Glenn C. Narvaez - Redwood City CA Shaw Wei Lee - Cupertino CA
Assignee:
National Semiconductor Corporation - Santa Clara CA
International Classification:
H01L 2302
US Classification:
257678, 257783, 438106
Abstract:
A number of techniques and substrate arrangements are described that working individually and in common have been found to significantly improve the environmental resistance of the resulting package. In one aspect, conductive pads (referred to herein as landing pads) on the top surface of a substrate are slightly undercut. This permits molding material applied during later packaging to flow into the undercut regions to help improve adhesion between the substrate and the molding material. In another aspect, metallic die attach pads formed on the substrate are patterned to provide better adhesion between the substrate and a solder mask that covers the die attach pads. More specifically, the metallic die attach pads are patterned to have a number of opening defined therein that leave corresponding portions of the substrate exposed. In substrates where a solder mask is applied over the die attach pad, the openings permit the solder mask to adhere directly to the substrate panel in the openings thereby strengthening the attachment of the solder mask to the substrate. In still another aspect, elongated slots are provided in the solder mask such that the slots expose one or more rows of adjacent landing pads instead of simply the landing pads themselves.
Core-Crush Resistant Fabric And Prepreg For Fiber Reinforced Composite Sandwich Structures
A core crush resistant prepreg for use in making a fiber reinforced composite panel structure is provided. The prepreg comprises a woven fabric consisting essentially of carbon fiber tow strands impregnated with a hardenable polymeric resin composition. Typically the fabric has an areal weight of from about 180 to about 205 grams per square meter. The prepreg has an average fiber tow aspect ratio of less than about 15. 4, a prepreg thickness of at least about 0. 245 mm, and a prepreg openness of at least about 1. 2 percent but less than about 6. 0 percent. Preferably, the resin composition is predominantly viscous in nature and has a tan value of between 0. 9 and 2. 0 at an elevated temperature between 70Â C. and 140Â C. , and an average epoxy functionality of greater than 2.
Core-Crush Resistant Fabric And Prepreg For Fiber Reinforced Composite Sandwich Structures
A core crush resistant prepreg for use in making a fiber reinforced composite panel structure is provided. The prepreg comprises a woven fabric consisting essentially of carbon fiber tow strands impregnated with a hardenable polymeric resin composition. Typically the fabric has an areal weight of from about 180 to about 205 grams per square meter. The prepreg has an average fiber tow aspect ratio of less than about 15. 4, a prepreg thickness of at least about 0. 245 mm, and a prepreg openness of at least about 1. 2 percent but less than about 6. 0 percent. Preferably, the resin composition is predominantly viscous in nature and has a tan value of between 0. 9 and 2. 0 at an elevated temperature between 70Â C. and 140Â C. , and an average epoxy functionality of greater than 2.
Solder Pad Configuration For Use In A Micro-Array Integrated Circuit Package
Jaime A. Bayan - Palo Alto CA, US Ashok S. Prabhu - San Jose CA, US Shaw Wei Lee - Cupertino CA, US
Assignee:
National Semiconductor Corporation - Santa Clara CA
International Classification:
H01L 23/495 H01L 23/04
US Classification:
257676, 257698, 257E23037
Abstract:
A solder pad configuration for use in an IC package is described. Various embodiments of the invention describe IC packages, lead-frames, or substrate panels configured with generally noncircular solder pads at their bottom surfaces. The noncircular shapes allow for greater surface area than circular solder pads having diameters equal to a major dimension of the noncircular shapes, while maintaining the same metal-to-metal clearance between the pads and adjacent leads. This increased surface area provides for stronger and more reliable solder joints.
Core-Crush Resistant Fabric And Prepreg For Fiber Reinforced Composite Sandwich Structures
Hao-Ming Hsiao - San Ramon CA Shaw Ming Lee - Danville CA Robert Albert Buyny - Clayton CA Cary Joseph Martin - Dublin CA
Assignee:
Hexcel Corporation - Pleasanton CA
International Classification:
B32B 502
US Classification:
428219
Abstract:
A core crush resistant prepreg for use in making a fiber reinforced composite panel structure is provided. The prepreg comprises a woven fabric consisting essentially of carbon fiber tow strands impregnated with a hardenable polymeric resin composition. Typically the fabric has an areal weight of from about 180 to about 205 grams per square meter. The prepreg has an average fiber tow aspect ratio of less than about 15. 4, a prepreg thickness of at least about 0. 245 mm, and a prepreg openness of at least about 1. 2 percent but less than about 6. 0 percent. Preferably, the resin composition is predominantly viscous in nature and has a tan. delta. value of between 0. 9 and 2. 0 at an elevated temperature between 70. degree. C. and 140. degree. C. , and an average epoxy functionality of greater than 2. A method for evaluating core crush resistance properties of a prepreg is also provided.