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1. 发明授权

US5504382A Field controlled permanent magnet alternator 失效
标题翻译：现场控制永磁发电机
公开(公告)号：US5504382A
公开(公告)日：1996-04-02
申请号：US185541
申请日：1994-01-24
申请人： Michael J. Douglass , Scot A. Webb
发明人： Michael J. Douglass , Scot A. Webb
IPC分类号： H02K1/27 , H02K21/04 , H02K21/20 , H02K21/12
CPC分类号： H02K1/278 , H02K21/046 , H02K21/20
摘要： An alternator, or the like including a stator assembly and a rotor assembly within the stator assembly, wherein the stator assembly includes a pair of axially spaced core sections with a stationary field coil located therebetween. The field coil is formed of convolutions extending circumferentially about the axis of the device. The rotor assembly has a homopolar core with a pair of axially spaced pole sections in locations corresponding to the respective stator core sections. A central yoke portion extends between the two pole sections and is axially aligned within the field coil. A plurality of permanent magnets are mounted circumferentially on each of the pole sections at symmetrically spaced locations between pole sectors of the respective section.
摘要翻译：交流发电机等包括在定子组件内的定子组件和转子组件，其中定子组件包括一对轴向间隔开的芯部分，其间具有固定磁场线圈。励磁线圈由绕设备的轴线周向延伸的卷积形成。转子组件具有在对应于相应的定子铁芯部分的位置中具有一对轴向间隔开的极部分的单极铁芯。中心轭部分在两个极部分之间延伸并且在励磁线圈内轴向对准。在相应部分的极区之间的对称间隔位置处，多个永磁体周向安装在每个极部分上。

2. 发明申请

US20090243228A1 Gas Turbine Engine Seals and Engines Incorporating Such Seals 有权
标题翻译：装有这种密封件的燃气轮机发动机密封和发动机
公开(公告)号：US20090243228A1
公开(公告)日：2009-10-01
申请号：US12056792
申请日：2008-03-27
申请人： Kurt R. Heinemann , Jose Paulino , Scot A. Webb , Mark Ring , Charles H. Warner
发明人： Kurt R. Heinemann , Jose Paulino , Scot A. Webb , Mark Ring , Charles H. Warner
IPC分类号： F02F11/00
CPC分类号： F01D11/005
摘要： Gas turbine engine seals and engines incorporating such seals are provided. In this regard, a representative seal includes: an annular seal body having an inner diameter and an outer diameter, the seal body extending along an axis of symmetry between a first end and a second end; the seal body being formed of a strip of material having first and second opposing edges, the strip of material being deformed to exhibit a first sealing surface at the first end, a second sealing surface at the second end, and a third sealing surface along the inner diameter, the first edge being located adjacent to the third sealing surface, the second edge being located adjacent to the second sealing surface; the first edge being spaced from the second edge to define an annular opening, the annular opening providing access to an annular cavity of the seal body.
摘要翻译：提供了包括这种密封件的燃气涡轮发动机密封件和发动机。在这方面，代表性的密封件包括：具有内径和外径的环形密封体，密封体沿第一端和第二端之间的对称轴延伸; 所述密封体由具有第一和第二相对边缘的材料条形成，所述材料条变形以在第一端处呈现第一密封表面，在第二端处具有第二密封表面，以及沿着所述第二密封表面的第三密封表面所述第一边缘邻近所述第三密封表面定位，所述第二边缘邻近所述第二密封表面定位; 所述第一边缘与所述第二边缘间隔开以限定环形开口，所述环形开口提供对所述密封体的环形腔的通路。

3. 发明授权

US09249681B2 Fan case rub system 有权
标题翻译：风箱磨擦系统
公开(公告)号：US09249681B2
公开(公告)日：2016-02-02
申请号：US13361990
申请日：2012-01-31
申请人： Thomas J. Robertson, Jr. , Scot A. Webb , Steven C. Clarkson
发明人： Thomas J. Robertson, Jr. , Scot A. Webb , Steven C. Clarkson
IPC分类号： F01D11/16 , F01D21/04 , F01D11/12 , F02K3/06
CPC分类号： F01D11/16 , F01D11/122 , F01D11/127 , F01D21/045 , F02K3/06 , F05D2250/75 , Y02T50/672
摘要： A turbine engine fan case assembly includes a structural case and a liner assembly. A radially accommodating attachment system connects the liner assembly to the structural case. The attachment system comprises a circumferentially-distributed plurality of longitudinally elongate radially outwardly open channels mounted to the liner assembly. The attachment system further comprises an associated plurality of inwardly-projecting tongues mounted to the structural case. Each tongue is accommodated in an associated such channel.
摘要翻译：涡轮发动机风扇壳体组件包括结构壳体和衬套组件。径向容纳的连接系统将衬套组件连接到结构壳体。附接系统包括安装到衬套组件上的周向分布的多个纵向细长的径向向外开放的通道。附接系统还包括安装到结构壳体上的相关联的多个向内突出的舌片。每个舌头容纳在相关联的这样的通道中。

4. 发明申请

US20130051993A1 ROTATING TURBOMACHINE SEAL 有权
标题翻译：旋转涡轮密封
公开(公告)号：US20130051993A1
公开(公告)日：2013-02-28
申请号：US13217210
申请日：2011-08-24
申请人： Scot A. Webb
发明人： Scot A. Webb
IPC分类号： F01D11/00
CPC分类号： F01D11/005 , F16J15/164
摘要： An exemplary turbomachine seal assembly includes a ring seal that has a radially-facing sealing surface, an axially-facing sealing surface, and a first tapered surface. The turbomachine seal assembly also includes a spacer that has a second tapered surface. The second tapered surface interfaces with the first tapered surface to bias the radially facing sealing surface and the axially facing sealing surface toward a sealing position.
摘要翻译：示例性的涡轮机械密封组件包括具有径向面对的密封表面，面向轴向的密封表面和第一锥形表面的环形密封件。涡轮机械密封组件还包括具有第二锥形表面的间隔件。第二锥形表面与第一锥形表面接合，以朝向密封位置偏压径向面对的密封表面和轴向面对的密封表面。

5. 发明授权

US08016297B2 Gas turbine engine seals and engines incorporating such seals 有权
标题翻译：燃气涡轮发动机密封件和包含这种密封件的发动机
公开(公告)号：US08016297B2
公开(公告)日：2011-09-13
申请号：US12056792
申请日：2008-03-27
申请人： Kurt R. Heinemann , Jose Paulino , Scot A. Webb , Mark Ring , Charles H. Warner
发明人： Kurt R. Heinemann , Jose Paulino , Scot A. Webb , Mark Ring , Charles H. Warner
IPC分类号： F16J15/02
CPC分类号： F01D11/005
摘要： Gas turbine engine seals and engines incorporating such seals are provided. In this regard, a representative seal includes: an annular seal body having an inner diameter and an outer diameter, the seal body extending along an axis of symmetry between a first end and a second end; the seal body being formed of a strip of material having first and second opposing edges, the strip of material being deformed to exhibit a first sealing surface at the first end, a second sealing surface at the second end, and a third sealing surface along the inner diameter, the first edge being located adjacent to the third sealing surface, the second edge being located adjacent to the second sealing surface; the first edge being spaced from the second edge to define an annular opening, the annular opening providing access to an annular cavity of the seal body.
摘要翻译：提供了包括这种密封件的燃气涡轮发动机密封件和发动机。在这方面，代表性的密封件包括：具有内径和外径的环形密封体，密封体沿第一端和第二端之间的对称轴延伸; 所述密封体由具有第一和第二相对边缘的材料条形成，所述材料条变形以在第一端处呈现第一密封表面，在第二端处具有第二密封表面，以及沿着所述第二密封表面的第三密封表面所述第一边缘邻近所述第三密封表面定位，所述第二边缘邻近所述第二密封表面定位; 所述第一边缘与所述第二边缘间隔开以限定环形开口，所述环形开口提供对所述密封体的环形腔的通路。

6. 发明授权

US08939710B2 Rotating turbomachine seal 有权
标题翻译：旋转涡轮机油封
公开(公告)号：US08939710B2
公开(公告)日：2015-01-27
申请号：US13217210
申请日：2011-08-24
申请人： Scot A. Webb
发明人： Scot A. Webb
IPC分类号： F01D11/00 , F16J15/16
CPC分类号： F01D11/005 , F16J15/164
摘要： An exemplary turbomachine seal assembly includes a ring seal that has a radially-facing sealing surface, an axially-facing sealing surface, and a first tapered surface. The turbomachine seal assembly also includes a spacer that has a second tapered surface. The second tapered surface interfaces with the first tapered surface to bias the radially facing sealing surface and the axially facing sealing surface toward a sealing position.
摘要翻译：示例性的涡轮机械密封组件包括具有径向面对的密封表面，面向轴向的密封表面和第一锥形表面的环形密封件。涡轮机密封组件还包括具有第二锥形表面的间隔件。第二锥形表面与第一锥形表面接合，以朝向密封位置偏压径向面对的密封表面和轴向面对的密封表面。

7. 发明申请

US20130195635A1 Fan Case Rub System 有权
标题翻译：风扇擦除系统
公开(公告)号：US20130195635A1
公开(公告)日：2013-08-01
申请号：US13361990
申请日：2012-01-31
申请人： Thomas J. Robertson, JR. , Scot A. Webb , Steven C. Clarkson
发明人： Thomas J. Robertson, JR. , Scot A. Webb , Steven C. Clarkson
IPC分类号： F01D25/24
CPC分类号： F01D11/16 , F01D11/122 , F01D11/127 , F01D21/045 , F02K3/06 , F05D2250/75 , Y02T50/672
摘要： A turbine engine fan case assembly includes a structural case and a liner assembly. A radially accommodating attachment system connects the liner assembly to the structural case. The attachment system comprises a circumferentially-distributed plurality of longitudinally elongate radially outwardly open channels mounted to the liner assembly. The attachment system further comprises an associated plurality of inwardly-projecting tongues mounted to the structural case. Each tongue is accommodated in an associated said channel.
摘要翻译：涡轮发动机风扇壳体组件包括结构壳体和衬套组件。径向容纳的连接系统将衬套组件连接到结构壳体。附接系统包括安装到衬套组件上的周向分布的多个纵向细长的径向向外开放的通道。附接系统还包括安装到结构壳体上的相关联的多个向内突出的舌片。每个舌头容纳在相关联的所述通道中。

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