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1. 发明授权

US07435055B2 Locking spacer assembly for a turbine engine 有权
标题翻译：用于涡轮发动机的锁定间隔件组件
公开(公告)号：US07435055B2
公开(公告)日：2008-10-14
申请号：US11093162
申请日：2005-03-29
申请人： Christian M. Hansen , Alfred P. Matheny , Brian Potter
发明人： Christian M. Hansen , Alfred P. Matheny , Brian Potter
IPC分类号： F01D5/32
CPC分类号： F01D5/32 , F01D5/3038
摘要： A locking spacer assembly for filling a void between adjacent components in a turbine engine. In at least one embodiment, the locking spacer assembly may be configured to be inserted between adjacent turbine blades in a disc groove in a turbine blade stage assembly. The locking spacer assembly may be formed from fore and aft end supports and a locking device having fore and aft angled surfaces for urging the fore and aft end supports into lateral recesses in the disc groove. The locking spacer assembly may also include a mid spacer positioned between the fore and aft end supports. A retainer may be attached to the locking device to draw the fore and aft angled surfaces of the locking device into contact with the fore and aft support surfaces and urge the first and second end supports into lateral recesses in the disc groove.
摘要翻译：一种用于填充涡轮发动机中的相邻部件之间的空隙的锁定间隔件组件。在至少一个实施例中，锁定间隔件组件可构造成在涡轮叶片级组件中的盘槽中插入相邻的涡轮叶片之间。锁定间隔件组件可以由前端支撑件和后端支撑件形成，并且锁定装置具有前后成角度的表面，用于将前端支撑件和后端支撑件推进到盘槽中的横向凹槽中。锁定间隔件组件还可以包括位于前端支撑件和后端支架之间的中间间隔件。保持器可以附接到锁定装置以拉动锁定装置的前后角度的表面与前后支撑表面接触并且将第一和第二端部支撑件推动到盘槽中的侧向凹部中。

2. 发明授权

US08128354B2 Gas turbine engine 有权
标题翻译：燃气轮机
公开(公告)号：US08128354B2
公开(公告)日：2012-03-06
申请号：US11654353
申请日：2007-01-17
申请人： Christian M. Hansen , Friedrich T. Rogers
发明人： Christian M. Hansen , Friedrich T. Rogers
IPC分类号： F01D1/04
CPC分类号： F01D9/044 , F01D5/225 , F01D25/246 , F04D29/542 , F04D29/644 , F05D2260/96
摘要： A gas turbine engine is provided comprising an outer casing and a plurality of circumferentially positioned vane segments. The outer casing is provided with a circumferential casing slot. The plurality of circumferentially positioned vane segments are coupled to the outer casing. Each vane segment comprises at least one vane airfoil, a radially inner shroud coupled to a first end of the airfoil, a radially outer shroud coupled to a second end of the airfoil, and a strongback fixedly coupled to axially spaced-apart portions of the outer shroud such that a gap is provided between the strongback and the outer shroud. The strongback may comprise axially spaced-apart first and second end portions received in the casing slot.
摘要翻译：提供一种燃气涡轮发动机，其包括外壳和多个周向定位的叶片段。外壳设有圆周壳体槽。多个周向定位的叶片段联接到外壳。每个叶片段包括至少一个叶片翼型件，联接到翼型件的第一端的径向内护罩，联接到翼型件的第二端的径向外护罩，以及固定地联接到外部的轴向间隔开的部分的强力护罩，使得在强弹和外护罩之间提供间隙。强力可以包括容纳在套管槽中的轴向间隔开的第一和第二端部。

3. 发明授权

US5704086A Passenger boarding bridge 失效
标题翻译：乘客登机桥
公开(公告)号：US5704086A
公开(公告)日：1998-01-06
申请号：US582053
申请日：1996-01-02
申请人： Christian M. Hansen , Kenneth John Stoddard
发明人： Christian M. Hansen , Kenneth John Stoddard
IPC分类号： B64F1/305 , E01D1/00
CPC分类号： B64F1/3055 , Y10T16/364 , Y10T16/376
摘要： Passenger boarding bridge extendable sections are provided with roller assemblies supporting one extendable bridge section relative to a second extendable bridge section wherein the roller assemblies assist in reducing the downward load in the overlapping area of the bridge sections.
摘要翻译：乘客登机桥可延伸部分设置有相对于第二可延伸桥接部分支撑一个可延伸的桥接部分的滚子组件，其中滚子组件有助于减小桥接部分的重叠区域中的向下的载荷。

4. 外观设计

USD347479S Bottle for a laboratory analyzer 失效
公开(公告)号：USD347479S
公开(公告)日：1994-05-31
申请号：US869344
申请日：1992-04-15
申请人： Christian M. Hansen , Robert C. Butcher, Jr. , Kevin D. Lear
设计人： Christian M. Hansen , Robert C. Butcher, Jr. , Kevin D. Lear

5. 发明申请

US20100266399A1 Gas turbine engine 有权
标题翻译：燃气轮机
公开(公告)号：US20100266399A1
公开(公告)日：2010-10-21
申请号：US11654353
申请日：2007-01-17
申请人： Christian M. Hansen , Friedrich T. Rogers
发明人： Christian M. Hansen , Friedrich T. Rogers
IPC分类号： F01D1/04 , F04D29/64 , F01D25/24
CPC分类号： F01D9/044 , F01D5/225 , F01D25/246 , F04D29/542 , F04D29/644 , F05D2260/96
摘要： A gas turbine engine is provided comprising an outer casing and a plurality of circumferentially positioned vane segments. The outer casing is provided with a circumferential casing slot. The plurality of circumferentially positioned vane segments are coupled to the outer casing. Each vane segment comprises at least one vane airfoil, a radially inner shroud coupled to a first end of the airfoil, a radially outer shroud coupled to a second end of the airfoil, and a strongback fixedly coupled to axially spaced-apart portions of the outer shroud such that a gap is provided between the strongback and the outer shroud. The strongback may comprise axially spaced-apart first and second end portions received in the casing slot.
摘要翻译：提供一种燃气涡轮发动机，其包括外壳和多个周向定位的叶片段。外壳设有圆周壳体槽。多个周向定位的叶片段联接到外壳。每个叶片段包括至少一个叶片翼型件，联接到翼型件的第一端的径向内护罩，联接到翼型件的第二端的径向外护罩，以及固定地联接到外部的轴向间隔开的部分的强力护罩，使得在强弹和外护罩之间提供间隙。强力可以包括容纳在套管槽中的轴向间隔开的第一和第二端部。

6. 外观设计

USD341204S Bottle for a laboratory analyzer 失效
公开(公告)号：USD341204S
公开(公告)日：1993-11-09
申请号：US784787
申请日：1991-10-30
申请人： Christian M. Hansen , Robert C. Butcher, Jr. , Kevin D. Lear
设计人： Christian M. Hansen , Robert C. Butcher, Jr. , Kevin D. Lear

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