Abstract:
A ceramic rotor is produced by sequentially forming a ceramic rotary body portion, measuring the dynamic unbalance of the ceramic rotary body portion, grinding the ceramic rotary body portion to adjust the dynamic unbalance and then integrally coupling a rotary shaft to the ceramic rotary body portion.
Abstract:
Metallizing pastes are disclosed, which contain, as inorganic materials, 15 to 50% by weight of a component to form a glass phase and 50 to 85% by weight of a metallic molybdenum powder. The glass phase essentially consists of 5 to 25% by weight of Al.sub.2 O.sub.3, 35 to 55% by weight of SiO.sub.2 and 30 to 55% by weight of MnO. A process for metallizing ceramic members is also disclosed. The metallizing paste is applied to surfaces of the ceramic member and the dried. The ceramic member with the dried metallizing paste is then fired in a temperature range from 1,200.degree. to 1,400.degree. C. for 0.5 to 10 hours in a mixed gas of hydrogen gas and nitrogen gas in which a ratio in partial pressure between steam and hydrogen, (P.sub.H.sbsb.2.sub.O /P.sub.H.sbsb.2), is adjusted in a range from 10.sup.-6 to 10.sup.0.
Abstract translation:公开了金属化糊料,其包含作为无机材料的15至50重量%的组分以形成玻璃相和50至85重量%的金属钼粉末。 玻璃相基本上由5至25重量%的Al 2 O 3,35至55重量%的SiO 2和30至55重量%的MnO组成。 还公开了用于金属化陶瓷构件的方法。 将金属化糊料施加到陶瓷构件的表面并干燥。 然后,在氢气和氮气的混合气体中,在1200〜1400℃的温度范围内,将具有干燥金属化糊料的陶瓷构件烧成0.5〜10小时,其中蒸汽与氢气之间的分压比, (PH 2 O / PH 2)调整为10-6〜100的范围。
Abstract:
A metal-ceramic composite article obtained by press fitting a projection of a ceramic member into a hole formed in a metallic member has a high bonding force in the press-fitted portion and is free from separation between the ceramic member and the metallic member. The composite article exhibits high thermal resistance or wear resistance when used as a piston crown in a piston for an adiabatic engine or when used as a cam contacting surface of a tappet.
Abstract:
This invention relates to engine parts having high durability, which can be used at high operating temperatures. The engine parts comprise component members consisting mainly of the partially stabilized zirconia having high strength which is excellent in thermal insulation and mechanical strength. As the partially stabilized zirconia having high strength, use is made of ones in which thermal expansion hysteresis (difference of thermal expansion at an optional temperature in the thermal expansion during heating up and the thermal shrinkage during cooling down) is less than 0.4% and thermal expansion coefficient is more than 10.times.10.sup.-6 /.degree.C. The preferable engine parts having higher durability and reliability comprise component members consisting of a ceramic-metal composite body wherein the partially stabilized zirconia having a difference of thermal expansion coefficient being less than 3.times.10.sup.-6 /.degree.C. and a metal are bonded.
Abstract:
Ceramic honeycomb type recuperative heat exchangers having a large number of parallel channels formed of partition walls are disclosed, in which fluids to be heat-exchanged are passed through respective channels that are produced by extruding a ceramic raw batch material into a honeycomb structural body, drying the shaped honeycomb structural body, prior to or after firing step cutting off partition walls in the given rows of the honeycomb structural body in the axial direction of the channels to a given depth from the end surface of the honeycomb structural body and sealing only the end surfaces of said rows.
Abstract:
A high pressure metal vapor lamp and a transparent polycrystalline alumina tube therefor have been disclosed. The average crystal grain size at ends of the tube is selectively made smaller than that of the middle portion of the tube so that the mechanical strength and the thermal shock resistance of the end portions are made higher than those in the middle portion. Accordingly, the tube hardly causes cracks by a thermal shock when the both ends of the tube are sealed and when the lamp using the tube is switched on and off. Whereas middle portion of the tube has an excellent transparency so that the lamp has a high luminance efficiency.
Abstract:
Polycrystalline translucent alumina having an average grain size of alumina crystal grain being not smaller than 20.mu. and an average surface roughness of the fired body being not larger than 1/10 of the maximum grain size of alumina crystal grain and capable of being used for an envelope of a high pressure vapor discharge lamp, which is produced by shaping alumina composition powders consisting mainly of alumina into a given shape, primarily firing the shaped body under vacuum or in an atmosphere of hydrogen gas or dissociated ammonia gas at a temperature within 1,500.degree. C. and then secondarily firing the primarily fired body at a temperature of 1,650.degree.-1,900.degree. C., at least the temperature from 1,400.degree. C. to 1,700.degree. C. being raised at a rate of not lower than 200.degree. C./hr.
Abstract:
A sintered silicon nitride body consists of not more than 10% by weight in total of at least two metal oxides selected from the group consisting of beryllium oxide, magnesium oxide and strontium oxide (provided that each of the metal oxides is not more than 5% by weight) and the remainder of silicon nitride and may further contain not more than 10% by weight of at least one rare earth metal oxide, and is produced by preparing a mixture having the said composition range and then molding and sintering it at 1,600.degree.-1,900.degree. C. in nitrogen or inert gas atmosphere.
Abstract:
A sintered silicon nitride body consists of not more than 10% by weight in total of at least two metal oxides selected from the group consisting of beryllium oxide, magnesium oxide and strontium oxide (provided that each of the metal oxides is not more than 5% by weight) and the remainder of silicon nitride and may further contain not more than 10% by weight of at least one rare earth metal oxide, and is produced by preparing a mixture having the said composition range and then molding and sintering it at 1,600.degree.-1,900.degree. C in nitrogen or inert gas atmosphere.