Periodic Reporting for period 1 - CONCERTO (Cabin nOise reductioN ground Checked by nEw loudspeakeR exciTatiOn)
Reporting period: 2020-07-01 to 2022-01-31
The current systems effectiveness is limited by the following aspects:
• fixed fuselage diameter and fixed position;
• absence of a control closed loop for reverberance control;
• manual input for each loudspeaker and third-octave band.
and CONCERTO removes these limits developing a smarter and modular system, making the testing phase simpler and faster and in addion avoiding the typical complex system setup procedures.
The main project outcome are:
- smart testing system
- innovative control loop, because it is a closed control loop to obtain high speed performance with a control strategy and a pre-test analysis to reduce the number of control microphones, time and costs in the test set-up
- modular structure, its mechanical structure and software are designed to accept fuselage of different diameters (from 2.5 m to 4 m) and customizable speakers/microphones configurations
- advanced sw, with a dedicated software implementation developed in order to allow an easy and user-friendly interface.
Closed the realization and the assembling of all structures, 3 rings, loudspeakers and subsystems, the consortium completed a great and challenge project as reported in the posts by social media and present on the official project's website.
The CONCERTO project had an important economic repercussions on the partners involved, which have a common denominator: the new 90-seat turbroprop (Next Generation TurboProp). The results of the project, in fact, will represent the state of the art that will see Leonardo Aircraft Division as the main actor in the production of the new regional aircraft and the interest about the noise reduction is an important focus to investigate and improve.
The innovative noise generation system consists of three modular frames that hold evenly distributed loudspeakers at a given distance around the fuselage circumference. The frames can be adjusted to accommodate fuselages of differing diameters. The sound pressure is measured by a number of microphones placed around the fuselage surface. The number and location of the microphones used in the control loop are selected using a pre-test optimisation analysis, which aims to reduce the time and cost of the test set-up. An iterative learning approach is then used to minimise the error between the target and the measured pressure fields.
Finally, CONCERTO project allowed to LND to have a facility to study and investigate the acoustic noise focusing the attention on different contributions related to the engines, fans, transformers and compressors radiate noise in order to noise increase the interior noise comfort levels, considering that the primary concern with noise in the low frequency range is not only the potential risk of damage to the hearing bacuase low frequency noise is annoying and during periods of long exposure it causes fatigue, discomfort and loss of concentration.
Some main numbers of CONCERTO:
- total mass (single array) 2.2 ton
- cable meters 700m
- peak power 26kW
- ring dimensions about 6.2m x 5.5m