Measurement of strain and vibration, at ambient conditions, on a dynamically pressurised aircraft fuel pump using optical fibre sensors

Abstract

Ever-increasing demands to improve fuel burn efficiency of aero gas turbines lead to rises in fuel system pressures and temperatures, posing challenges for the structural integrity of the pump housing and creating internal deflections that can adversely affect volumetric efficiency. Non-invasive strain and vibration measurements could allow transient effects to be quantified and considered during the design process, leading to more robust fuel pumps. Fuel pumps used on a high bypass turbofan engine were instrumented with optical fibre Bragg grating (FBG) sensors, strain gauges and thermocouples. A hydraulic hand pump was used to facilitate measurements under static conditions, while dynamic measurements were performed on a dedicated fuel pump test rig. The experimental data were compared with the outputs from a finite element (FE) model and, in general, good agreement was observed. Where differences were observed, it was concluded that they arose from the sensitivity of the model to the selection of nodes that best matched the sensor location. Strain and vibration measurements were performed over the frequency range of 0 to 2.5 kHz and demonstrated the ability of surface-mounted FBGs to characterise vibrations originating within the internal sub-components of the pump, offering potential for condition monitoring.United Kingdom Research and Innovation,113095; Engineering and Physical Sciences Research Council, EP/H02252X/1The authors acknowledge funding from the United Kingdom Research and Innovation (UKRI) through the support from Innovate UK, via the Aerospace Technology Institute (ATI) program, End-to-End Equipment Health Management (E2E EHM, Project Reference: 113095) [50] and by the Engineering and Physical Sciences Research Council (EPSRC), UK via a Platform Grant (EP/H02252X/1).Sensor