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1. 发明授权

EP2256383B1 Face seal for gas turbine engine 有权转让
标题翻译：机械密封用于燃气涡轮发动机
公开(公告)号：EP2256383B1
公开(公告)日：2015-02-25
申请号：EP10251010.4
申请日：2010-05-26
申请人： United Technologies Corporation
发明人： Dobek, Louis J. , Shaffer, Harold K. , Sonokawa, Masayoshi , Story, Mark
IPC分类号： F16J15/34
CPC分类号： F16J15/3468 , F16J15/3404

2. 发明授权

EP1010926B1 Seal assembly for an intershaft seal in a gas turbine engine 有权
标题翻译：之间，用于燃气涡轮发动机的轴密封组件
公开(公告)号：EP1010926B1
公开(公告)日：2005-07-20
申请号：EP99309231.1
申请日：1999-11-19
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Sheridan, William G. , Shaffer, Harold K.
IPC分类号： F16J15/34
CPC分类号： F16J15/3484 , F01D11/003 , F02C7/28 , F16J15/3464 , F16J15/3472

3. 发明公开

EP2256383A3 Face seal for gas turbine engine 有权转让
标题翻译：机械密封用于燃气涡轮发动机
公开(公告)号：EP2256383A3
公开(公告)日：2013-04-03
申请号：EP10251010.4
申请日：2010-05-26
申请人： United Technologies Corporation
发明人： Dobek, Louis J. , Shaffer, Harold K. , Sonokawa, Masayoshi , Story, Mark
IPC分类号： F16J15/34
CPC分类号： F16J15/3468 , F16J15/3404
摘要： A face seal (50) for a gas turbine engine comprises a seal body (56) that has a contact face (68) to engage a rotating surface. The contact face (68) is defined as an area extending radially between an inner diameter (D1) of the seal body (56) and an outer diameter (D2) of the seal body (56) at one seal end providing a radial width (W). The radial width (W) is greater than 0.15 inch (3.81 mm).

4. 发明公开

EP2256383A2 Face seal for gas turbine engine 有权转让
标题翻译： GleitringdichtungfürGasturbinenmotor
公开(公告)号：EP2256383A2
公开(公告)日：2010-12-01
申请号：EP10251010.4
申请日：2010-05-26
申请人： United Technologies Corporation
发明人： Dobek, Louis J. , Shaffer, Harold K. , Sonokawa, Masayoshi , Story, Mark
IPC分类号： F16J15/34
CPC分类号： F16J15/3468 , F16J15/3404
摘要： A face seal (50) for a gas turbine engine comprises a seal body (56) that has a contact face (68) to engage a rotating surface. The contact face (68) is defined as an area extending radially between an inner diameter (D1) of the seal body (56) and an outer diameter (D2) of the seal body (56) at one seal end providing a radial width (W). The radial width (W) is greater than 0.15 inch (3.81 mm).
摘要翻译：用于燃气涡轮发动机的面密封件（50）包括具有接合面（68）以接合旋转表面的密封体（56）。接触面（68）被定义为在一个密封端处在密封体（56）的内径（D1）和密封体（56）的外径（D2）之间径向延伸的区域，提供径向宽度 W）。径向宽度（W）大于0.15英寸（3.81mm）。

5. 发明公开

EP2080940A1 Face seal for gas turbine engine 有权转让
标题翻译： GleitringdichtungfürGasturbinenmotor
公开(公告)号：EP2080940A1
公开(公告)日：2009-07-22
申请号：EP09250079.2
申请日：2009-01-14
申请人： United Technologies Corporation
发明人： Dobek, Louis J. , Shaffer, Harold K. , Story, Mark
IPC分类号： F16J15/34
CPC分类号： F16J15/3404 , F16J15/3468
摘要： A face seal (50) for a gas turbine engine (10) comprises a seal body (56) that has a contact face (52) to engage a rotating surface (42). The contact face (52) is defined as an area extending radially between an inner diameter (D1) of the seal body (56) and an outer diameter (D2) of the seal body (56) at one seal end (52). A ratio of the outer diameter (D2) to the inner diameter (D1) is at least 1.054.
摘要翻译：用于燃气涡轮发动机（10）的面密封件（50）包括具有接合面（52）以接合旋转表面（42）的密封体（56）。接触面（52）被定义为在一个密封端（52）处在密封体（56）的内径（D1）和密封体（56）的外径（D2）之间径向延伸的区域。外径（D2）与内径（D1）之比至少为1.054。

6. 发明公开

EP1010926A3 Seal assembly for an intershaft seal in a gas turbine engine 有权
标题翻译：之间，用于燃气涡轮发动机的轴密封组件
公开(公告)号：EP1010926A3
公开(公告)日：2002-07-03
申请号：EP99309231.1
申请日：1999-11-19
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Sheridan, William G. , Shaffer, Harold K.
IPC分类号： F16J15/34
CPC分类号： F16J15/3484 , F01D11/003 , F02C7/28 , F16J15/3464 , F16J15/3472
摘要： A seal assembly 134 for use in an intershaft seal includes a first seal 136 that seals to a seal plate on an inner rotor shaft 40, a second seal 138 that seals to a seal plate on an outer rotor shaft 42, and an intermediate seal that is supported by a stator assembly 36 and seals to the first seal 134 and the second seal 136. The intermediate seal may include a seal segment 200 affixed to the stator assembly, a ring seal between the seal segment 200 and the first seal 136, and a ring seal between the seal segment 200 and the second seal 138. An intershaft seal with this seal assembly has less flex than a prior art intershaft seal and thereby results in greater durability and less seal wear.

7. 发明授权

EP2080940B1 Face seal for gas turbine engine 有权转让
标题翻译：机械密封用于燃气涡轮发动机
公开(公告)号：EP2080940B1
公开(公告)日：2012-10-17
申请号：EP09250079.2
申请日：2009-01-14
申请人： United Technologies Corporation
发明人： Dobek, Louis J. , Shaffer, Harold K. , Story, Mark
IPC分类号： F16J15/34
CPC分类号： F16J15/3404 , F16J15/3468

8. 发明公开

EP1010926A2 Seal assembly for an intershaft seal in a gas turbine engine 有权
标题翻译： Zwischenwellen-Dichtungsanordnungfürein Gasturbinentriebwerk
公开(公告)号：EP1010926A2
公开(公告)日：2000-06-21
申请号：EP99309231.1
申请日：1999-11-19
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Sheridan, William G. , Shaffer, Harold K.
IPC分类号： F16J15/34
CPC分类号： F16J15/3484 , F01D11/003 , F02C7/28 , F16J15/3464 , F16J15/3472
摘要： A seal assembly 134 for use in an intershaft seal includes a first seal 136 that seals to a seal plate on an inner rotor shaft 40, a second seal 138 that seals to a seal plate on an outer rotor shaft 42, and an intermediate seal that is supported by a stator assembly 36 and seals to the first seal 134 and the second seal 136. The intermediate seal may include a seal segment 200 affixed to the stator assembly, a ring seal between the seal segment 200 and the first seal 136, and a ring seal between the seal segment 200 and the second seal 138. An intershaft seal with this seal assembly has less flex than a prior art intershaft seal and thereby results in greater durability and less seal wear.
摘要翻译：用于轴间密封件的密封组件134包括密封在内转子轴40上的密封板的第一密封件136，密封到外转子轴42上的密封板的第二密封件138和中间密封件由定子组件36支撑并且密封到第一密封件134和第二密封件136.中间密封件可以包括固定到定子组件的密封段200，密封段200和第一密封件136之间的环形密封件，以及在密封段200和第二密封件138之间的环形密封。与该密封组件的轴间密封件比现有技术的轴向间密封件具有更小的挠曲，从而导致更大的耐用性和更小的密封磨损。

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