Device for testing cabin parts of commercial aircrafts
View Patent ↗A simulation arrangement is used for laboratory testing of enclosed partial cabins to be installed as resting cabins in commercial aircraft. The partial cabin is outfitted with vibration generators for simulating the excitation of structure-borne noise corresponding to noise that will be caused by the later connection to the aircraft fuselage. Elements for exciting airborne noise are also allocated to the partial cabin. The vibration generators and the elements for the airborne noise excitation are adjustable via control and regulating devices. The signals are generated via a computer unit with an input data file of knowledge-based information and/or by extrapolation of the acoustic values at the installation location and of the details of the construction of the partial cabin.
1. Apparatus for carrying out a laboratory testing of an enclosed partial cabin to be installed as a resting cabin in a commercial aircraft, for an acoustic design and testing, characterized in that the partial cabin ( 1 ) is arranged via at least one vibration generator ( 4 ) for the simulation of an excitation structure-borne noise in an area of connection elements ( 2 ) to be connected to a fuselage structure of the aircraft, and elements ( 5 ) for an airborne noise excitation are allocated to the partial cabin ( 1 ), whereby the at least one vibration generator ( 4 ) for the structure-borne noise and the elements ( 5 ) for the airborne noise excitation are adjustable via control and regulating devices ( 6 ), based on signals that are generatable via a computer unit ( 7 ) with an input data file ( 8 ) of knowledge-based data, as well as, if applicable, by extrapolation of acoustic values at an installation location of the partial cabin in the commercial aircraft and of the design of the partial cabin ( 1 ).
2. Apparatus according to claim 1 , characterized in that the input data file ( 8 ) of knowledge-based data contains at least components of various different noise transmissions from analyses of existing installed acoustically-designed partial cabins ( 1 ) as well as of measured noise values in the aircraft with respect to installation locations.
3. Apparatus according to claim 1 , characterized in that the at least one vibration generator ( 4 ) of the partial cabin ( 1 ) is respectively embodied as a piezo vibration generator.
4. Apparatus according to claim 1 , characterized in that the elements for the airborne noise excitation comprise an allocated loudspeaker arrangement ( 5 ) that is controlledly driveable or actuatable.
5. Apparatus according to claim 1 , characterized in that the elements for the airborne noise excitation comprise reverberation chambers arranged directly on sidewalls of the partial cabin ( 1 ).