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1. 发明授权

US5672327A Beneficiation of kish graphite 失效
标题翻译： kish石墨的获益
公开(公告)号：US5672327A
公开(公告)日：1997-09-30
申请号：US554249
申请日：1995-11-08
申请人： George W. Bennett , Maxime Leduc , Jean-Guy St-Hilaire , Christian Garceau
发明人： George W. Bennett , Maxime Leduc , Jean-Guy St-Hilaire , Christian Garceau
IPC分类号： C01B31/04
CPC分类号： C01B31/0407
摘要： A method and apparatus system are disclosed for the beneficiation of kish to produce coarse high purity graphite wherein a concentrate containing at least about 90% carbon is formed, treated with a dilute acid solution, and the pulp then subjected to an adjuvant-assisted attrition to form a novel synthetic flake graphite of 99+ wt. % carbon with at least 70% of the mass retained on +100 mesh, and an overall recovery of graphitic carbon from the feed of greater than 85% by weight.
摘要翻译：公开了一种方法和装置系统，用于选择kish以产生粗高纯石墨，其中形成含有至少约90％的碳的浓缩物，用稀酸溶液处理，然后将纸浆经受佐剂辅助的磨耗形成99重量％以上的新型合成片状石墨。％碳，其中至少70％的质量保持在+100目，并且来自进料的石墨碳的总体回收率大于85重量％。

2. 发明授权

US5560892A Apparatus system for beneficiation of kish graphite 失效
标题翻译： kish石墨选矿装置系统
公开(公告)号：US5560892A
公开(公告)日：1996-10-01
申请号：US425296
申请日：1995-04-20
申请人： George W. Bennett , Maxime Leduc , Jean-Guy St-Hilaire , Christian Garceau
发明人： George W. Bennett , Maxime Leduc , Jean-Guy St-Hilaire , Christian Garceau
IPC分类号： C01B31/04 , B01D11/02
CPC分类号： C01B31/0407
摘要： A apparatus system is disclosed for time beneficiation of kish to produce coarse high purity graphite wherein a concentrate containing at least about 90% carbon is formed, treated with a dilute acid solution, and the pulp then subjected to an adjuvant-assisted attrition to form a novel synthetic flake graphite of 99+ wt. % carbon with at least 70% of the mass retained on +100 mesh, and an overall recovery of graphitic carbon from the feed of greater than 85% by weight.
摘要翻译：公开了一种用于时间精选kish以生产粗高纯石墨的装置系统，其中形成含有至少约90％碳的浓缩物，用稀酸溶液处理，然后将纸浆经受佐剂辅助磨耗以形成 99重量％的新型合成片状石墨％碳，其中至少70％的质量保持在+100目，并且来自进料的石墨碳的总体回收率大于85重量％。

3. 发明授权

US5170365A Propeller speed and phase sensor 失效
标题翻译：螺旋桨速度和相位传感器
公开(公告)号：US5170365A
公开(公告)日：1992-12-08
申请号：US675066
申请日：1991-03-26
申请人： Paul D. Collopy , George W. Bennett
发明人： Paul D. Collopy , George W. Bennett
IPC分类号： B64C11/50 , G01P3/489 , G01P3/56
CPC分类号： G01P3/56 , B64C11/50 , G01P3/489
摘要： A speed and phase sensor counterrotates aircraft propellers. A toothed wheel is attached to each propeller, and the teeth trigger a sensor as they pass, producing a sequence of signals. From the sequence of signals, rotational speed of each propeller is computer based on time intervals between successive signals. The speed can be computed several times during one revolution, thus giving speed information which is highly up-to-date. Given that spacing between teeth may not be uniform, the signals produced may be nonuniform in time. Error coefficients are derived to correct for nonuniformities in the resulting signals, thus allowing accurate speed to be computed despite the spacing nonuniformities. Phase can be viewed as the relative rotational position of one propeller with respect to the other, but measured at a fixed time. Phase is computed from the signals.
摘要翻译：速度和相位传感器反击飞机螺旋桨。齿轮连接到每个螺旋桨上，齿通过时触发传感器，产生一系列信号。根据信号序列，每个螺旋桨的转速是基于连续信号之间的时间间隔的计算机。速度可以在一圈内计算好几次，从而提供高度最新的速度信息。假定齿之间的间距可能不均匀，所产生的信号可能在时间上是不均匀的。导出误差系数以校正所得到的信号中的不均匀性，从而允许精确的速度被计算，尽管间隔不均匀性。相位可以视为一个螺旋桨相对于另一个螺旋桨的相对旋转位置，但是在固定时间测量。相位根据信号计算。

4. 发明授权

US4338061A Control means for a gas turbine engine 失效
标题翻译：燃气轮机的控制装置
公开(公告)号：US4338061A
公开(公告)日：1982-07-06
申请号：US163122
申请日：1980-06-26
申请人： Richard S. Beitler , Frederick J. Sellers , George W. Bennett
发明人： Richard S. Beitler , Frederick J. Sellers , George W. Bennett
IPC分类号： F01D11/06 , F01D11/10 , F01D11/24 , F01D25/08
CPC分类号： F01D11/24
摘要： Clearance control means is provided for a gas turbine engine. In one embodiment relating to compressor blade clearance, means is provided for developing a first signal representative of the actual compressor casing temperature, a second signal representative of compressor inlet gas temperature, and a third signal representative of compressor speed. Schedule means is provided for receiving the gas temperature and compressor speed signals and developing a schedule output signal. The schedule output signal is representative of a reference casing temperature at which a predetermined compressor blade stabilized clearance is provided. Means is provided for comparing the actual compressor casing temperature signal and the reference casing temperature signal and developing a clearance control signal representative of the difference therebetween. The clearance control signal is coupled to a control valve which controls a flow of air to the compressor casing to control the clearance between the compressor blades and the compressor casing. Means is provided for modification of the clearance control signal to accommodate transient characteristics. Other embodiments are disclosed.
摘要翻译：提供了一种用于燃气涡轮发动机的间隙控制装置。在与压缩机叶片间隙相关的一个实施例中，提供了用于开发代表实际压缩机壳体温度的第一信号，代表压缩机入口气体温度的第二信号和表示压缩机速度的第三信号的装置。提供装置用于接收气体温度和压缩机速度信号，并开发时间表输出信号。时间表输出信号代表提供预定压缩机叶片稳定间隙的参考套管温度。提供了用于比较实际的压缩机壳体温度信号和参考壳体温度信号的装置，并且开发表示它们之间差异的间隙控制信号。间隙控制信号耦合到控制阀，该控制阀控制到压缩机壳体的空气流，以控制压缩机叶片与压缩机壳体之间的间隙。提供了用于修改间隙控制信号以适应瞬态特性的装置。公开了其他实施例。

5. 发明授权

US4772180A Aircraft thrust control 失效
公开(公告)号：US4772180A
公开(公告)日：1988-09-20
申请号：US902231
申请日：1986-08-29
申请人： Neil Walker , Stanley G. Day , Paul D. Collopy , George W. Bennett
发明人： Neil Walker , Stanley G. Day , Paul D. Collopy , George W. Bennett
IPC分类号： B64D31/12 , B64C11/30 , B64C11/50 , F02C9/58 , F02K3/072 , B64C11/48
CPC分类号： F02C9/58 , B64C11/306 , B64C11/50 , F02K3/072 , B64D2027/005 , Y02T50/66
摘要： An integrated control system for coaxial counterrotating aircraft propulsors driven by a common gas turbine engine. The system establishes an engine pressure ratio by control of fuel flow and uses the established pressure ratio to set propulsor speed. Propulsor speed is set by adjustment of blade pitch.

6. 发明授权

US4958289A Aircraft propeller speed control 失效
标题翻译：飞机螺旋桨速度控制
公开(公告)号：US4958289A
公开(公告)日：1990-09-18
申请号：US284261
申请日：1988-12-14
申请人： Michael J. Sum , George W. Bennett , Steven A. Merrell , Neil Walker
发明人： Michael J. Sum , George W. Bennett , Steven A. Merrell , Neil Walker
IPC分类号： B64D31/06 , B64C11/30 , F02C9/28 , F02C9/58
CPC分类号： F02C9/58 , B64C11/305
摘要： The invention concerns a control for an aircraft propeller. During operation in reverse pitch, as occurs upon thrust reversal during a landing maneuver, the speed of the propeller is controlled by adjusting pitch of the propeller, in order to prevent overspeeding. Further, during the transition period while the propeller is converting from forward pitch to reverse pitch, the propeller presents a light load to the engine. At this time, fuel flow to the engine is limited in order to restrict delivery of energy to the propeller, again, for the purpose of preventing overspeeding.
摘要翻译：本发明涉及飞机螺旋桨的控制。在反向间距操作期间，如在着陆操作中的推力反转时发生的那样，螺旋桨的速度通过调节螺旋桨的桨距来控制，以防止超速。此外，在螺旋桨从前进桨距转换成反向桨距的过渡期间，螺旋桨对发动机施加轻负荷。此时，限制向发动机的燃料流动，以限制向螺旋桨的能量输送，以防止超速。

7. 发明授权

US4772179A Aircraft thrust control 失效
标题翻译：飞机推力控制
公开(公告)号：US4772179A
公开(公告)日：1988-09-20
申请号：US902285
申请日：1986-08-29
申请人： George W. Bennett , Neil Walker
发明人： George W. Bennett , Neil Walker
IPC分类号： F02C9/58 , F02K3/072 , B64C11/48
CPC分类号： F02C9/58 , B64C11/308 , F02K3/072 , B64D2027/005 , Y02T50/66
摘要： An integrated control system for coaxial counterrotating aircraft propulsors driven by a common gas turbine engine. The system establishes an engine pressure ratio by control of fuel flow and uses the established pressure ratio to set propulsor speed. Propulsor speed is set by adjustment of blade pitch.
摘要翻译：由普通燃气涡轮发动机驱动的同轴逆转飞行器推进器的综合控制系统。该系统通过控制燃料流量建立发动机压力比，并使用建立的压力比设置推进器速度。推进速度是通过调整叶片间距来设定的。

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