This inventor holds 4 USPTO granted patents. Top assignee: Honeywell International Inc.. Active years: 2013-2014.
Location History:
- Karnataka, IN (2013 - 2014)
- Karnaraka, IN (2014)
Company Filing History:
Years Active: 2013-2014
Title: Dhinagaran Ramachandran: Innovator in Gas Turbine Technology
Introduction
Dhinagaran Ramachandran is a notable inventor based in Karnataka, India. He has made significant contributions to the field of gas turbine technology, holding a total of 4 patents. His work focuses on enhancing the efficiency and performance of gas turbine engines.
Latest Patents
Among his latest patents is the invention of inter-turbine ducts with guide vanes. This innovation involves a turbine section of a gas turbine engine that is annular about a longitudinal axis. It includes a first turbine with a first inlet and outlet, a second turbine with a second inlet and outlet, and an inter-turbine duct that directs airflow from the first turbine to the second turbine. Additionally, he has developed gas turbine engine components with cooling hole trenches. This patent describes an engine component that features a body with an interior and exterior surface, a cooling hole extending from the interior to the exterior surface, and a concave trench that extends from the cooling hole in a downstream direction.
Career Highlights
Dhinagaran Ramachandran is currently employed at Honeywell International Inc., where he continues to innovate and contribute to advancements in gas turbine technology. His expertise and dedication have positioned him as a key player in his field.
Collaborations
He has collaborated with notable coworkers such as Gopal Samy Muthiah and Balamurugan Srinivasan, further enhancing the innovative environment at Honeywell.
Conclusion
Dhinagaran Ramachandran's contributions to gas turbine technology through his patents and work at Honeywell International Inc. highlight his role as a significant inventor in the industry. His innovations continue to pave the way for advancements in energy efficiency and performance in gas turbine engines.