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公开(公告)号：US20090139398A1
公开(公告)日：2009-06-04
申请号：US11948278
申请日：2007-11-30
摘要： An inertial inlet particle separator system for a vehicle engine includes an inertial inlet particle separator and an adjustment mechanism. The separator includes a fluid inlet coupled to a scavenge channel and to a clean channel such that a first amount of fluid passing through the fluid inlet enters the scavenge channel and a second amount of fluid passing through the fluid inlet enters the clean channel. The scavenge channel is defined by a first wall and a splitter, and the clean channel is defined by a second wall and the splitter. The splitter and the second wall are stationary with respect to each other. The adjustment mechanism is coupled to the inertial inlet particle separator and configured to adjust a size of the scavenge channel. Although not necessarily, the adjustment mechanism may also be coupled to the scavenge fan speed.
摘要翻译： 用于车辆发动机的惯性入口颗粒分离器系统包括惯性入口颗粒分离器和调节机构。 分离器包括连接到扫气通道和清洁通道的流体入口，使得通过流体入口的第一量的流体进入扫气通道，并且穿过流体入口的第二量的流体进入清洁通道。 清扫通道由第一壁和分流器限定，并且清洁通道由第二壁和分离器限定。 分流器和第二壁相对于彼此是静止的。 调节机构耦合到惯性入口颗粒分离器并且被配置为调节清除通道的尺寸。 尽管不一定，调节机构也可以与清扫风扇速度相结合。
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公开(公告)号：US07927408B2
公开(公告)日：2011-04-19
申请号：US11948278
申请日：2007-11-30
IPC分类号： B01D45/00
摘要： An inertial inlet particle separator system for a vehicle engine includes an inertial inlet particle separator and an adjustment mechanism. The separator includes a fluid inlet coupled to a scavenge channel and to a clean channel such that a first amount of fluid passing through the fluid inlet enters the scavenge channel and a second amount of fluid passing through the fluid inlet enters the clean channel. The scavenge channel is defined by a first wall and a splitter, and the clean channel is defined by a second wall and the splitter. The splitter and the second wall are stationary with respect to each other. The adjustment mechanism is coupled to the inertial inlet particle separator and configured to adjust a size of the scavenge channel. Although not necessarily, the adjustment mechanism may also be coupled to the scavenge fan speed.
摘要翻译： 用于车辆发动机的惯性入口颗粒分离器系统包括惯性入口颗粒分离器和调节机构。 分离器包括连接到扫气通道和清洁通道的流体入口，使得通过流体入口的第一量的流体进入扫气通道，并且穿过流体入口的第二量的流体进入清洁通道。 清扫通道由第一壁和分流器限定，并且清洁通道由第二壁和分离器限定。 分流器和第二壁相对于彼此是静止的。 调节机构耦合到惯性入口颗粒分离器并且被配置为调节清除通道的尺寸。 尽管不一定，调节机构也可以与清扫风扇速度相结合。
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3.发明申请Systems And Methods For Reducing Pressure Loss Of Air Flowing From A First Area To A Second Area 审中-公开减少从第一个区域流向第二个区域的空气压力损失的系统和方法公开(公告)号：US20080203218A1
公开(公告)日：2008-08-28
申请号：US11678899
申请日：2007-02-26
CPC分类号： B64D13/00 , B64D33/02 , Y02T50/56 , Y10T29/49428
摘要： Systems and methods are provided for reducing pressure loss of air flowing from a first area in a first direction to a second area in a second direction. The systems include a flow surface, first and second fence walls, an opening, and a flow path. The flow surface defines a portion of the first area. The fence walls extend substantially parallel to each other along the flow surface in the first direction. The opening is formed in the flow surface and is disposed between the first and second fence walls. The flow path defines at least a portion of the second area and is in flow communication with the opening to receive a portion of the airflow and to direct the airflow in the second direction. Methods of using and manufacturing the systems are also provided.
摘要翻译： 提供的系统和方法用于减少从第一方向的第一区域流向第二方向的第二区域的空气的压力损失。 这些系统包括流动表面，第一和第二栅栏壁，开口和流动路径。 流动表面限定第一区域的一部分。 栅栏壁沿着第一方向上的流动表面基本上彼此平行地延伸。 开口形成在流动表面中并且设置在第一和第二栅栏壁之间。 流动路径限定第二区域的至少一部分并且与开口流动连通以接收气流的一部分并且引导气流沿第二方向。 还提供了使用和制造系统的方法。
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公开(公告)号：US20080057848A1
公开(公告)日：2008-03-06
申请号：US11515120
申请日：2006-08-31
IPC分类号： B60H1/00
CPC分类号： B64D41/00 , B64D2033/0213 , F01D17/145 , F05D2250/232 , Y02T50/671
摘要： A venturi gate valve assembly for extraction of bleed air flow from an auxiliary power unit (APU) and an APU compartment including the venturi gate valve assembly. The venturi gate valve assembly is configured to isolate and restrict bleed air flow from the APU via an extraction conduit. The venturi gate valve assembly includes an upstream valve flange, a throat area, a moveable valve gate, and a downstream valve flange, in fluid communication defining a bleed air flow path. A conical shaped diffuser is defined along the bleed air flow path from the throat area to the downstream flange.
摘要翻译： 一种文丘里闸阀组件，用于从辅助动力单元（APU）和包括文丘里闸阀组件的APU隔室抽取出气流。 文丘里闸阀组件被配置为隔离并限制经由抽出导管从APU排出的气流。 文丘里闸阀组件包括限定出气流动路径的流体连通的上游阀法兰，喉部区域，可动阀门和下游阀法兰。 沿着从喉部区域到下游凸缘的排气流动路径限定圆锥形扩散器。
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公开(公告)号：US06264137B1
公开(公告)日：2001-07-24
申请号：US09514203
申请日：2000-02-25
申请人： Yogendra Y. Sheoran
发明人： Yogendra Y. Sheoran
IPC分类号： B64B124
CPC分类号： F02C3/32 , B64D33/02 , B64D41/00 , B64D2033/0213 , B64D2041/002 , F05D2220/40 , F05D2260/601
摘要： An air inlet assembly for bringing air to an auxiliary power unit mounted in the compartment of an aircraft. The assembly includes a duct extending from an intake contoured to conform to the to the aircraft fuselage to an exit coupled to the inlet plenum of the auxiliary power unit. A first door hingeably mounted to the aft side of said intake and moveable from an open position to a closed position where said first door lies flush against intake, said first door having a closing wall and two side walls and a second door hingeably mounted to the forward end of said intake, said second door having a plate with two inwardly extending walls, each of said inwardly extending walls hinged to one of said side walls so that the second door rotates with said first door. During ground operation air that would have swirled around the side walls of the first door thus generating inlet corner vortices are now blocked by the side walls of the second door.
摘要翻译： 用于将空气引导到安装在飞行器舱室中的辅助动力单元的空气入口组件。 该组件包括一个从进气轮廓延伸到与飞机机身一致的导管，连接到辅助动力单元的入口气室。 第一门铰接地安装在所述入口的后侧，并且可从打开位置运动到关闭位置，在所述关闭位置，所述第一门与入口齐平，所述第一门具有封闭壁和两个侧壁以及可铰接地安装在所述第二门上的第二门 所述第二门的前端具有带有两个向内延伸的壁的板，每个所述向内延伸的壁铰接到所述侧壁中的一个，使得所述第二门与所述第一门旋转。 在地面操作期间，将围绕第一门的侧壁旋转的空气因此产生入口角旋涡现在被第二门的侧壁阻挡。
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6.发明授权Compact, light weight eductor oil cooler plenum and surge flow plenum design 有权紧凑，重量轻的喷射器油冷却器集气室和浪涌气流通风设计公开(公告)号：US07698896B2
公开(公告)日：2010-04-20
申请号：US11303180
申请日：2005-12-15
IPC分类号： F02K1/00
CPC分类号： F02C7/32 , B64D41/00 , B64D2033/0213 , B64D2041/002 , F01D25/18 , Y02T50/671
摘要： An eductor assembly is provided that includes a primary nozzle, a cooler plenum, and a surge plenum. In one embodiment, and by way of example only, the primary nozzle is configured to accelerate and discharge turbine exhaust gas therefrom and the cooler plenum surrounds the primary nozzle and includes at least a fluid inlet and a fluid outlet. The surge plenum partially surrounds the primary nozzle and the cooler plenum and includes at least a fluid inlet and a fluid outlet. The surge plenum fluid outlet axially aligns and is coterminous with the cooler plenum fluid outlet.
摘要翻译： 提供了一种喷射器组件，其包括主喷嘴，较冷气室和浪涌气室。 在一个实施例中，仅作为示例，主喷嘴构造成从其中加速和排放涡轮废气，并且冷却器压力室围绕主喷嘴并且至少包括流体入口和流体出口。 浪涌气室部分地围绕主喷嘴和冷却器气室，并且至少包括流体入口和流体出口。 浪涌增压室流体出口轴向对准并与冷却器增压室流体出口相连。
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公开(公告)号：US07665694B2
公开(公告)日：2010-02-23
申请号：US11691679
申请日：2007-03-27
申请人： Jeffrey M. Hein , Nicholas A. Williams , Yogendra Y. Sheoran , Cecilia S. Lam , Ora Morency Cowans , Benjamen Kurt Higuera , Andrew Stephen Peduchi , Ravisha Pramod Sellahewa , Daniel Brown
发明人： Jeffrey M. Hein , Nicholas A. Williams , Yogendra Y. Sheoran , Cecilia S. Lam , Ora Morency Cowans , Benjamen Kurt Higuera , Andrew Stephen Peduchi , Ravisha Pramod Sellahewa , Daniel Brown
CPC分类号： F02C7/04 , B64D33/02 , B64D41/00 , B64D2033/0213 , B64D2041/002 , F02C7/045 , F02C7/32 , F05D2220/50 , F05D2260/96
摘要： An inlet door assembly and method for reducing noise from an auxiliary power unit (APU) contained within an aircraft housing is provided. The inlet assembly includes an inlet duct, an actuator, and a door. The inlet duct is configured to extend from the auxiliary power unit to the aircraft housing and has a sidewall that defines a flow passage through which APU noise propagates. The actuator is disposed at least partially within the inlet duct. The door coupled to the actuator. The actuator is also configured to selectively rotate the door between at least a first position, in which at least a portion of the door deflects APU noise in a first direction, and a second position, in which at least a portion of the door deflects the APU noise in a second direction.
摘要翻译： 提供了一种用于降低包含在飞行器壳体内的辅助动力单元（APU）的噪声的入口门组件和方法。 入口组件包括入口管道，致动器和门。 入口管道被构造成从辅助动力单元延伸到飞行器壳体，并且具有限定APU噪声传播通过的流动通道的侧壁。 致动器至少部分地设置在入口管道内。 门连接到执行机构。 致动器还构造成在至少第一位置之间选择性地旋转门，其中门的至少一部分在第一方向上偏转APU噪声和第二位置，其中门的至少一部分偏转 APU噪声在第二个方向。
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公开(公告)号：US20080118347A1
公开(公告)日：2008-05-22
申请号：US11603424
申请日：2006-11-22
IPC分类号： F01D25/30
CPC分类号： F01D25/30 , F05D2250/191 , F05D2260/96
摘要： An exhaust muffler is provided for a turbine engine with at least first and second exhaust outlets. The exhaust muffler includes a first arm configured to be coupled to the first exhaust outlet of the turbine engine. The first arm includes an outer surface, and an inner surface that defines a first exhaust cavity. The first arm further includes a plurality of perforations extending between the inner and outer surfaces. The exhaust muffler further includes a second arm coupled to the first arm and configured to be coupled to the second exhaust outlet of the turbine engine. The second arm includes an outer surface, and an inner surface that defines a second exhaust cavity. The second arm also includes a plurality of perforations extending between the inner and outer surfaces.
摘要翻译： 为具有至少第一和第二排气出口的涡轮发动机提供排气消音器。 排气消声器包括构造成联接到涡轮发动机的第一排气出口的第一臂。 第一臂包括外表面和限定第一排气腔的内表面。 第一臂还包括在内表面和外表面之间延伸的多个穿孔。 排气消声器还包括联接到第一臂并被配置为联接到涡轮发动机的第二排气出口的第二臂。 第二臂包括外表面和限定第二排气腔的内表面。 第二臂还包括在内表面和外表面之间延伸的多个穿孔。
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公开(公告)号：US06520738B2
公开(公告)日：2003-02-18
申请号：US09809588
申请日：2001-03-15
IPC分类号： F01D2500
CPC分类号： B64D41/00 , B64D33/02 , B64D2033/0213 , F02C7/04 , F05D2220/50 , F15D1/04
摘要： A swirl generator for creating bulk swirl in a compressor plenum in the opposite direction to the direction of rotation of the compressor rotor. The generator includes a continuous flow passageway formed by an inlet duct and a compressor forming an angle in the range of about 0°-180° to one another. A non-uniform velocity gradient is created by forming an area of non-uniform cross-sectional area within the flow passageway. The non-uniform area may comprise a ramp with a tapered end line, a rounded line of intersection, a fillet or by lengthening one side wall of the inlet duct relative to the opposite side wall. Preferably, the non-uniform cross sectional area uniformly tapers from ones sidewall of the flow passageway to the opposite sidewall.
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公开(公告)号：US07210652B2
公开(公告)日：2007-05-01
申请号：US11299116
申请日：2005-12-08
申请人： Jeffrey M. Hein , Nicholas A. Williams , Yogendra Y. Sheoran , Cecilia S. Lam , Ora Morency Cowans , Benjamen Kurt Higuera , Andrew Stephen Peduchi , Ravisha Pramod Sellahewa , Daniel Brown
发明人： Jeffrey M. Hein , Nicholas A. Williams , Yogendra Y. Sheoran , Cecilia S. Lam , Ora Morency Cowans , Benjamen Kurt Higuera , Andrew Stephen Peduchi , Ravisha Pramod Sellahewa , Daniel Brown
IPC分类号： B64D33/02
CPC分类号： F02C7/04 , B64D33/02 , B64D41/00 , B64D2033/0213 , B64D2041/002 , F02C7/045 , F02C7/32 , F05D2220/50 , F05D2260/96
摘要： An inlet door assembly and method for reducing noise from an auxiliary power unit (APU) contained within an aircraft housing is provided. The inlet assembly includes an inlet duct, an actuator, and a door. The inlet duct is configured to extend from the auxiliary power unit to the aircraft housing and has a sidewall that defines a flow passage through which APU noise propagates. The actuator is disposed at least partially within the inlet duct. The door coupled to the actuator. The actuator is also configured to selectively rotate the door between at least a first position, in which at least a portion of the door deflects APU noise in a first direction, and a second position, in which at least a portion of the door deflects the APU noise in a second direction.
摘要翻译： 提供了一种用于降低包含在飞行器壳体内的辅助动力单元（APU）的噪声的入口门组件和方法。 入口组件包括入口管道，致动器和门。 入口管道被构造成从辅助动力单元延伸到飞行器壳体，并且具有限定APU噪声传播通过的流动通道的侧壁。 致动器至少部分地设置在入口管道内。 门连接到执行机构。 致动器还构造成在至少第一位置之间选择性地旋转门，其中门的至少一部分在第一方向上偏转APU噪声和第二位置，其中门的至少一部分偏转 APU噪声在第二个方向。
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