Fujifilm Medical Systems U.s.a., Inc.
Patent Agent
Pratt & Whitney Sep 1, 2005 - Jan 2017
Patent Agent at Pratt and Whitney
Nerac Sep 2004 - Sep 2005
Patent Analyst and Patent Agent
General Dynamics Jun 2003 - Sep 2004
Shift Test Engineering Supervisor
Pc25C Prototype Aug 1999 - Jan 2003
Manager
Education:
University of North Dakota 2012 - 2015
Bachelors, Bachelor of Science
Rensselaer Polytechnic Institute 2000 - 2002
Master of Science, Masters
United States Merchant Marine Academy 1993 - 1997
Bachelors, Bachelor of Science
Robert D. Szolomayer - Glastonbury CT, US David L. Motto - Ellington CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F01D 25/18 F16K 17/36
US Classification:
184 611, 137 38, 13756533, 137574, 137576
Abstract:
An assembly for holding a fluid includes an auxiliary reservoir inside a main reservoir. The auxiliary reservoir includes an auxiliary reservoir shell with a fill passage at or near its bottom. The auxiliary reservoir shell also has a vent passage at or near its top. The fill passage and the vent passage fluidically connect the auxiliary reservoir to the main reservoir. A fluid inlet is located inside the main reservoir and outside of the auxiliary reservoir. A fluid outlet located inside the auxiliary reservoir between the fill passage and the vent passage.
Robert D. Szolomayer - Marlborough CT, US David L. Motto - Ellington CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F01D 25/18 F16K 17/36
US Classification:
184 611, 137 38, 13756533, 137574, 137576
Abstract:
An assembly for holding a fluid includes an auxiliary reservoir inside a main reservoir. The auxiliary reservoir includes an auxiliary reservoir shell with a fill passage at or near its bottom. The auxiliary reservoir shell also has a vent passage at or near its top. The fill passage and the vent passage fluidically connect the auxiliary reservoir to the main reservoir. A fluid inlet is located inside the main reservoir and outside of the auxiliary reservoir. A fluid outlet located inside the auxiliary reservoir between the fill passage and the vent passage.
A Snowboard Support System capable of relieving the load placed on the snowboarder's bound downhill foot and leg while riding on a chair lift. This invention is lightweight, compact, self retractable and safe. Most notably, the Snowboard Support System comprises a hooking mechanism that attaches to the chair lift, has an emergency releasable buckle, and an adjustment mechanism to change the length of the webbing to suit each snowboarder's height. The hooking mechanism is self retracted into an outer structure via a spring mechanism. The outer structure is fixed to the snowboard via U brackets and threaded inserts.
Robert D. Szolomayer - Marlborough CT, US David L. Motto - Ellington CT, US
Assignee:
UNITED TECHNOLOGIES CORPORATION - Hartford CT
International Classification:
F01D 25/20 F01M 1/02 F01M 1/16
US Classification:
184 611, 137 1, 137 14
Abstract:
An assembly for holding a fluid includes an auxiliary reservoir inside a main reservoir. The auxiliary reservoir includes an auxiliary reservoir shell with a fill passage at or near its bottom. The auxiliary reservoir shell also has a vent passage at or near its top. The fill passage and the vent passage fluidically connect the auxiliary reservoir to the main reservoir. A fluid inlet is located inside the main reservoir and outside of the auxiliary reservoir. A fluid outlet located inside the auxiliary reservoir between the fill passage and the vent passage.
An exemplary fluid supply system for use on a turbomachine includes a turbomachine fluid container having a moveable barrier. A pressurized fluid is delivered to one side of the moveable barrier, and an opposing side of the flexible barrier communicates with a source of lubricant. Pressurized fluid is selectively delivered to the one side to move the moveable barrier between a flow-permitting position that permits flow from the source of lubricant to the turbomachine fluid container and a flow-restricting position that restricts flow from the source of lubricant to the turbomachine fluid container.
Seal With Integral Assembly Clip And Method Of Sealing
- Farmington CT, US Frederick M. Schwarz - Glastonbury CT, US David L. Motto - Fuquay Varina NC, US
International Classification:
F01D 11/00 F01D 25/24 F16J 15/08 F16J 15/06
Abstract:
A seal assembly for a gas turbine engine includes first and second split-ring seals. The first split-ring seal includes circumferentially separated first and second ends, laterally separated first and second edges, a first sealing lobe adjacent the first edge, and a first integral clip portion adjacent the second edge. The first sealing lobe has a curved surface extending laterally outward from the first edge. The second split-ring seal is slidably received and nested in the first seal. The second split-ring seal includes circumferentially separated third and fourth ends and laterally separated third and fourth edges.
Seal With Integral Assembly Clip And Method Of Sealing
- Hartford CT, US Frederick M. Schwarz - Glastonbury CT, US David L. Motto - Ellington CT, US
International Classification:
F01D 11/00 F16J 15/06
Abstract:
A seal assembly for a gas turbine engine includes first and second split-ring seals. The first split-ring seal includes circumferentially separated first and second ends, laterally separated first and second edges, a first sealing lobe adjacent the first edge, and a first integral clip portion adjacent the second edge. The first sealing lobe has a curved surface extending laterally outward from the first edge. The second split-ring seal is slidably received and nested in the first seal. The second split-ring seal includes circumferentially separated third and fourth ends and laterally separated third and fourth edges.
Pressurized Reserve Lubrication System For A Gas Turbine Engine
- Hartford CT, US David L. Motto - Ellington CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F01D 25/18
US Classification:
184 611
Abstract:
A lubrication system includes a control subsystem operable to selectively communicate lubricant from a reserve lubrication subsystem under a pressure to supplement lubricant from a main lubrication subsystem in response to identification of a prolonged reduced-G condition. A gas turbine engine includes a main lubrication subsystem in communication with a geared architecture; a reserve lubrication subsystem in communication with the geared architecture; and a control subsystem operable to selectively communicate lubricant from the reserve lubrication subsystem under a pressure in response to identification of a prolonged reduced-G condition. A method of reducing lubrication starvation from a lubrication system with a main lubrication subsystem and a reserve lubrication subsystem, the main lubrication system in communication with a geared architecture of a gas turbine engine, includes communicating lubricant under a pressure to the geared architecture in response to identifying of a prolonged reduced-G condition.
Name / Title
Company / Classification
Phones & Addresses
David Motto Principal
ADVANCED SECURITY AND AUTOMATION, LLC Whol Industrial Equipment
40 Cindy Rd, Ellington, CT 06029
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