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    Steam engine with improve inlet valve arrangement
    1.
    发明授权
    Steam engine with improve inlet valve arrangement 失效
    具有改进入口阀装置的蒸汽发动机

    公开(公告)号：US3881399A

    公开(公告)日：1975-05-06

    申请号：US3281570

    申请日：1970-04-29

    Applicant: GEN MOTORS CORP

    Inventor： SAGI CHARLES J ,  AMANN CHARLES A

    IPC: F01B17/04 ,  F01B25/02 ,  F01L31/08

    CPC classification number: F01B25/02 ,  F01B17/04 ,  F01L31/08

    Abstract: A piston type steam engine expander of the high speed, variable speed type having a poppet steam inlet valve and cylinder outlet ports and operable over a wide speed range on a throttled steam supply includes valve mechanism arranged to actuate the inlet valve through a fixed lift curve which provides a substantial change in effective steam cutoff at various speeds, as well as providing advantageous valve opening characteristics. Operating advantages similar to those of variable opening and closing inlet valves are provided by the use of a long valve open period including early opening and late closing of the valve, combined with unusually slow valve motion in the early stages of opening and the final stages of closing.

    Abstract translation: 具有提升阀蒸汽入口阀和气缸出口的高速变速型活塞式蒸汽发动机膨胀机可在节流蒸汽供应器上在宽速度范围内操作，包括阀机构，其布置成通过固定升力曲线致动入口阀 这提供了在各种速度下的有效蒸汽截断的显着变化，以及提供有利的阀打开特性。 与可变开启和关闭进气阀类似的操作优点是通过使用长阀打开时间段来提供的，包括阀的早期开启和后期关闭，以及在开启的早期阶段和最后阶段期间异常缓慢的阀运动 关闭。

    Gas turbine engine with combustion chamber bypass for fuel-air ratio control and turbine cooling
    2.
    发明授权
    Gas turbine engine with combustion chamber bypass for fuel-air ratio control and turbine cooling 失效
    燃气涡轮发动机燃烧空气比例控制和涡轮冷却燃烧室旁路

    公开(公告)号：US3584459A

    公开(公告)日：1971-06-15

    申请号：US3584459D

    申请日：1968-09-12

    Applicant: GEN MOTORS CORP

    Inventor： AMANN CHARLES A

    IPC: F02C9/18 ,  F02C9/02 ,  F02C7/12 ,  F02C9/14

    CPC classification number: F02C9/18

    Abstract: A gas turbine engine which may otherwise be of conventional configuration, single or plural shaft, regenerative or nonregenerative, is provided with a controlled bypass from the compressor to the turbine bypassing the combustion apparatus. Flow through this bypass is controlled so as to maintain the fuel-air ratio in the combustion chamber substantially constant notwithstanding variations in fuel flow and airflow with the load carried by the engine. Control of flow through the bypass may respond to setting of the fuel control device, to compressor discharge pressure, or to burner outlet temperature.

    Gas turbine with throttle responsive hydrokinetic torque converter and throttle responsive hydrokinetic torque converter
    3.
    发明授权
    Gas turbine with throttle responsive hydrokinetic torque converter and throttle responsive hydrokinetic torque converter 失效
    带有反作用力扭矩变扭器和扭矩响应式压力变矩器的气体涡轮机

    公开(公告)号：US3886729A

    公开(公告)日：1975-06-03

    申请号：US39285573

    申请日：1973-08-30

    Applicant: GEN MOTORS CORP

    Inventor： AMANN CHARLES A ,  SHERIDAN DAVID C

    IPC: F02C6/20 ,  B60K3/04 ,  B60K17/04 ,  F02C7/36 ,  F02C9/28 ,  F16H61/56 ,  F02D9/02 ,  F16D33/04

    CPC classification number: B60K3/04 ,  B60K17/04 ,  F02C7/36 ,  F16H61/56 ,  Y02T50/672

    Abstract: A gas turbine having a compressor and a turbine mounted on a single shaft and a throttle actuated fuel control responsive to parameters as compressor discharge pressure, engine speed and temperature to provide power increasing with engine speed as the throttle is advanced to a maximum limited by the fuel control. The engine drives a hydrodynamic torque converter having power absorption or capacity characteristics varying as a function of engine or input speed and substantially independent of output speed having variable pitch stator blades movable from a full power capacity position through a range of intermediate power capacity positions to a minimum power capacity position controlled as a function of throttle position and engine speed. When the throttle is in a closed position the fuel control provides starting or idle fuel feed and the stator control provides minimum capacity position of the stator blades for low drag during engine starting and low creep during engine idling. When the throttle is advanced to full throttle position the fuel control provides under steady state operating conditions power increasing with throttle advancement up to the maximum rated power and the stator control controls stator blade angle to provide torque converter capacity matching engine power. When the throttle is quickly advanced from some partial position to full throttle for maximum acceleration, the stator vanes are switched to an intermediate capacity position for acceleration up to maximum engine speed and then returned to the above steady state control mode.

    Abstract translation: 一种具有压缩机和安装在单个轴上的涡轮机的燃气轮机，以及响应于作为压缩机排放压力，发动机转速和温度的参数的节气门致动燃料控制，以随着节气门推进到最大限度的发动机转速而提高功率 燃油控制。 发动机驱动具有作为发动机或输入速度的函数变化的功率吸收或容量特性的流体动力学变矩器，并且基本上与输出速度基本上无关，具有可变节距定子叶片，其可从全功率容量位置通过中间功率容量位置的范围移动到 作为节气门位置和发动机转速的函数控制最小功率容量位置。 当节气门处于关闭位置时，燃油控制提供启动或空闲燃料供给，并且定子控制提供定子叶片的最小容量位置，用于发动机起动期间的低阻力以及在发动机怠速期间的低蠕变。 当节气门前进到全节气门位置时，燃油控制在稳态运行条件下提供功率增加，节气门提前达到最大额定功率，定子控制控制定子叶片角度，提供匹配发动机功率的变矩器容量。 当节气门从一些局部位置快速提升到全节气门以实现最大加速时，定子叶片切换到中间容量位置，以加速到最大发动机转速，然后返回到上述稳态控制模式。

    Power turbine deceleration control
    5.
    发明授权
    Power turbine deceleration control 失效
    动力涡轮减速控制

    公开(公告)号：US3893292A

    公开(公告)日：1975-07-08

    申请号：US38595173

    申请日：1973-08-06

    Applicant: GEN MOTORS CORP

    Inventor： AMANN CHARLES A ,  LIDDLE SIDNEY G

    IPC: F02C9/18 ,  F02C9/08

    CPC classification number: F02C9/18

    Abstract: A gas turbine engine connected to drive a motor vehicle includes valving to by-pass the regenerator of the engine when it is desired to decelerate the vehicle so that heat stored in the regenerator is not effective to provide positive power output from the turbine. The cold gas path of the heat exchanger only may be by-passed; or, compressed air may be diverted to atmosphere, by-passing the combustion apparatus, turbine and the entire heat exchanger. Opening of the by-pass is responsive to a request for zero or idling power output from the engine and to turbine rpm above a particular level.

    Abstract translation: 连接以驱动机动车辆的燃气涡轮发动机包括阀，以在需要使车辆减速时绕过发动机的再生器，使得存储在再生器中的热量不能有效地提供来自涡轮机的正功率输出。 热交换器的冷气路径只能被旁路; 或者压缩空气可以转移到大气中，绕过燃烧装置，涡轮机和整个热交换器。 旁路的打开响应于从发动机输出的零或空转功率的请求以及高于特定水平的涡轮转速。

    Gas turbine control with prewhirl of air entering the compressor
    6.
    发明授权
    Gas turbine control with prewhirl of air entering the compressor 失效
    具有进口压缩机空气的燃气涡轮机控制

    公开(公告)号：US3657881A

    公开(公告)日：1972-04-25

    申请号：US3657881D

    申请日：1969-09-02

    Applicant: GEN MOTORS CORP

    Inventor： AMANN CHARLES A ,  RUCINS ERIK H

    IPC: F02C9/20 ,  F02C9/54 ,  F02C9/56 ,  F02C9/14

    CPC classification number: F02C9/54 ,  F02C9/20 ,  F02C9/56 ,  Y10T477/40

    Abstract: A vehicle turbine of the gas-coupled type propels the vehicle through a change-speed transmission. To reduce vehicle acceleration time with an acceptable penalty with respect to fuel consumption, the compressor of the engine has variable inlet guide vanes which are shifted into a positive prewhirl angle at idling speeds when the transmission is shifted into a drive condition. Thus the engine gas generator has a low speed idle, with axially oriented guide vanes and normal air entrance, when the transmission is in neutral, and a high speed idle with positive prewhirl when the transmission is in drive condition. Also, the vanes are shifted at full speed of the gas generator to provide negative prewhirl and thus reduce the engine speed corresponding to maximum power output. Because of the higher idle and lower maximum speeds, the acceleration time of the gas generator, and thus of the power turbine, is reduced. Because positive prewhirl reduces compressor pressure ratio at the high speed idle, the power turbine does not have an undue tendency to cause creep of the vehicle in the high speed idle.

    Abstract translation: 气体联接式的车辆涡轮通过变速传动推动车辆。 为了以相对于燃料消耗的可接受的惩罚来减少车辆加速时间，发动机的压缩机具有可变的入口导向叶片，当变速器转换到驱动条件时，它们以空转速度偏移到正的预旋转角度。 因此，发动机气体发生器具有低速怠速，当变速器处于空档状态时，具有轴向定向的导向叶片和正常空气入口，以及当变速器处于驱动状态时具有正向预热的高速怠速。 此外，叶片以气体发生器的全速移动以提供负的前翅，并因此降低对应于最大功率输出的发动机转速。 由于较高的怠速和较低的最大速度，所以气体发生器和动力涡轮机的加速时间减小。 因为正偏压在高速怠速时降低了压缩机压力比，所以动力涡轮机不会在高速怠速时引起车辆蠕变的不适当倾向。

    Condensable vapor engine construction
    8.
    发明授权
    Condensable vapor engine construction 失效
    可冷凝蒸汽发动机结构

    公开(公告)号：US3638533A

    公开(公告)日：1972-02-01

    申请号：US3638533D

    申请日：1970-04-29

    Applicant: GEN MOTORS CORP

    Inventor： SHERIDAN DAVID CARL ,  AMANN CHARLES A ,  RICKETTS JAMES M

    IPC: F01B17/04 ,  F01L25/06 ,  F01L15/16

    CPC classification number: F01B17/04 ,  F01B2170/0423 ,  F01B2170/0476

    Abstract: A condensable vapor engine, such as a steam engine, wherein the piston reciprocates between a top dead center position adjacent the closed end of the cylinder and a bottom dead center position in which vapor outlet ports are uncovered and the vapor escapes. The engine includes a valve located in the cylinder head and in communication with the source of vapor, this valve being disposed in a cavity having a cylindrical caging surface and facing a valve seat. The valve is arranged in spaced relation to the cylindrical surface so as to permit freedom of opening and closing movement and tilt, and the valve and valve seat define cone-to-sphere cooperating surfaces providing full seating engagement despite tilt of the valve body.

    Abstract translation: 一种可冷凝蒸汽发动机，例如蒸汽发动机，其中活塞在邻近气缸的封闭端的上止点位置和蒸汽出口未被覆盖的下死点位置之间往复运动并且蒸汽逸出。 发动机包括位于气缸盖中并与蒸气源连通的阀，该阀设置在具有圆柱形笼形表面并且面向阀座的空腔中。 阀门与圆柱形表面间隔开设置，以允许打开和关闭运动和倾斜的自由度，阀和阀座限定圆锥对配合表面，尽管阀体倾斜，但提供了完全的座椅接合。

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