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11. 发明授权

US08294316B2 Electrical power generation apparatus for contra-rotating open-rotor aircraft propulsion system 有权
标题翻译：用于反旋转开放式飞机推进系统的发电装置
公开(公告)号：US08294316B2
公开(公告)日：2012-10-23
申请号：US12572342
申请日：2009-10-02
申请人： Mark J. Blackwelder , John Timothy Alt , Steven Gagne , Daniel Kent Vetters
发明人： Mark J. Blackwelder , John Timothy Alt , Steven Gagne , Daniel Kent Vetters
IPC分类号： H02K23/60
CPC分类号： H02K7/1823 , B64C11/48 , B64D15/12 , B64D2027/005 , B64D2027/026 , F02K3/072 , F05D2220/768 , Y02T50/66 , Y02T50/671
摘要： An electrical power generation apparatus is embedded in a contra-rotating propulsion system that includes overlapping first and second shafts operatively connected for counter-rotation about a common axis. The electrical power generation apparatus includes a winding mounted to one of the shafts and a field array mounted to the other of the shafts adjacent to the winding. Relative rotation of the winding and the field array induces electrical current in the winding.
摘要翻译：一个发电装置被嵌入在反向转动的推进系统中，该推进系统包括重叠的第一和第二轴，该第一和第二轴可操作地连接以围绕公共轴线反向旋转。发电装置包括安装到一个轴上的绕组和安装到与绕组相邻的另一个轴的场阵列。绕组和场阵列的相对旋转引起绕组中的电流。

12. 发明申请

US20110155859A1 AIRCRAFT VERTICAL LIFT DEVICE 有权
标题翻译：飞机垂直提升装置
公开(公告)号：US20110155859A1
公开(公告)日：2011-06-30
申请号：US12980420
申请日：2010-12-29
申请人： Daniel Kent Vetters , Andrew Barlow
发明人： Daniel Kent Vetters , Andrew Barlow
IPC分类号： B64C39/00 , B64C29/00
CPC分类号： B64C29/0025
摘要： A lift device is disclosed that can be used to provide vertical lift to an aircraft or other vehicle. The lift device can include a fan that produces an airflow and a vane box that can direct the airflow. In one form the fan can be oriented at an angle relative to a reference plane in the aircraft. In another form the vane box can be oriented at an angle. The vane box can be structured to provide a maximum flow area between an aft flow vector and a forward flow vector.
摘要翻译：公开了可用于向飞行器或其他车辆提供垂直升降的升降装置。提升装置可以包括产生气流的风扇和可引导气流的叶片盒。在一种形式中，风扇可以相对于飞行器中的参考平面成一定角度定向。在另一种形式中，叶片箱可以以一定角度定向。叶片箱可以被构造成在后向流矢量和向前流动矢量之间提供最大流动面积。

13. 发明申请

US20090175716A1 Integrated bypass engine structure 有权
标题翻译：集成旁路引擎结构
公开(公告)号：US20090175716A1
公开(公告)日：2009-07-09
申请号：US12006980
申请日：2008-01-08
申请人： Daniel Kent Vetters
发明人： Daniel Kent Vetters
IPC分类号： F02C9/16 , F04D29/52
CPC分类号： F04D29/52 , F01D25/24 , F02K3/04
摘要： One form of the present invention contemplates an apparatus comprising a gas turbine engine core, a gearbox accessory mounted to the engine core and substantially enclosed by an inner fairing; a nacelle having a plurality of panels, wherein the nacelle panels substantially enclose and overlap at least a portion of the inner fairing; and a bypass duct defined between an exterior surface of the inner fairing and an interior surface of at least some of the nacelle panels.
摘要翻译：本发明的一种形式涉及一种装置，包括燃气涡轮发动机芯，安装在发动机芯上的齿轮箱附件，并基本上由内部整流罩包围; 具有多个面板的机舱，其中所述机舱面板基本上包围并与所述内部整流罩的至少一部分重叠; 以及限定在内部整流罩的外表面与至少一些机舱面板的内表面之间的旁路管道。

14. 发明申请

US20170044921A1 FLEXIBLY MOUNTED CERAMIC MATRIX COMPOSITE SEAL SEGMENTS 审中-公开
标题翻译：柔性安装陶瓷基体复合密封件
公开(公告)号：US20170044921A1
公开(公告)日：2017-02-16
申请号：US14721684
申请日：2015-05-26
申请人： Daniel Kent Vetters , Todd Engel , Matt Brandt
发明人： Daniel Kent Vetters , Todd Engel , Matt Brandt
IPC分类号： F01D11/12 , F01D25/24
CPC分类号： F01D11/12 , F01D9/04 , F01D25/246 , F05D2220/32 , F05D2240/11 , F05D2260/30 , F05D2300/6033
摘要： A segmented turbine shroud for radially encasing a turbine in a gas turbine engine comprises a carrier comprising a flange; a ceramic matrix composite (CMC) seal segment comprising a portion defining a pin-receiving bore; an elongated pin extending through the pin-receiving bore; a bushing surrounding the elongated pin within the bore; and a flexible mounting member, the flexible mounting member being connected to the bushing and the carrier flange to thereby flexibly mount the CMC seal segment to the carrier.
摘要翻译：用于在燃气涡轮发动机中径向包围涡轮机的分段涡轮机罩包括：载体，其包括凸缘; 陶瓷基体复合材料（CMC）密封段，其包括限定销接收孔的部分; 延伸穿过销接收孔的细长销; 围绕孔内的细长销的衬套; 以及柔性安装构件，所述柔性安装构件连接到所述衬套和所述载体凸缘，从而将所述CMC密封段柔性地安装到所述载体上。

15. 发明申请

US20170044920A1 TURBINE SHROUD HAVING CERAMIC MATRIX COMPOSITE SEAL SEGMENT 审中-公开
标题翻译：具有陶瓷基体复合材料密封部分的涡轮机
公开(公告)号：US20170044920A1
公开(公告)日：2017-02-16
申请号：US14721651
申请日：2015-05-26
申请人： Daniel Kent Vetters , David J. Thomas , Douglas David Dierksmeier , Jun Shi , Todd Engel
发明人： Daniel Kent Vetters , David J. Thomas , Douglas David Dierksmeier , Jun Shi , Todd Engel
IPC分类号： F01D11/12 , F01D9/02
CPC分类号： F01D11/12 , F01D9/02 , F01D25/246 , F05D2220/32 , F05D2240/11 , F05D2250/15 , F05D2260/30 , F05D2260/38 , F05D2260/941 , F05D2300/6033
摘要： A segmented turbine shroud for radially encasing a rotatable turbine in a gas turbine engine comprising a carrier, a ceramic matrix composite (CMC) seal segment, and an elongated pin. The carrier defines a pin-receiving carrier bore and the CMC seal segment defines a pin-receiving seal segment bore. The elongated pin extends through the carrier bore and the seal segment bore. The pin-receiving carrier bore includes a cantilevered member such that the carrier bore has a length sufficient to effect radial flexion between the carrier bore and the pin received within the carrier bore during operation of the turbine.
摘要翻译：一种用于在包括载体，陶瓷基体复合（CMC）密封段和细长销）的燃气涡轮发动机中径向包围可旋转涡轮机的分段涡轮机罩。载体限定销接收载体孔，CMC密封段限定销接收密封部分孔。细长销延伸穿过承载孔和密封段孔。销接收载体孔包括悬臂构件，使得载体孔的长度足以在涡轮机的运行期间在承载孔和承载孔内的销之间实现径向弯曲。

16. 发明申请

US20160348528A1 CERAMIC MATRIX COMPOSITE SEAL SEGMENT FOR A GAS TURBINE ENGINE 有权
标题翻译：陶瓷基体复合材料密封段用于气体涡轮发动机
公开(公告)号：US20160348528A1
公开(公告)日：2016-12-01
申请号：US14721705
申请日：2015-05-26
申请人： Daniel Kent Vetters , David J. Thomas , Ted Freeman , Douglas David Dierksmeier , Jun Shi , Todd Engel
发明人： Daniel Kent Vetters , David J. Thomas , Ted Freeman , Douglas David Dierksmeier , Jun Shi , Todd Engel
IPC分类号： F01D11/08 , F01D25/24
CPC分类号： F01D11/08 , F01D9/04 , F01D25/24 , F01D25/246 , F05D2220/32 , F05D2240/24 , F05D2300/6033
摘要： A ceramic matrix composite (CMC) seal segment for use in a segmented turbine shroud for radially encasing a turbine in a gas turbine engine. The CMC seal segment comprises an arcuate flange having a surface facing the turbine and a portion defining a bore for receiving an elongated pin, with the bore having a length that is at least 70% of the length of the elongated pin received therein. The CMC seal segment is carried by the carrier by at least one of the elongated pins being received within the bore. The CMC seal segment portion defining a pin-receiving bore is radially spaced from the arcuate flange by a spacing flange extending radially outward from the arcuate flange.
摘要翻译：一种陶瓷基体复合材料（CMC）密封段，用于分段涡轮机罩，用于在燃气涡轮发动机中径向包围涡轮机。 CMC密封段包括具有面向涡轮的表面的弧形凸缘和限定用于接收细长销的孔的部分，孔的长度为其中接收的细长销的长度的至少70％。 CMC密封段由载体承载，其中至少一个细长销被接收在孔内。限定销接收孔的CMC密封段部分通过从弧形凸缘径向向外延伸的间隔凸缘与弓形凸缘径向间隔开。

17. 发明授权

US08215895B2 Vapor phase lubrication system 有权
标题翻译：气相润滑系统
公开(公告)号：US08215895B2
公开(公告)日：2012-07-10
申请号：US12041034
申请日：2008-03-03
申请人： Mark S. Henry , Daniel Kent Vetters
发明人： Mark S. Henry , Daniel Kent Vetters
IPC分类号： F04D27/02
CPC分类号： F01D9/065 , F01D25/162 , F01D25/18
摘要： Embodiments of the present invention include a method and system for carrying out vapor-phase lubrication of a component, such as a bearing for example. The method and apparatus can be applied to a turbine engine. The method includes the step of directing a first stream of fluid containing atomized lubricant to the component at a first velocity. The system provides a first fluid injection system configured to perform the first step. The method also includes the step of directing a second stream of fluid at a second velocity less than the first velocity to the component. The second stream is for controlling a temperature of the component. The system provides a second fluid injection system configured to perform the second step. Both of the directing steps are carried out concurrently.
摘要翻译：本发明的实施例包括用于对诸如轴承的部件进行气相润滑的方法和系统。该方法和装置可以应用于涡轮发动机。该方法包括以第一速度将含有雾化润滑剂的第一流体流引导到部件的步骤。该系统提供配置成执行第一步骤的第一流体注入系统。该方法还包括以低于第一速度的第二速度将第二流体流引向部件的步骤。第二流用于控制部件的温度。该系统提供配置成执行第二步骤的第二流体注射系统。两个指导步骤同时进行。

18. 发明申请

US20120167550A1 THRUST AUGMENTED GAS TURBINE ENGINE 审中-公开
标题翻译：悍马燃气涡轮发动机
公开(公告)号：US20120167550A1
公开(公告)日：2012-07-05
申请号：US13337993
申请日：2011-12-27
申请人： Victor Lewis Oechsle , Andrew James Elfert , Daniel Kent Vetters , Bradley Eugene Auker
发明人： Victor Lewis Oechsle , Andrew James Elfert , Daniel Kent Vetters , Bradley Eugene Auker
IPC分类号： F02K3/02 , F02K1/36
CPC分类号： F02K3/10 , F23R3/20
摘要： One embodiment of the present invention is a unique thrust augmented gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for thrust augmented gas turbine engines. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
摘要翻译：本发明的一个实施例是独特的推力增强燃气涡轮发动机。其他实施例包括用于推力增强燃气涡轮发动机的装置，系统，装置，硬件，方法和组合。本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。

19. 发明申请

US20110171012A1 ROTATING MACHINERY WITH DAMPING SYSTEM 有权
标题翻译：旋转机械与阻尼系统
公开(公告)号：US20110171012A1
公开(公告)日：2011-07-14
申请号：US12904730
申请日：2010-10-14
申请人： Daniel Kent Vetters , Timothy Hoffmann , Steven Arlen Klusman
发明人： Daniel Kent Vetters , Timothy Hoffmann , Steven Arlen Klusman
IPC分类号： F01D25/00
CPC分类号： F01D25/164 , F01D5/26 , F01D25/04 , F05D2240/50 , F05D2240/55 , F05D2260/96 , F16C19/06 , F16C19/14 , F16C27/045 , F16C33/60 , F16C35/077 , F16C2360/23
摘要： One embodiment of the present invention is a damping system for rotating machinery such as gas turbine engines. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for damping systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.
摘要翻译：本发明的一个实施例是用于旋转诸如燃气涡轮发动机的机械的阻尼系统。其他实施例包括用于阻尼系统的装置，系统，装置，硬件，方法和组合。本申请的其他实施例，形式，特征，方面，益处和优点将从本文提供的描述和图中变得显而易见。

20. 发明授权

US07842375B2 Fiber retention system for metal matrix composite preform 有权
标题翻译：金属基复合材料预制件的纤维保留系统
公开(公告)号：US07842375B2
公开(公告)日：2010-11-30
申请号：US11131168
申请日：2005-05-17
申请人： Daniel Kent Vetters
发明人： Daniel Kent Vetters
IPC分类号： B32B3/00 , B32B15/14 , B64C11/16
CPC分类号： C22C47/20 , B22F2999/00 , Y10T428/24479 , Y10T428/2457 , Y10T428/24612 , Y10T428/249927 , B22F3/15
摘要： A metal matrix composite preform including an angled curved groove in the surface of the matrix material. A reinforcing fiber is placed within the angled curved groove and the stiffness of the fiber causes it to be pressed against an outer wall member defining the groove. The fiber is retained within the metal matrix composite preform prior to hot isostatic pressing.
摘要翻译：一种金属基质复合预制件，其在基体材料的表面中包括成角度的弯曲凹槽。增强纤维被放置在成角度的弯曲槽内，并且纤维的刚度使其被压靠在限定凹槽的外壁构件上。在热等静压之前，纤维保留在金属基复合材料预制件内。

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