Method for enabling a substantially constant total fuel energy rate
within a dual fuel engine
    11.
    发明授权
    Method for enabling a substantially constant total fuel energy rate within a dual fuel engine 失效
    在双燃料发动机内实现基本恒定的总燃料能量速率的方法

    公开(公告)号:US5937800A

    公开(公告)日:1999-08-17

    申请号:US36199

    申请日:1998-03-06

    摘要: A method for delivering liquid fuel and gaseous fuel to a dual fuel engine operating in a dual fuel mode includes establishing a governor output value indicative of a total fuel energy rate desired to be delivered to the engine to maintain a desired engine speed. A first value indicative of a liquid pilot fuel energy rate desired to be delivered to the engine and a second value indicative of a gaseous fuel energy rate desired to be delivered to the engine are each determined such that the sum of the desired liquid pilot fuel energy rate and the desired gaseous fuel energy rate is substantially equal to the desired total fuel energy. A stored gaseous fuel energy content can be updated to assure continued accuracy of the fuel control system of the dual fuel engine.

    摘要翻译: 将液体燃料和气体燃料输送到以双燃料模式运行的双重燃料发动机的方法包括建立一个调节器输出值,其指示期望输送到发动机的总燃料能量速率以维持期望的发动机转速。 指示期望输送到发动机的液体先导燃料能量速率的第一值和指示期望输送到发动机的气体燃料能量速率的第二值各自被确定为使得期望的液体引燃燃料能量的总和 速率和期望的气体燃料能量速率基本上等于期望的总燃料能量。 可以更新储存的气体燃料能量含量以确保双燃料发动机的燃料控制系统的持续精度。

    Endoscopic knot tying tool and method
    12.
    发明授权
    Endoscopic knot tying tool and method 失效
    内镜结结扎工具及方法

    公开(公告)号:US5423836A

    公开(公告)日:1995-06-13

    申请号:US124675

    申请日:1993-09-22

    申请人: Scott C. Brown

    发明人: Scott C. Brown

    IPC分类号: A61B17/04 A61B17/06 A61B17/00

    摘要: A method and a tool for tying a stitch knot. The tool comprises a first elongated member and a grasping member. The first elongated member includes a helix on one end. The helix has a filament extending from the first end, and a threading device is attached to the free end of the filament. The grasping member is separate and apart from the first elongated member, and includes an elongated shaft. A grasper is mounted on the first end of the shaft, and a portion of the shaft near the grasper is sized to reside within the helix for axial movement therewith. The method for tying the stitch knot involves positioning the shaft within the helix. The grasper is used to insert the threading device and pull the free end of the filament through an area to be stitched, and then to grasp the free end of the filament near the threading device. The grasping member is removed from the inner space of the helix, thus drawing the free end of the filament through the helix. When the grasping member and helix are moved apart from each other and the filament is removed from the helix, a loop for the stitch knot is formed. Moving the grasping member and helix further apart tightens the loop to the area to be stitched.

    摘要翻译: 用于捆扎针结的方法和工具。 该工具包括第一细长构件和把持构件。 第一细长构件在一端包括螺旋。 螺旋具有从第一端延伸的细丝,并且穿线装置附接到细丝的自由端。 夹持构件与第一细长构件分离并分离,并且包括细长轴。 抓紧器安装在轴的第一端上,并且靠近抓紧器的轴的一部分的尺寸设置成位于螺旋线内以与其轴向移动。 用于捆扎针结的方法包括将轴定位在螺旋内。 夹持器用于插入穿线装置并将细丝的自由端拉过要缝合的区域,然后将螺丝的自由端靠近穿线装置。 把持部件从螺旋的内部空间中取出,由此将丝的自由端拉过螺旋。 当夹持构件和螺旋线彼此分离并且从螺旋线去除细丝时,形成用于针结的环。 将握持构件和螺旋线进一步分开将环圈收紧到要缝合的区域。

    Method for a controlled transition between operating modes of a dual
fuel engine
    15.
    发明授权
    Method for a controlled transition between operating modes of a dual fuel engine 失效
    双燃料发动机的操作模式之间受控转换的方法

    公开(公告)号:US6101986A

    公开(公告)日:2000-08-15

    申请号:US36198

    申请日:1998-03-06

    摘要: A method for transitioning between a first operating mode of a dual fuel engine and a second operating mode of the dual fuel engine includes establishing a final liquid fuel amount desired to be delivered to the engine upon completion of the transition to the second operating mode. Delivery of liquid fuel to the engine is adjusted by a first amount and, correspondingly, delivery of gaseous fuel to the engine is adjusted by a second amount, where an energy content of the first amount of liquid fuel is substantially the same as an energy content of the second amount of gaseous fuel. A determination is made as to whether liquid fuel is being delivered to the engine in an amount which is substantially the same as the desired final liquid amount previously established. The fuel adjustment step and the determination step are repeated until a determination is made that liquid fuel is being delivered to the engine in an amount which is substantially the same as the desired final liquid fuel amount, at which point the transition is considered complete.

    摘要翻译: 一种用于在双燃料发动机的第一操作模式和双燃料发动机的第二操作模式之间转换的方法包括在完成向第二操作模式的转变时建立期望输送到发动机的最终液体燃料量。 向发动机的液体燃料的输送被调节第一量,相应地,向发动机的气体燃料的输送被调节第二量,其中第一量的液体燃料的能量含量基本上与能量含量相同 的第二量的气体燃料。 确定液体燃料是否以与先前建立的所需最终液体量基本相同的量被输送到发动机。 重复燃料调节步骤和确定步骤,直到确定液体燃料以与期望的最终液体燃料量基本相同的量被输送到发动机为止,此时过渡被认为是完整的。

    Apparatus for an engine control system
    16.
    发明授权
    Apparatus for an engine control system 失效
    发动机控制系统的装置

    公开(公告)号:US6073592A

    公开(公告)日:2000-06-13

    申请号:US36366

    申请日:1998-03-06

    摘要: In one embodiment of the present invention an apparatus for controlling one or more engines by synchronizing the functions of two or more electronic control modules includes a master electronic control module, one or more slave electronic control modules, and one or more data links for transferring data between the electronic control modules. Engine control and monitoring functions are divided between the master electronic control module and the slave electronic control modules. The present invention may be used to control and monitor dual fuel engines and engines that operate on one type of fuel. The master electronic control module may transition operation of the engine to the diesel fuel only mode in the event of a failure of any dual fuel mode specific components. The master ECM coordinates timing and speed of fuel injection to engine cylinders using input from an adjustable engine speed command device and a speed sensor connected to each engine. The loads driven by the engines may be allocated evenly or unevenly.

    摘要翻译: 在本发明的一个实施例中,用于通过同步两个或多个电子控制模块的功能来控制一个或多个引擎的装置包括主电子控制模块,一个或多个从属电子控制模块和用于传送数据的一个或多个数据链路 电子控制模块之间。 发动机控制和监控功能分为主电子控制模块和从属电子控制模块。 本发明可以用于控制和监视在一种类型的燃料上操作的双燃料发动机和发动机。 在任何双燃料模式特定部件发生故障的情况下,主电子控制模块可以将发动机的操作转变为仅柴油燃料模式。 主机ECM使用来自可调发动机速度指令装置和连接到每个发动机的速度传感器的输入来协调对发动机气缸的燃料喷射的时间和速度。 由发动机驱动的负载可以均匀地或不均匀地分配。

    Method and apparatus for detecting gaseous fuel leakage through a
gaseous fuel admission valve within an engine
    17.
    发明授权
    Method and apparatus for detecting gaseous fuel leakage through a gaseous fuel admission valve within an engine 失效
    用于检测通过发动机内的气体燃料入口阀的气体燃料泄漏的方法和装置

    公开(公告)号:US6044806A

    公开(公告)日:2000-04-04

    申请号:US994693

    申请日:1997-12-19

    摘要: A method of detecting leakage through a gaseous fuel admission valve of a dual fuel engine including at least one such gaseous fuel admission valve and a gaseous fuel shut off valve includes determining a liquid fuel rate when the engine is operating in a liquid fuel mode and the gaseous fuel shut off valve is closed. The gaseous fuel shut off valve is thereafter opened while the engine is operating in the liquid fuel mode. A liquid fuel rate is determined after the gaseous fuel shut off valve is opened and the liquid fuel rate determined before opening of the gaseous fuel shut off valve is compared with the liquid fuel rate determined after opening of the gaseous fuel shut off valve. A detonation level within the engine cylinder may also be checked to determine if such detonation level exceeds a predetermined level indicative of gaseous fuel leakage. The detonation level check may also be utilized in a spark-ignited engine.

    摘要翻译: 检测通过包括至少一个这样的气体燃料入口阀和气体燃料截止阀的双燃料发动机的气体燃料入口阀的泄漏的方法包括当发动机以液体燃料模式运行时确定液体燃料速率, 气体燃料截止阀关闭。 之后气体燃料切断阀在发动机以液体燃料模式运转时打开。 在气体燃料截止阀打开之后并且在气体燃料切断阀打开之前确定的液体燃料比与在气体燃料截止阀打开之后确定的液体燃料比进行比较来确定液体燃料速率。 还可以检查发动机气缸内的爆震水平以确定这种爆震水平是否超过指示气体燃料泄漏的预定水平。 引爆水平检查也可用于火花点火发动机。

    Advancing gelation front cure technique
    18.
    依法登记的发明
    Advancing gelation front cure technique 失效
    推进凝胶化前固化技术

    公开(公告)号:USH559H

    公开(公告)日:1988-12-06

    申请号:US48856

    申请日:1987-05-12

    申请人: Scott C. Brown

    发明人: Scott C. Brown

    摘要: A method for curing resin in the fabrication of a composite material is described comprising enclosing the composite material within a flexible vacuum enclosure, and substantially simultaneously pressing the material within the enclosure between first and second platens of a press to preselected pressure, evacuating the enclosure, selectively heating one of the platens according to a preselected scheme to preselected cure temperature to cure the resin within the material, and cooling the other platen to maintain a preselected temperature differential between the platens across the thickness of the material, whereby cure of the resin is effected in the material first near the heated platen and progresses through the thickness of the material toward the cooler platen as the material is heated to the cure temperature.

    Method for achieving minimum liquid pilot fuel delivery to each cylinder of a dual fuel engine while operating in a dual fuel mode
    19.
    发明授权
    Method for achieving minimum liquid pilot fuel delivery to each cylinder of a dual fuel engine while operating in a dual fuel mode 失效
    用于在双燃料模式下操作时实现双燃料发动机的每个气缸的最小液体先导燃料输送的方法

    公开(公告)号:US06289871B1

    公开(公告)日:2001-09-18

    申请号:US09036045

    申请日:1998-03-06

    IPC分类号: F02B300

    摘要: A method for controlling and adjusting the delivery of liquid pilot fuel to each cylinder of a dual fuel engine during a dual fuel operating mode so as to both minimize the quantity of liquid pilot fuel being delivered to each individual cylinder while, at the same time, ensuring that such minimum quantity of liquid pilot fuel provides complete combustion performance within each such cylinder wherein certain cylinder performance parameters such as exhaust port temperature or cylinder pressure are evaluated on a per cylinder basis in order to determine cylinder performance. The present method establishes certain predetermined incremental changes in the selected cylinder performance parameters, which changes are indicative of poor or deteriorated combustion performance within any particular cylinder, and thereafter varies the amount of liquid pilot fuel delivered to such cylinder based upon an analysis and evaluation of changes occurring in the selected cylinder performance parameters. Although it is preferred that each cylinder be evaluated on an individual basis, it is recognized and anticipated that, in some applications, the present method may be used to control the delivery of liquid pilot fuel to two or more cylinders simultaneously.

    摘要翻译: 一种用于在双燃料运行模式期间控制和调节液体引燃燃料输送到双燃料发动机的每个气缸的方法,以便使输送到每个气缸的液体引燃燃料的量最小化,同时, 确保这种最小量的液体引燃燃料在每个这样的气缸内提供完整的燃烧性能,其中某些气缸性能参数(例如排气口温度或气缸压力)以每缸为基础进行评估,以便确定气缸性能。 本方法在所选择的气缸性能参数中建立某些预定的增量变化,该变化指示在任何特定气缸内的燃烧性能差或劣化,然后根据分析和评价来改变输送到这种气缸的液体引燃燃料的量 所选气缸性能参数发生变化。 虽然优选每个气缸在个别基础上进行评估,但是应当认识到并预期在某些应用中,本方法可用于控制液体引燃燃料同时向两个或多个气缸的输送。

    Method for balancing the air/fuel ratio to each cylinder of an engine
    20.
    发明授权
    Method for balancing the air/fuel ratio to each cylinder of an engine 有权
    用于将空气/燃料比与发动机的每个气缸平衡的方法

    公开(公告)号:US6158418A

    公开(公告)日:2000-12-12

    申请号:US388575

    申请日:1999-09-01

    摘要: A method for controlling delivery of fuel to each cylinder of an engine by adjusting the appropriate fuel valve duration times to each such cylinder based upon a predetermined detonation level. By using the detonation level measurements from each individual cylinder as a controlling parameter, the delivery of fuel to that particular cylinder can be trimmed to achieve the predetermined detonation level. Balancing the detonation level for each such cylinder to a common detonation level likewise produces a substantially identical air/fuel ratio in each such cylinder. The detonation control loop can be initiated at predetermined intervals so as to continuously maintain a balanced air/fuel ratio to each cylinder in any particular engine.

    摘要翻译: 通过基于预定的爆震水平调节每个这种气缸的适当的燃料阀持续时间来控制燃料对发动机的每个气缸的输送的方法。 通过使用来自每个单独气缸的爆轰水平测量作为控制参数,可以修剪向特定气缸的燃料输送以达到预定的爆震水平。 将每个这样的气缸的爆轰水平平衡到共同的爆震水平同样在每个这样的气缸中产生基本相同的空气/燃料比。 爆震控制回路可以以预定间隔开始,以便在任何特定的发动机中连续保持与每个气缸的平衡的空气/燃料比。