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ASTM C 1674 : 2023 : REDLINE

Current

Current

The latest, up-to-date edition.

Standard Test Method for Flexural Strength of Advanced Ceramics with Engineered Porosity (Honeycomb Cellular Channels) at Ambient Temperatures

Available format(s)

PDF

Language(s)

English

Published date

14-07-2023

€96.91
Excluding VAT

Committee
C 28
DocumentType
Redline
Pages
50
PublisherName
American Society for Testing and Materials
Status
Current
Supersedes

1.1This test method covers the determination of the flexural strength (modulus of rupture in bending) at ambient conditions of advanced ceramic structures with 2-dimensional honeycomb channel architectures.

1.2The test method is focused on engineered ceramic components with longitudinal hollow channels, commonly called “honeycomb” channels (see Fig. 1). The components generally have 30 % or more porosity and the cross-sectional dimensions of the honeycomb channels are on the order of 1 mm or greater. Ceramics with these honeycomb structures are used in a wide range of applications (catalytic conversion supports (1),2 high temperature filters (2, 3), combustion burner plates (4), energy absorption and damping (5), etc.). The honeycomb ceramics can be made in a range of ceramic compositions—alumina, cordierite, zirconia, spinel, mullite, silicon carbide, silicon nitride, graphite, and carbon. The components are produced in a variety of geometries (blocks, plates, cylinders, rods, rings).

FIG. 1General Schematics of Typical Honeycomb Ceramic Structures

General Schematics of Typical Honeycomb Ceramic Structures General Schematics of Typical Honeycomb Ceramic Structures

1.3The test method describes two test specimen geometries for determining the flexural strength (modulus of rupture) for a porous honeycomb ceramic test specimen (see Fig. 2):

FIG. 2Flexure Loading Configurations

Flexure Loading ConfigurationsFlexure Loading Configurations

L = Outer Span Length (for Test Method A, L = User defined; for Test Method B, L = 90 mm)

Note 1:4-Point-1/4Loading for Test Methods A1 and B.

Note 2:3-Point Loading for Test Method A2.

1.3.1Test Method A—A 4-point or 3-point bending test with user-defined specimen geometries, and

1.3.2Test Method B—A 4-point-1/4point bending test with a defined rectangular specimen geometry (13 mm × 25 mm × > 116 mm) and a 90 mm outer support span geometry suitable for cordierite and silicon carbide honeycombs with small cell sizes.

1.4The test specimens are stressed to failure and the breaking force value, specimen and cell dimensions, and loading geometry data are used to calculate a nominal beam strength, a wall fracture strength, and a honeycomb structure strength.

1.5Test results are used for material and structural development, product characterization, design data, quality control, and engineering/production specifications.

1.6The test method is meant for ceramic materials that are linear-elastic to failure in tension. The test method is not applicable to polymer or metallic porous structures that fail in an elastomeric or an elastic-ductile manner.

1.7The test method is defined for ambient testing temperatures. No directions are provided for testing at elevated or cryogenic temperatures.

1.8The values stated in SI units are to be regarded as standard (IEEE/ASTM SI 10). English units are sparsely used in this standard for product definitions and tool descriptions, per the cited references and common practice in the US automotive industry.

1.9This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use.

1.10This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

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