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1. 发明授权

US06896483B2 Blade track assembly 失效
标题翻译：刀片轨道组件
公开(公告)号：US06896483B2
公开(公告)日：2005-05-24
申请号：US10189121
申请日：2002-07-02
申请人： Douglas D. Dierksmeier , Tab Michael Heffernan , James C. Muskat
发明人： Douglas D. Dierksmeier , Tab Michael Heffernan , James C. Muskat
IPC分类号： F01D11/18
CPC分类号： F01D11/18 , F05D2240/40 , F05D2300/50212 , Y10T403/21 , Y10T403/213 , Y10T403/217
摘要： The clearances between an array of turbine blades and its surrounding blade track may be controlled by an expansion control material system supporting the blade tracks. The blade track support hoop is placed in tension by the expansion control material placed therein and the expansion control material is placed in compression.
摘要翻译：涡轮叶片阵列及其周围的叶片轨道之间的间隙可以由支撑叶片轨道的膨胀控制材料系统来控制。刀片轨道支撑环通过放置在其中的膨胀控制材料而被张紧，膨胀控制材料被压缩。

2. 发明授权

US5688108A High temperature rotor blade attachment 失效
标题翻译：高温转子叶片附件
公开(公告)号：US5688108A
公开(公告)日：1997-11-18
申请号：US509777
申请日：1995-08-01
申请人： Douglas D. Dierksmeier , Tab M. Heffernan
发明人： Douglas D. Dierksmeier , Tab M. Heffernan
IPC分类号： F01D5/08 , F01D5/28 , F01D5/30 , F04D29/34
CPC分类号： F01D5/3007 , F01D5/081 , F01D5/085 , F01D5/28 , F01D5/3061 , Y02T50/671 , Y02T50/676
摘要： A lightweight high temperature rotor blade attachment structure for use in a gas turbine engine. The lightweight high temperature rotor blade attachment lug being cast of a single crystal alloy and the lug is then bonded to a conventional nickel based wheel. A circular arc firtree is utilized to connect the insertable turbine blade between a pair of circumferentially spaced lugs that have been bonded to the turbine disk. In an alternate form of the present invention the attachment lug includes an internal cooling passage for receiving cooling fluid from a compressor. More particularly, the present invention discloses a single crystal attachment lug that is bonded to a powdered metal nickel alloy rotor disk and includes internal cooling passages, and in one form is designed for use with turbine blades that do not have a platform. Further, in another form of the present invention the single crystal attachment lug is bonded to the powdered metal nickel rotor disk and is designed to be used with turbine blades having a platform.
摘要翻译：一种用于燃气涡轮发动机的轻型高温转子叶片安装结构。轻型高温转子叶片安装凸耳由单晶合金铸造，然后将凸耳接合到常规的镍基轮上。使用圆形弧形管将可插入的涡轮叶片连接在已经结合到涡轮盘上的一对周向间隔开的凸耳之间。在本发明的替代形式中，附接凸耳包括用于从压缩机接收冷却流体的内部冷却通道。更具体地说，本发明公开了一种结合到粉末状金属镍合金转子盘上并包括内部冷却通道的单晶安装凸耳，其一种形式被设计用于不具有平台的涡轮叶片。此外，在本发明的另一形式中，单晶安装凸耳与粉末状金属镍转子盘结合，并被设计成与具有平台的涡轮叶片一起使用。

3. 发明授权

US5863183A High temperature rotor blade attachment 失效
标题翻译：高温转子叶片附件
公开(公告)号：US5863183A
公开(公告)日：1999-01-26
申请号：US783439
申请日：1997-01-16
申请人： Douglas D. Dierksmeier , Tab M. Heffernan
发明人： Douglas D. Dierksmeier , Tab M. Heffernan
IPC分类号： F01D5/08 , F01D5/28 , F01D5/30 , F04D29/38
CPC分类号： F01D5/3007 , F01D5/081 , F01D5/085 , F01D5/28 , F01D5/3061 , Y02T50/671 , Y02T50/676
摘要： A lightweight high temperature rotor blade attachment structure for use in a gas turbine engine. The lightweight high temperature rotor blade attachment lug being cast of a single crystal alloy and the lug is then bonded to a conventional nickel based wheel. A circular arc firtree is utilized to connect the insertable turbine blade between a pair of circumferentially spaced lugs that have been bonded to the turbine disk. In an alternate form of the present invention the attachment lug includes an internal cooling passage for receiving cooling fluid from a compressor. More particularly, the present invention discloses a single crystal attachment lug that is bonded to a powdered metal nickel alloy rotor disk and includes internal cooling passages, and in one form is designed for use with turbine blades that do not have a platform. Further, in amother form of the present invention the single crystal attachment lug is bonded to the powdered metal nickel rotor disk and is designed to be used with turbine blades having a platform.
摘要翻译：一种用于燃气涡轮发动机的轻型高温转子叶片安装结构。轻型高温转子叶片安装凸耳由单晶合金铸造，然后将凸耳接合到常规的镍基轮上。使用圆形弧形管将可插入的涡轮叶片连接在已经结合到涡轮盘上的一对周向间隔开的凸耳之间。在本发明的替代形式中，附接凸耳包括用于从压缩机接收冷却流体的内部冷却通道。更具体地说，本发明公开了一种结合到粉末状金属镍合金转子盘上并包括内部冷却通道的单晶安装凸耳，其一种形式被设计用于不具有平台的涡轮叶片。此外，在本发明的另一种形式中，单晶安装凸耳与粉末状金属镍转子盘结合，并被设计成与具有平台的涡轮叶片一起使用。

4. 发明授权

US06557621B1 Casting core and method of casting a gas turbine engine component 有权
标题翻译：铸造核心和铸造燃气涡轮发动机部件的方法
公开(公告)号：US06557621B1
公开(公告)日：2003-05-06
申请号：US09480331
申请日：2000-01-10
申请人： Douglas D. Dierksmeier , Jeffrey A. Ruppel
发明人： Douglas D. Dierksmeier , Jeffrey A. Ruppel
IPC分类号： B22C910
CPC分类号： B22C9/103
摘要： An integral ceramic casting core includes a base portion with a plurality of rods extending therefrom and a plurality of apertures formed therein. The base portion defines a passageway for the passage of a cooling media within a cast component. The plurality of rods forming cooling media inlet passages to the passageway and the plurality of apertures are adapted to receive molten metal therein and form heat transfer pedestals within the passageway.
摘要翻译：整体陶瓷铸造芯包括具有从其延伸的多个杆的基部和在其中形成的多个孔。基座部分限定用于铸造部件内的冷却介质通过的通道。形成到通道和多个孔的冷却介质入口通道的多个杆适于在其中容纳熔融金属，并在通道内形成热传递基座。

5. 发明授权

US4838584A Quick disconnect duct coupler 失效
标题翻译：快速断开管道耦合器
公开(公告)号：US4838584A
公开(公告)日：1989-06-13
申请号：US100385
申请日：1987-09-24
申请人： Douglas D. Dierksmeier
发明人： Douglas D. Dierksmeier
IPC分类号： B64D29/00 , F02K1/80 , F16B5/00
CPC分类号： F02K1/80 , B64D29/00 , F16B5/00 , Y02T50/672 , Y10S285/915
摘要： A coupling device utilizing first and second contiguous L-shaped coupling members affixed to terminal duct portions, and a slidable clamp having a T-shaped trough for gripping the L-shaped coupling members when slid thereover, locking them together to the close the duct. The clamp is slid away from the coupling members to rapidly open the duct.
摘要翻译：一种联接装置，其利用固定在终端导管部分上的第一和第二连续的L形联接件，以及一个可滑动的夹具，其具有一个T形槽，用于在其上滑动时夹住L形联接件，将它们锁定在一起以封闭导管。夹具从联接构件滑动，以快速打开管道。

6. 发明申请

US20090202355A1 Replaceable blade tip shroud 审中-公开
标题翻译：可更换刀片护罩
公开(公告)号：US20090202355A1
公开(公告)日：2009-08-13
申请号：US12069512
申请日：2008-02-11
申请人： Douglas D. Dierksmeier , Tab M. Heffernan
发明人： Douglas D. Dierksmeier , Tab M. Heffernan
IPC分类号： F01D5/20 , F01D5/14
CPC分类号： F01D5/225 , F01D5/284 , Y02T50/672
摘要： One embodiment of the present invention is a blade with a replaceable blade tip shroud that includes an airfoil shaped spar extending from a leading edge to a trailing edge between a root end and a tip end. It can also include a plurality of tiles coupled to an exterior of the spar; a tip shroud positioned to overlap at least a portion of the tip end of the spar; and means for anchoring the tip shroud to the tip end of the spar.
摘要翻译：本发明的一个实施例是具有可更换刀片护罩的刀片，其包括从前端到末端之间的前缘延伸到后缘的翼型翼梁。它还可以包括耦合到翼梁的外部的多个瓦片; 顶盖，其定位成与所述翼梁的顶端的至少一部分重叠; 以及用于将尖端护罩固定到翼梁的尖端的装置。

7. 发明授权

US5836742A High temperature rotor blade attachment 失效
标题翻译：高温转子叶片附件
公开(公告)号：US5836742A
公开(公告)日：1998-11-17
申请号：US784350
申请日：1997-01-16
申请人： Douglas D. Dierksmeier , Tab M. Heffernan
发明人： Douglas D. Dierksmeier , Tab M. Heffernan
IPC分类号： F01D5/08 , F01D5/28 , F01D5/30 , F04D29/58
CPC分类号： F01D5/3007 , F01D5/081 , F01D5/085 , F01D5/28 , F01D5/3061 , Y02T50/671 , Y02T50/676
摘要： A lightweight high temperature rotor blade attachment structure for use in a gas turbine engine. The lightweight high temperature rotor blade attachment lug being cast of a single crystal alloy and the lug is then bonded to a conventional nickel based wheel. A circular arc firtree is utilized to connect the insertable turbine blade between a pair of circumferentially spaced lugs that have been bonded to the turbine disk. In an alternate form of the present invention the attachment lug includes an internal cooling passage for receiving cooling fluid from a compressor. More particularly, the present invention discloses a single crystal attachment lug that is bonded to a powdered metal nickel alloy rotor disk and includes internal cooling passages, and in one form is designed for use with turbine blades that do not have a platform. Further, in another form of the present invention the single crystal attachment lug is bonded to the powdered metal nickel rotor disk and is designed to be used with turbine blades having a platform.
摘要翻译：一种用于燃气涡轮发动机的轻型高温转子叶片安装结构。轻型高温转子叶片安装凸耳由单晶合金铸造，然后将凸耳接合到常规的镍基轮上。使用圆形弧形管将可插入的涡轮叶片连接在已经结合到涡轮盘上的一对周向间隔开的凸耳之间。在本发明的替代形式中，附接凸耳包括用于从压缩机接收冷却流体的内部冷却通道。更具体地说，本发明公开了一种结合到粉末状金属镍合金转子盘上并包括内部冷却通道的单晶安装凸耳，其一种形式被设计用于不具有平台的涡轮叶片。此外，在本发明的另一形式中，单晶安装凸耳与粉末状金属镍转子盘结合，并被设计成与具有平台的涡轮叶片一起使用。

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