Indianapolis, IN, United States of America

Daniel T Jensen

This inventor holds 2 USPTO granted patents. Top assignee: The Boeing Company. Active years: 1997-1998.


% Patents Active = 100.0

Average Co-Inventor Count = 2.4

ph-index = 2

Forward Citations = 37(Granted Patents)


Location History:

  • Indianapolis, IN (US) (1997)
  • Mountlake Terrace, WA (US) (1998)

Company Filing History:


Years Active: 1997-1998

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2 patents (USPTO):Explore Patents

Title: Innovations by Daniel T Jensen

Introduction

Daniel T Jensen is an accomplished inventor based in Indianapolis, IN (US). He has made significant contributions to the field of gas turbine engine technology. With a total of 2 patents, Jensen's work focuses on improving the efficiency and safety of turbine engines.

Latest Patents

One of Jensen's latest patents is a flow control apparatus for gas turbine engine installation pressure. This improved pressure relief system includes a pressure relief door attached to the engine shroud at its forward edge. The aft edge of the door is free to pivot outward in the occurrence of a bleed duct failure. The door is mounted within a cutout in the engine shroud, which is designed to enhance airflow and reduce temperatures during operation. This innovation helps to eliminate the need for high-temperature materials or insulating blankets, thereby improving the overall performance of the turbine engine.

Career Highlights

Jensen is currently employed at The Boeing Company, where he continues to develop innovative solutions for aerospace technology. His work has been instrumental in advancing the safety and efficiency of gas turbine engines.

Collaborations

Jensen has collaborated with notable coworkers, including Ronald L Balzer and Michael L Sangwin, contributing to a team that drives innovation in the aerospace sector.

Conclusion

Daniel T Jensen's contributions to gas turbine engine technology exemplify the spirit of innovation in the aerospace industry. His patents reflect a commitment to enhancing performance and safety in turbine engines.

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