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1. 发明授权

US07770399B2 Gas turbine engine nozzle liner with thermally compliant attachment brackets 有权
标题翻译：燃气涡轮发动机喷嘴衬套，具有耐热兼容的附件支架
公开(公告)号：US07770399B2
公开(公告)日：2010-08-10
申请号：US11540310
申请日：2006-09-29
申请人： Andrew D. Burdick , Kyle J. Osga , Paul R. Senofonte , Richard F. Norman , Alex J. Simpson
发明人： Andrew D. Burdick , Kyle J. Osga , Paul R. Senofonte , Richard F. Norman , Alex J. Simpson
IPC分类号： F02K1/00
CPC分类号： F02K1/1207
摘要： A gas turbine engine has the convergent flaps and seals of an adjustable cross-sectional area nozzle connected to associated liners with a thermally compliant bracket. The bracket includes spaced feet with an intermediate notch spaced away from the liner. In this manner, a temperature gradient along the liner can be easily compensated at the connection of the bracket to the liner by adjustment within the notch. In other features, the bracket is riveted to the liner, providing further resistance to thermal expansion due to temperature gradiations.
摘要翻译：燃气涡轮发动机具有连接到具有热适应支架的相关衬套的可调节横截面积喷嘴的会聚翼片和密封件。支架包括间隔开的脚，其中间凹口与衬垫间隔开。以这种方式，通过在凹口内的调节，可以容易地在支架与衬套的连接处沿着衬套的温度梯度补偿。在其他特征中，支架铆接到衬垫上，由于温度梯度而进一步阻碍热膨胀。

2. 发明申请

US20090313998A1 AXIALLY SPLIT NOZZLE LINER FOR CONVERGENT NOZZLE 有权
标题翻译：用于转换喷嘴的AXIALLY SPLIT喷嘴衬管
公开(公告)号：US20090313998A1
公开(公告)日：2009-12-24
申请号：US11540279
申请日：2006-09-29
申请人： Paul R. Senofonte , Andrew D. Burdick , Richard F. Norman , Kyle J. Osga
发明人： Paul R. Senofonte , Andrew D. Burdick , Richard F. Norman , Kyle J. Osga
IPC分类号： F02K1/06
CPC分类号： F02K1/1215 , F02K1/822 , Y02T50/675
摘要： A convergent/divergent nozzle for a gas turbine engine includes liners that are attached to the convergent flaps and seals. The liner is formed of two separate plates. By splitting the liner into two separate plates, a thermal break is provided between the two. Thermal stresses on a downstream plate are not as readily transferred to an upstream plate. External stresses on the upstream plate are not transferred as readily to the downstream plate. The two liner plate portions, and a separate backing plate all have faces that abut and are riveted together. These faces provide a flow blocker to maintain a lower pressure downstream of the flow blocker.
摘要翻译：用于燃气涡轮发动机的收敛/扩散喷嘴包括附接到会聚翼片和密封件的衬垫。衬垫由两个单独的板形成。通过将衬套分成两个单独的板，两者之间提供热断裂。下游板上的热应力不易转移到上游板。上游板上的外部应力不会容易地转移到下游板。两个衬板部分和单独的背板都具有邻接并铆接在一起的面。这些面提供一个阻流器，以保持阻流器下游的较低压力。

3. 发明授权

US09217371B2 Mid-turbine frame with tensioned spokes 有权
标题翻译：带涡轮的中涡轮机架
公开(公告)号：US09217371B2
公开(公告)日：2015-12-22
申请号：US13548613
申请日：2012-07-13
申请人： Jorge I. Farah , Paul K. Sanchez , Andrew D. Burdick
发明人： Jorge I. Farah , Paul K. Sanchez , Andrew D. Burdick
IPC分类号： F02C7/20 , F01D25/28 , F01D25/16 , F02C7/06
CPC分类号： F02C7/20 , F01D25/162 , F01D25/28 , F02C7/06 , F05D2260/31 , F05D2260/941
摘要： A mid-turbine frame located in a gas turbine engine axially aft of a high-pressure turbine and fore of a low-pressure turbine includes an outer frame case, an inner frame case, and at least a first spoke connecting the outer frame case to the inner frame case. The first spoke is tightened so as to be in tension during substantially all operating conditions of the gas turbine engine.
摘要翻译：位于高压涡轮机轴向后方的燃气涡轮发动机的中涡轮机框架和低压涡轮机的前部包括外框架壳体，内框架壳体和至少第一轮辐，其将外框架壳体连接到内框框。在燃气轮机的基本上所有的操作条件下，第一轮辐被拧紧以致处于紧张状态。

4. 发明申请

US20140102110A1 MID-TURBINE FRAME WITH TENSIONED SPOKES 有权
标题翻译：中等涡轮机框架与张力调查
公开(公告)号：US20140102110A1
公开(公告)日：2014-04-17
申请号：US13548613
申请日：2012-07-13
申请人： Jorge I. Farah , Paul K. Sanchez , Andrew D. Burdick
发明人： Jorge I. Farah , Paul K. Sanchez , Andrew D. Burdick
IPC分类号： F02C7/20
CPC分类号： F02C7/20 , F01D25/162 , F01D25/28 , F02C7/06 , F05D2260/31 , F05D2260/941
摘要： A mid-turbine frame located in a gas turbine engine axially aft of a high-pressure turbine and fore of a low-pressure turbine includes an outer frame case, an inner frame case, and at least a first spoke connecting the outer frame case to the inner frame case. The first spoke is tightened so as to be in tension during substantially all operating conditions of the gas turbine engine.
摘要翻译：位于高压涡轮机轴向后方的燃气涡轮发动机的中涡轮机框架和低压涡轮机的前部包括外框架壳体，内框架壳体和至少第一轮辐，其将外框架壳体连接到内框框。在燃气轮机的基本上所有的操作条件下，第一轮辐被拧紧以致处于紧张状态。

5. 发明授权

US07685825B2 Axially split nozzle liner for convergent nozzle 有权
标题翻译：用于会聚喷嘴的轴向分流喷嘴衬套
公开(公告)号：US07685825B2
公开(公告)日：2010-03-30
申请号：US11540279
申请日：2006-09-29
申请人： Paul R. Senofonte , Andrew D. Burdick , Richard F. Norman , Kyle J. Osga
发明人： Paul R. Senofonte , Andrew D. Burdick , Richard F. Norman , Kyle J. Osga
IPC分类号： F02K1/00
CPC分类号： F02K1/1215 , F02K1/822 , Y02T50/675
摘要： A convergent/divergent nozzle for a gas turbine engine includes liners that are attached to the convergent flaps and seals. The liner is formed of two separate plates. By splitting the liner into two separate plates, a thermal break is provided between the two. Thermal stresses on a downstream plate are not as readily transferred to an upstream plate. External stresses on the upstream plate are not transferred as readily to the downstream plate. The two liner plate portions, and a separate backing plate all have faces that abut and are riveted together. These faces provide a flow blocker to maintain a lower pressure downstream of the flow blocker.
摘要翻译：用于燃气涡轮发动机的收敛/扩散喷嘴包括附接到会聚翼片和密封件的衬垫。衬垫由两个单独的板形成。通过将衬套分成两个单独的板，两者之间提供热断裂。下游板上的热应力不易转移到上游板。上游板上的外部应力不会容易地转移到下游板。两个衬板部分和单独的背板都具有邻接并铆接在一起的面。这些面提供一个阻流器，以保持阻流器下游的较低压力。

6. 发明申请

US20080078163A1 Gas turbine engine nozzle liner with thermally compliant attachment brackets 有权
标题翻译：燃气涡轮发动机喷嘴衬套，具有耐热兼容的附件支架
公开(公告)号：US20080078163A1
公开(公告)日：2008-04-03
申请号：US11540310
申请日：2006-09-29
申请人： Andrew D. Burdick , Kyle J. Osga , Paul R. Senofonte , Richard F. Norman , Alex J. Simpson
发明人： Andrew D. Burdick , Kyle J. Osga , Paul R. Senofonte , Richard F. Norman , Alex J. Simpson
IPC分类号： F02K3/02
CPC分类号： F02K1/1207
摘要： A gas turbine engine has the convergent flaps and seals of an adjustable cross-sectional area nozzle connected to associated liners with a thermally compliant bracket. The bracket includes spaced feet with an intermediate notch spaced away from the liner. In this manner, a temperature gradient along the liner can be easily compensated at the connection of the bracket to the liner by adjustment within the notch. In other features, the bracket is riveted to the liner, providing further resistance to thermal expansion due to temperature gradiations.
摘要翻译：燃气涡轮发动机具有连接到具有热适应支架的相关衬套的可调节横截面积喷嘴的会聚翼片和密封件。支架包括间隔开的脚，其中间凹口与衬垫间隔开。以这种方式，通过在凹口内的调节，可以容易地在支架与衬套的连接处沿着衬套的温度梯度补偿。在其他特征中，支架铆接到衬垫上，由于温度梯度而进一步阻碍热膨胀。

7. 发明授权

US6155928A Modular portable gaming simulator systems and methods 失效
标题翻译：模块化便携式游戏模拟器系统和方法
公开(公告)号：US6155928A
公开(公告)日：2000-12-05
申请号：US81127
申请日：1998-05-19
申请人： Andrew D. Burdick
发明人： Andrew D. Burdick
IPC分类号： A63F13/08 , A63F13/12 , B60P3/025 , A63F13/00
CPC分类号： B60P3/025 , A63F13/08 , A63F13/12 , A63F13/803 , A63F2300/8017
摘要： A modular portable gaming simulator system includes a transport trailer with at least one movable sidewall to which two or more gaming simulation stations are attached. The movable sidewall can be selectively raised and lowered between a transport or upright position for transporting the system, and a deployed or active position for displaying and operating the gaming simulation stations. The gaming simulation stations are interconnected so that the gaming simulation stations can interactively execute a software program application, such as in head-to-head competition. In the deployed position, the movable sidewall forms a stage on which the gaming simulation stations rest. In order to transport the system, the sidewall is raised into the upright or transportable position for transportation. During transportation, the gaming simulation stations remain attached to the sidewall in a horizontal, sideways position.
摘要翻译：模块化便携式游戏模拟器系统包括具有至少一个可移动侧壁的运输拖车，两个或多个游戏模拟站附接到该运送拖车。可移动侧壁可以在用于运送系统的运输或直立位置之间选择性地升高和降低，以及用于显示和操作游戏模拟站的部署或主动位置。游戏模拟站相互连接，使得游戏模拟站可以交互地执行诸如头对头竞争的软件程序应用。在展开位置，活动侧壁形成游戏模拟站休息的阶段。为了运输系统，侧壁被升高到用于运输的直立或运输位置。在运输过程中，游戏模拟站在水平的侧面位置保持附着在侧壁上。

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