公开(公告)号：US09540829B2

公开(公告)日：2017-01-10

申请号：US14335100

申请日：2014-07-18

Applicant: ALSTOM Technology Ltd

Inventor： Gaurav Pathak ,  Christopher Michael Robson

IPC: E04G3/24 ,  B66F3/35 ,  F01D25/28 ,  F02C7/00

CPC classification number: E04G3/24 ,  B66F3/35 ,  E04G3/246 ,  F01D25/285 ,  F02C7/00 ,  F05D2230/68 ,  F05D2230/72

Abstract: The maintenance assembly, for workers to perform maintenance activities within a gas turbine engine, is capable of being arranged within a cavity, generally around a combustor, accessible from a manhole of the gas turbine engine. The maintenance assembly includes a platform, and an inflatable member cooperatively configured to the platform. The inflatable member is at a normal condition, when placed outside of the cavity, being at a deflated position and is at a working condition, when arranged within the cavity, being at inflated position so as to accommodate a shape coordinating the cavity in such a manner that the platform is advance within the cavity up to a predetermined level to enable the workers on the platform to reach at a predetermined position within the cavity to perform the maintenance activities.

Abstract translation: 用于工人在燃气涡轮发动机内执行维护活动的维护组件能够被布置在可从燃气涡轮发动机的人孔接近的大致围绕燃烧器的空腔内。 维护组件包括平台和协作地配置到平台的可充气构件。 充气构件处于正常状态时，当放置在空腔外部时处于放气位置并且处于工作状态，当布置在空腔内时处于充气位置，以便容纳在这样的空间中协调空腔的形状 使得平台在腔内前进到预定水平，使得平台上的工人能够到达腔内的预定位置以执行维护活动。

公开(公告)号：US20150098792A1

公开(公告)日：2015-04-09

申请号：US14496856

申请日：2014-09-25

Applicant: ALSTOM Technology Ltd

Inventor： Klaus DOEBBELING ,  Christopher Michael Robson ,  Massimo Giusti

IPC: F01D21/14 ,  F02C9/48 ,  F01D21/00

CPC classification number: F01D21/14 ,  F01D19/00 ,  F01D21/00 ,  F01D21/003 ,  F01D21/006 ,  F01D21/02 ,  F02C9/48 ,  F05B2260/85 ,  F05B2260/90 ,  F05B2270/304

Abstract: The present invention relates to a method of decelerating a turbine rotor of a turbine engine. At least one electric motor is engaged with the turbine rotor. A braking system, preferably the starting system, is engaged with the at least one electric motor, preferably the generator of the turbine engine, so as to use the at least one electric motor to apply a negative (braking) torque on the turbine rotor. The method includes after flame off, the braking system being used for dissipating kinetic energy available in the turbine engine after flame off by means of the at least one electric motor.

Abstract translation: 本发明涉及一种减速涡轮发动机的涡轮转子的方法。 至少一个电动机与涡轮机转子接合。 优选地，起动系统的制动系统与至少一个电动机（优选地是涡轮发动机的发电机）接合，以便使用至少一个电动机来对涡轮转子施加负（制动）转矩。 该方法包括在火焰熄灭之后，制动系统用于通过至少一个电动机消除涡轮发动机可用的动能。