Bellevue, WA, United States of America

Gary D Lium

This inventor holds 1 USPTO granted patent. Top assignee: United States of America as Represented by the Secretary of the Air Force. Active years: 1976.


% Patents Active = 100.0

Average Co-Inventor Count = 3.0

ph-index = 1

Forward Citations = 4(Granted Patents)


Company Filing History:


Years Active: 1976

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1 patent (USPTO):Explore Patents

Title: The Innovations of Gary D. Lium

Introduction

Gary D. Lium is a notable inventor based in Bellevue, WA (US). He has made significant contributions to the field of solid propellants, particularly through his innovative patent. His work is recognized for enhancing the performance of propellant formulations, which is crucial for various applications in aerospace and defense.

Latest Patents

Lium holds a patent for "Burning rate modifiers for solid propellants." This patent describes a solid propellant formulation that incorporates low levels of transition metal fluorides, such as cupric fluoride and ferric fluoride. These modifying agents are designed to increase the propellant burning rate while simultaneously decreasing its pressure exponent. This innovation is vital for improving the efficiency and effectiveness of solid propellants.

Career Highlights

Gary D. Lium is associated with the United States of America as represented by the Secretary of the Air Force. His work in this capacity has allowed him to contribute to advancements in military and aerospace technologies. His expertise in propellant formulations has positioned him as a key figure in his field.

Collaborations

Lium has collaborated with notable colleagues, including Francisco Q. Roberto and Arnold M. Crelier. These partnerships have likely fostered a productive environment for innovation and research in solid propellant technologies.

Conclusion

Gary D. Lium's contributions to the field of solid propellants through his innovative patent demonstrate his commitment to advancing aerospace technology. His work continues to influence the development of more efficient propellant formulations.

Profile summary based on public USPTO records.
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