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公开(公告)号：US09429070B2
公开(公告)日：2016-08-30
申请号：US13782609
申请日：2013-03-01
摘要： System and method for starting a turbine engine are disclosed. These systems and methods for starting a turbine engine may be located on a vehicle, such as such as a Class 8 vehicle, equipped with a turbine engine as the prime mover or as a generator in a hybrid powertrain. In that regard, a fluid forcing device may be employed to start the turbine engine, such as an electric pump/compressor. The fluid forcing device may already be located on the vehicle for other purposes, and can include an electrically powered steering pump (also referred to as an electric pump) or an electrically powered air brake compressor (also referred to as an electric compressor). In order to start the turbine engine, the output of the electric pump/compressor drives an associated fluid circuit, which in turn, supplies fluid over a portion of the turbine shaft, wheel or scroll in order to impart rotational motion thereto. The rotational motion imparted to the turbine shaft, wheel or scroll aims to start the turbine engine. Once started, the output of the electric pump/compressor is either inhibited or redirected to power other devices, such as one or more vehicle accessories (e.g., steering gear, air brakes, power take off (PTO), air conditioner, etc).
摘要翻译： 公开了用于启动涡轮发动机的系统和方法。 用于启动涡轮发动机的这些系统和方法可以位于装备有作为原动机的涡轮发动机或混合动力系中的发电机的诸如8类车辆的车辆上。 在这方面，可以使用流体强制装置来启动涡轮发动机，例如电动泵/压缩机。 流体加压装置可能已经位于车辆上用于其他目的，并且可以包括电动转向泵（也称为电动泵）或电动空气制动压缩机（也称为电动压缩机）。 为了启动涡轮发动机，电动泵/压缩机的输出驱动相关联的流体回路，其又在涡轮机轴，轮或涡轮的一部分上提供流体，以便向其提供旋转运动。 赋予涡轮轴，轮或涡卷的旋转运动旨在启动涡轮发动机。 一旦开始，电动泵/压缩机的输出被禁止或重新定向以对其他装置（例如一个或多个车辆附件（例如舵机，空气制动器，动力输出（PTO），空调等））供电。
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公开(公告)号：US09157374B2
公开(公告)日：2015-10-13
申请号：US13600415
申请日：2012-08-31
CPC分类号： F02C7/32 , F02C7/27 , F05D2260/83 , F16K27/06 , F16K31/54 , Y10T137/0519
摘要： A valve skirt is connected to a shaft. The shaft extends in a rearward direction away from the skirt and has rack teeth at a location spaced away from the skirt. A tab is positioned between the skirt and the rack teeth, and has at least one flat surface. A rack support supports the rack for axial movement, and the rack support has a support ear that has a flat surface engaging the flat surface on the rack to prevent relative rotation of the rack when driven by a pinion gear. An air starter valve, a gas turbine engine and a method are also disclosed.
摘要翻译： 阀裙连接到轴。 轴沿向后的方向远离裙部延伸，并且在与裙部间隔开的位置处具有齿条齿。 突片位于裙部和齿条齿之间，并且具有至少一个平坦表面。 机架支架支撑机架以进行轴向移动，并且机架支架具有支撑耳，其具有与机架上的平坦表面接合的平坦表面，以防止由小齿轮驱动时齿条相对旋转。 还公开了一种空气起动阀，燃气轮机和方法。
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23.发明申请AIR TURBINE STARTER INCLUDING A LIGHTWEIGHT, LOW DIFFERENTIAL PRESSURE CHECK VALVE 审中-公开空气涡轮起动器，包括轻型低压差压检查阀公开(公告)号：US20150082805A1
公开(公告)日：2015-03-26
申请号：US14034058
申请日：2013-09-23
发明人： Peter Kenneth Zeiner , Benjamin Ho , Cindy Byers
CPC分类号： F02C7/277 , F01D19/00 , F01D25/18 , F02C7/06 , F02C7/27 , F02C7/32 , F05D2220/20 , F05D2250/241 , F05D2250/41 , F05D2260/98 , F05D2300/436
摘要： An air turbine starter includes a starter housing and a check valve. The check valve is disposed within the starter housing and is configured, in response to a pressure differential across the check valve, to selectively allow and prevent lubricant to flow therefrom. The check valve includes a valve includes a valve body, a valve seat, a valve bore, a valve element, and a plurality of rounded grooves. The valve bore is formed in the valve body between the valve seat and the lubricant outlet port. The valve element is disposed within the valve bore and is movable between a plurality of open positions and a closed position. The rounded grooves are formed in the valve body, and are disposed adjacent to, and in fluid communication with, the valve bore to improve lubricant to flow past the valve element when the valve element is in an open position.
摘要翻译： 空气涡轮起动器包括起动器壳体和止回阀。 止回阀设置在起动器壳体内，并且响应于止回阀两端的压力差而配置为选择性地允许和防止润滑剂从其中流出。 止回阀包括阀，阀包括阀体，阀座，阀孔，阀元件和多个圆形槽。 阀孔形成在阀体和阀座与润滑剂出口之间。 阀元件设置在阀孔内并且可以在多个打开位置和关闭位置之间移动。 圆形槽形成在阀体中，并且被设置为与阀孔相邻并且与阀孔流体连通，以在阀元件处于打开位置时改善润滑剂流过阀元件。
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公开(公告)号：US07171870B1
公开(公告)日：2007-02-06
申请号：US10963360
申请日：2004-10-12
CPC分类号： F02C7/27 , F02C7/275 , Y10T74/19014 , Y10T74/19158 , Y10T74/19358
摘要： In a system in which a large motor, to be energized from a power grid, is connected to drive a main fluid drive through a main impeller shaft that has a main impeller shaft gear mounted on it, a relatively small start-up motor is provided, driving a start-up fluid drive. A start-up gear is connected to be driven by the start-up fluid drive and selectively to drive the main impeller shaft gear, and to be disengaged from the main impeller shaft gear. In operation, the small motor is first started, with the start-up gear engaging the main impeller shaft gear, and brought up to a speed at which the large motor begins to rotate at close to synchronous speed with the electrical frequency of the grid, at which point the large motor is connected to the grid.
摘要翻译： 在从电力网通电的大型电动机连接驱动主流体驱动通过主叶轮轴的系统中，该主叶轮轴具有安装在其上的主叶轮轴齿轮，提供相对较小的起动马达 ，启动启动流体驱动。 启动齿轮被连接起来，由启动流体驱动驱动，并选择性地驱动主叶轮轴齿轮，并与主叶轮轴齿轮分离。 在运行中，首先启动小电机，起动齿轮与主叶轮轴齿轮接合，并使其达到与电网电气接近同步转速开始转速的速度， 此时大电机连接到电网。
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公开(公告)号：US6128896A
公开(公告)日：2000-10-10
申请号：US138551
申请日：1998-08-24
申请人： Manuel Munoz Saiz
发明人： Manuel Munoz Saiz
CPC分类号： B64D13/00 , B64C23/00 , B64D33/02 , F02C7/27 , F02C7/32 , B64C2230/04 , B64D2013/0622 , B64D2033/0226 , B64D2033/0286 , F05D2220/323 , Y02T50/166 , Y02T50/56
摘要： The device involves the placement of an air pump turbine and the aircraft outflow valve in a duct through which all the air flows, with the turbine shaft attached to that of an electric generator, to a hydraulic pump, and to the N2 and accessory gearbox inside the engine, the air is also sent through a duct to strike inclined against the tips of the fan blades and against the tips of the first stage of the low speed compressor blades of the turbine engine.
摘要翻译： 该装置涉及将空气泵涡轮机和飞机流出阀放置在所有空气流动的管道中，涡轮机轴连接到发电机的涡轮轴到液压泵，以及内部的N2和附件齿轮箱 发动机，空气也通过管道传送，以抵靠风扇叶片的尖端并抵靠涡轮发动机的低速压缩机叶片的第一级的尖端倾斜。
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公开(公告)号：US5303541A
公开(公告)日：1994-04-19
申请号：US29094
申请日：1993-03-10
申请人： Edward R. Goff , Dennis L. Cannon
发明人： Edward R. Goff , Dennis L. Cannon
CPC分类号： F02C9/28 , F02C7/262 , F02C7/27 , F05D2220/50
摘要： A fuel control system for accurately controlling the fuel flow rate to a gas turbine engine during the initial stages of startup is provided. The fuel control system has a novel, closed control loop that measures the actual fuel flow rate to the primary nozzles of the engine, and uses this measurement to trim the commanded fuel flow rate signal generated by preprogrammed schedules in the engine's electronic control unit. By the novel arrangement of proportional and integral controllers, the fuel control system maintains a forward path gain of unity while permitting the independent adjustment of the gain of the controllers to achieve the system stability and response necessary for quick correction of fuel flow rate errors.
摘要翻译： 提供了一种用于在启动初始阶段期间精确地控制燃气涡轮发动机的燃料流量的燃料控制系统。 燃料控制系统具有新颖的闭合控制回路，其测量到发动机的主喷嘴的实际燃料流量，并且使用该测量来修正由发动机的电子控制单元中的预编程计划产生的指令的燃料流量信号。 通过比例和积分控制器的新颖布置，燃料控制系统保持前向通路增益一致，同时允许独立调节控制器的增益，以实现快速校正燃油流量误差所需的系统稳定性和响应。
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公开(公告)号：US5131223A
公开(公告)日：1992-07-21
申请号：US379547
申请日：1989-07-13
申请人： William M. Owen
发明人： William M. Owen
摘要： The weight of a start cartridge in a cruise missile (10) of the type having a booster rocket (60) for initiating flight and a thrust producing gas turbine (12) for sustaining flight may be eliminated by placing the gas outlet (62) for the rocket engine (60) in ducting (64, 82) downstream of the gas turbine engine exhaust (20) so that operation of the rocket (60) to initiate flight of the missile (10), through eduction, draws sufficient air through the engine (12) to accelerate the same to starting speed.
摘要翻译： 具有用于启动飞行的助推器火箭（60）和用于维持飞行的推力产生燃气轮机（12）的类型的巡航导弹（10）中的起动卡盘的重量可以通过将气体出口（62）放置在 所述火箭发动机（60）在所述燃气涡轮发动机排气（20）下游的管道（64,82）中，使得所述火箭（60）通过排出开始飞行所述导弹（10）的操作通过所述第 发动机（12）加速相同的启动速度。
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公开(公告)号：US5054283A
公开(公告)日：1991-10-08
申请号：US409314
申请日：1989-09-19
申请人： Anthony Jones
发明人： Anthony Jones
IPC分类号： F02C7/27
CPC分类号： F02C7/27
摘要： In order to rapidly start turbine engines in a manner eliminating resort to complex mechanical components, an auxiliary impingement assembly is disclosed. The turbine engine will typically have a turbine rotor with impeller blades integral therewith. It will also include a combustor for producing hot gases of combustion and communicating with the turbine rotor through a turbine nozzle. The turbine engine will normally be driven by the hot gases of combustion produced by the combustor. With this arrangement, the auxiliary impingement assembly will include a self-contained independent source of hot gases which may be directed at the impeller blades to assist the combustor in starting the turbine engine.
摘要翻译： 为了以消除复杂的机械部件的方式快速启动涡轮发动机，公开了一种辅助冲击组件。 涡轮发动机通常将具有与其一体的叶轮叶片的涡轮转子。 它还将包括用于产生燃烧热气体并通过涡轮喷嘴与涡轮机转子连通的燃烧器。 涡轮发动机通常由燃烧器产生的燃烧热气体驱动。 利用这种布置，辅助冲击组件将包括独立的独立的热气源，其可以引导到叶轮叶片以辅助燃烧器启动涡轮发动机。
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公开(公告)号：US4712371A
公开(公告)日：1987-12-15
申请号：US797903
申请日：1985-11-14
申请人： Thomas Weber
发明人： Thomas Weber
CPC分类号： F02C7/272 , Y02T50/671
摘要： A process and a device for starting a gas turbine such as a jet engine which contains a compressor, a turbine and a combustion chamber by means of hot exhaust gases from an exhaust gas source, wherein the energy of the exhaust gases is transferred at least partially to the gas turbine for the starting process. For this purpose the hot exhaust gases are used for simultaneously driving the turbine and for igniting the combustion in the combustion chamber. A single exhaust gas source can be used. In this manner, a large number of component parts are eliminated and the reliability of the starting process is considerably increased overall.
摘要翻译： 一种用于启动诸如喷气发动机的燃气轮机的方法和装置，其包含来自废气源的热废气的压缩机，涡轮机和燃烧室，其中废气的能量至少部分地转移 到燃气轮机进行起动过程。 为此，热废气用于同时驱动涡轮并用于点燃燃烧室中的燃烧。 可以使用单个废气源。 以这种方式，消除了大量的部件，并且总体上大大提高了起动过程的可靠性。
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公开(公告)号：US3310936A
公开(公告)日：1967-03-28
申请号：US45459565
申请日：1965-05-10
申请人： ROLLS ROYCE
CPC分类号： B64C29/0058 , F02C7/27 , Y02T50/672
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