FORMATION OF HEAT INSULATING COATING SERIES
PROBLEM TO BE SOLVED: To provide a method for forming a heat insulating coating having resistance to spalling of gas turbine engine parts to be exposed to high temperature and also having low thermal conductivity. SOLUTION: A bonding coat is formed on the surface of parts 12, and then grit blasting...
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Main Authors | , , , , |
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Format | Patent |
Language | English |
Published |
04.04.2000
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Edition | 7 |
Subjects | |
Online Access | Get full text |
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Summary: | PROBLEM TO BE SOLVED: To provide a method for forming a heat insulating coating having resistance to spalling of gas turbine engine parts to be exposed to high temperature and also having low thermal conductivity. SOLUTION: A bonding coat is formed on the surface of parts 12, and then grit blasting is applied to the bonding coat by the medium of abrasives having 250-300 μm grain size. The parts 12 are supported in a coating chamber 10 containing an ingot 16 of desired ceramic material. An oxygen-containing gas has at least 0.006 mbar partial pressure of oxygen. The surface of the parts 12 is preheated to 1100 deg.C. The ceramic material, composed of yttria - stabilized zirconia, is evaporated by an electron beam at a rate of about 23.5 to 29.2 grams per minute. |
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Bibliography: | Application Number: JP19990123358 |