Matthew M Morrison

Address:

8615 Autumn Rdg Ct, Louisville, KY 40242

VIN:

5GTEN13E988168374

Make:

HUMMER

Model:

H3

Year:

2008

US Patent:

8169783, May 1, 2012

Filed:

Mar 30, 2009

Appl. No.:

12/414158

Inventors:

Michael J. Phillips - Camp Hill PA, US
Michael E. Cowher - Harrisburg PA, US
Matthew David Morrison - Duncannon PA, US

Assignee:

Tyco Electronics Corporation - Berwyn PA

International Classification:

H05K 7/00

US Classification:

361728, 361747

Abstract:

A latch assembly for a pluggable electronic module matable with a receptacle assembly includes a lever actuatable between a latched position and an unlatched position, a yoke assembly operatively coupled to the lever, and a latch element coupled to the latch end of the yoke assembly. The yoke assembly has a latch end rotatable between a latched position and an unlatched position. The latch element is movable between an engaged position and an unengaged position as the latch end is rotated between the latched and unlatched positions, respectively. The latch element is configured to engage the receptacle assembly to lock the pluggable electronic module within the receptacle assembly when the latch element is in the engaged position.

US Patent:

8348681, Jan 8, 2013

Filed:

Apr 19, 2010

Appl. No.:

12/762968

Inventors:

Michael J. Phillips - Camp Hill PA, US
Michael E. Cowher - Harrisburg PA, US
Matthew D. Morrison - Halifax PA, US

Assignee:

Tyco Electronics Corporation - Berwyn PA

International Classification:

H01R 13/648

US Classification:

439 99

Abstract:

A cable assembly includes a housing having a mating end and a cable end and receives a cable through the cable end. The housing has a mounting block proximate to the cable end. A ferrule is configured to be terminated to the cable. The ferrule has an inner bushing and an outer bushing, with the inner and outer bushings cooperating to capture a cable braid of the cable therebetween. The ferrule is retained within the mounting block such that the ferrule is housed interior of the housing.

US Patent:

8599559, Dec 3, 2013

Filed:

May 30, 2012

Appl. No.:

13/483338

Inventors:

Matthew David Morrison - Lemoyne PA, US
Michael John Phillips - Camp Hill PA, US
Michael Eugene Shirk - Grantville PA, US

Assignee:

Tyco Electronics Corporation - Berwyn PA

International Classification:

H05K 7/20

US Classification:

361702

Abstract:

A cage assembly is provided for receiving a pluggable module. The cage assembly includes a cage having a front end, a mounting side, and an internal compartment. The front end is open to the internal compartment of the cage. The internal compartment is configured to receive the pluggable module therein through the front end. A heat sink is mounted to the mounting side of the cage. The heat sink has a module side that is configured to thermally communicate with the pluggable module. An electromagnetic interference (EMI) gasket extends along at least a portion of an interface between the mounting side of the cage and the module side of the heat sink. The EMI gasket includes electrically conductive spring fingers that are engaged with and electrically connected to the mounting side of the cage.

US Patent:

20210309391, Oct 7, 2021

Filed:

Apr 7, 2020

Appl. No.:

16/842165

Inventors:

Matthew Morrison - Leonardtown MD, US

Assignee:

United States of America as represented by the Secretary of the Navy - Patuxent River MD

International Classification:

B64F 5/50

Abstract:

An arm removal system for removing an arm. The system includes an anvil, and a removal assembly with at least two jackscrews. The arm has an extension radially extending from the arm and an arm outer surface. The arm is disposed within a wedge shaped collet that is disposed within a socket in an aircraft with an aircraft outer surface. The removal assembly includes an extension engaging surface and threaded jackscrew holes for accepting the jackscrews, such that when the jackscrews are tightened within the jackscrew holes, the jackscrews apply force on the anvil and the aircraft outer surface in the direction away from the removal assembly such that the arm is eventually removed entirely from the aircraft.