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    • 5. 发明授权
    • Method and apparatus for resolving return from subroutine instructions
in a computer processor
    • 用于解决计算机处理器中子程序指令返回的方法和装置
    • US5604877A
    • 1997-02-18
    • US176065
    • 1994-01-04
    • Bradley D. HoytGlenn J. HintonDavid B. PapworthAshwani K. GuptaMichael A. FettermanSubramanian NatarajanSunil ShenoyReynold V. D'Sa
    • Bradley D. HoytGlenn J. HintonDavid B. PapworthAshwani K. GuptaMichael A. FettermanSubramanian NatarajanSunil ShenoyReynold V. D'Sa
    • G06F9/38G06F9/42
    • G06F9/3806G06F9/30054G06F9/4426
    • A method and apparatus for resolving Return From Subroutine instructions in a computer processor are disclosed. The method and apparatus resolve Return From Subroutine instructions in four stages. A first stage predicts Call Subroutine instructions and Return From Subroutine instructions within the instruction stream. The first stage stores a return address in a return register when a Call Subroutine instruction is predicted. The first stage predicts a return to the return address in the return register when a Return From Subroutine instruction is predicted. A second stage decodes each Call Subroutine and Return From Subroutine instruction in order to maintain a Return Stack Buffer that stores a stack of return addresses. Each time the second stage decodes a Call Subroutine instruction, a return address is pushed onto the Return Stack Buffer. Correspondingly, each time the second stage decodes a Return From Subroutine instruction, a return address is popped off of the Return Stack Buffer. The second stage verifies predictions made by the first stage and predicts return addresses for Return From Subroutine instructions that were not predicted by the first stage. A third stage executes Return From Subroutine instructions such that the predictions are verified. Finally, a fourth stage retires Return From Subroutine instructions and ensures that no instructions fetch after a mispredicted return address are committed into permanent state.
    • 公开了一种用于解决计算机处理器中的子程序返回指令的方法和装置。 该方法和设备分四个阶段解析子程序指令。 第一阶段预测指令流中的调用子程序指令和子程序返回指令。 当预测一个调用子程序指令时,第一阶段将返回地址存储在一个返回寄存器中。 第一阶段预测当返回从子程序指令被预测时返回寄存器中的返回地址。 第二阶段解码每个调用子程序和从子程序返回指令,以便维护一个存储一堆返回地址的返回栈缓冲区。 每次第二阶段解码一个调用子程序指令时,一个返回地址被推到返回栈缓冲区上。 相应地,每次第二级解码从子程序返回指令时,返回地址从返回堆栈缓冲区中弹出。 第二阶段验证第一阶段做出的预测,并预测第一阶段未预测的返回从子程序指令的返回地址。 第三阶段执行从子程序返回指令,使得预测得到验证。 最后,第四阶段退出从子程序返回指令,并确保在错误预测的返回地址之后没有指令提取到永久状态。
    • 6. 发明申请
    • FUEL EFFICIENT ULTRA-LOW EMISSION AND IMPROVED PATTERN FACTOR COLORLESS DISTRIBUTED COMBUSTION FOR STATIONARY AND PROPULSION GAS TURBINE APPLICATIONS
    • 燃油有效超低排放和改进的图案因子无级分布式燃烧用于定位和推进气体涡轮应用
    • US20110023492A1
    • 2011-02-03
    • US12686742
    • 2010-01-13
    • Ashwani K. Gupta
    • Ashwani K. Gupta
    • F02C7/22
    • F23R3/20F02C7/22F23C9/006F23C2900/99001Y02E20/342Y02T50/671
    • Colorless distributed combustion (CDC) reactors or green combustion gas turbine combustors having a combustion chamber are presented for improved performance of gas turbine combustion engines. The combustors are configured and designed for providing a superior pattern factor (uniform thermal field in the combustion zone) and a reduction or complete elimination of pollutants emission from the combustor (i.e., zero emission gas turbine combustor) and uniform thermal field in the entire combustion zone to provide significantly improved pattern factor. Colorless distributed combustion is achieved with fuel and air entering the combustion chamber via one or more injection ports as non-premixed, or premixed. Rectangular, cylindrical, stadium and elliptical shaped combustors are presented with injection ports and exit ports located in various locations of the combustors. The mixture preparation between fuel and air with the hot combustion products is carried out either with the gases present in the combustion chamber or via a communication link between the exit gases from the combustor back to the combustion chamber.
    • 提出了具有燃烧室的无色分散燃烧(CDC)反应器或绿色燃烧燃气涡轮燃烧器,以改善燃气轮机内燃机的性能。 燃烧器被配置和设计用于提供优异的模式因子(燃烧区域中的均匀热场)和减少或完全消除来自燃烧器(即,零排放燃气轮机燃烧器)的污染物排放和整个燃烧中的均匀热场 区域提供显着改善的模式因子。 无油分布式燃烧是通过燃料和空气通过一个或多个喷射口进入燃烧室而实现的,如非预混合或预混合。 矩形,圆柱形,体育场和椭圆形燃烧器都带有位于燃烧器各处的注射口和出口。 燃料和空气与热燃烧产物之间的混合物制备可以通过存在于燃烧室中的气体或通过来自燃烧器的出口气体到燃烧室之间的连通连接进行。
    • 8. 发明授权
    • Method and system for recovering sulfur in the thermal stage of a Claus reactor
    • 在克劳斯反应器的热级中回收硫的方法和系统
    • US08449860B2
    • 2013-05-28
    • US13127364
    • 2009-10-30
    • Ashwani K. Gupta
    • Ashwani K. Gupta
    • B01D53/76C01B17/04
    • B01D53/52B01D2251/102C01B17/0413C01B17/0417Y02P20/129
    • Method and system are presented for the combustion of hydrogen sulfide mixed with other gases for simultaneous recovery of sulfur and energy from hydrogen sulfide at higher efficiency. The amounts and velocity of the hydrogen sulfide into the reactor is selected in such a way that it is not possible to burn the hydrogen sulfide in a normal thin reaction zone during its combustion. The injected hydrogen sulfide gas is mixed in a thermal reactor with fresh air and hot active combustion gases in the reactor on account of internal jet pump effect and self-induced entrainment. The reaction is exothermic so that the chemical energy present in hydrogen sulfide is recovered together with the sulfur. Various reactors are shown capable of controlling the formation of a thermal distribution flow pattern based on the position, and position and direction (and other factors) regarding fluid introduction within a combustion chamber of the reactors.
    • 提出了与其他气体混合的硫化氢燃烧方法和系统,以更高效率同时从硫化氢中回收硫和能量。 选择硫化氢进入反应器的量和速度,使得在其燃烧期间不可能在正常的薄反应区中燃烧硫化氢。 注入的硫化氢气体在热反应器中与新鲜空气和热活性燃烧气体在反应器中混合,这是由于内部喷射泵效应和自身引发的夹带。 反应是放热的,因此存在于硫化氢中的化学能与硫一起回收。 示出了能够基于位于反应器的燃烧室内的流体引入的位置以及位置和方向(和其它因素)来控制形成热分布流动模式的各种反应器。
    • 9. 发明授权
    • Fuel efficient ultra-low emission and improved pattern factor colorless distributed combustion for stationary and propulsion gas turbine applications
    • 燃料效率超低排放和改进的模式因子无级分布式燃烧用于固定和推进燃气轮机应用
    • US08695350B2
    • 2014-04-15
    • US12686742
    • 2010-01-13
    • Ashwani K. Gupta
    • Ashwani K. Gupta
    • F02C3/34
    • F23R3/20F02C7/22F23C9/006F23C2900/99001Y02E20/342Y02T50/671
    • Colorless distributed combustion (CDC) reactors or green combustion gas turbine combustors having a combustion chamber are presented for improved performance of gas turbine combustion engines. The combustors are configured and designed for providing a superior pattern factor (uniform thermal field in the combustion zone) and a reduction or complete elimination of pollutants emission from the combustor (i.e., zero emission gas turbine combustor) and uniform thermal field in the entire combustion zone to provide significantly improved pattern factor. Colorless distributed combustion is achieved with fuel and air entering the combustion chamber via one or more injection ports as non-premixed, or premixed. Rectangular, cylindrical, stadium and elliptical shaped combustors are presented with injection ports and exit ports located in various locations of the combustors. The mixture preparation between fuel and air with the hot combustion products is carried out either with the gases present in the combustion chamber or via a communication link between the exit gases from the combustor back to the combustion chamber.
    • 提出了具有燃烧室的无色分散燃烧(CDC)反应器或绿色燃烧燃气涡轮燃烧器,以改善燃气轮机内燃机的性能。 燃烧器被配置和设计用于提供优异的模式因子(燃烧区域中的均匀热场)和减少或完全消除来自燃烧器(即,零排放燃气轮机燃烧器)的污染物排放和整个燃烧中的均匀热场 区域提供显着改善的模式因子。 无油分布式燃烧是通过燃料和空气通过一个或多个喷射口进入燃烧室而实现的,如非预混合或预混合。 矩形,圆柱形,体育场和椭圆形燃烧器都带有位于燃烧器各处的注射口和出口。 燃料和空气与热燃烧产物之间的混合物制备可以通过存在于燃烧室中的气体或通过来自燃烧器的出口气体到燃烧室之间的连通连接进行。