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1. 发明申请

US20050260033A1 Fastener assembly for attaching a non-metal component to a metal component 有权
标题翻译：用于将非金属部件附接到金属部件的紧固件组件
公开(公告)号：US20050260033A1
公开(公告)日：2005-11-24
申请号：US10850253
申请日：2004-05-20
申请人： Jaime Arbona , Donald Peters , Robert Miller
发明人： Jaime Arbona , Donald Peters , Robert Miller
IPC分类号： F01D25/24 , B62D29/04 , F02C7/00 , F02C7/20 , F02K1/12 , F16B1/00 , F16B5/02 , F16B35/06 , F16B37/04
CPC分类号： F16B35/06 , B62D29/048 , F16B5/0241 , F16B37/045 , F16B2001/0085 , F16B2200/30 , Y10T29/49947 , Y10T29/49948 , Y10T403/75
摘要： A fastener assembly for attaching components of dissimilar materials includes a fastener having a base portion and a protruding portion, and a mechanism for tightening the assembly. The base portion is shaped to be complementary for mating with an attachment feature formed within the non-metal component such that the base portion is retained within the non-metal component. The protruding portion including a base end and a distal end with the distal end including a threaded portion. The fastener assembly allows attachment of components fabricated from dissimilar materials without forming through holes in one of the components. Additionally, the fastener assembly compensates for differences in thermal expansion rates between the non-metal component and the metal component while providing a tight attachment therebetween.
摘要翻译：用于安装不同材料的部件的紧固件组件包括具有基部和突出部分的紧固件以及用于紧固组件的机构。基部被成形为互补以与非金属部件中形成的附接特征配合，使得基部保持在非金属部件内。所述突出部分包括基端和远端，所述远端包括螺纹部分。紧固件组件允许由不同材料制成的部件的附接，而不在其中一个部件中形成通孔。此外，紧固件组件补偿非金属部件和金属部件之间的热膨胀率的差异，同时在其间提供紧密的连接。

2. 发明申请

US20060213198A1 Reduced radar cross section exhaust nozzle assembly 有权
公开(公告)号：US20060213198A1
公开(公告)日：2006-09-28
申请号：US11091120
申请日：2005-03-28
申请人： Jaime Arbona , Meggan Harris , James Allore , Steven Laporte
发明人： Jaime Arbona , Meggan Harris , James Allore , Steven Laporte
IPC分类号： F02K1/06
CPC分类号： F02K1/1207 , F02K1/805
摘要： An exhaust nozzle assembly includes a plurality of interfitting flap assemblies that are moveable between a maximum area ratio and a minimum area ratio. Each of the pluralities of flap assemblies includes a slot and a wing. The wing fits within an adjacent slot of an adjacent flap assembly. Each of the flap assemblies includes a divergent element that provides a specific geometric shape forming the trailing edge surfaces. The flap element is attached to the divergent element and extends to a static structure. The flap element and the divergent element combine to form a continuous faceted outer surface of the exhaust nozzle assembly substantially void of gaps throughout the range of motion between the maximum and minimum area ratios.

3. 发明申请

US20070220735A1 Fastener assembly for attaching a non-metal component to a metal component 有权
公开(公告)号：US20070220735A1
公开(公告)日：2007-09-27
申请号：US11644363
申请日：2006-12-22
申请人： Jaime Arbona , Donald Peters , Robert Miller
发明人： Jaime Arbona , Donald Peters , Robert Miller
IPC分类号： B23P11/00 , B23P17/00
CPC分类号： F16B35/06 , B62D29/048 , F16B5/0241 , F16B37/045 , F16B2001/0085 , F16B2200/30 , Y10T29/49947 , Y10T29/49948 , Y10T403/75
摘要： A fastener assembly for attaching components of dissimilar materials includes a fastener having a base portion and a protruding portion, and a mechanism for tightening the assembly. The base portion is shaped to be complementary for mating with an attachment feature formed within the non-metal component such that the base portion is retained within the non-metal component. The protruding portion including a base end and a distal end with the distal end including a threaded portion. The fastener assembly allows attachment of components fabricated from dissimilar materials without forming through holes in one of the components. Additionally, the fastener assembly compensates for differences in thermal expansion rates between the non-metal component and the metal component while providing a tight attachment therebetween.

4. 发明申请

US20050260034A1 Fastener assembly for attaching a non-metal component to a metal component 有权
标题翻译：用于将非金属部件附接到金属部件的紧固件组件
公开(公告)号：US20050260034A1
公开(公告)日：2005-11-24
申请号：US10850257
申请日：2004-05-20
申请人： Jaime Arbona
发明人： Jaime Arbona
IPC分类号： F01D25/24 , B62D29/04 , F02C7/20 , F02K1/12 , F16B1/00 , F16B5/02 , F16B35/06 , F16B37/04 , F16B39/24
CPC分类号： F16B5/0241 , B62D29/048 , F16B35/06 , F16B37/045 , F16B2001/0085 , Y10T403/21 , Y10T403/217 , Y10T403/75
摘要： A fastener assembly for attaching components of dissimilar material includes a fastener, a spacer, and a mechanism for tightening the assembly. The spacer compensates for differences in thermal expansion rates between the non-metal component and the metal component while providing a tight attachment therebetween. An opening formed within the metal component is an elongated slot that accommodates the body portion of the fastener passing therethrough with the spacer and allows relative movement between the non-metal component and the metal component.
摘要翻译：用于连接不同材料的部件的紧固件组件包括紧固件，间隔件和用于紧固组件的机构。间隔件补偿非金属部件和金属部件之间的热膨胀率的差异，同时在其间提供紧密的连接。形成在金属部件内的开口是细长的槽，其容纳通过其间隔件的紧固件的主体部分，并且允许非金属部件和金属部件之间的相对移动。

5. 发明申请

US20050257529A1 Divergent flap for a gas turbine engine 有权
标题翻译：燃气涡轮发动机的不同翼片
公开(公告)号：US20050257529A1
公开(公告)日：2005-11-24
申请号：US10850252
申请日：2004-05-20
申请人： Jaime Arbona
发明人： Jaime Arbona
IPC分类号： F02C7/00 , F02K1/12 , F02K1/54 , F02K1/58 , F02K1/80 , F02K1/82
CPC分类号： F02K1/54 , F02K1/12 , F02K1/805 , F02K1/822 , F05D2300/21 , F05D2300/603 , Y02T50/672 , Y02T50/675
摘要： A divergent flap assembly of a gas turbine engine includes a hotsheet, a backbone structure for supporting the hotsheet, and a plow portion secured to the backbone structure to bridge a gap between the hotsheet and an external flap. The plow portion is fabricated from CMC material and has external geometry to complement and substantially continue geometry of the external flap to minimize plane detection. The plow portion is attached to the backbone structure such that when the backbone structure thermally expands, the plow portion is shifted to minimize an offset between a trailing edge of the hotsheet and the plow portion. The plow portion is fastened to the backbone structure by a plurality of fasteners, which are arranged to minimize thermal stresses.
摘要翻译：燃气涡轮发动机的发散板组件包括热表，用于支撑热表的主骨架结构，以及固定到主骨架结构上的犁部，用于桥接热板和外板之间的间隙。犁部分由CMC材料制成并具有外部几何形状以补充和基本上继续外部翼片的几何形状，以最小化平面检测。犁部分连接到骨架结构，使得当主骨架结构热膨胀时，犁部分移动以最小化热轧板的后缘和犁部之间的偏移。犁部分通过多个紧固件紧固到主体结构，这些紧固件被布置成最小化热应力。

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