公开(公告)号：USD639811S1

公开(公告)日：2011-06-14

申请号：US29364773

申请日：2010-06-28

Applicant: Steven Hwang ,  Christopher C. Jones

Designer： Steven Hwang ,  Christopher C. Jones

公开(公告)号：US20080142961A1

公开(公告)日：2008-06-19

申请号：US11611063

申请日：2006-12-14

Applicant: Christopher C. Jones ,  David Bach ,  Timothe Litt ,  Larry Binder ,  Kaladhar Radhakrishnan ,  Cengiz A. Palanduz

Inventor： Christopher C. Jones ,  David Bach ,  Timothe Litt ,  Larry Binder ,  Kaladhar Radhakrishnan ,  Cengiz A. Palanduz

IPC: H01L23/34

CPC classification number: H05K1/0231 ,  H01L25/0655 ,  H01L25/165 ,  H01L2224/16225 ,  H01L2224/16227 ,  H01L2224/16265 ,  H01L2924/1515 ,  H01L2924/15153 ,  H01L2924/15311 ,  H01L2924/19041 ,  H01L2924/19103 ,  H01L2924/19105 ,  H01L2924/3011 ,  H05K1/145 ,  H05K1/183 ,  H05K2201/10515 ,  H05K2201/10712 ,  H05K2201/10734

Abstract: A ceramic package substrate has a recess. This allows a device in that recess to be close to a die attached to the substrate's top side, for better performance. The device may be an array capacitor, an in-silicon voltage regulator, or another device or devices.

Abstract translation: 陶瓷封装基板具有凹部。 这使得该凹部中的器件靠近附接到衬底顶侧的管芯，以获得更好的性能。 该器件可以是阵列电容器，硅内电压调节器或其它器件。

公开(公告)号：US4891732A

公开(公告)日：1990-01-02

申请号：US126332

申请日：1987-11-30

Applicant: Christopher C. Jones

Inventor： Christopher C. Jones

IPC: B64D45/02 ,  F16B37/04

CPC classification number: F16B37/044 ,  B64D45/02

Abstract: A fastener for use with aircraft structures comprising composite materials has improved electrical characteristics designed to reduce damage by lightning strikes. The fastener comprises separate nut and bolt portions and a cage member (4, 1, 6). The nut (4) and the head portion of the bolt 1 both have beveled edges which in use are countersunk in the composite materials to enhance electrical contact between the fastener and aircraft structural members (2, 5). The nut (4) is captively mounted inside the cage member (6) and is moveable, within pre-determined limits, inside the cage (6) so that it may be axially aligned with and the bolt screwed therein, thus compensating for any initial non-aligment of the nut (4) and bolt (1) due to a complex shape of the aircraft structure necessitated by aerodynamic or other considerations.