会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 3. 发明申请
    • COMBUSTION LINER SEAL WITH HEAT TRANSFER AUGMENTATION
    • 燃烧内衬密封带热传递补偿
    • US20050262844A1
    • 2005-12-01
    • US10856592
    • 2004-05-28
    • Andrew GreenPeter StuttafordJeffrey BenoitVamsi DuraibabuHany Rizkalla
    • Andrew GreenPeter StuttafordJeffrey BenoitVamsi DuraibabuHany Rizkalla
    • F01D9/02F23R3/00F23R3/42F23R3/46
    • F23R3/002F01D9/023F23R3/46Y02T50/675
    • A gas turbine combustion liner is disclosed having an alternate interface region between it and a transition duct where the cooling effectiveness and heat transfer along the aft end of the combustion liner is improved, resulting in extended component life. The region of the combustion liner proximate its second end comprises a plurality of first feed holes, a plurality of spring seals that seal against a transition duct, a cooling ring having a plurality of second feed holes, that with the first feed holes pass a cooling fluid into an annulus formed between the cooling ring and combustion liner. The cooling fluid passes over a means for augmenting the heat transfer proximate the combustion liner second end, wherein the heat transfer augmentation preferably comprises a plurality of raised ridges that increases the surface area of the outer liner wall to turbulate the cooling fluid and maximize the cooling effectiveness.
    • 公开了一种燃气轮机燃烧衬套,其在其与过渡管道之间具有交替的界面区域,其中沿着燃烧衬套的后端的冷却效果和热传递得到改善,导致部件寿命延长。 靠近其第二端的燃烧衬套的区域包括多个第一进料孔,密封过渡管道的多个弹簧密封件,具有多个第二进料孔的冷却环,其中第一进料孔通过冷却 流体进入形成在冷却环和燃烧衬套之间的环形空间中。 冷却流体越过用于增加靠近燃烧衬套第二端的热传递的装置,其中传热增强优选地包括多个凸脊,其增加外衬套壁的表面积以使冷却流体紊乱并使冷却最大化 有效性
    • 4. 发明授权
    • Combustion liner seal with heat transfer augmentation
    • 具有传热增强的燃烧衬套密封
    • US07007482B2
    • 2006-03-07
    • US10856592
    • 2004-05-28
    • Andrew GreenPeter StuttafordJeffrey Arthur BenoitVamsi DuraibabuHany Rizkalla
    • Andrew GreenPeter StuttafordJeffrey Arthur BenoitVamsi DuraibabuHany Rizkalla
    • F02C7/12
    • F23R3/002F01D9/023F23R3/46Y02T50/675
    • A gas turbine combustion liner is disclosed having an alternate interface region between it and a transition duct where the cooling effectiveness and heat transfer along the aft end of the combustion liner is improved, resulting in extended component life. The region of the combustion liner proximate its second end comprises a plurality of first feed holes, a plurality of spring seals that seal against a transition duct, a cooling ring having a plurality of second feed holes, that with the first feed holes pass a cooling fluid into an annulus formed between the cooling ring and combustion liner. The cooling fluid passes over a means for augmenting the heat transfer proximate the combustion liner second end, wherein the heat transfer augmentation preferably comprises a plurality of raised ridges that increases the surface area of the outer liner wall to turbulate the cooling fluid and maximize the cooling effectiveness.
    • 公开了一种燃气轮机燃烧衬套,其在其与过渡管道之间具有交替的界面区域,其中沿着燃烧衬套的后端的冷却效果和热传递得到改善,导致部件寿命延长。 靠近其第二端的燃烧衬套的区域包括多个第一进料孔,密封过渡管道的多个弹簧密封件,具有多个第二进料孔的冷却环,其中第一进料孔通过冷却 流体进入形成在冷却环和燃烧衬套之间的环形空间中。 冷却流体越过用于增加靠近燃烧衬套第二端的热传递的装置,其中传热增强优选地包括多个凸脊,其增加外衬套壁的表面积以使冷却流体紊乱并使冷却最大化 有效性
    • 7. 发明授权
    • Gas turbine combustor hybrid dynamic-static probe
    • 燃气轮机燃烧室混合动静态探头
    • US06742394B1
    • 2004-06-01
    • US10341573
    • 2003-01-13
    • Peter StuttafordAndrew Green
    • Peter StuttafordAndrew Green
    • G01L700
    • F01D17/085F01D17/08F05D2270/301F05D2270/303
    • A removable instrumentation assembly and probe for use in simultaneously measuring dynamic pressure, at least one static pressure, and temperature for a gas turbine combustor. The instrumentation assembly allows combustor performance analysis as well as monitoring of component integrity through dynamic pressure fluctuations. The instrumentation assembly includes a probe having a plurality of passages, each connected to tubular conduits for measuring and recording respective pressures. In the preferred embodiment, dynamic pressures from within a combustion chamber are measured and recorded along with static pressures within the combustion chamber and outside of the combustion chamber, along with external air temperature.
    • 用于同时测量燃气轮机燃烧器的动态压力,至少一个静态压力和温度的可拆卸仪器组件和探头。 仪表组件允许燃烧器性能分析以及通过动态压力波动监测部件完整性。 仪器组件包括具有多个通道的探针,每个通道连接到用于测量和记录相应压力的管状导管。 在优选实施例中,燃烧室内的动态压力与外部空气温度一起被测量并记录在燃烧室内和燃烧室外部的静压力。