公开(公告)号：US07849668B2

公开(公告)日：2010-12-14

申请号：US11552750

申请日：2006-10-25

Applicant: William G. Sheridan

Inventor： William G. Sheridan

IPC: F02C7/06

CPC classification number: F01D25/20 ,  F01D15/10 ,  F01D15/12 ,  F01D21/006 ,  F02C7/32 ,  F05D2220/76 ,  F05D2260/40311 ,  F05D2270/09

Abstract: A journal bearing provides lubrication to planetary gears during windmilling operation of a fan section. A primary oil pump provides oil from an oil supply during driven operation of the fan and a secondary oil pump driven by a generator provides oil during windmilling operation of the fan. The generator acts as a dynamic brake when the aircraft is grounded to prevent windmilling. A switch selects between the primary and secondary oil pump and controls the brake application.

Abstract translation: 轴承轴承在风扇部分的风车操作期间为行星齿轮提供润滑。 主油泵在风扇的驱动运行期间从供油中提供油，并且由发电机驱动的辅助油泵在风扇的风车运转期间提供油。 当飞机接地时，发电机作为动态制动器，以防止风车。 开关选择主油泵和辅助油泵之间，并控制制动器的应用。

公开(公告)号：US20090126336A1

公开(公告)日：2009-05-21

申请号：US12126648

申请日：2008-05-23

Applicant: Jacques Rene Bart ,  Didier Rene Andre Escure ,  Claude Marcel Mons ,  Stephane Rousselin

Inventor： Jacques Rene Bart ,  Didier Rene Andre Escure ,  Claude Marcel Mons ,  Stephane Rousselin

IPC: F01D21/14

CPC classification number: F01D21/006 ,  F05D2230/90 ,  F05D2260/902 ,  F05D2300/21 ,  F05D2300/2102 ,  F05D2300/2118 ,  F05D2300/44 ,  F05D2300/601 ,  F05D2300/603 ,  F05D2300/611 ,  F05D2300/614

Abstract: The present invention relates to a device for, in a gas turbine engine, braking a turbine comprising a rotor driving a shaft capable of rotating with respect to a stator in the event of said shaft breaking. The device is one which comprises a first braking member (110) provided with at least one abrasive element (110A) and a second braking member (120) comprising a ring-shaped element (120A) made of a material capable of being eroded by the abrasive element (110A), the two braking members being secured one of them to the rotor and the other to the stator and coming into contact with one another through axial displacement of the rotor once the shaft has broken, the abrasive element (110A) of the first braking member (110) eroding the ring-shaped element (120A) of the second braking member (120).

Abstract translation: 本发明涉及一种用于在燃气涡轮发动机中制动涡轮的装置，该涡轮机包括在所述轴断裂的情况下驱动能够相对于定子旋转的轴的转子。 该装置包括设置有至少一个研磨元件（110A）的第一制动构件（110）和包括由能够被所述第一制动元件（110A）侵蚀的材料制成的材料制成的环形元件（120A））的第二制动构件 研磨元件（110A），两个制动构件将其中一个固定到转子并且另一个固定到定子并且一旦轴已经断裂就通过转子的轴向位移而彼此接触，研磨元件（110A） 第一制动构件（110）侵蚀第二制动构件（120）的环形元件（120A）。

公开(公告)号：US20080101917A1

公开(公告)日：2008-05-01

申请号：US11877037

申请日：2007-10-23

Applicant: Jacques Rene BART ,  Didier Rene Andre Escure ,  Stephane Rousselin

Inventor： Jacques Rene BART ,  Didier Rene Andre Escure ,  Stephane Rousselin

IPC: F01D21/02

CPC classification number: F01D21/02 ,  F01D21/006 ,  F04D27/0292 ,  F05D2270/021 ,  F05D2270/042 ,  F05D2270/304 ,  F05D2270/62

Abstract: A device (40) for limiting overspeed in a turbomachine in the event of breakage of the turbine shaft (24), comprising means (38, 44) of propelling a pin (42) into the path of the blades (22), these propelling means being controlled by means (36) that detect overspeed or that the turbine shaft has broken.

Abstract translation: 一种用于在涡轮轴（24）断裂的情况下限制涡轮机超速的装置（40），包括将销（42）推进到叶片（22）的路径中的装置（38,44），这些推进 意味着通过检测超速或涡轮轴已经断裂的装置（36）来控制。

公开(公告)号：US07225607B2

公开(公告)日：2007-06-05

申请号：US10927600

申请日：2004-08-27

Applicant: Ronald Trumper ,  Stephen Arthur Anderson ,  Kevin Allan Dooley ,  Joseph Horace Brand

Inventor： Ronald Trumper ,  Stephen Arthur Anderson ,  Kevin Allan Dooley ,  Joseph Horace Brand

IPC: F02C3/00 ,  F02C7/32

CPC classification number: F01D21/006 ,  F05D2220/50 ,  F05D2260/402 ,  Y10T477/644

Abstract: A device is provided which can serve one or more of the multiple functions of impeding rotation of a shaft de-coupled turbine rotor, selectively impeding rotation of a first spool of the engine, for example to permit a second spool to generate power for use in ground operation, and facilitating reduced aircraft ground speed.

Abstract translation: 提供了一种装置，其可以服务于阻止轴脱耦合的涡轮转子的旋转的多个功能中的一个或多个，选择性地阻碍发动机的第一卷轴的旋转，例如以允许第二卷轴产生用于 地面操作，并有助于降低飞机地面速度。

公开(公告)号：US07160159B2

公开(公告)日：2007-01-09

申请号：US11282711

申请日：2005-11-21

Applicant: John R Webster

Inventor： John R Webster

IPC: B63H21/22

CPC classification number: F01D21/006 ,  B63H11/08

Abstract: A drive apparatus (10) for propelling a vehicle across a body of water is described. The apparatus (10) comprises a prime mover, for example a gas turbine engine (12), and a propelling arrangement (26) driven by the prime mover for propelling the vehicle across the body of water and thereby provide a reaction force on the prime mover. The apparatus (10) also includes a braking arrangement (42) to apply a braking force to the propelling arrangement (26).

Abstract translation: 描述了用于将车辆推过水体的驱动装置（10）。 设备（10）包括原动机，例如燃气涡轮发动机（12）和由原动机驱动的推进装置（26），用于推动车辆穿过水体，从而在主体上提供反作用力 移动者 装置（10）还包括制动装置（42），用于向推进装置（26）施加制动力。

公开(公告)号：US20060257247A1

公开(公告)日：2006-11-16

申请号：US11130375

申请日：2005-05-16

Applicant: William Seidel ,  David Chapman

Inventor： William Seidel ,  David Chapman

IPC: F01D15/12

CPC classification number: F01D21/006 ,  F02K7/10

Abstract: A brake system for a ram air turbine (RAT) causes the RAT to slow or lock if the RAT achieves an over-speed condition with a centrifugal force operated trigger system that actuates a compression type brake pack to slow or lock the turbine hub

Abstract translation: 用于冲压式空气涡轮机（RAT）的制动系统使得如果RAT利用驱动压缩式制动器组件的离心力操作的触发系统达到超速状态来减慢或锁定RAT，以减慢或锁定涡轮机轮毂

公开(公告)号：US06883331B2

公开(公告)日：2005-04-26

申请号：US10605531

申请日：2003-10-06

Applicant: Bertil Jönsson ,  Lars Sundin

Inventor： Bertil Jönsson ,  Lars Sundin

IPC: F01D15/02 ,  F01D21/00 ,  F02C3/10 ,  F02C6/00 ,  F02C6/20 ,  F02C7/08 ,  F02C7/36 ,  F02C9/18 ,  F02C9/22 ,  F02C9/28 ,  F02C6/08

CPC classification number: F02C9/18 ,  F01D21/006 ,  F02C6/20

Abstract: Method and arrangement for providing a gas turbine (1) having a first compressor (2), a combustion chamber (16) and a first turbine (11), the turbine being adapted to drive the compressor via a first shaft (10a, 10b). The gas turbine also has a bleed valve (12) arranged upstream of the first turbine for conducting part of a gas compressed by the compressor past it during engine braking. The invention also relates to a method for engine-braking a gas turbine.

Abstract translation: 用于提供具有第一压缩机（2），燃烧室（16）和第一涡轮机（11）的燃气轮机（1）的方法和装置，所述涡轮机适于经由第一轴（10a， b）。 燃气轮机还具有布置在第一涡轮机上游的排放阀（12），用于在发动机制动期间使由压缩机压缩的气体的一部分进行通过。 本发明还涉及一种用于发动机制动燃气轮机的方法。

公开(公告)号：US5261233A

公开(公告)日：1993-11-16

申请号：US871049

申请日：1992-04-20

Applicant: Katsunobu Kishi

Inventor： Katsunobu Kishi

IPC: B24B23/02 ,  B24B55/00 ,  B25F5/00 ,  F01D1/32 ,  F01D15/06 ,  F01D21/00 ,  F15B11/08 ,  F03B13/04

CPC classification number: F01D1/32 ,  B24B23/026 ,  B24B55/00 ,  B25F5/001 ,  F01D15/06 ,  F01D15/062 ,  F01D21/006 ,  F05D2260/902 ,  Y10S415/904

Abstract: In an open state of a valve, when a valve outside sleeve is rotated in the rear portion of a housing, a valve inner sleeve is moved forward to close a fluid channel, thus stopping supply of compressed driving air. Simultaneously, a front end of the valve outside sleeve is moved forward while it abuts against the rear surface of a retainer. Therefore, brake rods biased by compression coil springs are also moved forward, and front surfaces of the brake rods are abutted against a brake disk to effect braking, thereby immediately stopping rotation of a rotor. The urging force applied on the brake disk is the compression force of the compression coil springs.

Abstract translation: 在阀的打开状态下，当阀外套筒在壳体的后部旋转时，阀内套筒向前移动以关闭流体通道，从而停止供应压缩的驱动空气。 同时，阀外套筒的前端向前移动，同时它抵靠保持器的后表面。 因此，由压缩螺旋弹簧偏压的制动杆也向前移动，并且制动杆的前表面与制动盘抵接以进行制动，从而立即停止转子的旋转。 施加在制动盘上的施加力是压缩螺旋弹簧的压缩力。

公开(公告)号：US5029439A

公开(公告)日：1991-07-09

申请号：US447407

申请日：1989-12-07

Applicant: Yves R. J. Berneuil ,  Gilles L. E. Delrieu

Inventor： Yves R. J. Berneuil ,  Gilles L. E. Delrieu

IPC: F01D21/00 ,  F01D21/04

CPC classification number: F01D21/045 ,  F01D21/006 ,  F05D2220/327 ,  Y02T50/672

Abstract: A gas turbine engine is provided with a braking device for stopping the compressor drive turbine if a common shaft interconnecting the turbine and compressor rotors breaks, the braking device including a conical ring carried by the turbine rotor at its downstream end and a structural member of a generally conical shape carried by the upstream end of the turbine exhaust casing such that the ring will frictionally interlock with the structural member if the shaft breaks.

Abstract translation: 燃气涡轮发动机设有制动装置，用于在连接涡轮机和压缩机转子的公共轴断开时停止压缩机驱动涡轮，该制动装置包括在其下游端由涡轮转子承载的锥形环和 通常由涡轮排气壳体的上游端承载的圆锥形状，使得如果轴断裂，环将与结构构件摩擦地互锁。

公开(公告)号：US4122668A

公开(公告)日：1978-10-31

申请号：US822568

申请日：1977-08-08

Applicant: Cheng-Chien Chou ,  Theodore L. Rosebrock

Inventor： Cheng-Chien Chou ,  Theodore L. Rosebrock

IPC: F01D21/00 ,  F02C6/06 ,  F02C6/20 ,  F04D27/02 ,  F02C7/02

CPC classification number: F04D27/0253 ,  F01D21/006 ,  F02C6/06 ,  F02C6/20

Abstract: A gas turbine engine of the two shaft free turbine type has a first gasifier turbine for driving a compressor to supply air to a combustor for combustion with fuel to produce motive fluid for driving the compressor turbine and a second free wheeling power turbine. An air brake with a compressor impeller directly coupled to the power turbine has an inlet and an exhaust and a close coupled iris throttle assembly for regulating the inlet flow of air into the compressor to obtain maximized power turn down ratios without aerodynamic instability.

Abstract translation: 两轴无级涡轮机类型的燃气涡轮发动机具有第一气化器涡轮机，用于驱动压缩机以向燃烧器供应空气以燃烧燃料，以产生用于驱动压缩机涡轮机的驱动流体和第二自由轮式动力涡轮机。 具有直接联接到动力涡轮机的压缩机叶轮的空气制动器具有入口和排气以及紧耦合的虹膜节流装置，用于调节进入压缩机的空气的入口流量，以获得最大化的功率调节比，而没有气动不稳定性。