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    Passive optical gaseous emissions sensor
    11.
    发明公开
    Passive optical gaseous emissions sensor 审中-公开
    无源光气体排放传感器

    公开(公告)号：EP2447706A3

    公开(公告)日：2012-08-01

    申请号：EP11250881.7

    申请日：2011-11-01

    Applicant: Rosemount Aerospace Inc.

    Inventor： Myhre, Douglas C. ,  Odd, Harald Steen Eriksen

    IPC: G01N21/35 ,  G01N33/00

    CPC classification number: G01N21/3504 ,  G01N21/554 ,  G01N21/8507

    Abstract: A probe assembly for measuring the concentration of exhaust's emissions in a turbine engine. The probe assembly (10) including a first probe member (14) configured and operable to passively generate a beam of light wherein the wavelength of the beam of light is contingent upon the configuration of the first probe member. A second probe member (24) positioned in the probe assembly to receive the beam of light generated by the first probe member, the second probe member configured and operable to attenuate the light passively generated from the first probe member contingent upon the gaseous species present in the exhaust emissions (20) of the turbine engine (100).

    Apparatus, system and method for observing combustor flames in a gas turbine engine
    14.
    发明公开
    Apparatus, system and method for observing combustor flames in a gas turbine engine 有权
    装置，系统和方法，用于在燃气涡轮机的燃烧器监视火焰

    公开(公告)号：EP2642205A3

    公开(公告)日：2014-04-09

    申请号：EP13160654.3

    申请日：2013-03-22

    Applicant: ROSEMOUNT AEROSPACE INC.

    Inventor： Myhre, Douglas C. ,  MIichel, Joseph R. ,  Aadland, Timothy

    IPC: F23N5/08

    CPC classification number: F23N5/08 ,  F23N5/082 ,  F23N2041/20

    Abstract: A fuel injector, 20, for a gas turbine engine is disclosed which includes a nozzle body, 28, for issuing fuel and air into a combustor, 30, and an on-axis optical probe, 50, located within the nozzle body, 28, for observing combustor flame radiation, wherein the optical probe, 50, includes a plurality of optical fiber bundles, 60a - 60g, extending to a distal end of the probe, 50, and a shaped lens, 56, is supported at the distal end of the probe, 50, to provide a multi-directional field of view of combustion characteristics and properties in an operating gas turbine engine combustor.

    Thermal sensor and method of measuring mass flow non-intrusively
    16.
    发明公开
    Thermal sensor and method of measuring mass flow non-intrusively 有权
    质量流量的非侵入式测量热传感器和方法

    公开(公告)号：EP1593940A3

    公开(公告)日：2007-11-28

    申请号：EP04258108.2

    申请日：2004-12-23

    Applicant: ROSEMOUNT AEROSPACE INC.

    Inventor： Myhre, Douglas C.

    IPC: G01F1/684 ,  G01F1/688

    CPC classification number: G01F1/6847 ,  G01F1/6888

    Abstract: A non-intrusive sensor for measuring mass flow of a medium flowing through a tube comprises: a probe having a predetermined length disposed along an external wall of the tube; a heater for heating the probe at a first point along the length thereof; a first temperature measuring device disposed at the first point for measuring a temperature of the probe and for generating a first signal T h representative thereof; a second temperature measuring device disposed at a second point along the length of the probe for measuring another temperature of the probe and for generating a second signal T t representative thereof; a third temperature measuring device disposed along the external wall of the tube a distance away from the probe for measuring an ambient temperature and for generating a signal T a representative thereof; and circuitry coupled to the first, second and third temperature measuring devices for generating a mass flow signal based on a ratio of temperature differential signals (T h - T a )/(T t - T a ). A counterpart method is also disclosed.

    Thermal sensor and method of measuring mass flow non-intrusively
    17.
    发明公开
    Thermal sensor and method of measuring mass flow non-intrusively 有权
    Thermischer传感器和Verfahren zur nichtintrusiven Massendurchflussmessung

    公开(公告)号：EP1593940A2

    公开(公告)日：2005-11-09

    申请号：EP04258108.2

    申请日：2004-12-23

    Applicant: ROSEMOUNT AEROSPACE INC.

    Inventor： Myhre, Douglas C.

    IPC: G01F1/684 ,  G01F1/688

    CPC classification number: G01F1/6847 ,  G01F1/6888

    Abstract: A non-intrusive sensor for measuring mass flow of a medium flowing through a tube comprises: a probe having a predetermined length disposed along an external wall of the tube; a heater for heating the probe at a first point along the length thereof; a first temperature measuring device disposed at the first point for measuring a temperature of the probe and for generating a first signal T h representative thereof; a second temperature measuring device disposed at a second point along the length of the probe for measuring another temperature of the probe and for generating a second signal T t representative thereof; a third temperature measuring device disposed along the external wall of the tube a distance away from the probe for measuring an ambient temperature and for generating a signal T a representative thereof; and circuitry coupled to the first, second and third temperature measuring devices for generating a mass flow signal based on a ratio of temperature differential signals (T h - T a )/(T t - T a ). A counterpart method is also disclosed.

    Abstract translation: 用于测量流过管的介质的质量流量的非侵入传感器包括：具有沿管的外壁设置的预定长度的探针; 加热器，其沿着其长度在第一点处加热探针; 第一温度测量装置，设置在第一点处，用于测量探针的温度，并产生代表其的第一信号T h; 第二温度测量装置，设置在沿探针长度的第二点处，用于测量探针的另一温度，并产生代表其的第二信号T t; 第三温度测量装置，沿着管的外壁离开探头一定距离，用于测量环境温度并产生代表其的信号T a; 以及耦合到第一，第二和第三温度测量装置的电路，用于基于温差信号（T h -T a）/（T t -T a）的比率产生质量流量信号。 还公开了一种对应方法。

    Apparatus, system and method for observing combustion conditions in a gas turbine
    20.
    发明公开
    Apparatus, system and method for observing combustion conditions in a gas turbine 有权
    VERrichtung，System and Verfahren zum Beobachten der Verbrennungsbedingungen in einer Gurburbine

    公开(公告)号：EP2508801A3

    公开(公告)日：2012-11-07

    申请号：EP12001631.6

    申请日：2005-03-30

    Applicant: ROSEMOUNT AEROSPACE INC.

    Inventor： Myhre, Douglas C.

    IPC: F23N5/08 ,  F02C9/26

    CPC classification number: F02C9/28 ,  F01D17/02 ,  F01D21/003 ,  F23N5/082 ,  F23N2029/04 ,  F23N2029/08 ,  F23N2041/20 ,  G01N21/76 ,  Y02T50/677

    Abstract: A system for stabilizing combustion in a gas turbine engine comprises a) optical sensing means embedded within a fuel injector for observing conditions within a combustion chamber of a gas turbine engine; b) means for detecting combustion instabilities based upon conditions observed by the optical sensing means; and c) means for modulating a fuel flow rate to reduce detected combustion instabilities.

    Abstract translation: 公开了一种用于燃气轮机燃烧器的燃料喷射器，其包括具有用于将喷射器安装在燃烧器内的凸缘（24）的进料臂（22）和从进料臂悬挂的用于将燃料喷射到燃烧器中的燃料喷嘴（26） 燃烧。 光学传感器阵列（34）位于燃料喷嘴内，用于观察燃烧器内的燃烧条件。

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