Monitoring Device for Aircraft Equipment

• US 20120143436A1
• Filed: 11/30/2011
• Published: 06/07/2012
• Est. Priority Date: 12/02/2010
• Status: Abandoned Application

• Current Assignee: Techspace Aã©Ro SA (Safran SA)
• Original Assignee: Techspace Aã©Ro SA (Safran SA)
• Inventors: Cornet, Albert, Doucet, Nicolas, Langohr, Philippe, Droeller, Matthieu, Raimarckers, Nicolas, Haudry, Fabrice, Saint-Mard, Michel, Leblond, Rémy
• Application Number:
  US13/307,177
• Publication Number:
  US 20120143436A1
• Time in Patent Office: Days
• US Class Current: 701/33.4
• CPC Class Codes: G07C 5/085 using electronic data carriers

Abstract

A device for monitoring aircraft equipment is adapted to be arranged on said equipment and to measure and memorize at least one operation parameter of said equipment. The monitoring device is configured to be activated only in the presence of one or more parameters, representative of said equipment.

Claims

1. A monitoring device for aircraft equipment adapted to be taken on board on the equipment, comprising:

an energy source having a sufficient capacity for the device to function;

at least one sensor adapted to measure an operation parameter of the equipment;

electronic control means; and

a memory adapted to store the values measured by the sensor;

wherein the monitoring device is configured to be automatically activated only in the presence of one or more parameters representative of the operation of the equipment, in the absence of an electric or electronic connection with the outside of the monitoring device.

2. The monitoring device according to claim 1, wherein the parameter representative of the equipment operation comprises:

at least one of temperature and vibrations.

3. The monitoring device according to claim 1, further comprising:

a vibration sensor used as a parameter for activating the monitoring device, the sensor being preferably configured to detect at least one determined frequency range.

4. The monitoring device according to claim 1, further comprising:

a temperature sensor used as a parameter for activating the monitoring device.

5. The monitoring device according to claim 1, wherein the energy source comprises:

a thermo-generator.

6. The monitoring device according to claim 5, wherein the thermo-generator ensures the activation of the monitoring device based on a temperature parameter.

7. The monitoring device according to claim 5, further comprising:

a vibration sensor ensuring the activation of the monitoring device based on a vibration parameter.

8. The monitoring device according to claim 6, wherein the energy source further comprises:

a piezoelectric generator.

9. The monitoring device according to claim 1, further comprising:

connectors adapted to enable a transfer of information stored in the memory to an external apparatus.

10. The monitoring device according to the claim 9, wherein the monitoring device is passive in terms of wavelength transmission.

11. The monitoring device according to claim 1, further comprising:

a support for housing the components of the monitoring device.

12. The monitoring device according to claim 11, wherein the support comprises:

a visible metallic part adapted to receive an identification plate of the equipment.

13. The monitoring device according to claim 11, wherein the support comprises:

a surface for assembly on the equipment, the surface being metallic and directly supporting the sensor adapted to measure an operation parameter of the equipment, the sensor being selected from among temperature and vibration sensors.

14. An aircraft, comprising:

selected equipment; and

a monitoring device comprising;

an energy source having a sufficient capacity for the device to function;

at least one sensor adapted to measure an operation parameter of the selected equipment;

electronic control means; and

a memory adapted to store the values measured by the sensor;

wherein the monitoring device is configured to be automatically activated only in the presence of one or more parameters representative of the operation of the selected equipment, in the absence of an electric or electronic connection with the outside of the device.

15. The aircraft according to claim 14, wherein the selected equipment has at least one equipment frequency, and the monitoring device comprises:

a vibration sensor adapted to detect a frequency range inclusive of the equipment frequency.