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公开(公告)号：US07810312B2
公开(公告)日：2010-10-12
申请号：US11785590
申请日：2007-04-18
IPC分类号： F02K99/00
CPC分类号： F02C7/141 , F02K3/06 , F02K3/115 , Y02T50/671 , Y02T50/675
摘要： In certain circumstances recovery of a fluid flow presented through a heat exchanger into another flow can create problems with respect to drag and loss of thrust. In gas turbine engines heat exchangers are utilized for providing cooling of other flows such as in relation to compressor air taken from the core of the engine and utilized for cabin ventilation and de-icing functions. By providing an outlet valve through an outlet duct in a wall of a housing the exhaust fluid flow from the heat exchanger can be returned to the by-pass flow with reduced drag effects whilst recovering thrust. The valve may take the form of a flap displaceable into the by-pass flow before an exit plan to create a reduction in static pressure drawing fluid flow through the heat exchanger.
摘要翻译： 在某些情况下，通过热交换器呈现的流体流的回收可以产生关于推力的阻力和损失的问题。 在燃气涡轮发动机中，使用热交换器来提供其它流量的冷却，例如相对于从发动机的核心取得的压缩空气，并用于机舱通风和除冰功能。 通过在壳体的壁中通过出口管提供出口阀，来自热交换器的排出流体流可以在恢复推力的同时以减小的阻力效应返回至旁通流。 阀可以采取在出口计划之前可移动到旁通流中的挡板的形式，以产生静压力的降低，从而吸引流过热交换器的流体流。
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公开(公告)号：US20070245738A1
公开(公告)日：2007-10-25
申请号：US11785590
申请日：2007-04-18
IPC分类号： F02C1/00
CPC分类号： F02C7/141 , F02K3/06 , F02K3/115 , Y02T50/671 , Y02T50/675
摘要： In certain circumstances recovery of a fluid flow presented through a heat exchanger into another flow can create problems with respect to drag and loss of thrust. In gas turbine engines heat exchangers are utilized for providing cooling of other flows such as in relation to compressor air taken from the core of the engine and utilized for cabin ventilation and de-icing functions. By providing an outlet valve through an outlet duct in a wall of a housing the exhaust fluid flow from the heat exchanger can be returned to the by-pass flow with reduced drag effects whilst recovering thrust. The valve may take the form of a flap displaceable into the by-pass flow before an exit plan to create a reduction in static pressure drawing fluid flow through the heat exchanger.
摘要翻译： 在某些情况下，通过热交换器呈现的流体流的回收可以产生关于推力的阻力和损失的问题。 在燃气涡轮发动机中，使用热交换器来提供其它流量的冷却，例如相对于从发动机的核心取得的压缩空气，并用于机舱通风和除冰功能。 通过在壳体的壁中通过出口管提供出口阀，来自热交换器的排出流体流可以在恢复推力的同时以减小的阻力效应返回至旁通流。 阀可以采取在出口计划之前可移动到旁通流中的挡板的形式，以产生静压力的降低，从而吸引流过热交换器的流体流。
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公开(公告)号：US07698884B2
公开(公告)日：2010-04-20
申请号：US12222551
申请日：2008-08-12
申请人： Alan R. Maguire , David C. Butt , Martyn Richards , Geoffrey E. Kirk , David A. Edwards , Glenn A. Knight
发明人： Alan R. Maguire , David C. Butt , Martyn Richards , Geoffrey E. Kirk , David A. Edwards , Glenn A. Knight
摘要： A power transmission arrangement comprises a first power transmission member connectable to a first main shaft of an engine. The arrangement also includes a second power transmission member connectable to a second main shaft of the engine and to a third power transmission member. A coupling assembly is provided which has a selectable coupling condition to couple the first power transmission member to the second power transmission member to allow power to be transmitted from the third power transmission member to the first main shaft of the engine via the first power transmission member. The coupling assembly has a decoupling condition to decouple the first power transmission member from the second power transmission member to allow power to be transmitted from the main shaft of the engine to the third power transmission member via the second power transmission member.
摘要翻译： 动力传递装置包括可连接到发动机的第一主轴的第一动力传递构件。 该装置还包括可连接到发动机的第二主轴和第三动力传递构件的第二动力传递构件。 提供了一种联接组件，其具有可选择的联接状态，以将第一动力传递构件联接到第二动力传递构件，以允许动力经由第一动力传递构件从第三动力传递构件传递到发动机的第一主轴 。 联接组件具有去耦条件，以将第一动力传递构件与第二动力传递构件分离，以允许动力经由第二动力传递构件从发动机的主轴传递到第三动力传递构件。
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公开(公告)号：US20060196192A1
公开(公告)日：2006-09-07
申请号：US11353097
申请日：2006-02-14
申请人： Martyn Richards , Nicholas Howarth
发明人： Martyn Richards , Nicholas Howarth
IPC分类号： F02C6/08
CPC分类号： F02C7/32 , F02C9/18 , F05D2260/96 , F05D2270/051
摘要： A Turbine Engine and Method of Operating a Turbine Engine Disparities between optimum engine thrust for aircraft operation and power necessary to drive an ancillary machine such an electrical power generator can cause problems within a turbine engine. Clearly, it is necessary to continue developing sufficient electrical power for control and other systems within an aircraft despite aircraft thrust requirements. Previously, some compressed air flow has been bypassed in order to maintain compressor stability, but unfortunately such bypass systems within turbine engines can have a thrust recovery regime such that there is excess thrust in comparison with that actually necessary. In accordance with the present invention, a proportion of the compressed air flow is bled directly through a bleed path to an exhaust nozzle 104 of an engine such that the compressor core can continue to provide work to drive an ancillary machine whilst engine thrust is limited to that actually required, achieving a significant saving in terms of fuel consumption and wear and tear upon brakes, etc under low power operation.
摘要翻译： 涡轮发动机和涡轮发动机的操作方法飞机运行的最佳发动机推力与驱动辅助机械如发电机所需的动力之间的差异可能导致涡轮发动机内的问题。 显然，尽管有飞机的推力要求，仍然需要为飞机内的控制系统和其他系统继续开发足够的电力。 以前，为了保持压缩机的稳定性，已经绕过一些压缩空气流，但不幸的是，涡轮发动机内的这种旁路系统可以具有推力恢复状态，使得与实际需要相比存在过大的推力。 根据本发明，压缩空气流的一部分直接通过排放通道排放到发动机的排气喷嘴104，使得压缩机芯可以继续提供工作来驱动辅助机器，同时发动机推力被限制到 实际上需要的是，在低功率运行下，在燃油消耗和刹车等磨损方面实现了显着的节省。
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公开(公告)号：US08419351B2
公开(公告)日：2013-04-16
申请号：US12647896
申请日：2009-12-28
申请人： Martyn Richards
发明人： Martyn Richards
IPC分类号： F01D15/12
CPC分类号： F01D25/34 , F02C7/36 , F05D2260/80 , Y10T74/19535
摘要： A selective rotation arrangement for a shaft, the arrangement including a housing mountable spaced from the shaft and an engagement member with distal and proximal ends which is selectively movable relative to the housing towards or away from the shaft between an operating position towards the shaft and a rest position clear of the shaft, the engagement member having a gear member at the distal end thereof which is engageable with the shaft in the operating position to permit turning of the shaft by the engagement member, but is disengaged from the shaft in the rest position.
摘要翻译： 一种用于轴的选择性旋转装置，该装置包括可安装成与轴间隔开的壳体和具有远端和近端的接合构件，所述接合构件可相对于壳体朝向或远离轴在朝向轴的操作位置和 静止位置远离轴，接合构件具有在其远端处的齿轮构件，其在操作位置可与轴接合，以允许轴由接合构件转动，但在静止位置与轴脱离 。
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公开(公告)号：US20080302082A1
公开(公告)日：2008-12-11
申请号：US12222551
申请日：2008-08-12
申请人： Alan R. Maguire , David C. Butt , Martyn Richards , Geoffrey E. Kirk , David A. Edwards , Glenn A. Knight
发明人： Alan R. Maguire , David C. Butt , Martyn Richards , Geoffrey E. Kirk , David A. Edwards , Glenn A. Knight
IPC分类号： F02C3/10
摘要： A power transmission arrangement comprises a first power transmission member connectable to a first main shaft of an engine. The arrangement also includes a second power transmission member connectable to a second main shaft of the engine and to a third power transmission member. A coupling assembly is provided which has a selectable coupling condition to couple the first power transmission member to the second power transmission member to allow power to be transmitted from the third power transmission member to the first main shaft of the engine via the first power transmission member. The coupling assembly has a decoupling condition to decouple the first power transmission member from the second power transmission member to allow power to be transmitted from the main shaft of the engine to the third power transmission member via the second power transmission member.
摘要翻译： 动力传递装置包括可连接到发动机的第一主轴的第一动力传递构件。 该装置还包括可连接到发动机的第二主轴和第三动力传递构件的第二动力传递构件。 提供了一种联接组件，其具有可选择的联接状态，以将第一动力传递构件联接到第二动力传递构件，以允许动力经由第一动力传递构件从第三动力传递构件传递到发动机的第一主轴 。 联接组件具有去耦条件，以将第一动力传递构件与第二动力传递构件分离，以允许动力经由第二动力传递构件从发动机的主轴传递到第三动力传递构件。
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公开(公告)号：US20070199331A1
公开(公告)日：2007-08-30
申请号：US10939422
申请日：2004-09-14
申请人： Alan Maguire , David Butt , Martyn Richards , Geoffrey Kirk , David Edwards
发明人： Alan Maguire , David Butt , Martyn Richards , Geoffrey Kirk , David Edwards
IPC分类号： F02C7/20
摘要： A power transmission arrangement comprises a first power transmission member connectable to a first main shaft of an engine. The arrangement also includes a second power transmission member connectable to a second main shaft of the engine and to a third power transmission member. A coupling assembly is provided which has a selectable coupling condition to couple the first power transmission member to the second power transmission member to allow power to be transmitted from the third power transmission member to the first main shaft of the engine via the first power transmission member. The coupling assembly has a decoupling condition to decouple the first power transmission member from the second power transmission member to allow power to be transmitted from the main shaft of the engine to the third power transmission member via the second power transmission member.
摘要翻译： 动力传递装置包括可连接到发动机的第一主轴的第一动力传递构件。 该装置还包括可连接到发动机的第二主轴和第三动力传递构件的第二动力传递构件。 提供了一种联接组件，其具有可选择的联接状态，以将第一动力传递构件联接到第二动力传递构件，以允许动力经由第一动力传递构件从第三动力传递构件传递到发动机的第一主轴 。 联接组件具有去耦条件，以将第一动力传递构件与第二动力传递构件分离，以允许动力经由第二动力传递构件从发动机的主轴传递到第三动力传递构件。
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公开(公告)号：US5064025A
公开(公告)日：1991-11-12
申请号：US587101
申请日：1990-09-24
申请人： Martyn Richards
发明人： Martyn Richards
IPC分类号： F16H57/04
CPC分类号： F16H57/0427 , F16H57/0431 , F16H57/045 , F16H57/0495 , Y10T74/19995
摘要： In an accessory drive unit e.g. as used in a gas turbine engine, some of the gears in a gear train are provided with pockets 20 in which drainage oil is collected on engine shut down. On re-starting of the engine, the collected oil is acted upon by ribs 16 and is flung onto the teeth of the gears so as to provide immediate lubrication, rather than experience a delay until main lubricant supply pressure is increased. Friction and wear on start up is reduced.
摘要翻译： 在附件驱动单元例如 如在燃气涡轮发动机中使用的，齿轮系中的一些齿轮设置有凹穴20，排气油在发动机关闭时被收集。 在重新启动发动机时，收集的油被肋条16作用，并且被排出到齿轮的齿上，以便提供即时的润滑，而不是经历延迟，直到主润滑油供应压力增加。 启动时的摩擦和磨损减少。
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公开(公告)号：US07891163B2
公开(公告)日：2011-02-22
申请号：US11896703
申请日：2007-09-05
申请人： Martyn Richards
发明人： Martyn Richards
IPC分类号： F02G3/00
CPC分类号： F02C7/052
摘要： In prop fan and contra fan gas turbine engines particularly utilized with regard to pusher configurations towards the aft of an aircraft, there is a significant problem with regard to debris and bird strikes resulting in particulate matter which may damage the engine thrust core. By providing an inlet rotor which fragments and creates a centrifugal aspect to the inlet flow, particulate matter can be directed to a bypass chute normally in the form of an annular section extending into a number of chute exits. In such circumstances, the particulate matter is removed continuously from the inlet flow and the chutes are normally angled to project any particulate matter towards propellers of the engine at robust positions.
摘要翻译： 在特别用于朝向飞机后部的推进器构造方面使用的风扇和反风扇燃气涡轮发动机中，对于可能损坏发动机推力芯的颗粒物质的碎片和鸟撞击存在显着的问题。 通过提供一个入口转子，其将入口流分解并产生离心方面，颗粒物质可以被引导到通常以延伸到多个斜槽出口的环形部分的形式的旁通通道。 在这种情况下，颗粒物质从入口流中连续地被去除，并且滑槽通常是成角度的，以将任何颗粒物质推向发动机的坚固位置的螺旋桨。
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公开(公告)号：US5580217A
公开(公告)日：1996-12-03
申请号：US404152
申请日：1995-03-14
申请人： Martyn Richards , David S. Knott
发明人： Martyn Richards , David S. Knott
CPC分类号： F01D11/006 , F01D11/008 , Y02T50/672
摘要： A stage of fan blades in a ducted fan gas turbine engine have the spaces between them filled by a rotary annulus wall filler which has a leading portion made from metal and a trailing portion made from a composite material. The metal portion resists the impact damage from the ingress of foreign bodies and the trailing portion provides a lighter structure.
摘要翻译： 风扇式燃气涡轮发动机中的风扇叶片的阶段具有由旋转环形壁填料填充的空间，旋转环形壁填料具有由金属制成的引导部分和由复合材料制成的尾部。 金属部分抵抗异物侵入的冲击损伤，尾部提供较轻的结构。
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