Automated self-test of cabin loudspeakers

Patent metadata

Field	Value
Publication number	US-11601688-B2
Application number	US-201916551886-A
Country	US
Kind code	B2
Filing date	Aug 27, 2019
Priority date	Aug 29, 2018
Publication date	Mar 7, 2023
Grant date	Mar 7, 2023

Abstract

A test module for functionally testing an audio device of an aircraft passenger service unit (PSU) is configured to allocate a first operating mode to a first individual audio device of one PSU of a set of PSUs during which, a test tone is emitted. The test module allocates a second operating mode to other audio devices different than the first audio device. In the second operating mode, the test tone emitted by the first audio device is intended to be received. The other audio devices each belong to different PSUs within the set of PSUs. The test module emits the test tone via the first audio device. The test module initiates a functional test of the first audio device. The functional test is based on the test tone received by the other audio devices. The test module may be part of a system and an aircraft.

First claim

The invention claimed is:

1. A test module for functionally testing an audio device of a passenger service unit (PSU) in an aircraft, wherein the test module is configured:
to allocate a first operating mode, in which a test tone is intended to be emitted, to an individual audio device belonging to one PSU from a set of PSUs;
to allocate a second operating mode, in which the test tone is intended to be received, to audio devices which differ from the individual audio device and each belong to different PSUs from the set of PSUs;
to cause emission of the test tone via the audio device to which the first operating mode is allocated; and
to initiate a functional test of the audio device, to which the first operating mode is allocated, based on the test tone received by the audio devices to which the second operating mode is allocated.

2. The test module according to claim 1 , wherein each PSU has only one audio device.

3. The test module according to claim 1 , wherein the test module is configured, in each step in a predetermined sequence of steps:
to allocate the first operating mode to an individual audio device belonging to a respective PSU from the set of PSUs and to simultaneously allocate the second operating mode to all other audio devices of respective other PSUs from the set of PSUs,
to initiate emission of the test tone by the individual audio device to which the first operating mode is allocated, and
to initiate a functional test of the individual audio device based on the test tone received by all other audio devices.

4. The test module according to claim 1 , wherein the test module is configured to determine a check of a correct functionality based on configuration information, wherein the configuration information contains information relating to an arrangement of the set of PSUs.

5. The test module according to claim 4 , wherein the configuration information also contains information relating to a distance at which and a configuration in which different PSUs from the set of PSUs are arranged.

6. The test module according to claim 4 , wherein the test module is configured to determine, based on the configuration information, whether a PSU in the set of PSUs is arranged at its correct location according to a previously determined assignment in the aircraft.

7. The test module according to claim 1 , wherein the test tone is based on a pseudorandom signal.

8. A system for functionally testing an audio device of a PSU in an aircraft, the system comprising:
a test module according to claim 1 , and
a set of PSUs in an aircraft.

9. An aircraft having a test module according to claim 1 .

10. An aircraft having a system according to claim 8 .

11. A method for functionally testing an audio device of a passenger service unit, PSU, in an aircraft by means of a test module, wherein the method comprises:
allocating, by means of a test module, a first operating mode, in which a test tone is intended to be emitted, to an individual audio device belonging to one PSU from a set of PSUs;
allocating, by means of the test module, a second operating mode, in which the test tone is intended to be received, to audio devices which differ from the individual audio device and each belong to different PSUs from the set of PSUs;
causing, by means of the test module, emission of the test tone via the audio device to which the first operating mode is allocated; and
initiating, by means of the test module, a functional test of the audio device, to which the first operating mode is allocated, based on the test tone which is received by the audio devices to which the second operating mode is allocated.

12. The method according to claim 11 , wherein the method also comprises:
carrying out the functional test and outputting a corresponding item of information via the test module in an event of a negative result of the functional test.

Assignees

• Airbus Operations Gmbh

Inventors

• Heinisch Matthias
• Klose Peter
• Geyer Fabien

Classifications

• H04N21/2146 Primary

  located in mass transportation means, e.g. aircraft, train or bus (flight-deck installations for entertainment or communications B64D11/0015; arrangements specially adapted for transportation systems in broadcast systems H04H20/62; moving wireless networks H04W84/005) · CPC title

• H04L67/12

  specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks · CPC title

• B64D11/0015

  Arrangements for entertainment or communications, e.g. radio, television · CPC title

• H04R29/007 Primary

  for public address systems (public address systems per se H04R27/00) · CPC title

• B64F5/60 Primary

  Testing or inspecting aircraft components or systems · CPC title