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公开(公告)号：US20090158738A1
公开(公告)日：2009-06-25
申请号：US12197712
申请日：2008-08-25
IPC分类号： F02K5/00
CPC分类号： F01K23/108 , Y02E20/16
摘要： Methods and apparatus for fast starting and loading a combined cycle power system are described. In one example embodiment, a method for starting a combined cycle power generation system is provided. The system includes a gas turbine and a steam turbine. The method includes loading the gas turbine at a loading rate that is facilitated to be at an increased loading rate, setting a first predetermined value for a bypass pressure set point for high-pressure steam, and increasing the first predetermined value to a second predetermined value at a predetermined rate.
摘要翻译： 描述了用于快速启动和加载联合循环电力系统的方法和装置。 在一个示例实施例中，提供了一种用于启动组合循环发电系统的方法。 该系统包括燃气轮机和汽轮机。 该方法包括以便于加载速度加快的负载速度装载燃气轮机，为高压蒸汽设定旁路压力设定点的第一预定值，将第一预定值增加到第二预定值 以预定速率。
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公开(公告)号：US20090145104A1
公开(公告)日：2009-06-11
申请号：US12331824
申请日：2008-12-10
申请人： Michael J. Alexander , Mark S. Schroder , Bradley D. Crawley , Gordon R. Smith , Mark J. Steffen , John C. Maters , David A. Snider
发明人： Michael J. Alexander , Mark S. Schroder , Bradley D. Crawley , Gordon R. Smith , Mark J. Steffen , John C. Maters , David A. Snider
IPC分类号： F01K23/06
CPC分类号： F01K23/101 , Y02E20/16 , Y02E20/18
摘要： A combined cycle (CC) power plant comprises a gas turbine; a steam turbine; a condenser; a heat recovery steam generator (HRSG), the HRSG comprising an attemperator and a high pressure superheater and attemperator, the high pressure superheater and attemperator disposed at a discharge terminal of the high pressure superheater and attemperator and at a discharge terminal of the HRSG reheater; a generator, and a fuel supply. The steam turbine is connected by multiple conduits to the heat recovery steam generator (HRSG) and the steam turbine exhaust is connected to the condenser wherein support multiple ancillary and reserves to load follow, execute regulation, and meet intermediate power generation service needs in an expedited start process.
摘要翻译： 联合循环（CC）发电厂包括燃气轮机; 蒸汽轮机; 冷凝器 热回收蒸汽发生器（HRSG），HRSG包括调温器和高压过热器和调温器，高压过热器和调温器设置在高压过热器和调温器的排放端以及HRSG再热器的排放端; 发电机和燃料供应。 蒸汽涡轮机通过多个管道连接到热回收蒸汽发生器（HRSG），蒸汽轮机排气口连接到冷凝器，其中支撑多个辅助和储备以加载跟随，执行调节并满足中间发电服务需求 启动过程。
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公开(公告)号：USD560484S1
公开(公告)日：2008-01-29
申请号：US29268999
申请日：2006-11-17
申请人： Gordon R. Smith
设计人： Gordon R. Smith
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公开(公告)号：US4760770A
公开(公告)日：1988-08-02
申请号：US544865
申请日：1983-10-03
CPC分类号： F41G3/323
摘要： A fire control system comprises a platform (10) rotatable in azimuth on which are mounted a gun (11) first and second sighting devices (15,25) each of which is movable in elevation, each sighting device (15,25) having its sight line nominally aligned with the barrel axis of the gun (11), the first sighting device (15) incorporates a lens (39) defining the sight line thereof, a graticule (41) defining an alignment mark and a mechanism (19,20) coupled to the lens (29) for alignment adjustment. Gun (11) comprises a muzzle reference mirror (12) and the first sighting device (15) incorporates a direction-finding means which is arranged to enable the position of an image in the muzzle reference mirror (12) to be identified with respect to the alignment mark of the graticule (41), the mechanism (19,20) being operable to effect alignment of that mark with the image seen in the muzzle reference mirror position. Mechanism (19,20) further comprises signal-generating sensors (21,22) arranged automatically to provide alignment adjustment identification signals which are processed to provide an electronic graticule in the second sighting device (25) so that the sight line of the second sighting device (25) is automatically aligned with the sight line of the first sighting device (15).
摘要翻译： 消防控制系统包括可在方位旋转的平台（10），在该平台上安装有枪（11），第一和第二瞄准装置（15,25），每个瞄准装置可高度移动，每个瞄准装置（15,25）具有 第一瞄准装置（15）包括限定其瞄准线的透镜（39），限定对准标记的刻度（41）和机构（19,20） ）耦合到透镜（29）以进行对准调整。 枪（11）包括枪口参考反射镜（12），并且第一瞄准装置（15）包括一个方向调查装置，其被布置成能够使枪口参考镜（12）中的图像的位置相对于 刻度（41）的对准标记，机构（19,20）可操作以使该标记与在枪口参考镜位置中看到的图像对准。 机构（19,20）还包括信号发生传感器（21,22），其自动布置以提供对准调整识别信号，所述对准调整识别信号被处理以在第二瞄准装置（25）中提供电子刻度，使得第二瞄准线 装置（25）自动地与第一瞄准装置（15）的瞄准线对准。
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公开(公告)号：USD540158S1
公开(公告)日：2007-04-10
申请号：US29227458
申请日：2005-04-12
申请人： Gordon R. Smith
设计人： Gordon R. Smith
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公开(公告)号：US4494198A
公开(公告)日：1985-01-15
申请号：US352696
申请日：1982-02-26
摘要： A gun fire control system comprises a computer (15) having a first memory (15A) preprogrammed with true range to standard ballistic range conversion data and is operable on receipt of a true range value from a rangefinder (16) to output the corresponding standard ballistic range value. A second memory (15B) of the computer (15) is preprogrammed with correction coefficients (A,B,M,N) arranged in sets pertaining to different types of ammunition one set being operable according to the position of a selector switch (13) and being delivered to a calculator (15C) together with an operator correction value (COR) (from buttons 14A, 14B) which is a judgment on the magnitude and direction by which a projectile misses a target sighted according to the range value presented at display (11). Calculator (15C) operates according to a predetermined algorithm to establish parameter correction changes (.DELTA.AD, .DELTA.CT) and delivers these changes to calculator/store (15D) which updates and stores parameter values (AD, CT). An arithmetic unit (15F) evaluates a range correction factor from the data available from memory (15B) and unit (15D) at the ballistic range established by memory (15A). This range correction factor is combined with the ballistic range established by memory (15A) in unit (15G) and the corrected ballistic range made visibly available in display (11) to the operator. To establish initial values of the parameters (AD, CT) for use in a system restart mode when elapsed time between consecutive operations of the rangefinder (16) exceeds a preset value high and low operator correction averages (HCOR, LCOR) are evaluated on each operation of the system and stored in memory (15E).
摘要翻译： 枪消防控制系统包括一计算机（15），该计算机（15）具有对标准弹道范围转换数据进行预编程的实际范围的第一存储器（15A），并可在从测距仪（16）接收到真实范围值时输出相应的标准弹道 范围值。 计算机（15）的第二存储器（15B）被预编程有与根据选择器开关（13）的位置可操作的不同类型的弹药相关的校正系数（A，B，M，N） 并与来自按钮14A，14B的操作员校正值（COR）一起被递送到计算器（15C），该操作者校正值（COR）是根据在显示器上呈现的范围值来确定射出物未瞄准目标的大小和方向的判断 （11）。 计算器（15C）根据预定算法操作以建立参数校正改变（DELTA AD，DELTA CT），并将这些改变传送到更新并存储参数值（AD，CT）的计算器/存储器（15D）。 算术单元（15F）根据由存储器（15A）建立的弹道范围的存储器（15B）和单元（15D）中可获得的数据来评估范围校正因子。 该范围校正因子与由单元（15G）中的存储器（15A）建立的弹道范围相结合，并且对显示器（11）可见的校正弹道范围与操作者相结合。 为了建立在系统重启模式下使用的参数（AD，CT）的初始值，当测距仪（16）的连续操作超过预设值高和低操作者校正平均值（HCOR，LCOR）时，每个 系统的操作并存储在存储器（15E）中。
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公开(公告)号：US4418361A
公开(公告)日：1983-11-29
申请号：US373734
申请日：1982-04-30
摘要： In a system (10) comprising a trunnion-mounted aiming device (11) and a trunnion-mounted sighting device (14) interconnected by a tracking link (13) and having an associated visual display (16) providing an image of the field of view containing the sight line (15) of the sighting device (14) there is provided a means of accurately positioning an aiming mark designating the pointing direction (12) of the aimed device (11) in the visual display (16). This positioning arrangement is provided by an elevation sensor (18) associated with the aimed device (11), an elevation sensor (19) associated with the sighting device (14), an electronic indicator mark generator (28) and an electronic processor (20), the latter being operable according to the measurements from the sensors (18,19) to deflect the mark generated by the generator (28) so as to compensate in the elevation axis for backlash and inertia of the link (13) and in the traverse axis for lack of parallelism of the trunnion mountings of the devices (11,14). The indicator mark may be generated by a CRT (28,40) in relation to which the processor (20) controls the X and Y drive circuits. Alternatively the processor (20) may generate video bright-up pulses in the raster scan of a scanned raster device forming part of the visual display (16).
摘要翻译： 在包括耳轴安装的瞄准装置（11）和通过跟踪连杆（13）互连的耳轴安装的瞄准装置（14）的系统（10）中，并具有相关联的视觉显示器（16），该视觉显示器提供 提供了包含瞄准装置（14）的瞄准线（15）的视图，其中提供了将瞄准装置（11）的指向方向（12）精确定位在可视显示器（16）中的瞄准标记的装置。 该定位装置由与目标装置（11）相关联的高度传感器（18），与瞄准装置（14）相关联的高度传感器（19），电子指示标记发生器（28）和电子处理器（20） ），后者可根据来自传感器（18,19）的测量值进行操作，以偏转由发电机（28）产生的标记，以便在高度轴上补偿链路（13）的间隙和惯性，并且在 横穿轴，因为装置（11,14）的耳轴安装件的平行度不足。 指示符标记可以由处理器（20）控制X和Y驱动电路的CRT（28,40）生成。 或者，处理器（20）可以在构成视觉显示器（16）的一部分的扫描光栅装置的光栅扫描中产生视频亮起脉冲。
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公开(公告)号：US20070289268A1
公开(公告)日：2007-12-20
申请号：US11455451
申请日：2006-06-19
申请人： Gordon R. Smith
发明人： Gordon R. Smith
IPC分类号： B01D46/00
CPC分类号： B01D46/002 , B01D46/0049 , F02M35/024 , F02M35/04 , F02M35/10019 , F02M35/10262 , F02M35/116 , Y02T10/146
摘要： An air filter assembly is disclosed. An illustrative embodiment of the air filter assembly includes a generally cylindrical air filter housing having a filter housing interior; a carburetor opening provided in the air filter housing and communicating with the filter housing interior; a first housing inlet arm and a second housing inlet arm carried by the air filter housing in spaced-apart relationship with respect to each other and communicating with the filter housing interior; a first air filter and a second air filter communicating with the first housing inlet arm and the second housing inlet arm, respectively; and an air flow deflector provided in the filter housing interior at generally a center of the air filter housing.
摘要翻译： 公开了一种空气过滤器组件。 空气过滤器组件的说明性实施例包括具有过滤器壳体内部的大致圆柱形的空气过滤器壳体; 设置在空气过滤器壳体中并与过滤器壳体内部连通的化油器开口; 第一壳体入口臂和第二壳体入口臂，其由空气过滤器壳体以彼此间隔开的关系承载，并且与过滤器壳体内部连通; 第一空气过滤器和第二空气过滤器分别与第一壳体入口臂和第二壳体入口臂连通; 以及设置在过滤器壳体内部的空气过滤器壳体的大致中心处的空气流动偏转器。
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公开(公告)号：US3966143A
公开(公告)日：1976-06-29
申请号：US437187
申请日：1974-01-28
申请人： Gordon R. Smith
发明人： Gordon R. Smith
CPC分类号： B64C31/02
摘要： An aircraft of variable geometry and certain unique features which allow its operation along the surface of water, ice or the ground under sail power provided by tilting the wings up into a cross-wind to attain sufficient speed to be self launched into gliding flight in two modes -- while close to the surface in wind shear, circling and climbing in a regenerative flight path powered by changes in wind speed with altitude until sufficient altitude is attained to soar on rising air currents.
摘要翻译： 一种具有可变几何形状和某些独特特征的飞机，允许其沿着水，冰或地面下的水面，冰面或地面的运动，通过将翼倾斜成十字风来提供足够的速度以自动发射到两个滑翔飞行中 模式 - 在风切变附近接近表面，在由风速随高度变化驱动的再生飞行路径中盘旋和爬升，直到达到足够高度才能在气流上升时飙升。
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