Location History:
- Harbor City, CA (US) (1988 - 1995)
- Rancho Palos Verdes, CA (US) (2003 - 2006)
Company Filing History:
Years Active: 1988-2006
Title: Michael S. Koerner: Innovator in Gas and Fuel Systems
Introduction
Michael S. Koerner is a notable inventor based in Harbor City, California. He has made significant contributions to the fields of gas and fuel systems, holding a total of 10 patents. His innovative designs have advanced the efficiency and functionality of various systems.
Latest Patents
One of his latest patents is a "System for warming pressurized gas." This invention involves a plurality of vessels that contain pressurized gas, with each vessel fluidly communicating with an adjacent vessel through a line. A heat exchanger is strategically positioned in a heat-conducting relationship with each line. The system includes an exhaust valve that communicates with lower pressure. In one embodiment, the vessels communicate in series, with only one vessel connected to the exhaust valve. Alternatively, the vessels can be arranged in a loop configuration, allowing two vessels to communicate with the exhaust valve through respective lines, each containing a shutoff valve. The two shutoff valves are designed to open and close in concert, causing the flow in the system to alternate directions during the exhaust process. In a third configuration, two vessels communicate through a singular line, with the vessel connected to the exhaust valve enclosing the other vessel. Heat transfer fins are located in the enclosed vessel, extending into the enclosing vessel, while a heat exchanger is positioned to heat the gas flowing from the enclosed vessel, with the fins conducting part of this heat to the gas still inside.
Another significant patent is the "Jet fuel and air system for starting auxiliary power unit." This system includes an air control valve assembly located in the airflow passageway between a source of pressurized air and a turbine power modulator. Additionally, a fuel control valve assembly is located in the fuel flow passageway between a source of jet fuel and the turbine power modulator. Upon energizing both the air control and fuel control valves, a mixture of compressed air and jet fuel enters the turbine power module, igniting to create a flow stream of hot gases that drive a gas turbine to power the auxiliary power unit.
Career Highlights
Throughout his career, Michael has worked with prominent companies such as AlliedSignal Inc. and Honeywell International Inc. His experience in these organizations has contributed to his expertise in developing innovative systems.
Collaborations
Michael has collaborated with notable coworkers, including Scott J. Goldberg and Francis K. Weig