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1. 发明申请

US20090205738A1 INSULATED ARTICLE AND METHOD OF MAKING SAME 有权
标题翻译：绝缘制品及其制造方法
公开(公告)号：US20090205738A1
公开(公告)日：2009-08-20
申请号：US12433244
申请日：2009-04-30
申请人： Jason Todd HERBORTH , Vittorio Bruno
发明人： Jason Todd HERBORTH , Vittorio Bruno
IPC分类号： F16L9/14
CPC分类号： F16L57/04 , B29C53/58 , B29C63/10 , B29D23/001 , B29K2105/0827 , B29K2305/02 , B29K2305/10 , B29K2305/12 , B29K2995/0015 , D04C1/02 , F01D25/18 , F02C7/24 , F16L59/145
摘要： A tube is thermally insulated for protecting a fluid flowing therethrough from a high temperature surrounding environment of a gas turbine engine. The tube comprises a conduit, an insulating layer wrapped around the conduit, and an elongated contractible braided sleeve for preventing a separation of the insulating layer from the rigid conduit. The contractible braided sleeve is flexible along a longitudinal axis thereof and removably pulled over the insulating layer to snugly surround and maintain the insulating layer around the conduit.
摘要翻译：管是热绝缘的，用于保护从燃气涡轮发动机的高温周围环境流过的流体。管包括导管，围绕导管缠绕的绝缘层，以及用于防止绝缘层与刚性导管分离的细长收缩编织套管。可收缩的编织套筒沿其纵向轴线是柔性的，并且可移除地拉过绝缘层，以紧密地围绕和保持导管周围的绝缘层。

2. 发明授权

US07532969B2 Gas turbine speed detection 有权
标题翻译：燃气轮机速度检测
公开(公告)号：US07532969B2
公开(公告)日：2009-05-12
申请号：US11370830
申请日：2006-03-09
申请人： Vittorio Bruno , Francis Bonacorsi
发明人： Vittorio Bruno , Francis Bonacorsi
IPC分类号： G06F19/00
CPC分类号： F02C7/32 , F01D17/06 , F01D25/20
摘要： A gas turbine engine having at least a rotor shaft operatively connecting a compressor apparatus and a turbine apparatus, comprises an auxiliary gear box and a phonic wheel apparatus. The auxiliary gear box is drivingly connected to the rotor shaft and the phonic wheel apparatus includes an oil pump having toothed gear and a sensor mounted to the oil pump for sensing a rotational speed of the toothed gear.
摘要翻译：具有可操作地连接压缩机装置和涡轮机装置的至少一个转子轴的燃气涡轮发动机包括辅助齿轮箱和声轮装置。辅助齿轮箱驱动地连接到转子轴，并且声轮设备包括具有齿轮的油泵和安装到油泵的传感器，用于感测齿轮的转速。

3. 发明授权

US07377100B2 Bypass duct fluid cooler 有权
标题翻译：旁路管道流体冷却器
公开(公告)号：US07377100B2
公开(公告)日：2008-05-27
申请号：US10926967
申请日：2004-08-27
申请人： Vittorio Bruno , Bryan Olver , John Adam Logan
发明人： Vittorio Bruno , Bryan Olver , John Adam Logan
IPC分类号： F02K3/00 , F02C7/12
CPC分类号： F02K3/06 , F01D25/12 , F01D25/18 , F02C7/14 , F02K3/04 , F02K3/115 , Y02T50/671 , Y02T50/675
摘要： A method and apparatus for cooling a fluid in a bypass gas turbine engine involves directing the fluid to the bypass duct of the engine to allow for heat exchange from the fluid to bypass air passing through the bypass air duct.
摘要翻译：用于冷却旁路燃气涡轮发动机中的流体的方法和装置包括将流体引导到发动机的旁路管道，以允许来自流体的热交换以绕过通过旁路空气管道的空气。

4. 发明申请

US20080063333A1 Integral tandem bearing for high speed flexible shafts 有权
标题翻译：用于高速柔性轴的整体串联轴承
公开(公告)号：US20080063333A1
公开(公告)日：2008-03-13
申请号：US11530088
申请日：2006-09-08
申请人： Vittorio Bruno , Edward Dusza , Michel Labbe , Tibor Urac
发明人： Vittorio Bruno , Edward Dusza , Michel Labbe , Tibor Urac
IPC分类号： F16C19/49
CPC分类号： F16C19/49 , F01D25/16 , F01D25/164 , F16C19/54 , F16C35/061 , F16C2360/23
摘要： An integral tandem bearing assembly for supporting a main shaft in a gas turbine engine is provided. The tandem bearing assembly comprises two bearing assemblies connected by integrated inner ring.
摘要翻译：提供一种用于支撑燃气涡轮发动机中的主轴的整体式串联轴承组件。串联轴承组件包括通过集成内圈连接的两个轴承组件。

5. 发明申请

US20070114055A1 Insulated article and method of making same 有权
标题翻译：绝缘制品及其制作方法
公开(公告)号：US20070114055A1
公开(公告)日：2007-05-24
申请号：US11283838
申请日：2005-11-22
申请人： Jason Herborth , Vittorio Bruno
发明人： Jason Herborth , Vittorio Bruno
IPC分类号： H02G3/04
CPC分类号： F16L57/04 , B29C53/58 , B29C63/10 , B29D23/001 , B29K2105/0827 , B29K2305/02 , B29K2305/10 , B29K2305/12 , B29K2995/0015 , D04C1/02 , F01D25/18 , F02C7/24 , F16L59/145
摘要： A method of insulating an article comprising: surrounding at least a portion of the article with an insulating layer, inserting the article portion surrounded by the insulating layer into an outer protective sleeve, and shrinking the outer protective sleeve around the insulating layer.
摘要翻译：一种制品的绝缘方法，包括：用绝缘层包围所述制品的至少一部分，将由所述绝缘层包围的所述制品部分插入到外保护套中，以及使所述外保护套围绕所述绝缘层收缩。

6. 发明授权

US07013651B2 Compact quick attach starter-generator installation 有权
标题翻译：紧凑型快速起动发电机安装
公开(公告)号：US07013651B2
公开(公告)日：2006-03-21
申请号：US11024496
申请日：2004-12-30
申请人： Vittorio Bruno , Bryan Olver
发明人： Vittorio Bruno , Bryan Olver
IPC分类号： F02C7/18 , F02C7/268
CPC分类号： F02C7/32 , F05D2260/39 , H02K5/20 , H02K7/1823
摘要： A mounting system for mounting an air-cooled device to a mount, the device having a mounting flange and a cooling air outlet radially inward of an outer periphery of the device, the mounting flange adapted to cooperate with the mount, where the mounting system has a cooling air exhaust collection shroud adapted to surround the device and at least a portion of the mount, the shroud having a discharge outlet.
摘要翻译：一种用于将空气冷却装置安装到安装件的安装系统，该装置具有安装凸缘和设备外周径向向内的冷却空气出口，该安装凸缘适于与安装件配合，其中安装系统具有适于围绕所述装置和所述安装件的至少一部分的冷却空气排气收集罩，所述护罩具有排放出口。

7. 发明申请

US20060042225A1 Bypass duct fluid cooler 有权
标题翻译：旁路管道流体冷却器
公开(公告)号：US20060042225A1
公开(公告)日：2006-03-02
申请号：US10926967
申请日：2004-08-27
申请人： Vittorio Bruno , Bryan Olver , John Logan
发明人： Vittorio Bruno , Bryan Olver , John Logan
IPC分类号： F02K3/02
CPC分类号： F02K3/06 , F01D25/12 , F01D25/18 , F02C7/14 , F02K3/04 , F02K3/115 , Y02T50/671 , Y02T50/675
摘要： A method and apparatus for cooling a fluid in a bypass gas turbine engine involves directing the fluid to the bypass duct of the engine to allow for heat exchange from the fluid to bypass air passing through the bypass air duct.
摘要翻译：用于冷却旁路燃气涡轮发动机中的流体的方法和装置包括将流体引导到发动机的旁路管道，以允许来自流体的热交换以绕过通过旁路空气管道的空气。

8. 发明申请

US20050244272A1 ROTOR BALANCING DEVICE AND METHOD 有权
标题翻译：转子平衡装置及方法
公开(公告)号：US20050244272A1
公开(公告)日：2005-11-03
申请号：US10683358
申请日：2003-10-14
申请人： Vittorio Bruno , Jason Fish
发明人： Vittorio Bruno , Jason Fish
IPC分类号： F01D5/02 , F01D5/10 , F01D25/18 , F16F15/28
CPC分类号： F16F15/28 , F01D5/027 , F01D5/10 , F01D25/18 , F16C19/26 , F16C33/6677 , Y10T74/2117 , Y10T74/2122 , Y10T74/2127
摘要： The present invention includes a rotor assembly comprising a shaft, a first component coaxially attached to the shaft for performing a first function in the rotor assembly and acting as a first counterbalance weight, and a second component coaxially attached to the shaft for performing a second function in the rotor assembly and acting as a second counterbalance weight, whereby the first and second counterbalance weights combine to balance the rotor assembly. The present invention also includes a method of balancing a rotor assembly having a shaft and a residual imbalance, the method comprising the steps of coaxially attaching a first component performing a first function and having a first counterbalance weight integral therewith onto the shaft, and coaxially attaching a second component performing a second function and having a second counterbalance weight integral therewith onto the shaft, so that the first and second components counter the residual imbalance.
摘要翻译：本发明包括转子组件，其包括轴，第一部件，其同轴地附接到轴，用于在转子组件中执行第一功能并且用作第一平衡重量;以及第二部件，其同轴地附接到轴以执行第二功能在转子组件中并用作第二平衡重，由此第一和第二平衡重组合起来以平衡转子组件。本发明还包括平衡具有轴的转子组件和残余不平衡的方法，所述方法包括以下步骤：将执行第一功能的第一部件同轴地附接并且具有与所述轴一体的第一平衡重量并同轴地附接第二部件执行第二功能并且具有与所述轴成一体的第二平衡重量，使得所述第一和第二部件抵消所述残余不平衡。

9. 发明申请

US20050155341A1 Axisymmetric flap on gas turbine exhaust centerbody 有权
标题翻译：燃气轮机排气中心体轴对称翼片
公开(公告)号：US20050155341A1
公开(公告)日：2005-07-21
申请号：US10759015
申请日：2004-01-20
申请人： Patrick Germain , Vittorio Bruno
发明人： Patrick Germain , Vittorio Bruno
IPC分类号： F02C3/32 , F02K1/36 , F02K1/00
CPC分类号： F02K1/36 , F02C3/32
摘要： The present invention includes a gas turbine engine exhaust centerbody comprising a forward portion having at least one flap at a downstream end thereof to induce a local low pressure zone in the exhaust gas flow without significantly impeding it, a tailcone partially inserted into the forward portion so that at least part of the at least one flap overlaps a portion of the tailcone, a centerbody cavity containing gas at a pressure higher than the local low pressure, and at least one opening between the forward portion and the tailcone adjacent to and upstream of one of the local low pressure zones and providing fluid communication between the cavity and the exhaust gas flow. A ventilation flow out of the centerbody cavity through each opening is induced by a positive difference between the pressure of the gas in the centerbody cavity and the low pressure of the adjacent zone.
摘要翻译：本发明包括燃气涡轮发动机排气中心体，其包括在其下游端具有至少一个翼片的前部，以在排气流中引起局部低压区而不显着阻碍其，部分地插入到前部中的尾巴所述至少一个翼片的至少一部分与所述尾骨的一部分重叠，包含在高于所述局部低压力的压力下的气体的中心体腔，以及在所述前端部分与所述尾部之间的至少一个开口，的局部低压区，并且在空腔和废气流之间提供流体连通。通过每个开口的中心体腔内的通风流由中心体腔中的气体压力与相邻区域的低压之间的正差异引起。

10. 发明授权

US07156618B2 Low cost diffuser assembly for gas turbine engine 有权
标题翻译：燃气涡轮发动机的低成本扩散器组件
公开(公告)号：US07156618B2
公开(公告)日：2007-01-02
申请号：US10989311
申请日：2004-11-17
申请人： Jason Araan Fish , Vittorio Bruno , Kenneth Parkman
发明人： Jason Araan Fish , Vittorio Bruno , Kenneth Parkman
IPC分类号： F04D29/44
CPC分类号： F04D29/441 , F05B2240/12 , F05D2250/52
摘要： A gas turbine diffuser assembly and a method for assembling same, includes providing a loose fit between the diffuser body and the diffuser pipes. Damper members provide a snug attachment.
摘要翻译：燃气轮机扩散器组件及其组装方法包括在扩散器主体和扩散管之间提供松配合。阻尼器构件提供了舒适的附件。

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