaces, for various aerospace components.
        • RVDT projects for other aerospace companies such as Comar and Goodrich.
        • More applications of FPGAs are being looked into by CCS for a variety of other projects, including other fault-detection rigs and onsite data analysis.
        • International Clients are an increasingly large part of CCS’s client base, with an multinational reputation and on-site visits key to our work.

             

            Case studies

            Aerospace

            View all aerospace case studies

            Automotive

            View all automotive case studies

            Energy

            View all energy case studies

            Transport

            View all transport case studies

            Flow Test Bench Update

            BAE Systems is a British multinational defence, security, and aerospace company. To support their aircraft supplied worldwide, they provide a support package, modelled and tailored for each individual customer. Within this support package, is a second line testing solution that is used to conduct standard serviceability tests on the Line Replacement Units (LRU’s) removed from the aircraft. These component parts have mainly remained stable throughout the life of the aircraft, with only a few minor obsolescence changes have taken place.

            The Problem. The current testing solution is now suffering from obsolescence however to the extent that BAE Systems have sought a new modern solution.

            The Solution. The intention is to supply a bespoke fixture to serve as a dedicated test bench and act as a supply source to carry out all the necessary tests, taking the support package forward over the next 25 years.

              Managing Updates

              Key Issues and Proposed Solutions

              What risk does the engine update have to previously completed LRU tests? Risk has been minimised by validation testing on over 95% of test routes on the rig since 23/01/19. There will also be a checklist of manual validation checks and normal process daily test development.

              What LRU’s are affected by the engine update? To fit the new rudder control requirements on the existing FPGA hardware a refactoring of low-level channel control was required, which is easily validated. There is also a requirement to change the milliamp current output control for the autostablisation function of the rudder.

              Can the pending engine update be rolled back to remove the rudder test updates without affecting LRU’s recently completed? This could possibly pose more risk than using the latest engine build we can do this by retesting the new plugin, developed for use with recent LRUs. Also fault reports have been corrected and verified in the latest build and several requested features to assist the operator in running tests have been included in the latest build.

              What is the level of software risk or implications to all systems and LRU software? As discussed previously but also to increase confidence there is a further recommendation to re-test a small selection of older LRU’s to cover a range of functions.

              Results

              With the delivery of the updated system, CCS also provided them with a Post-Delivery Support Scheme for future updates and possible issues.

               

              Similar Projects

              • Test Rig Upgrades for a variety of rigs including a load cell tester, hydraulic test rigs and pressure rigs.
              • Aerospace Projects including a wide range of test rigs, data acquisition systems and control interfaces, various aerospace components.

              Contact

              Ian Billingsley

              Certified LabView Architect at CCS

              Lead Software Developer on Project

              Tel: +44 (0)1926 485532 Ext:105

              Email: ian@ccsln.com

              Case studies

              Aerospace

              View all aerospace case studies

              Automotive

              View all automotive case studies

              Energy

              View all energy case studies

              Transport

              View all transport case studies

              Future Railway Pantograph Rig

              Birmingham Centre for Railway Research and Education (BCRRE) is a Nationally Recognised Research Centre based in the University of Birmingham Engineering and Physical Sciences Department. They specialise in training engineers and developing world-leading technologies, with collaboration between industry and academia to drive UK and global rail innovation.

              BCRRE’s Condition Monitoring and Sensing Research Area develops bespoke instrumentation and processing systems to measure and predict the health of various railway subsystems.

              Development of a laboratory-based test rig for evaluating and characterising pantograph dynamic loading performance. More specifically identifying changes in its dynamic behaviour, including friction and damping, when compared against an exemplar pantograph.

               Requirements

              • Hold the pantograph in test in a fixed, known, repeatable position near the floor.
              • Move the actuator over a range of:
                • Vertical positions within the boundaries of where the pantograph can reach.
                • Laterally positions within limits and at a speed of around 750mm/s.
              • Apply a vertical force to the pantograph contact strips from above at the same height with controls for lateral position, frequency of applied force, time-history of the applied force, and a limit on vertical forces.
              • Measure:
                • Applied force.
                • Individual applied forces to the contact strips.
                • Vertical displacement between the actuator and contact strips.
                • Lateral force in the actuator at two contact points
                • Relative lateral positions of the actuator and contact strips
              •  Detect loss of contact between actuator and contact strips over a time of 5 ms, logging the history of the loss of contact and the correlation between loss of contact and applied force.
              • Carry out autonomous test including: an automatic dropping device test, a hysteresis test, a frequency domain test, a playback test.
              • Operate on 415V, 3φ supply, with no more than 16A per phase.
              • Fully safety compliant to the national standards for fixed electrical/mechanical equipment and Network Rail standards for fixed plant.
              • Identify vertical and lateral frequency response at different lateral positions and calculate the hysteresis curve critical parameters.
              • Produce:
                • Analysis of test results.
                • Automated test report.
                • Go/No go indication for the pantograph.

               

              Design

              Hardware

              • Supplies: 400V 16A 3-phase cabinet supply and x3 UoB 13A wall sockets.
              • Cabinet 800 x 1800 x 400mm, with front door mounted isolator, top cabinet mounted braking resistors and 200mm plinth for cable exits. With an ABB isolator, Schneider MCBs, Murr PSUs, Weidmuller Terminals, NI FPGA based hardware, and Pilz safety relays.
              • Control PC running Windows 7 Pro, with an ethernet connection, VESA mounted and dual monitors.
              • x2 Parker Servo drives one for each axis.
              • Flexible cable routing to the motors and transducers.
              • Utilise the Safe Torque Off feature of the Compax 3S drive.
              • Key Exchange to safely remove power to the drive via STO.

              Software

              • Calibration Interface with Analogue Input & Output set-up (for Units, Gain, Offset, Precision, Filter, Min/Max limits, Voltage, Scaled), Simulation Mode set-up, and manual position control of Vertical and Horizontal axes.
              • Control Interface with Vertical and Horizontal Control Profiles loaded from a library of profiles and including the amplitude of the Y-axis and the period of the profile.
              • Data Acquisition Interface which displays up to 10 channels during the test of the recorded transducer feedback and servo demand values at variable acquisition rates.
              • Analysis Interface which analyses the test data in parallel with a test running, applies a frequency response algorithm and hysteresis curve algorithm, and then exports the final report to PDF.

              Results

              The first UK laboratory-based pantograph dynamic test rig that can carry out a wide range of dynamic tests.

              Future

              • Movement of the test rig to the new BCRRE facility in 2020.
              • Commercialisation of a depot-based pantograph dynamic test rig to automatically assess the condition and serviceability of pantographs and which recommend maintenance or repair as appropriate.

               

              Case studies

              Aerospace

              View all aerospace case studies

              Automotive

              View all automotive case studies

              Energy

              View all energy case studies

              Transport

              View all transport case studies