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公开(公告)号：US20110194943A1
公开(公告)日：2011-08-11
申请号：US13023651
申请日：2011-02-09
CPC分类号： F01D5/187 , F01D5/22 , F05D2260/221
摘要： A turbine blade assembly in a turbine engine. The turbine blade assembly includes a turbine blade and a first snubber structure. The turbine blade includes an internal cooling passage containing cooling air. The first snubber structure extends outwardly from a sidewall of the turbine blade and includes a hollow interior portion that receives cooling air from the internal cooling passage of the turbine blade.
摘要翻译： 涡轮发动机中的涡轮叶片组件。 涡轮叶片组件包括涡轮叶片和第一缓冲结构。 涡轮机叶片包括内部冷却通道，其包含冷却空气。 第一缓冲结构从涡轮机叶片的侧壁向外延伸并且包括从涡轮叶片的内部冷却通道接收冷却空气的中空内部部分。
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公开(公告)号：US08684692B2
公开(公告)日：2014-04-01
申请号：US13023651
申请日：2011-02-09
CPC分类号： F01D5/187 , F01D5/22 , F05D2260/221
摘要： A turbine blade assembly in a turbine engine. The turbine blade assembly includes a turbine blade and a first snubber structure. The turbine blade includes an internal cooling passage containing cooling air. The first snubber structure extends outwardly from a sidewall of the turbine blade and includes a hollow interior portion that receives cooling air from the internal cooling passage of the turbine blade.
摘要翻译： 涡轮发动机中的涡轮叶片组件。 涡轮叶片组件包括涡轮叶片和第一缓冲结构。 涡轮机叶片包括内部冷却通道，其包含冷却空气。 第一缓冲结构从涡轮机叶片的侧壁向外延伸并且包括从涡轮叶片的内部冷却通道接收冷却空气的中空内部部分。
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3.发明申请公开(公告)号：US20140230441A1
公开(公告)日：2014-08-21
申请号：US13768038
申请日：2013-02-15
申请人： Clinton A. Mayer , Jesse Eng , Cheryl A. Schopf
发明人： Clinton A. Mayer , Jesse Eng , Cheryl A. Schopf
IPC分类号： F02C7/12
CPC分类号： F02C7/12 , F01D25/26 , F05D2260/231
摘要： A heat shield manifold system for an inner casing between a compressor and turbine assembly is disclosed. The heat shield manifold system protects the outer case from high temperature compressor discharge air, thereby enabling the outer case extending between a compressor and a turbine assembly to be formed from less expensive materials than otherwise would be required. In addition, the heat shield manifold system may be configured such that compressor bleed air is passed from the compressor into the heat shield manifold system without passing through a conventional flange to flange joint that is susceptible to leakage.
摘要翻译： 公开了一种用于压缩机和涡轮机组件之间的内壳的隔热罩歧管系统。 隔热罩歧管系统保护外壳免受高温压缩机排放空气的影响，从而使压缩机和涡轮机组件之间延伸的外壳由不需要的材料形成。 此外，隔热罩歧管系统可以被配置成使得压缩机排出的空气从压缩机传递到隔热管歧管系统中，而不会通过常规的法兰到容易泄漏的法兰接头。
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公开(公告)号：US09714611B2
公开(公告)日：2017-07-25
申请号：US13768038
申请日：2013-02-15
申请人： Clinton A. Mayer , Jesse Eng , Cheryl A. Schopf
发明人： Clinton A. Mayer , Jesse Eng , Cheryl A. Schopf
CPC分类号： F02C7/12 , F01D25/26 , F05D2260/231
摘要： A heat shield manifold system for an inner casing between a compressor and turbine assembly is disclosed. The heat shield manifold system protects the outer case from high temperature compressor discharge air, thereby enabling the outer case extending between a compressor and a turbine assembly to be formed from less expensive materials than otherwise would be required. In addition, the heat shield manifold system may be configured such that compressor bleed air is passed from the compressor into the heat shield manifold system without passing through a conventional flange to flange joint that is susceptible to leakage.
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