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    • 4. 发明授权
    • Time of flight mass spectrometry apparatus
    • 飞行时间质谱仪
    • US06781122B2
    • 2004-08-24
    • US10221378
    • 2002-11-25
    • Alexander William ColburnPeter John DerrickAnastassios Giannakopulos
    • Alexander William ColburnPeter John DerrickAnastassios Giannakopulos
    • H01L4940
    • H01J49/405H01J49/004
    • Mass spectrometry apparatus 105 comprises a serial arrangement of an ion source 110, first time of flight means, a field free region 120, means to fragment the molecules, a second time of flight means and a large area detector 160 The second time of flight means includes an ion mirror 150, the ion mirror 150 being arranged to produce a reflecting substantially quadratic field. The first time of flight means is arranged to provide spatial focusing concomitant with time focusing of ions at or near the entrance to the ion mirror 150. The means provided to fragment the ions from the first time of flight means can be a collision cell 140 or in the field free region 220 or in the first time of flight means. The means to fragment the molecules has a potential which is different from the potential at the entrance to the ion mirror 150, and the detecting surface of the detector 160 is mounted in the time focal surface of the ion mirror 150.
    • 质谱装置105包括离子源110的串行排列,第一飞行时间装置,无场区域120,分裂分子的装置,第二飞行时间装置和大面积检测器160第二飞行时间装置 包括离子镜150,离子镜150被布置成产生反射基本上二次场。 第一次飞行装置被设置成提供与离子在离子反射镜150的入口处或附近的时间聚焦的空间聚焦。提供用于从第一次飞行装置分离离子的装置可以是碰撞单元140或 在现场自由区域220或在第一次飞行中的装置。 分解分子的方法具有与入射到离子镜150的电位不同的电位,并且检测器160的检测表面安装在离子反射镜150的时间焦点表面中。
    • 6. 发明授权
    • Liquid propellant rocket motor
    • 液体推进剂火箭发动机
    • US06895743B1
    • 2005-05-24
    • US10655723
    • 2003-09-05
    • Terry McElheranWilliam Colburn
    • Terry McElheranWilliam Colburn
    • F02K9/42F02K9/64F02K9/95
    • F02K9/425F02K9/64F02K9/95F05D2260/203F05D2260/232F05D2300/21
    • The present invention provides a transpiration cooled rocket motor which operates at low combustion pressures, inherently provides stabilized combustion, and operates over a desired range of L-star. In a preferred embodiment the inventive transpiration cooled rocket motor includes: a housing; a porous injector sleeve; a propellant injector; and a nozzle. Preferably the injector sleeve lines the inside walls of the housing such that the inside volume of the sleeve forms the chamber for the motor. Liquid fuel passes inwardly through the pores of the injector sleeve and is injected from the sleeve into the chamber, thus cooling the walls of the rocket motor.
    • 本发明提供了一种在低燃烧压力下工作的蒸腾冷却的火箭发动机,固有地提供了稳定的燃烧,并在所需的L星级范围内运行。 在优选实施例中,本发明的蒸腾冷却火箭发动机包括:壳体; 多孔注射器套筒; 推进剂注射器; 和喷嘴。 优选地,喷射器套筒沿壳体的内壁排列,使得套筒的内部容积形成用于马达的腔室。 液体燃料向内通过喷射器套筒的孔,并从套筒注入到腔室中,从而冷却火箭发动机的壁。
    • 9. 发明授权
    • Time of flight mass spectrometry apparatus
    • 飞行时间质谱仪
    • US07075065B2
    • 2006-07-11
    • US10925192
    • 2004-08-24
    • Alexander William ColburnPeter John DerrickAnastassios Giannakopulos
    • Alexander William ColburnPeter John DerrickAnastassios Giannakopulos
    • H01L49/40
    • H01J49/405H01J49/004
    • Mass spectrometry apparatus 105 comprises a serial arrangement of an ion source 110, first time of flight means, a field free region 120, means to fragment the molecules, a second time of flight means and a large area detector 160. The second time of flight means includes an ion mirror 150, the ion mirror 150 being arranged to produce a reflecting substantially quadratic field. The first time of flight means is arranged to provide spatial focusing concomitant with time focusing of ions at or near the entrance to the ion mirror 150. The means provided to fragment the ions front the first time of flight means can be a collision cell 140 or in the field free region 220 or in the first time of flight means. The means to fragment the molecules has a potential which is different from the potential at the entrance to the ion mirror 150, and the detecting surface of the detector 160 is mounted in the time focal surface of the ion mirror 150.
    • 质谱装置105包括离子源110的串行排列,第一飞行时间装置,无场区域120,分解分子的装置,第二时间飞行装置和大面积检测器160。 第二次飞行装置包括离子镜150,离子镜150被布置成产生反射基本上二次场。 第一次飞行装置被设置成提供空间聚焦,伴随着离子在离子反射镜150的入口处或附近的时间聚焦。 提供用于在飞行装置的第一时间前面分离离子的装置可以是碰撞室140或场自由区域220或在第一次飞行装置中。 分解分子的方法具有与入射到离子镜150的电位不同的电位,并且检测器160的检测表面安装在离子反射镜150的时间焦点表面中。