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    • 1. 发明申请
    • Pneumatic rock drill
    • 气动凿岩机
    • US20070000694A1
    • 2007-01-04
    • US10548584
    • 2004-03-15
    • Michael DaviesDavid GeeJames CreswellStephen Jones
    • Michael DaviesDavid GeeJames CreswellStephen Jones
    • E21B10/36
    • B25D17/24B25D17/265B25D2216/0023B25D2222/72
    • The invention relates to a pneumatic rockdrill (99) comprising: a housing, including an air supply inlet for receiving compressed air, and a cylinder (50), connected to the air supply inlet by a set of air passages; an impact piston (14), at least part of which is reciprocable within the cylinder (50); and air-flow control means for controlling the supply of compressed air from the air supply inlet to the cylinder (50); the rockdrill (99) including at least one pair of corresponding contact surfaces at which relatively-moving parts contact one another; and the rockdrill being characterized by including at least one water supply inlet and water paths connected to the water supply inlet(s) and configured so as in operation to convey water to a drilling tool so as to flush a hole being drilled and to supply water to wet the aforesaid contact surfaces.
    • 本发明涉及一种气动钻石(99),包括:壳体,包括用于接收压缩空气的空气供应入口,以及通过一组空气通道连接到空气供应入口的气缸(50); 冲击活塞(14),其至少一部分可在气缸(50)内往复运动; 以及气流控制装置,用于控制从空气供应入口到气缸(50)的压缩空气的供应; 所述岩石钻(99)包括至少一对相应的接触表面,相对移动的部分彼此接触; 并且所述岩屑的特征在于包括至少一个供水入口和连接到所述供水入口的水路径,并且被构造成在操作中将水输送到钻孔工具,以便冲洗所钻孔并供水 以润湿上述接触表面。
    • 2. 发明授权
    • Device for inhibiting the flow of oil along a rotating shaft
    • 用于抑制沿着旋转轴的油流动的装置
    • US08147181B2
    • 2012-04-03
    • US12757987
    • 2010-04-10
    • David GeeJonathon HeslopIain Taylor
    • David GeeJonathon HeslopIain Taylor
    • F01D25/18
    • F01D25/183F04D29/063F04D29/102F05D2220/40F05D2240/70F05D2250/232F05D2250/314F16C17/02F16C17/18F16C33/10F16C33/74F16C2360/24F16J15/441
    • An oil control device inhibits the flow of oil along a shaft (8) rotating about an axis. The oil control device comprises an annular body (19) for rotation with said shaft (8) and includes a first face (30) extending generally radially from said axis. A second radially outer circumferential surface (40) is provided, extending generally axially. An oil slinging groove (32) extends into said body (19) and has a mouth (37) defined between a first circumferentially extending rim (38) and a second circumferentially extending rim (39). The second rim (39) is spaced both radially and axially from the first rim (38). The groove (32) is defined at least in part by a wall (34) which meets the first rim (38) at an acute angle to a radial plane. The groove (32) is also defined at least in part by a wall (35) which meets the second rim (39) at an acute angle to the direction of the axis.
    • 油控制装置抑制沿着绕轴旋转的轴(8)的油流。 油控制装置包括用于与所述轴(8)一起旋转的环形体(19),并且包括从所述轴线大致径向延伸的第一面(30)。 设置有大致轴向延伸的第二径向外圆周表面(40)。 一个油料悬挂槽(32)延伸到所述本体(19)中并且具有限定在第一周向延伸的边缘(38)和第二周向延伸的边缘(39)之间的口(37)。 第二边缘(39)在第一边缘(38)的径向和轴向间隔开。 凹槽(32)至少部分地由与径向平面呈锐角相遇的第一边缘(38)的壁(34)限定。 凹槽(32)至少部分地由与该轴线方向呈锐角相遇的第二边缘(39)的壁(35)限定。
    • 4. 发明授权
    • Turbomachine
    • 涡轮机
    • US08328509B2
    • 2012-12-11
    • US12757992
    • 2010-04-10
    • David GeeChris EnrightRobert Holroyd
    • David GeeChris EnrightRobert Holroyd
    • F01D25/08
    • F01D25/183F01D11/003F01D25/145F01D25/186F02C7/28F05D2220/40F05D2240/40F05D2240/70F05D2250/314F16J15/006F16J15/164F16J15/441
    • A turbomachine comprises a housing (71) defining a bearing cavity (71) and a turbine chamber (77a) separated by a first wall. A heat shield (72) is disposed between the first wall and the turbine wheel (77), a heat shield cavity (78) being defined between the first wall and the heat shield (72). The shaft (81) extends through a passage (85) defined at least in part by a first aperture (86) in said wall and a second aperture (87) in the heat shield (72). A first seal (88) is provided between the shaft (81) and said first aperture (86). The housing defines a first gas channel (79) communicating with the heat shield cavity (78) for connection to a pressure source for raising pressure within the heat shield cavity (78). A second channel (92) is provided between the heat shield cavity (78) and said passage (85), the second channel opening to said passage (85) on the opposite side of said first seal (88) to said bearing assembly (82). A second seal (89) is provided between the shaft (81) and said second aperture (87).
    • 涡轮机包括限定轴承腔(71)的壳体(71)和由第一壁分隔开的涡轮室(77a)。 隔热罩(72)设置在第一壁和涡轮机叶轮(77)之间,隔热罩(78)限定在第一壁和隔热罩(72)之间。 轴(81)延伸穿过至少部分地由所述壁中的第一孔(86)限定的通道(85)和隔热罩(72)中的第二孔(87)。 第一密封件(88)设置在轴(81)和所述第一孔(86)之间。 壳体限定与隔热腔(78)连通的第一气体通道(79),用于连接到用于升高隔热腔(78)内的压力的压力源。 第二通道(92)设置在隔热罩(78)和所述通道(85)之间,第二通道与所述第一密封件(88)相对的所述通道(85)通向所述轴承组件(82) )。 第二密封件(89)设置在轴(81)和所述第二孔(87)之间。
    • 6. 发明申请
    • Method of determining a data rate and apparatus therefor
    • 确定数据速率的方法及其装置
    • US20050165579A1
    • 2005-07-28
    • US11014250
    • 2004-12-17
    • David Gee
    • David Gee
    • H04L25/02G06F101/14
    • H04L25/0262
    • A data rate determination apparatus includes an edge detection and clock generation circuit for receiving an input bit stream. The edge detection and clock generation circuit generates a pulse for each edge detected in the input bit stream. The pulses are passed to a programmable re-triggerable monostable multivibrator circuit coupled to a binary counter, which counts how many pulses are received within a time period determined by the number of pulses received at a rate higher than a predetermined rate. The binary counter is coupled to a Gray code counter coupled to a processing unit. The processing unit uses different counts that are accumulated over different sampling periods with different predetermined rates to establish statistical data, which can be compared to known data for different data rate standards or formats.
    • 数据速率确定装置包括用于接收输入比特流的边缘检测和时钟生成电路。 边缘检测和时钟产生电路在输入比特流中检测到的每个边缘产生脉冲。 脉冲被传递到耦合到二进制计数器的可编程可重复触发的单稳态多谐振荡器电路,二进制计数器计数在由高于预定速率的速率接收的脉冲数确定的时间段内接收多少个脉冲。 二进制计数器耦合到耦合到处理单元的格雷码计数器。 处理单元使用在具有不同预定速率的不同采样周期上累积的不同计数来建立统计数据,其可以与用于不同数据速率标准或格式的已知数据进行比较。
    • 7. 发明申请
    • TURBOMACHINE
    • 涡轮机
    • US20100196148A1
    • 2010-08-05
    • US12757992
    • 2010-04-10
    • David GeeChris EnrightRobert Holroyd
    • David GeeChris EnrightRobert Holroyd
    • F01D25/08F04D29/12
    • F01D25/183F01D11/003F01D25/145F01D25/186F02C7/28F05D2220/40F05D2240/40F05D2240/70F05D2250/314F16J15/006F16J15/164F16J15/441
    • A turbomachine comprises a housing (71) defining a bearing cavity (71) a and a turbine chamber (77a) separated by a first wall. A heat shield (72) is disposed between the first wall and the turbine wheel (77), a heat shield cavity (78) being defined between the first wall and the heat shield (72). The shaft (81) extends through a passage (85) defined at least in part by a first aperture (86) in said wall and a second aperture (87) in the heat shield (72). A first seal (88) is provide between the shaft (81) and said first aperture (86). The housing defines a first gas channel (79) communicating with the heat shield cavity (78) for connection to a pressure source for raising pressure within the heat shield cavity (78). A second channel (92) is provided between the heat shield cavity (78) and said passage (85), the second channel opening to said passage (85) on the opposite side of said first seal (88) to said bearing assembly (82). A second seal (89) is provided between the shaft (81) and said second aperture (87).
    • 涡轮机包括限定轴承腔(71)a的壳体(71)和由第一壁分隔开的涡轮室(77a)。 隔热罩(72)设置在第一壁和涡轮机叶轮(77)之间,隔热罩(78)限定在第一壁和隔热罩(72)之间。 轴(81)延伸穿过至少部分地由所述壁中的第一孔(86)限定的通道(85)和隔热罩(72)中的第二孔(87)。 在轴(81)和所述第一孔(86)之间提供第一密封件(88)。 壳体限定与隔热腔(78)连通的第一气体通道(79),用于连接到用于升高隔热腔(78)内的压力的压力源。 第二通道(92)设置在隔热罩(78)和所述通道(85)之间,第二通道与所述第一密封件(88)相对的所述通道(85)通向所述轴承组件(82) )。 第二密封件(89)设置在轴(81)和所述第二孔(87)之间。
    • 9. 发明申请
    • DEVICE FOR INHIBITING THE FLOW OF OIL ALONG A ROTATING SHAFT
    • 用于抑制旋转轴上的油流动的装置
    • US20100196140A1
    • 2010-08-05
    • US12757987
    • 2010-04-10
    • David GeeJonathon HeslopIain Taylor
    • David GeeJonathon HeslopIain Taylor
    • F04D29/06F16N7/26
    • F01D25/183F04D29/063F04D29/102F05D2220/40F05D2240/70F05D2250/232F05D2250/314F16C17/02F16C17/18F16C33/10F16C33/74F16C2360/24F16J15/441
    • An oil control device inhibits the flow of oil along a shaft (8) rotating about an axis. The oil control device comprises an annular body (19) for rotation with said shaft (8) and includes a first face (30) extending generally radially from said axis. A second radially outer circumferential surface (40) is provided, extending generally axially. An oil slinging groove (32) extends into said body (19) and has a mouth (37) defined between a first circumferentially extending rim (38) and a second circumferentially extending rim (39). The second rim (39) is spaced both radially and axially from the first rim (38). The groove (32) is defined at least in part by a wall (34) which meets the first rim (38) at an acute angle to a radial plane. The groove (32) is also defined at least in part by a wall (35) which meets the second rim (39) at an acute angle to the direction of the axis.
    • 油控制装置抑制沿着绕轴旋转的轴(8)的油流。 油控制装置包括用于与所述轴(8)一起旋转的环形体(19),并且包括从所述轴线大致径向延伸的第一面(30)。 设置有大致轴向延伸的第二径向外圆周表面(40)。 一个油料悬挂槽(32)延伸到所述本体(19)中并且具有限定在第一周向延伸的边缘(38)和第二周向延伸的边缘(39)之间的口(37)。 第二边缘(39)在第一边缘(38)的径向和轴向间隔开。 凹槽(32)至少部分地由与径向平面呈锐角相遇的第一边缘(38)的壁(34)限定。 凹槽(32)至少部分地由与该轴线方向呈锐角相遇的第二边缘(39)的壁(35)限定。