This inventor holds 4 USPTO granted patents. Top assignee: United Technologies Corporation. Active years: 2006-2008.
Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile
Company Filing History:
Years Active: 2006-2008
Title: Terrence J. McMullen and Rocket Engine Innovation.
Introduction
Terrence J. McMullen is an inventor associated with Palm Beach Gardens, Florida, and United Technologies Corporation. His work includes patented rocket-engine designs focused on the combustion chamber, nozzle transition, and cooling system. He is credited with 4 patents.
Latest Patents
McMullen’s listed recent patents address the construction and assembly of a rocket engine with a transition zone between the combustion chamber and the smooth-wall nozzle.
“Rocket Engine Combustion Chamber” describes an engine construction with a coolant system in the transition zone. The system includes a manifold made from a non-copper material through which coolant flows. For high-heat-transfer applications, the design also provides an additional manifold made from a copper-based material.
“Method of Assembling a Rocket Engine with a Transition Zone Between the Combustion Chamber and the Coolant System” concerns assembling an engine with a similar chamber, smooth-wall nozzle, and cooled transition zone. Its described construction likewise uses a non-copper manifold and, in a high-heat-transfer embodiment, an additional copper-based manifold.
Career Highlights
McMullen’s patent work reflects an engineering focus on rocket-engine construction and thermal management. The described designs place particular emphasis on cooling the transition zone, where heat transfer is an important consideration.
Collaborations
McMullen is associated with United Technologies Corporation. His listed coworkers include Gregg W. Jones and Micki A. Marshall.
Conclusion
Terrence J. McMullen’s recorded inventions center on rocket-engine design, especially the construction and cooling of the transition zone between the combustion chamber and nozzle.
Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile
