Erosion test apparatus, accelerator and erosion test method
View Patent ↗An erosion test apparatus includes a combustor configured to obtain a combustion gas by mixing and combusting compressed air and a fuel, and an erodent supply unit configured to supply an erodent to the combustion gas. The erosion test apparatus further includes an accommodation support unit configured to accommodate and support a test piece having a front surface coated through thermal barrier coating, and an accelerator configured to accelerate the combustion gas including the erodent to collide with the test piece.
1. An erosion test apparatus comprising:
a combustor configured to mix and combust compressed air and a fuel to obtain a combustion gas;
an erodent supply unit configured to supply an erodent to the combustion gas;
an accommodation support unit configured to accommodate and support a test piece having a front surface coated through thermal barrier coating;
an accelerator configured to accelerate the combustion gas including the erodent to collide with the test piece; and
a cooling unit configured to blow a coolant to a back surface of the test piece to cool the test piece,
wherein the accelerator comprises:
a tubular throttling section connected to the combustor and having a flow path cross-sectional area that reduces downstream in a direction in which the combustion gas is to flow; and
a straight pipe section extending in a straight pipe shape having a constant flow path cross-sectional area and connecting a downstream end section of the tubular throttling section and the accommodation support unit,
wherein the straight pipe section extends from the downstream end section of the tubular throttling section to an inside of an accommodation space of the accommodation support unit,
wherein a downstream end section of the straight pipe section is disposed immediately over the test piece, and
wherein the combustor comprises an air supply unit configured to supply air for temperature adjustment to the combustion gas.
2. The erosion test apparatus according to claim 1 , wherein the accommodation support unit comprises an observation window in communication with the accommodation space configured to accommodate the test piece.
3. An accelerator comprising:
a tubular throttling section having a flow path cross-sectional area that reduces downstream; and
a straight pipe section extending in a straight pipe shape having a constant flow path cross-sectional area downstream from a downstream end section of the tubular throttling section,
wherein an upstream end section of the tubular throttling section is connected to a combustor configured to mix and combust compressed air and a fuel to obtain a combustion gas,
wherein a downstream end of the straight pipe section is connected to an accommodation support unit configured to accommodate and support a test piece having a front surface coated through thermal barrier coating,
wherein the straight pipe section extends from the downstream end section of the tubular throttling section to an inside of an accommodation space of the accommodation support unit,
wherein a downstream end section of the straight pipe section is disposed immediately over the test piece, and
wherein an inclination angle of the tubular throttling section is larger than a repose angle of the erodent.
4. The accelerator according to claim 3 , wherein a length of the straight pipe section has an acceleration distance in a range of 0 to 1 m.
5. An erosion test method comprising:
a first step of supplying an erodent to a combustion gas obtained by mixing and combusting compressed air and a fuel,
a second step in which cooling air is blown from a back surface to a test piece on which thermal barrier coating is performed via a cooling unit,
a third step of accelerating a flow velocity of the combustion gas including the erodent by decreasing a flow path cross-sectional area, and
a fourth step of causing the combustion gas including the erodent accelerated to collide by using an accelerator with the test piece on which the thermal barrier coating is performed,
wherein, in the third step, the combustion gas including the erodent is accelerated to a flow velocity at which the erodent reaches a target velocity, and
wherein, in the fourth step, the erodent accelerated to the target velocity sequentially collides with the test piece on which the thermal barrier coating is performed,
wherein the accelerator comprises:
a tubular throttling section having a flow path cross-sectional area that reduces downstream in a direction in which the combustion gas is to flow; and
a straight pipe section extending in a straight pipe shape having a constant flow path cross-sectional area and connecting a downstream end section of the tubular throttling section and an accommodation support unit configured to accommodate and support the test piece,
wherein the straight pipe section extends from the downstream end section of the tubular throttling section to an inside of an accommodation space of the accommodation support unit, and
wherein a downstream end section of the straight pipe section is disposed immediately over the test piece.
6. The erosion test method according to claim 5 , wherein a target value of a particle velocity of the erodent is 200 m/s.