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    • 1. 发明申请
    • Chassis Having a Bypass Channel for Air Flow
    • 具有旁路通道用于气流的底盘
    • US20090109612A1
    • 2009-04-30
    • US11926890
    • 2007-10-29
    • David L. MossPaul T. ArtmanWilliam Coxe, IIIShawn P. Hoss
    • David L. MossPaul T. ArtmanWilliam Coxe, IIIShawn P. Hoss
    • H05K7/20G06F1/20
    • G06F1/20
    • A chassis having a bypass channel for air flow is disclosed. The chassis include a bypass channel that is proximate one side of the chassis. The bypass channel may be formed by the side of the chassis and a module of the computing system, such as the processor module of the computing system. A second module exists in the rear of the chassis. A physical barrier may be used to direct air from the bypass channel to the second module, which may be an I/O module. A plenum is placed on the opposite side of I/O module from the air flow. The presence of the plenum creates a negative pressure on the opposite side of the second module, causing air to cross the second module into the plenum. A fan in the rear of the chassis causes air to leave the plenum and exit the chassis.
    • 公开了一种具有用于空气流动的旁路通道的底架。 底盘包括靠近机箱一侧的旁路通道。 旁路通道可以由机箱的侧面和计算系统的模块(诸如计算系统的处理器模块)形成。 第二个模块位于机箱的后部。 可以使用物理障碍物将空气从旁路通道引导到第二模块,其可以是I / O模块。 在空气流动的I / O模块的相对侧放置一个增压室。 增压室的存在在第二模块的相对侧产生负压,导致空气穿过第二模块进入增压室。 机箱后部的风扇使空气离开集气室并离开机箱。
    • 2. 发明授权
    • Chassis having a bypass channel for air flow
    • 底盘具有用于气流的旁路通道
    • US07751186B2
    • 2010-07-06
    • US11926890
    • 2007-10-29
    • David L. MossPaul T. ArtmanWilliam CoxeShawn P. Hoss
    • David L. MossPaul T. ArtmanWilliam CoxeShawn P. Hoss
    • H05K7/20H05K5/00G06F1/20
    • G06F1/20
    • A chassis having a bypass channel for air flow is disclosed. The chassis include a bypass channel that is proximate one side of the chassis. The bypass channel may be formed by the side of the chassis and a module of the computing system, such as the processor module of the computing system. A second module exists in the rear of the chassis. A physical barrier may be used to direct air from the bypass channel to the second module, which may be an I/O module. A plenum is placed on the opposite side of I/O module from the air flow. The presence of the plenum creates a negative pressure on the opposite side of the second module, causing air to cross the second module into the plenum. A fan in the rear of the chassis causes air to leave the plenum and exit the chassis.
    • 公开了一种具有用于空气流动的旁路通道的底架。 底盘包括靠近机箱一侧的旁路通道。 旁路通道可以由机箱的侧面和计算系统的模块(诸如计算系统的处理器模块)形成。 第二个模块位于机箱的后部。 可以使用物理障碍物将空气从旁路通道引导到第二模块,其可以是I / O模块。 在空气流动的I / O模块的相对侧放置一个增压室。 增压室的存在在第二模块的相对侧产生负压,导致空气穿过第二模块进入增压室。 机箱后部的风扇使空气离开集气室并离开机箱。
    • 4. 发明授权
    • Heat dissipation apparatus utilizing empty component slot
    • 利用空组件槽的散热装置
    • US07480147B2
    • 2009-01-20
    • US11549453
    • 2006-10-13
    • Shawn P. HossPaul T. Artman
    • Shawn P. HossPaul T. Artman
    • H05K7/20H01R13/00
    • G06F1/20H01L2924/0002H01L2924/00
    • A heat dissipation apparatus includes a first commponent connector defining a first component slot immediately adjacent the first component connector, wherein the first component connector is located adjacent to and spaced apart from a second component connector that defines a second component slot. A heat dissipating member is thermally coupled to a heat producing component such that the heat dissipating member is located in the second component slot that is defined by the second component connector when the heat producing component is coupled to the first component connector and located in the first component slot. The heat dissipation apparatus may be coupled to a heat producing component and used to dissipate heat from the heat producing component when there are empty component connector slots located adjacent the component connector that the heat producing component is coupled to.
    • 散热装置包括限定紧邻第一部件连接器的第一部件槽的第一部件连接器,其中第一部件连接器位于与限定第二部件槽的第二部件连接器相邻并间隔开的位置。 散热构件热耦合到发热部件,使得当发热部件联接到第一部件连接器并位于第一部件连接器中时,散热部件位于由第二部件连接器限定的第二部件槽中 组件插槽 散热装置可以耦合到发热部件,并且当存在位于发热部件耦合到的部件连接器附近的空的部件连接器插槽时,用于散发来自发热部件的热量。
    • 9. 发明申请
    • Synthetic Air Jet Cooling System
    • 合成喷气冷却系统
    • US20110122571A1
    • 2011-05-26
    • US12624002
    • 2009-11-23
    • Paul T. ArtmanDominick LovicottShawn P. HossWilliam K. Coxe, III
    • Paul T. ArtmanDominick LovicottShawn P. HossWilliam K. Coxe, III
    • G06F1/20
    • G06F1/206Y02D10/16
    • A synthetic air jet cooling system includes a first component. A fan is in fluid communication with the first component. A synthetic air jet is located adjacent the first component. A thermal management engine is coupled to the first component, the fan, and the synthetic air jet. The thermal management engine is operable to receive a first component operating condition, compare the first component operating condition to a target operating condition, and increase a fan fluid flow rate from the fan and a synthetic air jet fluid flow rate from the synthetic air jet in order to reduce the difference between the first component operating condition the target operating condition. The thermal management engine increases the synthetic air jet fluid flow rate from the synthetic air jet to a predetermined synthetic air jet fluid flow rate prior to increasing the fan fluid flow rate from the fan in order to provide improvements in power consumption, airflow, and acoustics.
    • 合成空气喷射冷却系统包括第一部件。 风扇与第一部件流体连通。 合成空气射流位于第一组件附近。 热管理引擎联接到第一部件,风扇和合成空气喷嘴。 热管理引擎可操作以接收第一部件操作条件,将第一部件操作条件与目标操作条件进行比较,并且增加来自风扇的风扇流体流速和来自合成空气射流的合成空气喷射流体流速 以减少第一部件运行状态与目标运行状态的差异。 在增加来自风扇的风扇流体流速之前,热管理引擎将合成空气射流流体从合成空气射流增加到预定的合成空气喷射流体流速,以提供功率消耗,气流和声学方面的改进 。