Device and method for determining the state of ageing of a hydraulic fluid of a hydraulic system of a vehicle

• US 8,874,307 B2
• Filed: 10/18/2012
• Issued: 10/28/2014
• Est. Priority Date: 04/20/2010
• Status: Active Grant

• Current Assignee: Airbus Operations GmbH (Airbus SE)
• Original Assignee: Airbus Operations GmbH (Airbus SE)
• Inventors: Behr, Robert, Baumbach, Volker
• Primary Examiner(s): Cheung, Calvin
• Assistant Examiner(s): Martinez Borrero, Luis A
• Application Number:
  US13/654,598
• Publication Number:
  US 20130096770A1
• Time in Patent Office: 740 Days
• Field of Search: 701/31.4, 701/29, 701/32.1, 952/48, 210/195.1, 340/457.4, 340/525, 324/321, 137/266, 73/6, 737/08, 737/16, 73/530.5, 73/10.2, 73/745.6, 73/645.6, 73/530.1, 604/13, 417/32, 417/390, 244/50, 702/28, 702/177
• US Class Current: 701/32.1
• CPC Class Codes: F15B 19/005 Fault detection or monitoring

Abstract

A device for determining ageing of a hydraulic fluid in a hydraulic system with a multitude of hydraulic components is provided. The device comprises at least one temperature determination device and at least one ageing determination device, wherein the temperature determination device determines the respective temperature of each discrete fluid volume of the hydraulic fluid in the hydraulic system, and from the aforesaid the ageing determination device determines an increase in ageing. Generally, the temperature determination device carries out a numerical thermal simulation of the hydraulic system, component by component, including determining at least one temperature of at least one hydraulic component of the hydraulic system, which simulation is supported by measuring the temperatures of individual hydraulic components by means of temperature sensors.

Claims

1. A device for determining ageing of a hydraulic fluid in a hydraulic system with a multitude of hydraulic components, comprising:

at least one temperature determination device that determines the respective temperature of each discrete fluid volume of the hydraulic fluid in the hydraulic system; and

at least one ageing determination device that determines an increase in ageing of the hydraulic fluid from the following equation;

2. The device of claim 1, further comprising a calculation unit that determines, from the respective increases in ageing of the discrete fluid volumes over a predetermined duration, the entire increase in ageing of the hydraulic fluid contained in the hydraulic system.

3. The device of claim 1, wherein the temperature determination device carries out a numerical thermal simulation, component by component, and determines at least one temperature of at least one hydraulic component of the hydraulic system.

4. The device of claim 3, wherein the numerical thermal simulation determines a heat flow relating to at least one discrete fluid volume of the respective hydraulic component relative to the environment of the hydraulic component.

5. The device of claim 3, wherein the temperature determination device further comprises an interface device that is connectable to a control unit of the hydraulic system that simulates loads of hydraulic components in the numerical thermal simulation.

6. The device of claim 3, wherein the temperature determination device is connectable to at least one ambient temperature sensor and acquires the ambient temperature of at least one hydraulic component by means of the ambient temperature sensor.

7. The device of claim 3, wherein the temperature determination device is connectable to at least one temperature sensor and acquires the temperature of a discrete fluid volume of the hydraulic fluid in a respective hydraulic component, and based on the numerical thermal simulation module of the hydraulic system determines the temperatures of hydraulic components whose temperature is not monitored.

8. The device of claim 1, wherein the hydraulic fluid is in the hydraulic system of an aircraft.

9. A method for determining ageing of a hydraulic fluid in a hydraulic system of a vehicle comprising a multitude of hydraulic components, comprising:

determining, by a calculation unit, the temperature of a discrete fluid volume within at least one hydraulic component;

generating, by a calculation unit, an observation period based on an operating state of the vehicle;

determining an increase in ageing of a respective discrete fluid volume by means of the ageing determination device using the following equation;

10. The method of claim 9, further comprising:

measuring the temperature of at least one discrete fluid volume within at least one hydraulic component by means of a temperature sensor.

11. The method of claim 9, further comprising:

carrying out a thermal simulation of at least one discrete fluid volume within at least one hydraulic component whose temperature is not monitored.

12. An aircraft, comprising:

at least one hydraulic system that includes a hydraulic fluid;

at least one temperature determination device that determines the respective temperature of each discrete fluid volume of the hydraulic fluid in the hydraulic system;

at least one ageing determination device that determines an increase in ageing of the hydraulic fluid from the following equation;

13. The aircraft of claim 12, wherein the temperature determination device carries out a numerical thermal simulation, component by component, and determines at least one temperature of at least one hydraulic component of the hydraulic system.

14. The aircraft of claim 13, wherein the numerical thermal simulation determines a heat flow relating to at least one discrete fluid volume of the respective hydraulic component relative to the environment of the hydraulic component.

15. The aircraft of claim 13, wherein the temperature determination device further comprises an interface device that is connectable to a control unit of the hydraulic system that simulates loads of hydraulic components in the numerical thermal simulation.

16. The aircraft of claim 13, wherein the temperature determination device is connectable to at least one ambient temperature sensor and acquires the ambient temperature of at least one hydraulic component by means of the ambient temperature sensor.

17. The aircraft of claim 13, wherein the temperature determination device is connectable to at least one temperature sensor and acquires the temperature of a discrete fluid volume of the hydraulic fluid in a respective hydraulic component, and based on the numerical thermal simulation module of the hydraulic system determines the temperatures of hydraulic components whose temperature is not monitored.

18. The aircraft of claim 13, wherein the specified observation period in an ascent to cruising altitude phase is shorter than the specified observation period in a cruising phase.