This inventor holds 2 USPTO granted patents. Top assignee: United Technologies Corporation. Active years: 1997-2011.
Location History:
- Jupiter, FL (US) (1997)
- Middletown, CT (US) (2011)
Company Filing History:
Years Active: 1997-2011
Title: Joseph A Scricca: Innovator in Turbine Technology
Introduction
Joseph A Scricca is a notable inventor based in Middletown, CT (US). He has made significant contributions to the field of turbine technology, holding a total of 2 patents. His work focuses on enhancing the efficiency and performance of turbine engines.
Latest Patents
Joseph A Scricca's latest patents include a hybrid seal assembly for a fan-turbine rotor of a tip turbine engine. This innovative hybrid seal assembly is designed to work with rotating surfaces that may experience significant deflections. It effectively seals between flanges and mating surfaces typical of the annular seal face surface of a diffuser section of a tip turbine engine. Another notable patent is the enhanced film cooling slot for turbine blade outer air seals. This invention provides a cooling enhancement for gas turbine engine outer air seals, utilizing impingement cooling and convective cooling through tortuous cooling air passages. The design also incorporates cooling air discharge slots that are oriented to minimize momentum exchange between the cooling air and the working fluid.
Career Highlights
Joseph A Scricca is associated with United Technologies Corporation, where he has been instrumental in developing advanced turbine technologies. His work has contributed to the company's reputation as a leader in aerospace and industrial systems.
Collaborations
Joseph has collaborated with various professionals in his field, including his coworker George W Kelch. Their combined expertise has led to innovative solutions in turbine technology.
Conclusion
Joseph A Scricca's contributions to turbine technology through his patents and work at United Technologies Corporation highlight his role as an influential inventor. His innovations continue to impact the efficiency and performance of turbine engines.
