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    • 2. 发明授权
    • Integral electric pressure probe for aircraft
    • 用于飞机的一体电压探头
    • US06591696B2
    • 2003-07-15
    • US09904400
    • 2001-07-12
    • Thomas J Bachinski
    • Thomas J Bachinski
    • G01F146
    • G01P5/165
    • An electric pressure probe for an aircraft comprises: a pitot tube assembly for collecting pneumatically air pressure in the vicinity of the assembly; a strut including one end mountable to a surface of the aircraft, the pitot tube assembly being coupled to another end of the strut for being supported away from the aircraft surface; a pressure sensor integral to the strut and pneumatically coupled to the pitot tube assembly for converting the pneumatic pressure collected thereby to an electrical pressure signal; and circuitry integral to the strut and coupled to the pressure sensor for signal conditioning the electrical pressure signal, the circuitry including at least one output lead for conducting the conditioned electrical signal from the probe. A method of making an integral electric pressure probe comprises the steps of: coupling one end of a housing to a pitot tube assembly; molding a moldable material into the form of a strut including one end for being mounted to a surface of an aircraft; and molding another end of the housing to another end of the strut.
    • 一种用于飞行器的电压探针包括:皮托管组件,用于收集组件附近的气压气压; 支架,其一端可安装到飞行器的表面,皮托管组件联接到支柱的另一端,用于支撑远离飞机表面; 压力传感器与支柱成一体并气动联接到皮托管组件,用于将由此收集的气压转换成电压信号; 以及与所述支柱成一体并耦合到所述压力传感器以用于对所述电压信号进行信号调节的电路,所述电路包括用于从所述探针传导经调节的电信号的至少一个输出引线。 制造一体电压探针的方法包括以下步骤:将壳体的一端耦合到皮托管组件; 将可模制材料模制成支柱的形式,包括一端以安装在飞行器的表面上; 并将壳体的另一端模制成支柱的另一端。
    • 3. 发明授权
    • Standoff mounting for air data sensing probes on a helicopter
    • 直升机上的空中数据传感探头的支架安装
    • US06419186B1
    • 2002-07-16
    • US09540142
    • 2000-03-31
    • Thomas J. BachinskiTimothy T. GollyRobert G. Syring, Jr.Ronald J. PetriDouglas G. Conley
    • Thomas J. BachinskiTimothy T. GollyRobert G. Syring, Jr.Ronald J. PetriDouglas G. Conley
    • B64C2700
    • B64D43/02G01P5/165G01P13/025
    • A standoff arm and probe assembly for a helicopter has a standoff mounting arm that extends outwardly from the helicopter body in a selected direction, preferably forwardly. The standoff arm has an outer end that mounts a low lateral speed sensing probe that is positioned with an axis substantially parallel to the axis of a helicopter rotor, and within the downwash region of air movement causes by the rotor. The low lateral speed sensing probe has ports that are arranged annularly around the probe, and the pressures sensed at selected annular or peripheral locations on the probe are measured to determine low air speeds. Additionally, the standoff arm can mount a plurality of other sensors such as a pitot pressure probe extending forwardly from the arm, a lateral pressure sensing probe along a lateral side of the arm, and the arm can mount outside air temperature sensors, ice detectors, and total air temperature sensors, if desired.
    • 用于直升机的支座臂和探针组件具有支架安装臂,该支架安装臂从直升机主​​体沿所选方向向外延伸,优选地向前延伸。 支架臂具有一个外端,该外端安装一个低侧速度传感探头,该探头的基本上平行于直升机转子轴线的轴线定位,并且在由转子引起的空气运动的下降区域内。 低横向速度感测探头具有围绕探针环形布置的端口,并且测量在探针上的选定环形或周边位置处感测到的压力以确定低空气速度。 此外,支架臂可以安装多个其它传感器,例如从臂向前延伸的皮托管压力探头,沿着臂的横向侧的侧向压力传感探头,并且臂可以安装在室外空气温度传感器,冰探测器, 和空气温度传感器。
    • 4. 发明授权
    • Apparatus for handling tubing used in medical procedures
    • 用于处理用于医疗程序的管道的装置
    • US6136007A
    • 2000-10-24
    • US303224
    • 1999-04-30
    • David S. GoldsteenThomas J. BachinskiDaniel J. Sullivan
    • David S. GoldsteenThomas J. BachinskiDaniel J. Sullivan
    • A61F2/00A61F2/06A61F11/00
    • A61F2/064A61F2/958A61F2002/8486A61F2250/0098A61M2025/0293A61M25/04
    • Methods and apparatus are provided for such uses as attaching grafts of tubing (e.g., lengths of saphenous vein) between sites in a patient's body via the patient's existing arteries and veins. Grafts may be held in place during graft delivery using a partially inflated proximal balloon and a partially inflated distal balloon which frictionally engage axially spaced portions of the graft (e.g., pronged attachment rings that pierce the graft adjacent its ends). After aligning the distal balloon and distal end of the graft with the distal attachment site, the distal balloon may be further inflated to help attach the distal end of the graft to the distal attachment site (e.g., by driving the prongs of the distal attachment ring into the distal attachment site). The proximal balloon may then be inflated to similarly help attach the proximal end of the graft to the proximal attachment site. The balloons are deflated to facilitate withdrawal of the apparatus from the installed graft. The insertion instrument allows the distance between the distal and proximal balloons to be adjusted, thereby accommodating grafts of various lengths. The separation between distal and proximal balloons may be fixed or substantially fixed using a locking mechanism.
    • 提供了用于例如通过患者现有的动脉和静脉将患者体内的位置之间的管(例如,隐静脉长度)的移植物附接的方法和装置。 移植物可以在移植物输送期间使用部分充气的近端球囊和部分充气的远端球囊保持在适当位置,所述远端球囊摩擦地接合移植物的轴向间隔的部分(例如,穿过邻近其端部的移植物的插入连接环)。 在使远端球囊和远端附着部位对准移植物的远端后,远端球囊可以进一步膨胀以帮助将移植物的远端附接到远侧附接部位(例如,通过驱动远侧附接环的尖头 进入远端附件部位)。 然后可以将近端球囊充气以类似地帮助将移植物的近端附接到近端附着部位。 气囊被放气以便于将装置从装载的移植物中取出。 插入器械允许调节远端和近端气球之间的距离,从而容纳各种长度的移植物。 远端和近端球囊之间的分离可使用锁定机构固定或基本固定。