Rocco S Cuva, 8711419 178Th Rd N, Jupiter, FL 33478
Rocco Cuva Phones & Addresses
11419 178Th Rd, Jupiter, FL 33478 561-7465070
South Glastonbury, CT
42 Crossroads Ln, Glastonbury, CT 06033 860-6331785
Palm Beach Gardens, FL
Mentions for Rocco S Cuva
Publications & IP owners
Us Patents
Engine Signature Assessment System
US Patent:
2013034, Dec 26, 2013
Filed:
Jun 21, 2012
Appl. No.:
13/529305
Inventors:
Roger Neama - Windsor CT, US
Brian London - Atascosa TX, US
Larry R. Breen - Plantsville CT, US
Rocco S. Cuva - South Glastonbury CT, US
Alun L. Buttermore - South Windsor CT, US
Brian London - Atascosa TX, US
Larry R. Breen - Plantsville CT, US
Rocco S. Cuva - South Glastonbury CT, US
Alun L. Buttermore - South Windsor CT, US
International Classification:
G06F 7/00
US Classification:
701 294, 701 291, 701 344
Abstract:
The disclosed method and system utilizes inspection information from individual components to predict a value for a system performance parameter. The predicted system performance parameter is utilized to determine if corrective action is required for any of the system components. No corrective action is recommended if the predicted system performance parameter is within desired limits. Further, corrective action for a specific component of the system is performed and indicated independent of the inspection results of a specific component.
Coated And Uncoated Surface-Modified Airfoils For A Gas Turbine Engine Component And Methods For Controlling The Direction Of Incident Energy Reflection From An Airfoil
US Patent:
2017015, Jun 8, 2017
Filed:
Dec 2, 2015
Appl. No.:
14/957208
Inventors:
- Hartford CT, US
ADAM M. ROSENKRANTZ - Newington CT, US
ROCCO S. CUVA - South Glastonbury CT, US
ADAM M. ROSENKRANTZ - Newington CT, US
ROCCO S. CUVA - South Glastonbury CT, US
Assignee:
UNITED TECHNOLOGIES CORPORATION - Hartford CT
International Classification:
F01D 5/14
F01D 5/28
F01D 5/28
Abstract:
A surface-modified airfoil for a gas turbine engine component is provided. The surface-modified airfoil includes an airfoil having an exterior surface at a leading edge, a trailing edge, a suction side, and a pressure side. A surface feature in at least a portion of the exterior surface comprises at least one of a protrusion feature or a depression feature. The surface feature is operatively configured for one of anchoring a coating on at least the portion of the exterior surface or controlling a direction of incident energy reflected from the surface-modified airfoil.
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