This inventor holds 1 USPTO granted patent. Top assignee: Morton Thiokol Inc.. Active years: 1988.
Company Filing History:
Years Active: 1988
Title: The Innovations of Charles R Voris
Introduction
Charles R Voris is a notable inventor based in Brigham City, Utah. He is recognized for his contributions to rocket motor technology, particularly through his innovative designs that enhance missile guidance systems. Voris has been instrumental in developing solutions that address critical challenges in aerospace engineering.
Latest Patents
One of Voris's significant patents is the segmented case rocket motor. This invention features a segmented rocket motor case that includes wedge members designed to eliminate free play at the joint of the case segments. This design is crucial as it prevents interference with the missile's guidance system, ensuring that the missile remains on target. The patent also includes a lap joint member with a shoulder that facilitates the attachment of a membrane seal assembly for pulsed rocket motors. Additionally, a through bulkhead initiator is integrated into the design, allowing for a more efficient ignition process without the need for external explosive transfer lines.
Career Highlights
Charles R Voris has made substantial contributions to the field of aerospace engineering during his career. He has worked with Morton Thiokol Inc., a company known for its advancements in rocket propulsion and aerospace technologies. His work has significantly impacted the development of reliable and efficient rocket systems.
Collaborations
Throughout his career, Voris has collaborated with several talented individuals, including E Wayne Tackett and Bradley W Smith. These collaborations have fostered innovation and have led to advancements in rocket motor technology.
Conclusion
Charles R Voris is a distinguished inventor whose work in rocket motor technology has made a lasting impact on the aerospace industry. His innovative designs continue to influence missile guidance systems and enhance the reliability of rocket propulsion.