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17 条记录 (耗时 0.052 秒)

    DEVICE OF AN AIRCRAFT ENGINE FOR SEPARATING OIL FROM AN AIR-OIL VOLUME FLOW
    1.
    发明申请
    DEVICE OF AN AIRCRAFT ENGINE FOR SEPARATING OIL FROM AN AIR-OIL VOLUME FLOW 有权
    用于从空气流量分离油的飞机发动机的装置

    公开(公告)号：US20150321130A1

    公开(公告)日：2015-11-12

    申请号：US14692122

    申请日：2015-04-21

    申请人： Rolls-Royce Deutschland Ltd &Co KG

    发明人： Juergen BEIER ,  Gideon VENTER

    IPC分类号： B01D45/16 ,  F02C7/32 ,  F01M11/03

    CPC分类号： B01D47/06 ,  B01D45/12 ,  B01D47/027 ,  B01D2247/101 ,  F01D25/18 ,  F02C7/06 ,  Y02T50/671

    摘要： A device of an aircraft engine for separating oil from an air-oil volume flow and an apparatus for introducing oil into the air-oil volume flow. An outlet area of the apparatus for introducing oil is provided in a closed line section, into which the air-oil volume flow can be introduced via an inlet area. In accordance with the invention, a flow cross-section of the line section downstream of the outlet area of the apparatus tapers at least partially like a nozzle and at least in some sections inside a confusor area.

    摘要翻译： 用于将油与空气 - 油体积流分离的飞机发动机的装置和用于将油引入空气 - 油体积流的装置。 用于引入油的装置的出口区域设置在封闭的管线部分中，空气 - 油体积流可以通过入口区域被引入该区域。 根据本发明，设备出口区域下游的管线部分的流动横截面至少部分地类似于喷嘴，并且至少在混乱区域内的一些部分中逐渐变细。

    AERO ENGINE WITH A BEARING CHAMBER AND AN APPLIANCE FOR INTRODUCING OIL
    3.
    发明申请
    AERO ENGINE WITH A BEARING CHAMBER AND AN APPLIANCE FOR INTRODUCING OIL 审中-公开
    具有轴承座的AERO发动机和用于介绍油的器具

    公开(公告)号：US20160076449A1

    公开(公告)日：2016-03-17

    申请号：US14847500

    申请日：2015-09-08

    申请人： Rolls-Royce Deutschland Ltd & Co KG

    发明人： Juergen BEIER

    IPC分类号： F02C7/06 ,  F02C3/04

    CPC分类号： F02C7/06 ,  F01D25/18 ,  F02C3/04 ,  F05D2250/14 ,  F05D2250/232 ,  F05D2260/98 ,  F16C33/6659 ,  F16C2360/23

    摘要： What is proposed is an aero engine (1) with a bearing chamber (12), which is confined by a first wall area (32) and a second wall area (33) which is embodied so as to be rotatable with respect to the first wall area (32) and in which at least one bearing appliance as well as at least one appliance (38, 39, 40) for introducing oil are arranged. Oil can be introduced into the bearing chamber (12) via at least one appliance (38, 39, 40) for introducing oil substantially against a rotational direction of the first wall area (32) and/or of the second wall area (33) and substantially tangentially to at least one surface (43) of at least one wall area (32, 33) that is facing the bearing chamber (12).

    摘要翻译： 所提出的是具有轴承室（12）的航空发动机（1），所述轴承室（12）由第一壁区域（32）和第二壁区域（33）限定，所述第一壁区域和第二壁区域被构造成可相对于第一壁区域 壁区域（32），并且其中布置有用于引入油的至少一个轴承装置以及至少一个装置（38,39,40）。 油可以经由至少一个用于将油基本上抵靠第一壁区域（32）和/或第二壁区域（33）的旋转方向引入的装置（38,39,40）引入到轴承室（12） 并且基本切向地相对于面向轴承腔（12）的至少一个壁区域（32,33）的至少一个表面（43）。

    JET ENGINE COMPRISING A DEVICE FOR SPRAYING OIL
    4.
    发明申请
    JET ENGINE COMPRISING A DEVICE FOR SPRAYING OIL 有权
    喷射喷射装置喷射油的喷射发动机

    公开(公告)号：US20150135663A1

    公开(公告)日：2015-05-21

    申请号：US14532819

    申请日：2014-11-04

    申请人： Rolls-Royce Deutschland Ltd. & Co., KG

    发明人： Juergen BEIER ,  Gideon VENTER

    IPC分类号： F01D25/18 ,  B01D45/14

    CPC分类号： F01D25/18 ,  B01D45/14 ,  B01D47/06 ,  F02C3/30 ,  F02C7/06 ,  F05D2210/13 ,  F05D2260/609 ,  F05D2260/98

    摘要： The present invention describes a jet engine with a device for spraying oil into an air-oil volume flow guided inside a flow cross-section limited by a wall area. The air-oil volume flow is guidable through an oil separator in order to separate the oil. In accordance with the invention, the oil can be sprayed into the air-oil volume flow in the area of the device via an outlet area rigidly connected to the wall area.

    摘要翻译： 本发明描述了一种喷射发动机，其具有将油喷射到由壁面限制的流动横截面内引导的空气 - 油体积流中的装置。 空气 - 油体积流量可通过油分离器引导，以分离油。 根据本发明，油可以经由刚刚连接到壁区域的出口区域喷射到装置区域中的空气 - 油体积流中。

    OIL TANK
    5.
    发明申请
    OIL TANK 审中-公开

    公开(公告)号：US20170267411A1

    公开(公告)日：2017-09-21

    申请号：US15457040

    申请日：2017-03-13

    申请人： Rolls-Royce Deutschland Ltd & Co KG

    发明人： Juergen BEIER ,  Andrew PATERSON

    IPC分类号： B65D25/56 ,  F02C7/06 ,  G02B27/02 ,  F02C3/04

    CPC分类号： B65D25/56 ,  F02C3/04 ,  F02C7/06 ,  F05D2220/323 ,  F16N19/003 ,  G01F23/02 ,  G02B27/025

    摘要： An oil tank includes an outer wall with a side limitation and an interior enclosed by the outer wall. A view passage extending from the side limitation into the interior of the tank allows external visual reading of the oil fill level of the tank at or close to the tank center, where changes in the oil fill level caused by inclined positions of the tank are minimal. The view passage includes a beginning of the passage formed in the area of the side limitation that includes a first optically transparent window. An end of the passage includes a second optically transparent window. A passage wall extending between the beginning and end of the passage delimits the view passage against the interior of the tank.

    TANK DEVICE OF AN AERO ENGINE WITH AN APPLIANCE FOR INTRODUCING OIL
    8.
    发明申请
    TANK DEVICE OF AN AERO ENGINE WITH AN APPLIANCE FOR INTRODUCING OIL 有权
    用于引进油的AERO发动机的油箱装置

    公开(公告)号：US20160076399A1

    公开(公告)日：2016-03-17

    申请号：US14847553

    申请日：2015-09-08

    申请人： Rolls-Royce Deutschland Ltd & Co KG

    发明人： Juergen BEIER ,  Gideon VENTER

    IPC分类号： F01D25/18 ,  F01D25/12

    CPC分类号： F01D25/18 ,  F01D25/12 ,  F01D25/20 ,  F01M2013/0427 ,  F02C7/06 ,  F02C7/32 ,  F05D2260/20 ,  F05D2260/609 ,  F05D2260/98 ,  F16N19/00

    摘要： A tank device of an aero engine, which has an inlet appliance for the supply of an air-oil volume flow into a tank space of the tank device, a separation appliance for the separation of oil from the air-oil volume flow that is supplied to the tank space, a conduit area which is confined by at least one wall and in which an air-oil volume flow can be guided in the area of the tank space at least in certain areas, and an outlet appliance, in the area of which a volume flow can be discharged via a valve appliance from the tank space of the tank device. At least one appliance for introducing oil is provided, by means of which oil can be supplied into the area of the conduit area substantially against a flow direction of the air-oil volume flow which is forming during operation in the conduit area.

    摘要翻译： 一种航空发动机的储罐装置，其具有用于向罐装置的罐空间供应空气 - 油体积流的入口装置，用于将油与供给的空气 - 油体积流分离的分离装置 至少一个区域内的至少一个壁限制的导管区域，至少在某些区域可以在罐空间的区域中引导空气 - 油体积流量的管道区域和出口设备 其可以通过阀装置从罐装置的罐空间排出体积流量。 提供至少一种用于引入油的器具，通过该器具可以将油可以基本上抵抗在管道区域中操作期间形成的空气 - 油体积流的流动方向而被供应到管道区域的区域中。

    JET ENGINE DEVICE WITH AT LEAST ONE COMPONENT THAT IS ARRANGED IN A CASING AND THAT IS ROTATABLE TO THE CASING
    9.
    发明申请
    JET ENGINE DEVICE WITH AT LEAST ONE COMPONENT THAT IS ARRANGED IN A CASING AND THAT IS ROTATABLE TO THE CASING 审中-公开
    喷气发动机装置至少有一个组件安装在壳体上，并且可旋转到壳体

    公开(公告)号：US20150176447A1

    公开(公告)日：2015-06-25

    申请号：US14570423

    申请日：2014-12-15

    申请人： Rolls-Royce Deutschland Ltd & Co KG

    发明人： Juergen BEIER

    IPC分类号： F01M13/04 ,  F02C7/32

    CPC分类号： F01M13/04 ,  B01D45/12 ,  F01D25/18 ,  F01M2013/0422 ,  F02C7/06 ,  F02C7/32 ,  F16N7/32

    摘要： The present invention describes a device of a jet engine with at least one component arranged in a casing and designed rotatable relative to said casing. At least one air-oil volume flow can be passed out of an area of the jet engine into the casing. In accordance with the invention the air-oil volume flow can be introduced into the casing via an introducing facility at least approximately tangentially to an area of the rotatable component close to at least an outer circumferential area.

    摘要翻译： 本发明描述了一种喷气发动机的装置，其具有布置在壳体中并且相对于所述壳体可旋转的至少一个部件。 至少一个空气 - 油体积流量可以从喷气发动机的区域流出到壳体中。 根据本发明，空气 - 油体积流动可以经由导入设备至少大致切向地相对于可旋转部件的接近至少外周区域的区域被引入到壳体中。