Advanced vibration control measures for high performance rotating machines

Find Similar History 31 Claim Ownership Request Data Change Add Favourite

Title
Advanced vibration control measures for high performance rotating machines

CoPED ID
98030f65-b8da-4008-a15d-6c5b69345131

Status
Active

Funder

Value
No funds listed.

Start Date
Sept. 30, 2022

End Date
Sept. 29, 2026

Description

More Like This


Overview:
Aero-Engine Rotor Dynamics invariably plays a central role in modern aero-engine design and there is a tremendous opportunity for a new-generation of approaches as the old rule-based design methods fade away and as an outgoing generation of rotordynamics is retiring. Background summary
Damping is an invaluable tool in all vibration contexts where it is possible that some excitation frequency may coincide with system resonance. In the context of aero-engines, that means when the engine rotor spin speed is the same as a so-called "critical speed". The main existing approach to damping is to exploit squeeze-film dampers (SDFs). Many of the options that engineers would naturally take for other vibration problems are not applicable in aero-engines because the dampers must be tolerant to reasonably high temperatures and they must not degrade over thousands of hours of operation.
Aim
The key research objectives of this PhD study are:
Understand the operation of existing SFDs better
Develop an improved insight into how the intrinsic highly non-linear behaviour of SFDs manifests itself inside the vibration characteristics of aero-engines
Achieve insight into the distribution of vibration responses that can arise from a single engine design based on small variations in geometry and material properties
Propose and analyse design evolutions / revolutions for SFDs or other damping provisions that will improve the robustness of future aero-engine designs by delivering more consistent performance
Obtain further experimental evidence to support the above.
Methods and timescale
The research will be conducted at the University of Nottingham within the Gas Turbines and Transmissions research centre - a research group of 50 people. It will be supported actively by experts from Rolls-Royce. The project is essentially timely at present because a new generation of aero-engines is being engineered that will have more critical speeds within the range of normal running speeds. As such, there is significant scope for this work to make a real difference to future designs.

University of Nottingham LEAD_ORG
Rolls-Royce plc STUDENT_PP_ORG

Robert Yorke STUDENT_PER

Subjects by relevance
  1. Oscillations
  2. Rotors
  3. Planning and design
  4. Research and development operations
  5. Technology
  6. Design (artistic creation)
  7. Vibration

Extracted key phrases
  1. Advanced vibration control measure
  2. Single engine design
  3. Engine Rotor Dynamics
  4. Engine rotor spin speed
  5. Vibration context
  6. High performance
  7. Vibration problem
  8. Vibration characteristic
  9. Vibration response
  10. Modern aero
  11. Consistent performance
  12. High temperature
  13. Future aero
  14. Design method
  15. Future design

Related Pages

UKRI project entry

UK Project Locations