This inventor holds 2 USPTO granted patents and 2 EPO patents. Top assignee: United Technologies Corporation. Active years: 2018-2019.
Company Filing History:
Years Active: 2018-2019
Title: Innovations of Peter Tu in Gas Turbine Technology
Introduction
Peter Tu is an accomplished inventor based in Rocky Hill, CT (US). He has made significant contributions to the field of gas turbine technology, holding a total of 2 patents. His work focuses on enhancing the efficiency and functionality of fuel supply systems in gas turbine engines.
Latest Patents
Peter Tu's latest patents include innovative designs for a spherical ball bearing housing and a fuel supply manifold for gas turbine engines. The spherical ball bearing housing patent describes a method for assembling a fuel supply manifold that includes a plurality of fuel supply tubes, a fitting connecting at least two members of the tubes, and a bearing housing that incorporates a ball bearing. This design aims to improve the assembly and performance of gas turbine engines. The second patent, related to the fuel supply manifold, outlines a system that features multiple double-barrel fittings in communication with both primary and secondary fuel circuits, enhancing the overall efficiency of fuel delivery in gas turbine applications.
Career Highlights
Peter Tu is currently employed at United Technologies Corporation, where he continues to innovate and develop advanced technologies for gas turbines. His work has been instrumental in pushing the boundaries of what is possible in this critical area of engineering.
Collaborations
Throughout his career, Peter has collaborated with notable colleagues, including Robert F. Sheil and Thomas Bruce Avis. These partnerships have fostered a creative environment that encourages the development of groundbreaking technologies.
Conclusion
Peter Tu's contributions to gas turbine technology through his patents and collaborations highlight his role as a key innovator in the field. His work continues to influence advancements in energy efficiency and performance in gas turbine engines.
