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    • 4. 发明授权
    • Method and apparatus for providing fuel to an aircraft engine
    • 向飞机发动机提供燃料的方法和装置
    • US07658184B2
    • 2010-02-09
    • US12121242
    • 2008-05-15
    • Scott MatasCharles SchneiderAllan Watson
    • Scott MatasCharles SchneiderAllan Watson
    • F02B23/00B60T7/12
    • F02D41/1475F02D41/1446
    • An aircraft engine includes an aircraft engine controller configured to detect an actual peak exhaust gas temperature of a cylinder assembly. The aircraft engine controller detects an intersection between a first function representing a relationship between a set of rich exhaust gas temperature signals and a corresponding set of rich fuel-air ratio values and a second function representing a relationship between a set of lean exhaust gas temperature signals and a set of lean fuel-air ratio values. Based upon the intersection between the first and second functions, the engine controller detects an actual peak fuel-air ratio value for the cylinder assembly and can determine if a correction in the fuel-air ratio of a fuel-air mixture provided to the cylinder assembly is required. Accordingly, the engine controller provides each cylinder assembly of the aircraft engine with an accurate fuel-air mixture to allow for operation of the engine with optimal fuel economy.
    • 飞机发动机包括被配置为检测气缸组件的实际峰值排气温度的飞机发动机控制器。 飞机发动机控制器检测表示一组富排气温度信号与相应的一组富燃比之间的关系的第一函数和表示一组贫排气温度信号之间的关系的第二函数 和一组贫燃油比值。 基于第一功能和第二功能之间的交点,发动机控制器检测气缸组件的实际峰值燃油比值,并且可以确定提供给气缸组件的燃料 - 空气混合物的燃料空气比的校正 是必须的。 因此,发动机控制器为飞机发动机的每个气缸组件提供精确的燃料 - 空气混合物,以允许具有最佳燃料经济性的发动机的操作。
    • 5. 发明申请
    • METHOD AND APPARATUS FOR PROVIDING FUEL TO AN AIRCRAFT ENGINE
    • 用于向飞机发动机提供燃料的方法和装置
    • US20090283080A1
    • 2009-11-19
    • US12121242
    • 2008-05-15
    • Scott MatasCharles SchneiderAllan Watson
    • Scott MatasCharles SchneiderAllan Watson
    • F02D41/00
    • F02D41/1475F02D41/1446
    • An aircraft engine includes an aircraft engine controller configured to detect an actual peak exhaust gas temperature of a cylinder assembly. The aircraft engine controller detects an intersection between a first function representing a relationship between a set of rich exhaust gas temperature signals and a corresponding set of rich fuel-air ratio values and a second function representing a relationship between a set of lean exhaust gas temperature signals and a set of lean fuel-air ratio values. Based upon the intersection between the first and second functions, the engine controller detects an actual peak fuel-air ratio value for the cylinder assembly and can determine if a correction in the fuel-air ratio of a fuel-air mixture provided to the cylinder assembly is required. Accordingly, the engine controller provides each cylinder assembly of the aircraft engine with an accurate fuel-air mixture to allow for operation of the engine with optimal fuel economy.
    • 飞机发动机包括被配置为检测气缸组件的实际峰值排气温度的飞机发动机控制器。 飞机发动机控制器检测表示一组富排气温度信号与相应的一组富燃比之间的关系的第一函数和表示一组贫排气温度信号之间的关系的第二函数 和一组贫燃油比值。 基于第一功能和第二功能之间的交点,发动机控制器检测气缸组件的实际峰值燃油比值,并且可以确定提供给气缸组件的燃料 - 空气混合物的燃料空气比的校正 是必须的。 因此,发动机控制器为飞机发动机的每个气缸组件提供精确的燃料 - 空气混合物,以允许具有最佳燃料经济性的发动机的操作。
    • 7. 发明授权
    • Slide caliper assembly and method of use
    • 滑动卡钳组装及使用方法
    • US07076886B2
    • 2006-07-18
    • US11086891
    • 2005-03-22
    • William Thomas JohnChristopher Paul PennaDale Allan Watson
    • William Thomas JohnChristopher Paul PennaDale Allan Watson
    • G01B3/20
    • G01B3/205
    • A slide caliper assembly comprises a caliper including a shaft defining a gaging surface. A first jaw is coupled to and a second jaw is slidably coupled to the shaft. Each jaw defines a gaging surface. One of the jaws is adjustably pivotable relative to the shaft about a pivot axis coinciding with an intersection of the gaging surface of the shaft and another axis extending along the associated gaging surface of one of the jaws. A case houses the caliper, and has a plurality of side edge sections defining a periphery of the case. One side edge section and an adjacent side edge section form a non-right angle therebetween such that the shaft can abut the side edge section, the first jaw can abut an adjacent side edge section, and the second jaw can abut another adjacent side edge section for calibrating or demonstrating the use of the caliper.
    • 滑动卡钳组件包括包括限定出测量表面的轴的卡钳。 第一钳口联接到第一钳口并且第二钳口可滑动地联接到所述轴。 每个钳口定义了测量表面。 夹爪中的一个可相对于轴围绕枢转轴线可调节地枢转,所述枢转轴线与轴的测量表面与沿其中一个夹爪的相关联的表面延伸的另一轴线的交点相重合。 壳体容纳卡钳,并且具有限定壳体的周边的多个侧边缘部分。 一个侧边缘部分和相邻的侧边缘部分之间形成非直角,使得轴可以抵靠侧边缘部分,第一钳口可以邻接相邻的侧边缘部分,并且第二钳口可以邻接另一个相邻的侧边缘部分 用于校准或展示卡尺的使用。
    • 8. 发明授权
    • Slide calipers
    • 滑动卡钳
    • US06990746B2
    • 2006-01-31
    • US10832696
    • 2004-04-27
    • Christopher Paul PennaDale Allan Watson
    • Christopher Paul PennaDale Allan Watson
    • G01B3/20
    • G01B3/205
    • A slide caliper includes an elongated shaft defining a gaging surface for abutting against a first surface of an object to be measured. A first jaw is coupled to the shaft and defines a gaging surface for abutting against a second surface of the object. A second jaw is slidably coupled to the shaft and defines a gaging surface for abutting against a third surface or edge of the object. The second jaw along the shaft is adjustable between a first position where the gaging surfaces of the jaws generally abut each other to a second position where the gaging surfaces of the jaws are maximally spaced from each other. At least one of the jaws is adjustably pivotable relative to the shaft about a pivot axis coinciding with an intersection of the gaging surface of the shaft and another axis extending along the associated gaging surface of the pivotable jaw.
    • 滑动卡钳包括限定用于抵靠待测量物体的第一表面的计量表面的细长轴。 第一钳口联接到轴并且限定用于抵靠物体的第二表面的计量表面。 第二钳口可滑动地联接到所述轴并且限定用于抵靠所述物体的第三表面或边缘的计量表面。 沿着轴的第二钳口在第一位置和第二位置之间是可调节的,其中钳口的表面大体上彼此邻接到第二位置,在第二位置,钳口的计量表面彼此最大间隔开。 夹爪中的至少一个相对于轴可相对于轴可调节地枢转,该枢转轴线与轴的测量表面与沿着可枢转钳口的相关联的表面延伸的另一轴线的相交重合。