Mode detection with an optimised array in a model turbofan engine intake at varying shaft speeds
Mode detection with an optimised array in a model turbofan engine intake at varying shaft speeds
Modal measurement techniques in engine intakes have been used previously to analyse the generated fan noise. A proven method is to use a wall-mounted array of Kulite transducers and operate the (model) turbofan under constant shaft speeds. A drawback of this method is the large number of (expensive) microphones and acquisition channels needed to obtain complete m-mode spectra at high engine orders. Furthermore, to get a full scan of the m-mode spectra as a function of shaft speed, many measurements are required. The issue of the large number of microphones was addressed by using a sparse array instead of an equidistant array. An array optimisation technique, similar to a technique used for the design of phased microphone arrays for sound source localisation, was used to define such a sparse intake array. This array consists of 100 Kulites and is able to determine without aliasing the modal spectrum from m = (79 to m = (79, which is appropriate to determine the modal content up to 3 BPF of a modern turbofan. This array was tested in a Rolls-Royce model fan rig at Ansty as a part of the RESOUND project. A new digital data-acquisition system made it possible to simultaneously and continuously record the Kulite pressure data as the engine speed was varied continuously from idle to maximum speed or vice versa, with each acceleration/deceleration lasting for a period of 9 minutes. Time histories of the Kulites were processed giving power spectra of the engine orders, which revealed the rotor locked tonal components. For each rotor revolution, a Discrete Fourier Transform was applied and, after averaging over a number of revolutions, the m-mode spectra were determined. In this way, a full modal scan with respect to shaft speed in a very limited testing time was obtained.
Rademaker, E.D.
7c38b562-e889-4e56-a70b-f311c8f10c21
Sijtsma, P.
0655cb93-eda5-4a82-9ad4-9e9e550b3d49
Tester, B.J.
1bd4a793-131b-4173-93cc-3eca70b2d116
2001
Rademaker, E.D.
7c38b562-e889-4e56-a70b-f311c8f10c21
Sijtsma, P.
0655cb93-eda5-4a82-9ad4-9e9e550b3d49
Tester, B.J.
1bd4a793-131b-4173-93cc-3eca70b2d116
Rademaker, E.D., Sijtsma, P. and Tester, B.J.
(2001)
Mode detection with an optimised array in a model turbofan engine intake at varying shaft speeds.
7th AIAA/CEAS Aeroacoustics Conference, Maastricht, The Netherlands.
27 - 29 May 2001.
Record type:
Conference or Workshop Item
(Paper)
Abstract
Modal measurement techniques in engine intakes have been used previously to analyse the generated fan noise. A proven method is to use a wall-mounted array of Kulite transducers and operate the (model) turbofan under constant shaft speeds. A drawback of this method is the large number of (expensive) microphones and acquisition channels needed to obtain complete m-mode spectra at high engine orders. Furthermore, to get a full scan of the m-mode spectra as a function of shaft speed, many measurements are required. The issue of the large number of microphones was addressed by using a sparse array instead of an equidistant array. An array optimisation technique, similar to a technique used for the design of phased microphone arrays for sound source localisation, was used to define such a sparse intake array. This array consists of 100 Kulites and is able to determine without aliasing the modal spectrum from m = (79 to m = (79, which is appropriate to determine the modal content up to 3 BPF of a modern turbofan. This array was tested in a Rolls-Royce model fan rig at Ansty as a part of the RESOUND project. A new digital data-acquisition system made it possible to simultaneously and continuously record the Kulite pressure data as the engine speed was varied continuously from idle to maximum speed or vice versa, with each acceleration/deceleration lasting for a period of 9 minutes. Time histories of the Kulites were processed giving power spectra of the engine orders, which revealed the rotor locked tonal components. For each rotor revolution, a Discrete Fourier Transform was applied and, after averaging over a number of revolutions, the m-mode spectra were determined. In this way, a full modal scan with respect to shaft speed in a very limited testing time was obtained.
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Published date: 2001
Additional Information:
AIAA 2001-2181
Venue - Dates:
7th AIAA/CEAS Aeroacoustics Conference, Maastricht, The Netherlands, 2001-05-27 - 2001-05-29
Identifiers
Local EPrints ID: 10254
URI: http://eprints.soton.ac.uk/id/eprint/10254
PURE UUID: eea9b6ca-e00d-4919-bad8-2859f3c84ff8
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Date deposited: 16 May 2005
Last modified: 09 Jan 2022 09:55
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Contributors
Author:
E.D. Rademaker
Author:
P. Sijtsma
Author:
B.J. Tester
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