System and method for the measurement and prevention of icing in a conduit

• US 8,794,018 B2
• Filed: 12/23/2008
• Issued: 08/05/2014
• Est. Priority Date: 12/28/2007
• Status: Active Grant

• Current Assignee: Airbus Operations GmbH (Airbus SE)
• Original Assignee: Airbus Operations GmbH (Airbus SE)
• Inventors: Gleine, Wolfgang
• Primary Examiner(s): Tyler, Cheryl J
• Assistant Examiner(s): Bradford, Jonathan
• Application Number:
  US12/810,929
• Publication Number:
  US 20110005247A1
• Time in Patent Office: 2,051 Days
• Field of Search: 62125-129, 62139-140, 621/50, 73/240.4, 731/702.6, 340/582
• US Class Current: 62/150
• CPC Class Codes: B64D 13/06 the air being conditioned pressurising B64D13/02
• CPC Class Codes: B64D 2013/0607 providing hot air or liquid for deicing aircraft parts, e.g. aerodynamic surfaces or windows
• CPC Class Codes: G01M 7/027 Specimen mounting arrangements, e.g. table head adapters

Abstract

A system for preventing icing in a conduit, as can occur in an aircraft'"'"'s air conditioning system, includes at least one sensor for acquiring mechanical oscillations of the conduits, an electronic evaluation unit and an electronic control unit. The sensor is connected to the electronic evaluation unit, which knows characteristics relating to the oscillation behavior of the conduit and is equipped to compare the measured conduit oscillations with these characteristics, and through correlation to interpret them as conduit icing, and in the case of conduit icing to emit a signal to the control unit. If the operation-associated oscillations are inadequate, oscillations can be generated or amplified through an actuator. With this system an icing state within the conduit can be detected without the use of sensors located in the interior cross section of the conduit, which itself serves as a sensitive element.

Claims

1. A system for the measurement and prevention of icing in a conduit, comprising a plurality of sensors for acquiring mechanical oscillations of the conduit, an electronic evaluation unit and an electronic control unit,

wherein the sensors are connected to the electronic evaluation unit, the evaluation unit comprises characteristics relating to the oscillation behaviour of the conduit and is equipped to compare the measured conduit oscillations with the characteristics, and by means of correlation to interpret them as conduit icing, and in the case of conduit icing to emit a signal to the control unit,

wherein the evaluation unit is equipped, from sensor data and correlation with known characteristics that are associated with the conduit, to determine local and global increases in the mass of the conduit and thus of an ice layer, and, if a specified local or global thickness of the ice layer is exceeded, to emit a signal to the control unit for triggering a de-icing procedure.

2. The system of claim 1, wherein the sensors are acceleration sensors.

3. The system of claim 1, wherein the sensors are piezoresistive strain gauges.

4. The system of claim 1, wherein the sensors are piezoelectric elements.

5. The system of claim 1, comprising at least one actuator, arranged on the conduit, for generating oscillation.

6. The system of claim 5, wherein the actuator is a piezoelectric element and is configured at the same time to be used as a sensor.

7. The system of claim 1, wherein the actuator is an electrodynamic actuator.

8. The system of claim 1, wherein the sensors are arranged on the outer conduit surface.

9. The system of claim 1, wherein, for the purpose of de-icing, the temperature of air flowing through the conduit is increased.

10. A method for the measurement and prevention of icing in a conduit, comprising:

measuring oscillation by a plurality of sensors for measuring mechanical oscillations of the conduit, selectively generating oscillation for measuring the ice build-up if the conduit is not made to sufficiently oscillate as a result of operation of the air conditioning system,

determining of local and global increases of weight by correlating the sensor data with known characteristics associated with the conduit and, if a predetermined local or global thickness of an ice layer has been exceeded,

emitting a signal to trigger a de-icing process.

11. The method of claim 10, wherein, for the purpose of de-icing, the temperature of the air flowing through the conduit is increased.

12. An aircraft comprising an air conditioning system, including a system for the measurement and prevention of icing in a conduit, the system comprising:

a plurality of sensors for acquiring mechanical oscillations of the conduit, an electronic evaluation unit and an electronic control unit,

wherein the sensors are connected to the electronic evaluation unit, the evaluation unit comprises characteristics relating to the oscillation behaviour of the conduit and is equipped to compare the measured conduit oscillations with the characteristics, and by means of correlation to interpret them as conduit icing, and in the case of conduit icing to emit a signal to the control unit,

wherein the evaluation unit is equipped, from sensor data and correlation with known characteristics that are associated with the conduit, to determine local and global increases in the mass of the conduit and thus of an ice layer, and, if a specified local or global thickness of the ice layer is exceeded, to emit a signal to the control unit for triggering a de-icing procedure.