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1. 发明授权

US06842158B2 Wideband low profile spiral-shaped transmission line antenna 失效
标题翻译：宽带低调螺旋形传输线天线
公开(公告)号：US06842158B2
公开(公告)日：2005-01-11
申请号：US10331105
申请日：2002-12-27
申请人： Young-Min Jo , Young-Ki Kim , Kyu-Young Han , Sean F. Sullivan , Jay A. Kralovec
发明人： Young-Min Jo , Young-Ki Kim , Kyu-Young Han , Sean F. Sullivan , Jay A. Kralovec
IPC分类号： H01Q1/24 , H01Q1/38 , H01Q9/27 , H01Q9/28 , H01Q1/36
CPC分类号： H01Q9/285 , H01Q1/243 , H01Q1/38 , H01Q9/27
摘要： An antenna incorporating slow wave structures. The antenna comprises at least two conductive serpentine structures disposed on a dielectric substrate and further comprising an oppositely disposed conductive top plate electrically connected to the conductive serpentine structures and farther electromagnetically connected thereto. In one embodiment the antenna further comprises a ground plane below the dielectric substrate.
摘要翻译：结合慢波结构的天线。该天线包括至少两个设置在电介质基片上的导电蛇形结构，并且还包括与导电蛇形结构电连接并且与其进一步电磁连接的相对设置的导电顶板。在一个实施例中，天线还包括在电介质基底下方的接地平面。

2. 发明授权

US06469675B1 High gain, frequency tunable variable impedance transmission line loaded antenna with radiating and tuning wing 有权
标题翻译：高增益，频率可调阻抗传输线负载天线，带辐射和调谐机翼
公开(公告)号：US06469675B1
公开(公告)日：2002-10-22
申请号：US09643302
申请日：2000-08-22
申请人： Young-Min Jo , Michael H. Thursby , Sean F. Sullivan
发明人： Young-Min Jo , Michael H. Thursby , Sean F. Sullivan
IPC分类号： H01Q1114
CPC分类号： H01Q21/205 , H01Q1/243 , H01Q5/357 , H01Q9/0421 , H01Q9/0442 , H01Q9/36 , H01Q11/14 , H01Q13/20
摘要： There is disclosed a meanderline loaded antenna comprising a ground plane, two vertical elements orthogonally affixed thereto, and a horizontal element between the two vertical elements. A meanderline coupler interconnects the horizontal element, at each of its ends, to the vertical elements. The antenna further includes an additional radiating element extending from the horizontal element in approximately planer relationship therewith. Additionally, the antenna includes a tuning element extending from the horizontal element and forming an acute angle with the adjacent vertical element.
摘要翻译：公开了一种弯曲线加载天线，其包括接地平面，垂直固定到其上的两个垂直元件和两个垂直元件之间的水平元件。曲折线耦合器将水平元件在其每个端部处互连到垂直元件。天线还包括从水平元件以大致平面关系延伸的附加辐射元件。此外，天线包括从水平元件延伸并与相邻垂直元件形成锐角的调谐元件。

3. 发明授权

US06429820B1 High gain, frequency tunable variable impedance transmission line loaded antenna providing multi-band operation 有权
标题翻译：高增益，频率可调阻抗传输线路负载天线提供多频段操作
公开(公告)号：US06429820B1
公开(公告)日：2002-08-06
申请号：US09724332
申请日：2000-11-28
申请人： Michael H. Thursby , Kerry L. Greer , Sean F. Sullivan , Young-Min Jo
发明人： Michael H. Thursby , Kerry L. Greer , Sean F. Sullivan , Young-Min Jo
IPC分类号： H01Q1112
CPC分类号： H01Q13/20 , H01Q5/357 , H01Q7/00 , H01Q9/42 , H01Q11/14
摘要： There is disclosed a meanderline loaded antenna comprising a ground plane, a plurality of vertical elements orthogonally affixed thereto, a driven vertical element affixed thereto and a horizontal element between the vertical elements. All but one of the plurality of vertical elements have an effective electrical length that is a quarter wavelength of the antenna operating frequency. Thus, these vertical elements represent an open and do not effect the antenna performance characteristics. One of the plurality of vertical elements will be operative and therefore the antenna length comprises the length of the operative element, the length of the driven element, and the length of the top plate therebetween.
摘要翻译：公开了一种弯曲线加载天线，其包括接地平面，垂直固定到其上的多个垂直元件，固定到其上的从动垂直元件和垂直元件之间的水平元件。多个垂直元件中的一个除了一个之外，具有作为天线工作频率的四分之一波长的有效电长度。因此，这些垂直元件表示开路并且不影响天线性能特征。多个垂直元件中的一个将是有效的，因此天线长度包括操作元件的长度，从动元件的长度以及它们之间的顶板的长度。

4. 发明授权

US06486844B2 High gain, frequency tunable variable impedance transmission line loaded antenna having shaped top plates 有权
公开(公告)号：US06486844B2
公开(公告)日：2002-11-26
申请号：US09871047
申请日：2001-05-31
申请人： Michael H. Thursby , Sean F. Sullivan , Floyd A. Asbury
发明人： Michael H. Thursby , Sean F. Sullivan , Floyd A. Asbury
IPC分类号： H01Q1112
CPC分类号： H01Q11/14 , H01Q1/243 , H01Q1/36 , H01Q5/357 , H01Q9/0421 , H01Q9/0442 , H01Q9/36 , H01Q13/20 , H01Q21/205
摘要： There is disclosed a meanderline loaded antenna comprising a ground plane, a non-driven vertical element affixed thereto, a driven vertical element and a shaped top radiating element conductively connected between the driven and non-driven vertical elements. One or more segments or regions of the top plate are resonant depending on the input signal frequency. Since top plate presents several such segments or portions, several different resonant frequencies (a band of closely spaced resonant frequencies or multiple bands of disparate resonant frequencies) are presented to the antenna driving signal, thus allowing the antenna to resonate at several different frequencies and bands. In another embodiment, the antenna comprises a plurality of top radiating elements in parallel spaced relation or in a single plane, wherein each top radiating element is resonant at a different frequency, when considered with the effective lengths of the other antenna elements. Thus the plurality of top radiating plates accommodate multiple resonant frequencies and wideband operation. A plurality of such antennae can be used as elements to form an antenna array. The antenna functions similarly in a receive mode in accordance with the antenna reciprocity therein.

5. 发明授权

US08875520B2 Gas turbine engine device 有权
标题翻译：燃气轮机发动机装置
公开(公告)号：US08875520B2
公开(公告)日：2014-11-04
申请号：US12634606
申请日：2009-12-09
申请人： Gregory W. P. Zeaton , David L. Sutterfield , Sean F. Sullivan
发明人： Gregory W. P. Zeaton , David L. Sutterfield , Sean F. Sullivan
IPC分类号： F02C7/20 , F02K1/80 , F02K1/04 , F02K1/08
CPC分类号： F02K1/80 , F02K1/04 , F02K1/08 , F05D2240/14 , Y02T50/67 , Y02T50/672
摘要： A gas turbine engine adapter is provided. In one form the adapter is segmented and may be attached to a gas turbine engine support ring. The adapter can provide a channel that may receive part of a gas turbine engine component such as, but not limited to, a plug nozzle. The adapter can include a load bearing support to counteract axial forces experienced by the plug nozzle during operation of the gas turbine engine. A compressible seal can be provided between the plug nozzle and the adapter. A leaf seal can also be provided to seal between segments of the adapter. The plug nozzle can be discouraged from rotating relative to the adapter.
摘要翻译：提供燃气涡轮引擎适配器。在一种形式中，适配器被分段并且可以附接到燃气涡轮发动机支撑环。适配器可以提供可以接收燃气涡轮发动机部件的一部分的通道，例如但不限于塞子喷嘴。适配器可以包括承载支撑件，用于抵消在燃气涡轮发动机操作期间由塞子喷嘴经受的轴向力。可以在塞子喷嘴和适配器之间提供可压缩密封。还可以提供叶密封件以在适配器的段之间进行密封。塞子喷嘴可以不被阻止相对于适配器旋转。

6. 发明授权

US06965348B2 Broadband antenna structures 失效
标题翻译：宽带天线结构
公开(公告)号：US06965348B2
公开(公告)日：2005-11-15
申请号：US10878909
申请日：2004-06-28
申请人： Frank M. Caimi , Sean F. Sullivan
发明人： Frank M. Caimi , Sean F. Sullivan
IPC分类号： H01Q1/36 , H01Q9/27 , H01Q11/12 , H01Q13/20 , H01Q1/00 , H01Q9/00
CPC分类号： H01Q9/27 , H01Q1/36 , H01Q11/12 , H01Q13/20
摘要： There is disclosed an antenna exhibiting resonance over a broad frequency band or over a plurality of closely-spaced frequency bands, comprising a ground plane, a non-driven element affixed substantially perpendicular to the ground plane, a driven element affixed substantially perpendicular to the ground plane and a horizontal conductor electrically connected between the driven and the non-driven elements and disposed substantially parallel to the ground plane. The non-driven and the driven elements further comprise periodic slow wave structures. The periodic slow wave structures are configured to provide a substantially constant propagation factor with respect to the applied signal frequency, such that the antenna exhibits broad resonance characteristics.
摘要翻译：公开了一种在宽频带上或多个紧密间隔的频带上呈现谐振的天线，包括接地平面，基本上垂直于接地平面固定的非驱动元件，基本上垂直于地面固定的从动元件平面和水平导体，电连接在被驱动元件和非驱动元件之间，并且基本上平行于接地平面设置。非驱动和从动元件还包括周期性的慢波结构。周期性慢波结构被配置为相对于所施加的信号频率提供基本上恒定的传播因子，使得天线具有宽的谐振特性。

7. 发明申请

US20100162725A1 GAS TURBINE ENGINE DEVICE 有权
标题翻译：气体涡轮发动机装置
公开(公告)号：US20100162725A1
公开(公告)日：2010-07-01
申请号：US12634606
申请日：2009-12-09
申请人： Gregory W. P. Zeaton , David L. Sutterfield , Sean F. Sullivan
发明人： Gregory W. P. Zeaton , David L. Sutterfield , Sean F. Sullivan
IPC分类号： F02C7/20
CPC分类号： F02K1/80 , F02K1/04 , F02K1/08 , F05D2240/14 , Y02T50/67 , Y02T50/672
摘要： A gas turbine engine adapter is provided. In one form the adapter is segmented and may be attached to a gas turbine engine support ring. The adapter can provide a channel that may receive part of a gas turbine engine component such as, but not limited to, a plug nozzle. The adapter can include a load bearing support to counteract axial forces experienced by the plug nozzle during operation of the gas turbine engine. A compressible seal can be provided between the plug nozzle and the adapter. A leaf seal can also be provided to seal between segments of the adapter. The plug nozzle can be discouraged from rotating relative to the adapter.
摘要翻译：提供燃气涡轮引擎适配器。在一种形式中，适配器被分段并且可以附接到燃气涡轮发动机支撑环。适配器可以提供可以接收燃气涡轮发动机部件的一部分的通道，例如但不限于塞子喷嘴。适配器可以包括承载支撑件，用于抵消在燃气涡轮发动机操作期间由塞子喷嘴经受的轴向力。可以在塞子喷嘴和适配器之间提供可压缩密封。还可以提供叶密封件以在适配器的段之间进行密封。塞子喷嘴可以不被阻止相对于适配器旋转。

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