Company Filing History:
Years Active: 2014-2015
Title: Reed A Kakuska: Innovator in Rocket Engine Fluid-Flow Systems
Introduction
Reed A Kakuska is a notable inventor based in Juno, Florida, recognized for his contributions to rocket engine fluid-flow systems. With a total of 2 patents, Kakuska has made significant advancements in the field of engineering.
Latest Patents
Kakuska's latest patents include a "Reversible flow discharge orifice," which describes a rocket engine fluid-flow system that integrates a pump to connect a fluid source to a combustion chamber. This innovative design features a nozzle in fluid communication with the combustion chamber, incorporating coolant tubes arranged between the pump and the combustion chamber. The orifice in this system has a throat and is strategically positioned between the pump and the coolant tubes, with entrance and exit ramps designed to optimize fluid flow. The exit ramp is particularly noteworthy, featuring a surface with a divergent angle of less than a right angle, enhancing the efficiency of the system.
Another significant patent is the "Method for chemical milling an apparatus with a flow passage." This method outlines a process for manufacturing an apparatus with a preform flow passage. It involves determining the flow area of the preform flow passage and comparing it to reference flow area data to facilitate chemical milling based on the flow area comparison data.
Career Highlights
Throughout his career, Reed A Kakuska has worked with prominent companies such as United Technologies Corporation and Raytheon Technologies Corporation. His experience in these organizations has contributed to his expertise in fluid-flow systems and engineering innovations.
Collaborations
Kakuska has collaborated with notable individuals in the industry, including David R Wiley and Jim A Clark. These collaborations have likely enriched his work and contributed to the development of his patented technologies.
Conclusion
Reed A Kakuska stands out as an innovative inventor in the field of rocket engine fluid-flow systems. His patents reflect a commitment to advancing engineering solutions, and his career highlights demonstrate his significant contributions to the industry.