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1. 发明公开

EP3436666A1 RADIAL TURBOMACHINE WITH AXIAL THRUST COMPENSATION 有权
公开(公告)号：EP3436666A1
公开(公告)日：2019-02-06
申请号：EP17722154.6
申请日：2017-03-29
申请人： Exergy S.p.A.
发明人： SPADACINI, Claudio , RIZZI, Dario
IPC分类号： F01D1/06 , F01D3/00 , F01D5/04
CPC分类号： F01D5/048 , F01D1/06 , F01D3/00 , F01D3/02 , F01D5/041 , F01D11/001
摘要： The present invention relates to a radial turbomachine with axial thrust compensation, comprising: a fixed casing (3); a plurality of main concentric bladed rings (9′,9″,9′″,9″″) arranged in the fixed casing (3) around a central axis (X-X); a plurality of concentric auxiliary bladed rings (15′, 15″, 15′″) arranged in the fixed casing (3) around the central axis (X-X) and radially alternated with the main bladed rings (9′,9″,9′″,9″″). A rotor (2, 2′) comprising a rotor disc (6, 6′) and a rotation shaft (4, 4′, 4″) integral with the rotor disc (6, 6′) is rotatable in the fixed casing (3) around the central axis (X-X) and carries, on a front face (7, 7′), the main bladed rings (9′,9″,9′″,9″″). The main (9′,9″,9′″,9″″) and auxiliary (15′, 15″, 15′″) bladed rings delimit, with the rotor disc (6, 6′), a plurality of concentric front main chambers (30, 33, 35, 36) at different pressures. A plurality of concentric rear annular main chambers (41′,41″,41′″,41″″), each in fluid communication with a respective front main chamber (30, 33, 35, 36) and at the same pressure as the respective front main chamber (30, 33, 35, 36), is delimited between a rear face (8, 8′) of the rotor disc (6, 6′) and the fixed casing (3). A rear annular area (A_1p, A_2p, A_3p, A_4p, A′_4p) of the rotor disc (6, 6′) delimiting one of the rear annular main chambers (41′,41″,41′″,41″″) is equal to or substantially equal to a front area (A_1f, A_2f, A_3f, A_4f) of the rotor disc (6, 6′) delimiting a respective front main chamber (30, 33, 35, 36), so that the force exerted by the pressure of the working fluid in each rear annular main chamber (41′,41″,41′″,41″″) substantially balances the force exerted by the pressure of the working fluid in the respective front main chamber (30, 33, 35, 36).

2. 发明公开

EP2807345A4 THRUST BALANCE SYSTEM FOR GAS TURBINE ENGINE 有权转让
标题翻译：推力补偿系统的燃气涡轮发动机
公开(公告)号：EP2807345A4
公开(公告)日：2015-11-04
申请号：EP13796982
申请日：2013-01-16
申请人： UNITED TECHNOLOGIES CORP
发明人： GLAHN JORN A , ACKERMANN WILLIAM K , STRIPINIS PHILIP S , SCHMITZ JOHN T , CRAWLEY JR CLIFTON J
IPC分类号： F01D17/08 , F01D3/00 , F01D11/02 , F16J15/44
CPC分类号： F01D11/001 , F01D3/00 , F01D11/025 , F05D2260/38 , F16J15/442
摘要： A gas turbine engine has a thrust balance chamber defined between a static housing and a rotating component. The thrust balance chamber is sealed by a first non-contact seal at a radially inner location and a second non-contact seal at a radially outer location.

3. 发明公开

EP2884047A1 Compressor or turbine with back-disk seal and vent 有权转让
标题翻译： Kompressor oder Turbine mit Back-Disk-Dichtung undEntlüftung
公开(公告)号：EP2884047A1
公开(公告)日：2015-06-17
申请号：EP14193937.1
申请日：2014-11-19
申请人： Honeywell International Inc.
发明人： Reyenga, James W. , Thompson, Glenn F. , Guidry, Mike
IPC分类号： F01D3/04 , F01D11/02 , F04D29/051 , F04D29/16
CPC分类号： F01D3/00 , F01D3/04 , F01D11/02 , F04D17/10 , F04D29/0413 , F04D29/0516 , F04D29/2266 , F04D29/284
摘要： A turbine or compressor wheel mounted in a housing. The wheel is carried on two radial bearings(151, 153) both mounted in a wall of the housing. The wall has a venting orifice (131) that is not impeded by moving parts such as bearings. The wall also has a circular seal member (141) extending toward a back-disk of the wheel with only a very small clearance. The seal member is composed of a material significantly softer than the material of the wheel.
摘要翻译：安装在壳体中的涡轮或压缩机叶轮。车轮承载两个安装在外壳壁上的径向轴承（151,153）。壁具有通气孔（131），其不会通过移动诸如轴承的部件而受阻。壁还具有圆形密封构件（141），其仅具有非常小的间隙朝向车轮的后盘延伸。密封构件由比轮的材料显着柔软的材料构成。

4. 发明公开

EP2611993A4 EDDY CURRENT DAMPER AND METHOD 审中-公开
标题翻译：涡流阻尼器及其方法
公开(公告)号：EP2611993A4
公开(公告)日：2015-01-14
申请号：EP11822293
申请日：2011-07-30
申请人： DRESSER RAND CO
发明人： MAIER MARTIN D
IPC分类号： F16C32/04 , F01D3/00 , F01D3/04 , F01D25/16 , F16C39/02 , F16C39/06
CPC分类号： F01D3/00 , F01D25/16 , F05D2240/511 , F05D2240/515 , F16C32/0442 , F16C39/02 , F16C39/06

5. 发明授权

EP1219777B1 Methods and apparatus for controlling bearing loads 有权
标题翻译： Methode und Einrichtung zur Beeinflussung von Lagerbelastungen
公开(公告)号：EP1219777B1
公开(公告)日：2007-04-04
申请号：EP01310621.6
申请日：2001-12-19
申请人： GENERAL ELECTRIC COMPANY
发明人： Przytulski, James Charles , Willey, James Elbert , Haaser, Frederic Gardner , Ceccopieri, Fernando , Handelsman, Steven Keith
IPC分类号： F01D3/04 , F01D25/16 , G05D7/01 , F16K3/00
CPC分类号： F04D27/0207 , F01D3/00 , F01D9/065 , F01D17/105 , F01D25/16 , F04D29/0516 , F05D2270/11

6. 发明公开

EP1541803A2 Anordnung zur Lagerentlastung in einer Gasturbine 有权
标题翻译： Gurburbine，umfassend eine Anordnung zur Lagerentlastung
公开(公告)号：EP1541803A2
公开(公告)日：2005-06-15
申请号：EP04090471.6
申请日：2004-11-29
申请人： Rolls-Royce Deutschland Ltd & Co KG
发明人： Friedl, Winfried-Hagen, Dipl.-Ing.
IPC分类号： F01D3/00 , F01D5/08
CPC分类号： F01D3/04 , F01D3/00 , F01D5/082 , F05D2220/321 , F05D2220/323 , F05D2240/56 , Y02T50/676
摘要： Zur kontrollierten Lagerlastreduzierung in einer Gasturbine wird die Verdichterlast abgesenkt und die Turbinenlast erhöht, indem an der Hochdruckwelle (2) am Verdichter (1) eine gegen die Verdichterluft abgeschirmte Niedrigdruckkammer (8) und an der Turbine eine mit Verdichterluft versorgte Hochdruckkammer (9) gebildet ist. Die jeweiligen Drücke sind in bestimmten Grenzen einstellbar. Aufgrund der kontrollierten Lagerlastminderung können hohe Drehzahlen eine lange Lebensdauer der Lager erreicht werden.
摘要翻译：飞机燃气轮机发电厂具有降低压缩机负载并增加涡轮机载荷的气体密封装置。电动机具有压缩机（1）级高压轴（2），压缩空气与低压室（8）和高空气压力室（9）密封。相应的压力可在给定范围内调节。

7. 发明公开

EP1509688A1 HIGH EFFICIENCY GAS TURBINE POWER GENERATOR SYSTEMS 审中-公开
标题翻译：高性能燃机发电系统
公开(公告)号：EP1509688A1
公开(公告)日：2005-03-02
申请号：EP03726652.5
申请日：2003-05-07
申请人： PAUL, Marius A.
发明人： PAUL, Marius A.
IPC分类号： F02C3/067
CPC分类号： F02C3/05 , F01D1/28 , F01D3/00 , F01D13/02 , F01D15/10 , F02C3/067 , F02C3/30 , F02C5/02 , H02K7/1823
摘要： A gas turbine power generator with ultra high efficiency, the generator being an assembly of electric motor-generator machines (171, 172, 173) and turbine configurations (110, 140) used in combination with combustor systems (180) for operation of select integrated turbine configurations.

8. 发明公开

EP0657623A1 Anti-contamination thrust balancing system for gas turbine engines 失效
标题翻译： Kontaminationsfreies SchubausgleichsystemfürGasturbine。
公开(公告)号：EP0657623A1
公开(公告)日：1995-06-14
申请号：EP94309045.6
申请日：1994-12-06
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Mize, Christopher D , Pirsig, William W. , Vercellone, Peter T.
IPC分类号： F01D5/08
CPC分类号： F01D5/081 , F01D3/00 , F05D2260/607 , Y02T50/672 , Y02T50/676
摘要： A buffer zone (56) disposed between the TOBI discharge cavity (50) and the forward rotor cavity (42) of a gas turbine engine serves to maintain the TOBI air relatively pollutant free by judiciously controlling the flow to maintain the pressure of the buffer cavity (56) below the adjacent cavities. The buffer cavity air and the forward rotor cavity air are bled to the dead rim area (90) of the turbine rotor disk (44) through tangentially oriented discharge ports (88) formed in the circumferentially spaced plenums (80) formed in the stator support. Plates (82) on the bottom of some of the plenums (80) block off the flow from the forward rotor cavity (42) and buffer air from the buffer cavity (56) flows through these closed off plenums (80) through openings (84) to maintain the proper pressure relationship amongst the cavities.
摘要翻译：设置在TOBI（切向车载喷射器）排出腔和燃气涡轮发动机的前转子腔之间的缓冲区用于通过明智地控制流量来保持TOBI空气相对无污染物的空气，以将缓冲腔的压力维持在相邻的腔。缓冲腔空气和前转子空腔空气通过形成在形成在定子支撑件中的周向隔开的通气室中的切向定向的排出口而被排放到涡轮转子盘的死角区域。一些增压室底部的板阻挡了从前转子空腔的流动，并且来自缓冲空腔的缓冲空气流过这些关闭的通风室，以保持空腔之间适当的压力关系。

9. 发明授权

EP0128850B1 Thrust balancing and cooling system 失效
标题翻译：平衡与冷却系统
公开(公告)号：EP0128850B1
公开(公告)日：1988-12-07
申请号：EP84630069.7
申请日：1984-04-27
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Brodell, Robert F. , Laurello, Vincent P.
IPC分类号： F02C7/28 , F01D3/00 , F01D11/00 , F01D25/12 , F01D25/16 , F04D29/04
CPC分类号： F02C7/28 , F01D3/00 , F01D25/125 , F01D25/16 , Y02T50/675

10. 发明授权

EP3712376B1 ROTOR SYSTEM AND CONTROL METHOD THEREFOR, GAS TURBINE GENERATOR SET AND CONTROL METHOD THEREFOR 有权
公开(公告)号：EP3712376B1
公开(公告)日：2024-05-29
申请号：EP18899593.0
申请日：2018-08-31
IPC分类号： F01D5/02 , F01D3/00 , F01D3/04 , F01D25/16
CPC分类号： F01D5/02 , F02C6/00 , F02C7/06 , F02C9/00 , F01D25/16 , F01D3/00 , F01D3/04 , F05D2240/5120130101 , F05D2240/5220130101 , F05D2240/5320130101 , F05D2240/5420130101

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