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公开(公告)号:US09259161B2
公开(公告)日:2016-02-16
申请号:US13469485
申请日:2012-05-11
申请人: Todd M. Suchecki , Alan K. Evans
发明人: Todd M. Suchecki , Alan K. Evans
IPC分类号: A61B5/02 , A61B5/0215 , A61B5/026 , A61B5/00 , A61M25/00
CPC分类号: A61B5/7221 , A61B5/0066 , A61B5/02007 , A61B5/0215 , A61B5/02158 , A61B5/026 , A61B5/4842 , A61B5/6851 , A61M2025/0002
摘要: Methods and systems for calculating a corrected Fractional Flow Reserve. Methods include delivering a pressure sensing device including a pressure sensor to a location in an artery having a stenosis, positioning the pressure sensor distal to the stenosis, measuring the distal pressure, measuring the proximal pressure, and calculating a corrected Fractional Flow Reserve using the measured proximal and distal pressures and applying a correction factor or correction equation. The correction factor or correction equation corrects for changes in the measured distal pressure caused by a presence of the pressure sensing device. A data set of correction factors or correction equations may be stored in a memory component of the system. The corrected Fractional Flow reserve may approximate the Fractional Flow Reserve that would be obtained if a different sized device was used to measure the distal pressure, such as a pressure sensing guidewire having a 0.014 inch outer diameter.
摘要翻译: 用于计算校正分数流量储备的方法和系统。 方法包括将包括压力传感器的压力感测装置递送到具有狭窄的动脉中的位置,将压力传感器远离狭窄定位,测量远端压力,测量近端压力,以及使用所测量的近端压力计算校正的分数流量储备 近端和远端压力,并应用校正因子或校正方程。 校正因子或校正方程校正由压力感测装置的存在引起的测量的远端压力的变化。 校正因子或校正方程的数据集可以存储在系统的存储器组件中。 校正的分数流量储备可以接近如果使用不同尺寸的装置来测量远端压力将获得的分数流量储备,例如具有0.014英寸外径的压力感测导线。
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公开(公告)号:US08511062B2
公开(公告)日:2013-08-20
申请号:US12485559
申请日:2009-06-16
申请人: Jihad I. Ramlaoui , Geoffrey Pinto , Daniel Shetzer , Daniel M. Amkraut , Andrew Robert Hawksworth , John Harvey , Alan K. Evans , Vikram Chandarana , Roger Moorhouse
发明人: Jihad I. Ramlaoui , Geoffrey Pinto , Daniel Shetzer , Daniel M. Amkraut , Andrew Robert Hawksworth , John Harvey , Alan K. Evans , Vikram Chandarana , Roger Moorhouse
CPC分类号: F02K1/763 , F02K1/09 , F02K1/30 , F02K1/70 , F02K1/72 , F02K3/06 , F05D2250/34 , Y10T74/18576 , Y10T74/18648
摘要: A variable area fan nozzle assembly for a turbofan engine includes a nacelle having an aft edge and a translating thrust reverser sleeve with a trailing edge. The thrust reverser sleeve is movably disposed aft of the nacelle's aft edge and is movable between a forward position and an aft position. A translating fan nozzle having a forward edge is movably disposed behind the trailing edge, and is movable between a stowed position and a deployed position. An upstream bypass flow exit is defined between the trailing edge and the forward edge when the fan nozzle is in the deployed position. An extendable actuation system is configured to move the fan nozzle between the stowed position and the deployed position.
摘要翻译: 用于涡轮风扇发动机的可变区域风扇喷嘴组件包括具有后缘的机舱和具有后缘的平移推力反向器套筒。 推力反向器套筒可移动地设置在机舱的后边缘的后部并且可以在前进位置和后部位置之间移动。 具有前边缘的平移风扇喷嘴可移动地设置在后缘的后面,并且可在收起位置和展开位置之间移动。 当风扇喷嘴处于展开位置时,在后缘和前缘之间限定上游旁路流出口。 可延伸致动系统构造成使风扇喷嘴在收起位置和展开位置之间移动。
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公开(公告)号:US20130131523A1
公开(公告)日:2013-05-23
申请号:US13469485
申请日:2012-05-11
申请人: Todd M. Suchecki , Alan K. Evans
发明人: Todd M. Suchecki , Alan K. Evans
IPC分类号: A61B5/0215
CPC分类号: A61B5/7221 , A61B5/0066 , A61B5/02007 , A61B5/0215 , A61B5/02158 , A61B5/026 , A61B5/4842 , A61B5/6851 , A61M2025/0002
摘要: Methods and systems for calculating a corrected Fractional Flow Reserve. Methods include delivering a pressure sensing device including a pressure sensor to a location in an artery having a stenosis, positioning the pressure sensor distal to the stenosis, measuring the distal pressure, measuring the proximal pressure, and calculating a corrected Fractional Flow Reserve using the measured proximal and distal pressures and applying a correction factor or correction equation. The correction factor or correction equation corrects for changes in the measured distal pressure caused by a presence of the pressure sensing device. A data set of correction factors or correction equations may be stored in a memory component of the system. The corrected Fractional Flow reserve may approximate the Fractional Flow Reserve that would be obtained if a different sized device was used to measure the distal pressure, such as a pressure sensing guidewire having a 0.014 inch outer diameter.
摘要翻译: 用于计算校正分数流量储备的方法和系统。 方法包括将包括压力传感器的压力感测装置递送到具有狭窄的动脉中的位置,将压力传感器远离狭窄定位,测量远端压力,测量近端压力,以及使用所测量的近端压力计算校正的分数流量储备 近端和远端压力,并应用校正因子或校正方程。 校正因子或校正方程校正由压力感测装置的存在引起的测量的远端压力的变化。 校正因子或校正方程的数据集可以存储在系统的存储器组件中。 校正的分数流量储备可以接近如果使用不同尺寸的装置来测量远端压力将获得的分数流量储备,例如具有0.014英寸外径的压力感测导线。
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公开(公告)号:US20100229528A1
公开(公告)日:2010-09-16
申请号:US12485559
申请日:2009-06-16
申请人: Jihad I. Ramlaoui , Geoffrey Pinto , Daniel Shetzer , Daniel M. Amkraut , Andrew Robert Hawksworth , John Harvey , Alan K. Evans , Vikram Chandarana , Roger Moorhouse
发明人: Jihad I. Ramlaoui , Geoffrey Pinto , Daniel Shetzer , Daniel M. Amkraut , Andrew Robert Hawksworth , John Harvey , Alan K. Evans , Vikram Chandarana , Roger Moorhouse
CPC分类号: F02K1/763 , F02K1/09 , F02K1/30 , F02K1/70 , F02K1/72 , F02K3/06 , F05D2250/34 , Y10T74/18576 , Y10T74/18648
摘要: A variable area fan nozzle assembly for a turbofan engine includes a nacelle having an aft edge and a translating thrust reverser sleeve with a trailing edge. The thrust reverser sleeve is movably disposed aft of the nacelle's aft edge and is movable between a forward position and an aft position. A translating fan nozzle having a forward edge is movably disposed behind the trailing edge, and is movable between a stowed position and a deployed position. An upstream bypass flow exit is defined between the trailing edge and the forward edge when the fan nozzle is in the deployed position. An extendable actuation system is configured to move the fan nozzle between the stowed position and the deployed position.
摘要翻译: 用于涡轮风扇发动机的可变区域风扇喷嘴组件包括具有后缘的机舱和具有后缘的平移推力反向器套筒。 推力反向器套筒可移动地设置在机舱的后边缘的后部并且可以在前进位置和后部位置之间移动。 具有前边缘的平移风扇喷嘴可移动地设置在后缘的后面,并且可在收起位置和展开位置之间移动。 当风扇喷嘴处于展开位置时,在后缘和前缘之间限定上游旁路流出口。 可延伸致动系统构造成使风扇喷嘴在收起位置和展开位置之间移动。
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