公开(公告)号：US5890874A

公开(公告)日：1999-04-06

申请号：US780619

申请日：1997-01-07

申请人： David M Lambert ,  David S Knott ,  Peter R Beckford

发明人： David M Lambert ,  David S Knott ,  Peter R Beckford

IPC分类号： F01D11/00 ,  F04D29/38

CPC分类号： F01D11/008

摘要： A rotor for a ducted fan gas turbine engine includes a rotor disc on which a number of circumferentially spaced apart blades are mounted. Wall members are positioned to bridge the space between adjacent blades. The wall members correspond in profile with the blades adjacent thereto. A seal is mounted on a side face of each wall member and is bonded to a flexible mounting which is bonded itself to the wall member. The flexible mounting has elastic properties so as to allow the seal to deflect relative to the wall member under centrifugal loading during operation.

摘要翻译： 用于管道式风扇燃气涡轮发动机的转子包括其上安装有多个周向间隔开的叶片的转子盘。 壁构件定位成桥接相邻叶片之间的空间。 壁构件与与其相邻的叶片的轮廓对应。 密封件安装在每个壁构件的侧面上并且结合到柔性安装件，该柔性安装件本身粘合到壁构件。 柔性安装件具有弹性特性，以便在操作期间允许密封件在离心负载下相对于壁构件偏转。

公开(公告)号：US6155788A

公开(公告)日：2000-12-05

申请号：US334940

申请日：1999-06-17

申请人： Peter R Beckford ,  David R Midgelow ,  David S Knott

发明人： Peter R Beckford ,  David R Midgelow ,  David S Knott

IPC分类号： F01D5/30

CPC分类号： F01D5/303 ,  F01D5/3007

摘要： A fan rotor assembly (30) for a gas turbine engine (10) comprises a fan rotor (32) and a plurality of radially extending fan blades (34). Each fan blade (34) has a root (64) which is retained in a corresponding groove (54) in the periphery of the hub (54) of the fan rotor (32). Each fan blade root (64) comprises four axially spaced root portions (66, 68, 70 and 72) which locate in a corresponding number of axially spaced groove portions (56, 58, 60 and 62). The flanks (94, 98) of two of the root portions (66, 70) are arranged at an angle to the axis of the fan rotor (32) and the flanks (96, 100) of the other two root portions (68, 72) are arranged at an angle in the opposite sense. The flanks (74, 76, 78 and 80) of the groove portions (56, 58, 60 and 62) are arranged at the same angle as the flanks (94, 96, 98 and 100) of the corresponding root portions (66, 68, 70 and 72). The arrangement provides improved retention of the fan blades (34) and reduces the weight of the fan blades (34) and fan rotor (32).

摘要翻译： 一种用于燃气涡轮发动机（10）的风扇转子组件（30）包括风扇转子（32）和多个径向延伸的风扇叶片（34）。 每个风扇叶片（34）具有根部（64），其保持在风扇转子（32）的轮毂（54）的周边中的对应的凹槽（54）中。 每个风扇叶片根部（64）包括四个轴向间隔开的根部（66,68,70和72），其位于相应数量的轴向隔开的槽部分（56,58,60和62）中。 两个根部（66,70）两侧的侧面（94,98）与风扇转子（32）的轴线成一定角度，另外两个根部（68，70）的侧面（96,100） 72）以相反的意义上的角度排列。 槽部分（56,58,60和62）的侧面（74,76,78和80）以与相应根部（66,68和60）的侧面（94,96,98和100）相同的角度布置， 68,70和72）。 该装置提供了风扇叶片（34）的改进的保持并且减小了风扇叶片（34）和风扇转子（32）的重量。

公开(公告)号：US08424280B2

公开(公告)日：2013-04-23

申请号：US12379594

申请日：2009-02-25

申请人： Gareth E Moore ,  David R Trainer ,  David P Scothern ,  David S Knott ,  Paul Simms

发明人： Gareth E Moore ,  David R Trainer ,  David P Scothern ,  David S Knott ,  Paul Simms

IPC分类号： F02C6/00

CPC分类号： F02C7/32 ,  F05D2220/50 ,  F05D2260/40311 ,  Y02T50/671

摘要： A gas turbine engine arrangement comprises a first gas turbine engine, a second gas turbine engine, a differential gearbox and an electrical generator. The differential gearbox has a first input drive, a second input drive and an output drive. The output drive of the differential gearbox is arranged to drive the electrical generator via an external, accessory, gearbox. The external, accessory, gearbox drives other accessories. The first gas turbine is arranged to drive the first input drive of the differential gearbox and the second gas turbine engine is arranged to drive the second input drive of the differential gearbox. The electrical generator and accessories are driven at a constant frequency speed/frequency.

摘要翻译： 燃气涡轮发动机装置包括第一燃气涡轮发动机，第二燃气涡轮发动机，差速齿轮箱和发电机。 差速齿轮箱具有第一输入驱动器，第二输入驱动器和输出驱动器。 差速齿轮箱的输出驱动器被布置成经由外部附件齿轮箱来驱动发电机。 外部，附件，齿轮箱驱动其他配件。 第一燃气轮机被布置成驱动差速齿轮箱的第一输入驱动器，并且第二燃气涡轮发动机被布置成驱动差动齿轮箱的第二输入驱动器。 发电机和附件以恒定的频率/频率进行驱动。

公开(公告)号：US06575694B1

公开(公告)日：2003-06-10

申请号：US09924104

申请日：2001-08-08

申请人： Ewan F Thompson ,  Ian G Martindale ,  David S Knott ,  Kenneth F Udall ,  David Geary ,  Julian M Reed ,  Sivasubramaniam K Sathianathan

发明人： Ewan F Thompson ,  Ian G Martindale ,  David S Knott ,  Kenneth F Udall ,  David Geary ,  Julian M Reed ,  Sivasubramaniam K Sathianathan

IPC分类号： F01D2100

CPC分类号： F01D21/045 ,  F05D2250/15 ,  F05D2250/25 ,  F05D2250/61 ,  Y02T50/671

摘要： A turbofan gas turbine engine (10) comprises a fan rotor (32) carrying a plurality of radially extending fan blades (34). A fan blade containment assembly (38) surrounds the fan blades (34) and the fan blade containment assembly (34) comprises a generally annular, or frustoconical, cross-section casing (52). At least one corrugated sheet metal ring surrounds the casing (52) wherein the corrugations extend with axial and/or circumferential components.

摘要翻译： 涡轮风扇燃气涡轮发动机（10）包括承载多个径向延伸的风扇叶片（34）的风扇转子（32）。 风扇叶片容纳组件（38）围绕风扇叶片（34）并且风扇叶片容纳组件（34）包括大致环形或截头圆锥形的横截面壳体（52）。 至少一个波纹板金属环围绕壳体（52），其中波纹随轴向和/或周向部分延伸。

公开(公告)号：US07533526B2

公开(公告)日：2009-05-19

申请号：US11396553

申请日：2006-04-04

申请人： Alan R Maguire ,  David S Knott

发明人： Alan R Maguire ,  David S Knott

IPC分类号： F16D33/02 ,  F16D57/04

CPC分类号： F01D17/26 ,  F01D5/026 ,  F02C3/107 ,  F02C3/113 ,  F02C7/36 ,  F02K3/06 ,  F05D2260/406 ,  F16D33/04 ,  Y10T74/19033

摘要： A drive arrangement for driving, or for being driven by, a fluid is disclosed. The drive arrangement comprises a rotatable member (40) for receiving the fluid, and having mounted thereon a plurality of drive members (56). The drive members (56) are movable between a drive position, in which the drive members can drive, or be driven by, the fluid, and a non-drive position in which the drive members (56) are substantially prevented from driving or being driven by a fluid received in the rotatable member (40).

摘要翻译： 公开了用于驱动或由流体驱动的驱动装置。 驱动装置包括用于接收流体的可旋转构件（40），并且其上安装有多个驱动构件（56）。 驱动构件（56）可以在驱动构件可以驱动的驱动位置或由驱动驱动的驱动位置和驱动构件（56）基本上不被驱动的驱动位置 由容纳在可旋转构件（40）中的流体驱动。

公开(公告)号：US06220602B1

公开(公告)日：2001-04-24

申请号：US09289542

申请日：1999-04-12

申请人： John R Webster ,  David S Knott

发明人： John R Webster ,  David S Knott

IPC分类号： F16J1543

CPC分类号： F16J15/3288 ,  F16J15/445

摘要： A seal arrangement (40) between relatively movable components (42,48) includes at least one magnet (54) on a first component (48) and at least one magnet (56) on the second component (42). A clearance (55) is defined between the at least one magnet (54) on the first component (48) and the at least one magnet (56) on the second component (42). Springs (58) bias the at least one magnet (54) on the first component (48) and the at least one magnet (56) on the second component (42) towards each other. The at least one magnet (54) on the first component (42) and the at least one magnet (56) on the second component (42) are arranged to repel each other against the spring (58) to control the clearance (55).

摘要翻译： 相对可移动部件（42,48）之间的密封装置（40）包括在第一部件（48）上的至少一个磁体（54）和第二部件（42）上的至少一个磁体（56）。 间隙（55）限定在第一部件（48）上的至少一个磁体（54）和第二部件（42）上的至少一个磁体（56）之间。 弹簧（58）将第一部件（48）上的至少一个磁体（54）和第二部件（42）上的至少一个磁体（56）朝向彼此偏置。 第一部件（42）上的至少一个磁体（54）和第二部件（42）上的至少一个磁体（56）被布置成抵抗弹簧（58）相互排斥以控制间隙（55） 。

公开(公告)号：US06860721B2

公开(公告)日：2005-03-01

申请号：US10262971

申请日：2002-10-03

申请人： David S Knott ,  Michael R Lawson

发明人： David S Knott ,  Michael R Lawson

IPC分类号： F01D5/30 ,  F04D29/32

CPC分类号： F01D5/3007 ,  F01D5/30 ,  F04D29/322

摘要： An indentor for contacting a bearing surface, the indentor comprising a contact surface complimentary to that of the bearing surface, wherein the indentor comprises an integral tapering portion which tapering portion defines part of the contact surface, the tapering portion at its distal edge defining an edge of contact between the contact surface and the bearing surface.

摘要翻译： 用于接触支承表面的压头，所述压头包括与所述支承表面互补的接触表面，其中所述压头包括整体锥形部分，所述锥形部分限定所述接触表面的一部分，所述锥形部分在其远侧边缘处限定边缘 接触表面和支承表面之间的接触。

公开(公告)号：US06669447B2

公开(公告)日：2003-12-30

申请号：US10020315

申请日：2001-12-18

申请人： Jennifer M Norris ,  David S Knott ,  Adrian M Jones ,  David R Midgelow ,  Robert M Hall

发明人： Jennifer M Norris ,  David S Knott ,  Adrian M Jones ,  David R Midgelow ,  Robert M Hall

IPC分类号： F01D510

CPC分类号： F01D5/16 ,  F01D5/147 ,  F01D5/18 ,  Y10S416/50 ,  Y10T29/49339

摘要： A gas turbine engine fan blade (26) comprises a root portion (40) and an aerofoil portion (42). The aerofoil portion (42) has a leading edge (44), a trailing edge (46), a concave metal wall portion (50) extending from the leading edge (44) to the trailing edge (46) and a convex metal wall portion (52) extending from the leading edge (44) to the trailing edge (46). The aerofoil portion (42) has a hollow interior (54) and the interior (54) of the aerofoil portion (42) is at least partially filled with a vibration damping material (56). The vibration damping material (56) comprises a material having viscoelasticity for example one formed by mixing an amine terminated polymer and bisphenol a-epichlorohydrin epoxy resin.

公开(公告)号：US08915058B2

公开(公告)日：2014-12-23

申请号：US13067484

申请日：2011-06-03

申请人： David S Knott ,  Alexis Lambourne ,  Andrew M Rolt ,  Cosimo Buffone

发明人： David S Knott ,  Alexis Lambourne ,  Andrew M Rolt ,  Cosimo Buffone

IPC分类号： F28F13/14 ,  F02C7/047 ,  F01D5/18

CPC分类号： F01D5/18 ,  B64D15/00 ,  F01D25/02 ,  F02C7/047 ,  F05D2220/325 ,  Y02T50/67 ,  Y02T50/672 ,  Y02T50/673 ,  Y02T50/676 ,  Y10T29/49353

摘要： A heat transfer arrangement for a fluid-washed body having first and second ends and a fluid-washed surface extending there-between. The arrangement includes a heat transfer member extending from the first end at least part way along the body towards the second end. A heat source is arranged in use to heat the heat transfer member in the vicinity of the first end of the body. A plurality of thermal control layers are provided on the heat transfer member, each of the layers having a different thermal conductivity and being juxtaposed so as to create a thermal conductivity profile which varies along the length of the member. The arrangement may be used for prevention of icing of an aerofoil body such as a blade, vane or the like.

摘要翻译： 用于具有第一和第二端部的流体冲洗体和在其之间延伸的流体冲洗表面的热传递装置。 该装置包括从第一端至少部分地沿主体朝向第二端延伸的传热构件。 热源设置在使用中以加热身体第一端附近的传热构件。 多个热控制层设置在传热构件上，每个层具有不同的导热性并且并置，以便产生沿构件的长度变化的热导率分布。 该装置可以用于防止诸如叶片，叶片等的翼面体的结冰。

公开(公告)号：US07364118B2

公开(公告)日：2008-04-29

申请号：US10847853

申请日：2004-05-19

申请人： David S Knott ,  Christopher Freeman

发明人： David S Knott ,  Christopher Freeman

IPC分类号： B64D27/18 ,  B64D33/04

CPC分类号： B64C21/025 ,  B64C2230/04 ,  B64D27/02 ,  Y02T50/166 ,  Y02T50/44 ,  Y02T50/55

摘要： In order to achieve greater operational efficiency a propulsive arrangement is provided in which a relatively large number of small propulsive assemblies 9; 31, 32, 33 are provided in aircraft structures in particular the wing 7; 30. The assemblies 9; 31, 32, 33 comprise a flow path within which a compressor 39, 43, 47 is positioned to propel an air flow for propulsion. The compressors 39, 43, 47 are powered by electricity from an electricity generator 8 and possibly supplemented by solar cells or fuel cells or wing tip turbine generators 11. The assemblies 9, 31, 32, 33 are small to allow easy removal for maintenance and repair.

摘要翻译： 为了实现更高的操作效率，提供了一种推进装置，其中相对大量的小推进组件9; 31,32,33设置在飞行器结构中，特别是机翼7; 30。 组件9; 31,32,33包括流动路径，压缩机39,43,47定位在该流动路径中，以推动用于推进的空气流。 压缩机39,43,47由来自发电机8的电力供电，并且可能由太阳能电池或燃料电池或翼尖涡轮发电机11补充。 组件9,31,32,33很小，以便容易地进行维护和维修。