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    • 4. 发明申请
    • Chemical vapor deposition apparatus and method
    • 化学气相沉积装置及方法
    • US20060046059A1
    • 2006-03-02
    • US10926889
    • 2004-08-26
    • Alan AricoDavid ParkerAkshay WaghrayBrian MillerDavid Shaw
    • Alan AricoDavid ParkerAkshay WaghrayBrian MillerDavid Shaw
    • B32B9/00
    • C23C16/46C23C16/045Y10S427/10Y10T428/30
    • Apparatus such as a furnace muffle (11) for use in a CVI/CVD furnace. The apparatus includes a bottom (12), a top (13), and an outer wall (3) defining an interior space (1) in the apparatus, and a passive heat distribution element (7, 9) located within the interior space (1) and apart from the outer wall (3). Preferably, the bottom (12) and top (12) include perforated plates and the outer wall (3) is cylindrical in shape and all are made of graphite or carbon-carbon composite material and the passive heat distribution element (7, 9) is cylindrical in shape and includes graphite or carbon-carbon composite discs having no spacers therebetween. Also, a method for densifying a porous carbon preform (5), which method includes the steps of: (a) providing the apparatus (11); (b) charging the apparatus (11) with a plurality of stacks of annular porous carbon preforms (5), the preforms being separated from one another by spacers (15); (c) locating the charged apparatus (11) in a furnace at a temperature in the range of 950-1100° C. and a pressure in the range of 5-40 torr; and (d) circulating a natural gas reactant blended with up to 15% propane through the apparatus for 150-900 hours. Also, a batch of carbon-carbon composite preforms made by the method, wherein the density of the batch of preforms is at least 0.5 g/cc higher than the density of a batch of preforms made by an otherwise identical process in which the apparatus does not contain a passive heat distribution element located within its interior. The preforms may be configured as aircraft landing system brake discs or racing car brake discs.
    • 诸如用于CVI / CVD炉的炉马弗炉(11)的设备。 该装置包括底部(12),顶部(13)和限定设备中的内部空间(1)的外壁(3),以及位于内部空间内的被动热分配元件(7,9) 1)并且与外壁(3)分开。 优选地,底部(12)和顶部(12)包括多孔板,并且外壁(3)是圆柱形的,并且全部由石墨或碳 - 碳复合材料制成,并且被动散热元件(7,9) 圆柱形,包括在其间没有间隔物的石墨或碳 - 碳复合盘。 另外,一种致密化多孔碳预制件(5)的方法,该方法包括以下步骤:(a)提供装置(11); (b)用多个环状多孔碳预制件(5)堆叠装置(11),预型件通过间隔件(15)彼此分离; (c)将加料装置(11)定位在炉中,温度范围为950-1100℃,压力范围为5-40托; 和(d)将与多达15%丙烷混合的天然气反应物通过该装置循环150-900小时。 另外,通过该方法制造的一批碳 - 碳复合预成型件,其中预成型件批次的密度比通过其他相同工艺制造的一批预成型件的密度高至少0.5g / cc 不包含位于其内部的被动散热元件。 预成型件可以被配置为飞机着陆系统制动盘或赛车制动盘。
    • 5. 发明申请
    • Support structure for radiative heat transfer
    • 辐射传热支撑结构
    • US20070014990A1
    • 2007-01-18
    • US11480863
    • 2006-07-06
    • Alan AricoAkshay WaghrayDavid Parker
    • Alan AricoAkshay WaghrayDavid Parker
    • B32B9/00
    • C23C16/045C04B35/83C04B2235/614C23C16/26C23C16/4583C23C16/46Y10T428/30
    • Method for densifying porous carbon preforms. The method including: providing an apparatus charged with at least one stack of annular porous carbon-carbon composite preforms, the preforms being separated from one another by spacers emanating from a passive heat distribution element centrally located within a cylindrical space formed by the stack of annular preforms; locating the charged apparatus in a furnace at a temperature of 950-1100° C. and a pressure of 5-40 torr; and circulating a carbon-containing gas reactant through the apparatus for 150 to 900 hours. Also, an apparatus for practicing this method. The preforms are densified with less physical damage due to the weight of the preforms being treated than are preforms made by otherwise identical processes that do not separate preforms from the preforms immediately above and below them by spacer elements comprising tabs or shelves emanating from a central passive heat distribution structural member.
    • 密实多孔碳预制棒的方法。 该方法包括:提供装有至少一个环形多孔碳 - 碳复合预成型件堆叠的装置,预成型件通过间隔件彼此分隔开,该间隔物从位于由环形堆叠形成的圆柱形空间内的被动散热元件发出 预制件 将装料装置放置在炉中,温度为950-1100℃,压力为5-40托; 并将含碳气体反应物循环通过该设备150至900小时。 另外,实施这种方法的装置。 由于待处理的预成型件的重量,预成型件的加工比由比其他相同工艺制成的预成型件更小的物理损伤致密化,而不是通过间隔元件将预成型件与预制件分离,所述间隔元件包括从中心被动 配热结构件。