Device for detecting impacts, associated detection system and aircraft equipped with such a system

Patent metadata

Field	Value
Publication number	US-12227302-B2
Application number	US-202017783509-A
Country	US
Kind code	B2
Filing date	Dec 8, 2020
Priority date	Dec 11, 2019
Publication date	Feb 18, 2025
Grant date	Feb 18, 2025

Abstract

An autonomous impact detection device includes at least one impact detector; at least one wireless transmission device configured to transmit the information collected by the impact detector; at least one energy storage device configured to supply the impact detector and the wireless transmission device with energy; at least one Seebeck module configured to supply the storage device with energy when a temperature gradient is applied thereto; the wireless transmission device being configured to supply the storage device with energy when the temperature gradient to which the Seebeck module is exposed is not sufficient.

First claim

The invention claimed is:

1. An autonomous impact detection device comprising:
at least one impact detector;
at least one wireless transmission device configured to transmit information collected by the impact detector;
at least one energy storage device configured to supply the impact detector and the wireless transmission device with energy;
a first Seebeck module configured to supply the energy storage device with energy when a temperature gradient is applied thereto, and

a second Seebeck module configured to supply the energy storage device with energy when a temperature gradient is applied thereto, wherein the first Seebeck module is arranged according to a first configuration and wherein the second Seebeck module is arranged according to a second configuration such that, when the autonomous impact detection device is subjected to a temperature gradient, a voltage generated by the first Seebeck module is of opposite sign to a voltage generated by the second Seebeck module.

2. The autonomous impact detection device according to claim 1 , wherein the wireless transmission device is also configured to receive energy by radio frequency in order to supply the energy storage device.

3. The autonomous impact detection device according to claim 1 , comprising a supervisor configured to distribute energy to different components of the autonomous impact detection device.

4. The autonomous impact detection device according to claim 1 , comprising a memory configured to store measurements made by the impact detector or detectors and a computing system coupled to the memory, the computing system being configured to perform a pre-processing or a processing of the data acquired by the impact detector.

5. The autonomous impact detection device according to claim 1 , comprising a first set comprising the impact detector and a second set comprising at least one Seebeck module selected from the group consisting of the first Seebeck module and the second Seebeck module, the first set and the second set being connected such that the energy generated by the at least one Seebeck module of the second set can be transmitted to the first set.

6. An impact detection system for detecting impacts on a structure, the detection system comprising:
a plurality of autonomous impact detection devices according to claim 1 positioned on a surface of the structure, each detection device being associated with an identifier relating to a predetermined zone of the structure;
a plurality of communication devices close to the structure and configured to communicate with the autonomous impact detection devices so as to collect measurements made by said autonomous impact detection devices and to associate the measurements with the identifier of the corresponding device.

7. The impact detection system according to claim 6 , wherein each communication device comprises an energy storage device and/or a memory.

8. An aircraft comprising a fuselage and a detection system according to claim 6 configured to detect impacts on the fuselage, the autonomous impact detection devices of the impact detection system being arranged on an inner surface of the fuselage and the plurality of communication devices of the impact detection system being arranged in the aircraft.

Assignees

• Safran Electrical & Power
• Safran Electronics & Defense

Inventors

• Fanton Nicolas
• Roques Serge Thierry
• Couturier Emmanuel
• Paris Nicolas

Classifications

• H02J2105/32

  for aircrafts · CPC title

• G08C17/02

  using a radio link · CPC title

• B64D2045/0085

  Devices for aircraft health monitoring, e.g. monitoring flutter or vibration · CPC title

• H10N10/17

  characterised by the structure or configuration of the cell or thermocouple forming the device · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title