This inventor holds 1 USPTO granted patent. Top assignee: Hughes Aircraft Company. Active years: 1993.
Company Filing History:
Years Active: 1993
Title: The Innovations of Robert A. Bueker
Introduction
Robert A. Bueker is an accomplished inventor based in Anaheim Hills, CA. He is known for his significant contributions to the field of structural health monitoring. With a focus on innovative solutions, Bueker has developed technologies that enhance the safety and reliability of aircraft structures.
Latest Patents
Bueker holds a patent for a "Conformal circuit for structural health monitoring and assessment." This invention features a strain gauge with crack sensing traces that are integrated into a conformal structural health monitoring circuit. The design includes a preprocessor and provisions for connectorization to a central processing system. The strain gauge is attached to an aircraft structural surface, allowing for effective monitoring of strain, cracks, and acoustic emissions. The multi-layered construction of the circuit effectively attenuates stress forces, ensuring the integrity of the monitored structure.
Career Highlights
Bueker has made significant strides in his career, particularly during his time at Hughes Aircraft Company. His work has focused on developing advanced technologies that contribute to the safety and performance of aircraft. His innovative approach has led to the creation of solutions that address critical challenges in structural health monitoring.
Collaborations
Bueker has collaborated with notable colleagues, including Lynn O. Waters and Joseph P. Smalanskas. These partnerships have fostered an environment of innovation and have contributed to the advancement of technologies in the aerospace sector.
Conclusion
Robert A. Bueker's contributions to the field of structural health monitoring exemplify the impact of innovation in aerospace technology. His patented inventions and collaborative efforts highlight the importance of continuous improvement in ensuring the safety and reliability of aircraft structures.
