Rory C Keogh, Age 564545 California St, San Francisco, CA 94118

8318370, Nov 27, 2012

Mar 31, 2010

12/752076

Rory C. Keogh - San Francisco CA, US

H01M 8/04
F28D 17/00

429439, 165 10

A heat exchanger includes a first regenerator core and a second regenerator core and a four-way valve coupled to a cold section of the first regenerator core and to a cold section of the second regenerator core. The four-way valve directs input air to the first regenerator core or to the second regenerator core. A high-temperature passive check valve is coupled to a hot section of the first regenerator core and to a hot section of the second regenerator core. The high-temperature passive check valve comprises an inlet header coupled to the hot section of the first regenerator core or the second regenerator core, a valve poppet coupled to a valve stem and a valve seat located on a surface parallel to a surface of the valve poppet. Air entering the inlet header moves the valve poppet away from the valve seat, creating an opening through which air passes.

2009014, Jun 11, 2009

Aug 28, 2006

11/467913

Rory Keogh - San Francisco CA, US

F02K 3/02

602261, 60805

A turbofan jet engine design that utilizes aerodynamic coupling to transmit power from a high-speed engine core to a lower speed fan, thereby simplifying the design and improving the thrust-to-weight ratio compared to previous turbofan designs. The engine uses a low speed co-rotating power turbine located upstream of the engine core to drive the fan. The high-speed core uses a centrifugal impeller to pressurize the inlet flow, the flow exits the high-speed impeller without diffusing its high-speed angular momentum and enters directly into the low speed co-rotating power turbine impeller. The incoming flow is then turned by the low speed co-rotating turbine impeller and exits the turbine opposing its direction of rotation, thereby extracting power from the flow to drive the fan. The exit flow from the low speed power turbine then enters the combustor inlet. This engine configuration enables the power turbine to be constructed from high strength, low-density materials (that are not suitable for use in higher temperature power turbines) thereby reducing the weight of the engine. This engine configuration also eliminates the need for the core compressor diffuser, the power turbine nozzle guide varies, and the low speed shaft that connects the fan to the power turbine in conventional turbofans.