Lisa G Burns

US Patent:

7180617, Feb 20, 2007

Filed:

May 18, 2001

Appl. No.:

09/861339

Inventors:

John Dibiasi - Shelton CT, US
Lisa D. Burns - Vernon CT, US
Allen Joslin - Norwich CT, US
Steven C. Hoffman - Sandy Hook CT, US

Assignee:

Metavante Corporation - Milwaukee WI

International Classification:

G06F 15/00

US Classification:

358 115, 358 118

Abstract:

A printing system includes: a data storage device configured to store data representing a plurality of elements; a creation device configured to define at least one piece of printed material, the at least one piece of printed material including at least one of the plurality of elements; and a data processing device configured to read from the data storage device the data corresponding to the at least one of the plurality of elements in accordance with the at least one piece of printed material defined by the creation device and to generate data representing the at least one piece of printed material. A printing method includes the steps of: storing data representing a plurality of elements in a data storage device; defining at least one piece of printed material, the at least one piece of printed material including at least one of the plurality of elements; reading from the data storage device the data corresponding to the at least one of the plurality of elements in accordance with the at least one piece of printed material defined in the defining step; and generating data representing the at least one piece of printed material.

US Patent:

20120102965, May 3, 2012

Filed:

Nov 10, 2011

Appl. No.:

13/373344

Inventors:

William C. Pfefferle - Branford CT, US
Lisa Burns - Branford CT, US

International Classification:

F02C 1/00

US Classification:

60772

Abstract:

A method for operating a hydrogen-fueled gas turbine is provided wherein a supply of fuel is passed to a gas turbine combustor, and a supply of nitrogen and sufficient air to provide at least sufficient compressed air to the gas turbine for fuel combustion is passed to a compressor. A sufficient portion of the compressor discharge flow is passed to a combustor for fuel rich combustion of the fuel flow to the combustor and the fuel is combusted to produce hot combustion gases that are, in turn, passed to a turbine.