Method of detecting defects in honeycomb structural body

Patent metadata

Field	Value
Publication number	US-9709457-B2
Application number	US-201414329407-A
Country	US
Kind code	B2
Filing date	Jul 11, 2014
Priority date	Jul 11, 2013
Publication date	Jul 18, 2017
Grant date	Jul 18, 2017

Abstract

In a method of detecting defects generated in a honeycomb structural body, both end sections of the honeycomb structural body is sealed along a flowing direction of exhaust gas. Air is supplied in the flowing direction of the exhaust gas from one end section to the other end section of the honeycomb structural body. Microphones are arranged at outer periphery of the honeycomb structural body and detect sounds of air leaking from a skin layer of the honeycomb structural body. A judgment step judges whether or not defects such as holes having not less than a predetermined diameter and cracks are generated on the basis of a magnitude of the detected sounds of the leaking air.

First claim

What is claimed is:

1. A method of detecting defects generated in a honeycomb structural body comprised of a plurality of cell walls arranged in a lattice shape and with a skin layer, the cell walls being arranged to form a plurality of cells, each of the cells having a polygonal shape in a cross section of the honeycomb structural body perpendicular to a gas supply direction, and an outer peripheral surface of the honeycomb structural body being covered with the skin layer, the method comprising steps of:
sealing both end sections of the honeycomb structural body;
supplying gas from one end section to the other end section of the honeycomb structural body;
detecting sounds of gas leaking from the skin layer of the honeycomb structural body by using one or more microphones arranged at an outer periphery of the skin layer; and
judging a presence of defects such as holes having a predetermined diameter and cracks generated in the skin layer on the basis of a detected magnitude of sounds of the leaking gas;
wherein in the sealing step, balloons hold and support the outer periphery near to the end sections of the honeycomb structural body in order to seal both the end sections of the honeycomb structural body by using the balloons.

2. The method of detecting defects of the honeycomb structural body according to claim 1 , wherein in the sealing step, the balloons hold and support both the end sections of the honeycomb structural body by a pressure within a range of 0.1 to 0.5 MPa.

3. The method of detecting defects of the honeycomb structural body according to claim 1 , wherein
the one or more microphones are arranged parallel to a cell formation direction in the honeycomb structural body around the outer periphery of the skin layer of the honeycomb structural body, and
in the detection step of detecting sounds of gas leaking from the skin layer of the honeycomb structural body, and the honeycomb structural body and the one or more microphones are rotated relatively to each other along a peripheral direction of the skin layer by not less than one rotation, and
the judgment step compares a relative strength of sounds of gas leaking from the honeycomb structural body during the relative rotation of the honeycomb structural body and the one or more microphones, and judges whether or not defects are generated in the honeycomb structural body on the basis of the comparison results.

4. The method of detecting defects of the honeycomb structural body according to claim 3 , wherein
in the detection step, the gas has a pressure of not less than 0.1 MPa and is supplied to the inside of the honeycomb structural body.

5. The method of detecting defects of the honeycomb structural body according to claim 4 , wherein in the sealing step, the balloons hold and support both the end sections of the honeycomb structural body by a pressure within a range of 0.1 to 0.5 MPa.

6. The method of detecting defects of the honeycomb structural body according to claim 3 , wherein
in the detection step, the honeycomb structural body is rotated around the one or more microphones along the peripheral direction of the skin layer by not less than one rotation.

7. The method of detecting defects of the honeycomb structural body according to claim 3 , wherein
in the detection step, the one or more microphones are rotated around the peripheral direction of the skin layer of the honeycomb structural body by not less than one rotation.

8. A method of detecting defects generated in a honeycomb structural body comprised of a plurality of cell walls arranged in a lattice shape and with a skin layer, the cell walls being arranged to form a plurality of cells, each of the cells having a polygonal shape in a cross section of the honeycomb structural body perpendicular to a gas supply direction, and an outer peripheral surface of the honeycomb structural body being covered with the skin layer, the method comprising steps of:
sealing both end sections of the honeycomb structural body;
supplying gas from one end section to the other end section of the honeycomb structural body;
detecting sounds of gas leaking from the skin layer of the honeycomb structural body by using one or more microphones arranged at an outer periphery of the skin layer; and
judging a presence of defects such as holes having a predetermined diameter and cracks generated in the skin layer on the basis of a detected magnitude of sounds of the leaking gas; wherein:
in the detection step, the gas has a pressure of not less than 0.1 MPa and is supplied to the inside of the honeycomb structural body; and
in the sealing step, balloons hold and support the outer periphery near to the end sections of the honeycomb structural body in order to seal both the end sections of the honeycomb structural body by using the balloons.

9. The method of detecting defects of the honeycomb structural body according to claim 8 , wherein in the sealing step, the balloons hold and support both the end sections of the honeycomb structural body by a pressure within a range of 0.1 to 0.5 MPa.

Assignees

• Denso Corp

Inventors

• Sugiyama Tomio
• Miyamura Yasushi
• Inada Hiromi
• Hori Kouji
• Matsubara Kazuo

Classifications

• G01M3/24 Primary

  using infrasonic, sonic or ultrasonic vibrations · CPC title

• B01D46/2418

  Honeycomb filters (used for filtering exhaust gases of an internal combustion engine F01N3/022; ceramic honeycomb structures per se C04B38/0006) · CPC title