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公开(公告)号:US09051849B2
公开(公告)日:2015-06-09
申请号:US13371525
申请日:2012-02-13
申请人: Mark David Ring , Jonathan J. Earl
发明人: Mark David Ring , Jonathan J. Earl
CPC分类号: F01D25/246 , F01D9/042 , F05D2240/12 , F05D2240/80 , F05D2260/30 , Y02T50/673
摘要: A stator assembly for a turbofan gas turbine engine is disclosed. The stator assembly is coupled to a shroud of the engine. The stator assembly includes an endless case fixedly coupled to the engine shroud. The case includes a forward portion, an aft portion and a central portion disposed therebetween. The case extends about an axis of the engine. The forward and aft portions of the case include rails that extend towards each other and form forward and aft pockets with the central portion respectfully. The stator assembly also includes a locking stator segment. The locking stator segment includes a shroud that includes a forward hook and a pair of aft hooks with a platform disposed therebetween. The forward and aft hooks are retained in the forward and aft pockets of the case respectfully.
摘要翻译: 公开了一种用于涡轮风扇燃气涡轮发动机的定子组件。 定子组件联接到发动机的护罩上。 定子组件包括固定地连接到发动机罩的环形壳体。 壳体包括前部,后部和设置在其间的中心部。 壳体围绕发动机的轴线延伸。 壳体的前部和后部包括彼此相对延伸的轨道,并且相对地形成具有中心部分的前后袋。 定子组件还包括锁定定子段。 锁定定子段包括护罩,其包括前钩和一对后钩,其间具有平台。 前后钩被保留在箱子的前后袋中。
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公开(公告)号:US20130209248A1
公开(公告)日:2013-08-15
申请号:US13371525
申请日:2012-02-13
申请人: Mark David Ring , Jonathan J. Earl
发明人: Mark David Ring , Jonathan J. Earl
CPC分类号: F01D25/246 , F01D9/042 , F05D2240/12 , F05D2240/80 , F05D2260/30 , Y02T50/673
摘要: A stator assembly for a turbofan gas turbine engine is disclosed. The stator assembly is coupled to a shroud of the engine. The stator assembly includes an endless case fixedly coupled to the engine shroud. The case includes a forward portion, an aft portion and a central portion disposed therebetween. The case extends about an axis of the engine. The forward and aft portions of the case include rails that extend towards each other and form forward and aft pockets with the central portion respectfully. The stator assembly also includes a locking stator segment. The locking stator segment includes a shroud that includes a forward hook and a pair of aft hooks with a platform disposed therebetween. The forward and aft hooks are retained in the forward and aft pockets of the case respectfully.
摘要翻译: 公开了一种用于涡轮风扇燃气涡轮发动机的定子组件。 定子组件联接到发动机的护罩上。 定子组件包括固定地连接到发动机罩的环形壳体。 壳体包括前部,后部和设置在其间的中心部。 壳体围绕发动机的轴线延伸。 壳体的前部和后部包括彼此相对延伸的轨道,并且相对地形成具有中心部分的前后袋。 定子组件还包括锁定定子段。 锁定定子段包括护罩,其包括前钩和一对后钩,其间具有平台。 前后钩被保留在箱子的前后袋中。
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公开(公告)号:US20130340966A1
公开(公告)日:2013-12-26
申请号:US13529041
申请日:2012-06-21
申请人: Susan M. Tholen , Dominic J. Mongillo , Paul M. Lutjen , James N. Knapp , Virginia L. Ross , Jonathan J. Earl , Eric A. Hudson
发明人: Susan M. Tholen , Dominic J. Mongillo , Paul M. Lutjen , James N. Knapp , Virginia L. Ross , Jonathan J. Earl , Eric A. Hudson
摘要: A hybrid sacrificial core for forming an impingement space and an internal cooling passageway network separate from the impingement space of a part may comprise a ceramic core having a first surface portion for forming the impingement space, and a refractory metal core that forms a plurality of passages of the internal cooling passageway network.
摘要翻译: 用于形成与部件的冲击空间分离的冲击空间和内部冷却通道网的混合牺牲芯可以包括具有用于形成冲击空间的第一表面部分的陶瓷芯体和形成多个通道的难熔金属芯体 的内部冷却通道网络。
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公开(公告)号:US09650905B2
公开(公告)日:2017-05-16
申请号:US13596194
申请日:2012-08-28
申请人: Jonathan J. Earl , Eric A. Kuehne
发明人: Jonathan J. Earl , Eric A. Kuehne
CPC分类号: F01D9/042 , F01D25/246 , F05D2230/60 , F05D2260/30 , Y10T29/49229
摘要: A vane cluster for a gas turbine engine includes multiple singlet vanes and a forward wear liner connecting a forward edge of each singlet vane, thereby allowing the vane cluster to be manipulated as a single component.
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公开(公告)号:US20140060081A1
公开(公告)日:2014-03-06
申请号:US13596194
申请日:2012-08-28
申请人: Jonathan J. Earl , Eric A. Kuehne
发明人: Jonathan J. Earl , Eric A. Kuehne
IPC分类号: F01D9/04
CPC分类号: F01D9/042 , F01D25/246 , F05D2230/60 , F05D2260/30 , Y10T29/49229
摘要: A vane cluster for a gas turbine engine includes multiple singlet vanes and a forward wear liner connecting a forward edge of each singlet vane, thereby allowing the vane cluster to be manipulated as a single component.
摘要翻译: 用于燃气涡轮发动机的叶片组包括多个单线叶片和连接每个单线叶片的前边缘的前磨损衬套,从而允许叶片组作为单个部件被操纵。
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