Bastnagel
Maryann Bastnagel, Potomac, MD US
Patent application number | Description | Published |
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20110093384 | SYSTEM AND METHOD FOR MODIFYING ATTRIBUTE DATA PERTAINING TO FINANCIAL ASSETS IN A DATA PROCESSING SYSTEM - A processing system for modifying attributes of a plurality of loans is described. The processing system includes an attribute change processor for receiving and implementing a proposed change to an attribute of at least one of the plurality of loans and a loan pricing processor for generating a pricing value associated with the proposed change to the attribute of the at least one loan. | 04-21-2011 |
20130066765 | SYSTEM AND METHOD FOR PROCESSING DATA PERTAINING TO FINANCIAL ASSETS - A method of processing data in connection with a security is provided. The security is collateralized by a plurality of home mortgage loans or by portions of the plurality of home mortgage loans. The method comprises generating payment projections regarding principal and interest payment projections for the plurality of home mortgage loans; determining that the payment projections have errors; and modifying loan characteristic data to eliminate errors in the loan characteristic data that cause errors in the payment projections. According to another embodiment, a method comprises receiving payment data regarding the plurality of loans a plurality of times separated by a plurality of days during the reporting cycle. Each time the payment data is received, the payment data is processed and the opportunity to make corrections is provided. | 03-14-2013 |
Philip M. Bastnagel, Indianapolis, IN US
Patent application number | Description | Published |
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20100162716 | PANELED COMBUSTION LINER - The present invention relates to combustors, and provides a combustion liner that may at least partially contain a combustion process. The combustion liner may include a support structure that supports a plurality of panels. The panels may be in the form of thermal barrier panels, e.g., that are attached to the support structure and/or other parts of the machine. | 07-01-2010 |
20110185738 | GAS TURBINE ENGINE COMPONENT CONSTRUCTION - A gas turbine engine component is disclosed having a construction that permits a working fluid to flow from one side of the component to the other. In one embodiment the construction includes multiple layers, and in one particular embodiment the construction includes three layers. One or more layers can have different properties. Additionally, one or more layers of the construction can include a cellular structure. In one embodiment the component is a gas turbine engine combustor liner. | 08-04-2011 |
Philip Michael Bastnagel, Indianapolis, IN US
Thomas E. Bastnagel, Danville, IN US
Patent application number | Description | Published |
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20140250899 | GAS TURBINE ENGINE THERMALLY CONTROLLED FLOW DEVICE - An apparatus includes a gas turbine engine flow device having an inner member and a surrounding member. The inner member has a first coefficient of thermal expansion; and the surrounding member at least partially surrounds the inner member and has a second coefficient of thermal expansion that is different from the first coefficient of thermal expansion. The surrounding member includes at least two walls that form a variable flow gap therebetween. The inner member is oriented relative to the at least two walls of the surrounding member such that, based on the difference in the first and second coefficients of thermal expansion, the inner member expands relatively greater than the surrounding member or the surrounding member expands relatively greater than the inner member, according to a temperature change to correspondingly enlarge or reduce the size of the variable flow gap between the at least two walls. | 09-11-2014 |