公开(公告)号：EP3272905B1

公开(公告)日：2018-09-26

申请号：EP16776412.5

申请日：2016-03-24

申请人： Aisin Seiki Kabushiki Kaisha ,  Akros Co., Ltd.

发明人： TAGUCHI, Yosuke ,  MATSUMOTO, Akikazu ,  HIRATSUKA, Ichiro ,  KATO, Masaki ,  KOBAYASHI, Daishi ,  SUGISAWA, Megumi ,  NIIMI, Takuya ,  IKAI, Yusuke ,  SAAI, Kazuki ,  MIZUNO, Shun

IPC分类号： F02F3/12 ,  C25D11/04 ,  C23C18/12 ,  F02K1/82 ,  C23C28/00 ,  B32B15/01

CPC分类号： F02F3/14 ,  B32B9/041 ,  B32B15/017 ,  C23C18/1212 ,  C23C18/1216 ,  C23C18/122 ,  C23C18/127 ,  C23C20/08 ,  C23C28/04 ,  C23C28/321 ,  C23C28/324 ,  C23C28/34 ,  C25D11/022 ,  C25D11/08 ,  C25D11/10 ,  C25D11/246 ,  F01D25/145 ,  F02F1/243 ,  F02F3/12 ,  F02K1/822 ,  F05D2220/40 ,  F05D2230/90 ,  F05D2300/20 ,  F05D2300/44 ,  F05D2300/502 ,  F05D2300/603 ,  F16J1/01

摘要： This vehicle mechanical component includes a mechanical component body, a heat insulating layer formed on the mechanical component body, and a protective layer formed on the heat insulating layer and including an inorganic compound that includes an alkoxide and scale-like inorganic solid particles dispersed in the inorganic compound.

公开(公告)号：EP3004555B1

公开(公告)日：2017-10-18

申请号：EP14731757.2

申请日：2014-05-28

申请人： SNECMA

发明人： FRIBOURG, Guillaume ,  DELALEAU, Pierre ,  TELLIER, Florian

IPC分类号： F01D5/14 ,  B23P11/02 ,  B23P15/04 ,  F16B4/00

CPC分类号： F01D9/041 ,  B23P11/025 ,  B23P15/04 ,  F01D5/147 ,  F05D2230/60 ,  F05D2240/12 ,  F05D2300/43 ,  F05D2300/502 ,  F16B4/008

公开(公告)号：EP3099912A1

公开(公告)日：2016-12-07

申请号：EP15742745.1

申请日：2015-01-05

申请人： United Technologies Corporation

发明人： COOK, III Grant O. ,  TWELVES, Wendell V.

IPC分类号： F02C7/20 ,  F02C7/24 ,  F01D25/24

CPC分类号： F01D5/288 ,  F01D5/147 ,  F01D5/282 ,  F01D5/284 ,  F04D19/00 ,  F05D2220/32 ,  F05D2240/30 ,  F05D2300/10 ,  F05D2300/20 ,  F05D2300/502 ,  F05D2300/611 ,  F05D2300/615 ,  Y02T50/672

摘要： A component for a gas turbine engine comprises an underlying substrate. A plurality of ceramic panels have intermediate thermal expansion joints bonded by a bond layer to the underlying substrate. The thermal expansion joints are formed of a material having a greater coefficient of expansion than a material forming the ceramic panels. The ceramic panels and the thermal expansion joints are positioned to define an outer surface for the component. A gas turbine engine and a component for a gas turbine engine are also disclosed.

摘要翻译： 用于燃气涡轮发动机的部件包括下面的基板。 多个陶瓷板具有通过接合层与下面的基底结合的中间热膨胀接头。 热膨胀接头由具有比形成陶瓷板的材料更大的膨胀系数的材料形成。 陶瓷面板和热膨胀接头被定位成限定组件的外表面。 还公开了一种燃气涡轮发动机和用于燃气涡轮发动机的部件。

公开(公告)号：EP3004555A1

公开(公告)日：2016-04-13

申请号：EP14731757.2

申请日：2014-05-28

申请人： SNECMA

发明人： FRIBOURG, Guillaume ,  DELALEAU, Pierre ,  TELLIER, Florian

IPC分类号： F01D5/14 ,  B23P11/02 ,  B23P15/04 ,  F16B4/00

CPC分类号： F01D9/041 ,  B23P11/025 ,  B23P15/04 ,  F01D5/147 ,  F05D2230/60 ,  F05D2240/12 ,  F05D2300/43 ,  F05D2300/502 ,  F16B4/008

摘要： A hollow vane, consisting of a main portion (1), of which the cavity (4) is closed by a cover (5), is produced by expanding the main portion (1) relative to the cover (5), for example by means of differential thermal expansion, then by placing the cover (5) at the bottom (11) of the opening (8) of the cavity (4), before allowing the main portion (1) to close again, closing a nesting between a protrusion (6) at the bottom of the cover (5) and a widening (10) at the bottom of the opening (8). This avoids disadvantages relating to the use of welding, glue or indeed assembly parts.

摘要翻译： 中空叶片包括主要部分，其中空腔被盖封闭，其通过例如通过差别热膨胀使主体部分相对于盖膨胀而产生，然后通过将盖放置在 在允许主要部分再次闭合之前，使空腔的开口闭合，从而封闭盖的底部的突起与开口底部的加宽之间的嵌套。 与使用焊接，胶水或甚至组装部件相关的缺点也是如此避免。

公开(公告)号：EP2932052A1

公开(公告)日：2015-10-21

申请号：EP13862300.4

申请日：2013-12-10

申请人： United Technologies Corporation

发明人： COSTA, Mark W. ,  ROBERTSON, Thomas J. ,  LUSSIER, Darin S.

IPC分类号： F01D25/24 ,  F02C7/00

CPC分类号： F01D21/045 ,  F05D2300/121 ,  F05D2300/431 ,  F05D2300/501 ,  F05D2300/502 ,  Y02T50/672

摘要： A fan section of a gas turbine engine includes a fan containment case assembly includes an outer case of an aluminum alloy. The outer case extends circumferentially around an axial centerline. A thermally conforming liner assembly is located inwardly of the outer case. The thermally conforming liner assembly includes a circumferential liner of an aluminum alloy. A ballistic liner is located between the outer case and the thermally conforming liner assembly.

公开(公告)号：EP2890826A1

公开(公告)日：2015-07-08

申请号：EP13747613.1

申请日：2013-08-01

申请人： General Electric Company

发明人： ROSENZWEIG, Larry, Steven ,  RUUD, James, Anthony ,  SIVARAMAKRISHNAN, Shankar

IPC分类号： C23C4/00 ,  C23C4/02 ,  C23C4/12 ,  C23C4/18

CPC分类号： F01D5/288 ,  C23C4/00 ,  C23C4/02 ,  C23C4/10 ,  C23C4/12 ,  C23C4/134 ,  C23C4/18 ,  F01D9/02 ,  F05D2220/32 ,  F05D2230/312 ,  F05D2240/35 ,  F05D2300/21 ,  F05D2300/502 ,  Y10T428/24355 ,  Y10T428/31

摘要： A coating comprising a first surface and a second surface is provided. The coating includes a plurality of growth domains. An orientation of at least one growth domain of the plurality of growth domains is non-vertical with respect to the first surface of the coating. One or more growth domains of the plurality of growth domains comprise a plurality of at least partially melted and solidified particles.

摘要翻译： 提供一种涂布基板表面的方法。 该方法包括提供悬浮液或前体，其包含悬浮在液体介质中的原料。 此外，该方法包括以与表面切线小于约75度的喷射角度将悬浮液或前体喷涂到表面上。

公开(公告)号：EP2722509A1

公开(公告)日：2014-04-23

申请号：EP13188184.9

申请日：2013-10-10

申请人： General Electric Company

发明人： Giri, Sheo Narain ,  Jha, Sanjeev ,  Pemmi, Bhaskar ,  Bommanakatte, Harish ,  Donkada, Santhosh ,  Gumpina, Krishna Kishore ,  Saha, Rajarshi

IPC分类号： F02C6/08 ,  F01D5/08

CPC分类号： F01D17/10 ,  F01D5/08 ,  F01D5/082 ,  F01D17/105 ,  F01D25/08 ,  F01D25/12 ,  F01D25/14 ,  F02C3/04 ,  F02C6/08 ,  F02C7/12 ,  F02C7/141 ,  F02C7/18 ,  F02C9/18 ,  F04D29/522 ,  F04D29/582 ,  F05D2220/32 ,  F05D2240/35 ,  F05D2260/20 ,  F05D2300/173 ,  F05D2300/502 ,  F05D2300/504 ,  F05D2300/505

摘要： A cooling arrangement for a gas turbine engine. The cooling arrangement comprises a discharge channel (30) for air flow from a compressor, a first cooling channel (44) and at least one aperture (40) providing communication between the flow of air through the discharge channel (30) and the first cooling channel (44). A restrictor device (42) in the aperture (40) regulates the flow of air between the discharge channel (30) and the first cooling channel (44). The restrictor device (42) deforms to vary air flowing through the aperture (40) in response to a physical condition of the engine. This physical condition of the engine may be that of the temperature of air flowing through the discharge channel, the restrictor device (42) responding to regulate the flow of air based on that temperature. The restrictor device (42) may be a two-way shape memory alloy.

摘要翻译： 一种用于燃气涡轮发动机的冷却装置。 冷却装置包括用于从压缩机流动的排放通道（30），第一冷却通道（44）和至少一个孔（40），其提供通过排出通道（30）的空气流与第一冷却 通道（44）。 孔（40）中的限流装置（42）调节排放通道（30）和第一冷却通道（44）之间的空气流。 限制器装置（42）响应于发动机的物理状态变形以改变流过孔（40）的空气。 发动机的这种物理状态可以是流过排放通道的空气的温度，限制装置（42）响应于基于该温度调节空气流量。 限流装置（42）可以是双向形状记忆合金。

公开(公告)号：EP1752638B1

公开(公告)日：2013-11-27

申请号：EP06253616.4

申请日：2006-07-11

申请人： Rolls-Royce plc

发明人： Rowe, Arthur Laurence ,  Brook, Anthony John

IPC分类号： F02C9/28

CPC分类号： F02C9/28 ,  F05D2270/303 ,  F05D2300/502

公开(公告)号：EP2388354B1

公开(公告)日：2013-09-11

申请号：EP11250422.0

申请日：2011-04-04

申请人： United Technologies Corporation

发明人： Gero, Peter F. ,  Schlichting, Kevin W. ,  Neal, James W.

IPC分类号： C23C4/10 ,  C23C30/00 ,  F01D5/28 ,  C23C14/02 ,  C23C14/22

CPC分类号： F01D25/08 ,  C23C4/11 ,  C23C14/027 ,  C23C14/228 ,  C23C30/00 ,  F01D5/288 ,  F05D2230/90 ,  F05D2260/95 ,  F05D2300/502 ,  F05D2300/611 ,  Y10T428/12021 ,  Y10T428/12458 ,  Y10T428/1259 ,  Y10T428/12618 ,  Y10T428/12736 ,  Y10T428/12743 ,  Y10T428/26 ,  Y10T428/266

摘要： A multilayer coating (100) includes a bond coat layer (102) and a first barrier layer (104) applied on the bond coat layer. The first barrier layer (104) has a compositional gradient comprising a majority of a first rare earth stabilized zirconia material proximate the bond coat layer (102) to a majority of a second rare earth stabilized zirconia material away from the bond coat layer. The first and second rare earth stabilized zirconia materials are different.

公开(公告)号：EP1752638A3

公开(公告)日：2012-11-14

申请号：EP06253616.4

申请日：2006-07-11

申请人： Rolls-Royce plc

发明人： Rowe, Arthur Laurence ,  Brook, Anthony John

IPC分类号： F02C9/28

CPC分类号： F02C9/28 ,  F05D2270/303 ,  F05D2300/502

摘要： It is known that overshoot in fuel flow rate as a result of compensating for engine heat soak effects can create transient over values in desired thrust parameters. By adjusting the normally calculated fuel flow rate to a fuel regulator (22) by the introduction of a fuel flow adjustment dependent upon a variable which is related to heat soak effects it is possible to reduce the extent of overshoot as well as the transient time period of that overshoot to ongoing operational state. The variable used may be direct or indirect and will generally utilise a temperature sensor (25) within the engine and/or other engine control procedures which may be extrapolated from such sensor values to provide a variable for heat soak compensation.