A new engine concept from NASA’s Glenn Research Center allows for truly distributed propulsion. The concept enables airframe and system modularity by allowing parts to be swapped or repaired easily. Design changes can be applied to individual components and not the entire propulsion system. The NASA Glenn innovation eliminates heavy shafts and disks, and allows for airplane modularity as well. This design also enables subsonic to high supersonic flight with the same flowpath. If parts are damaged during flight, only a small percentage of thrust is lost. In addition, the blades can be retracted to enable ramjet or scramjet mode.

A new engine concept from NASA’s Glenn Research Center allows for truly distributed propulsion.

The novel design replaces a conventional jet engine with a linear array of flapping blades and diffusing vanes for compression, a combustor, and a linear array of expansion ducts. These expansion ducts convert thermal energy to magnetic energy using reverse magnetic hyperthermia, where the turbine ducts are lined with superparamagnetic composites that respond to thermal loads by generating alternating magnetic fields. The magnetic energy can be used to drive the electromagnetic actuators required for flapping. Kinetic energy is delivered to the air using rapid oscillations rather than by rotation. This is converted to internal energy by the vanes.

The technology is versatile because the airframe can be modified to accommodate more or fewer passengers as needed. Because of the modular design, the thrust/lift is not lost completely if there is damage to the propulsion. In addition, parts of the propulsion system can be jettisoned in case of an emergency need to lower weight.

This engine concept can be used in aviation and marine propulsion. This is an early-stage technology requiring additional development. Glenn welcomes co-development opportunities.

NASA is actively seeking licensees to commercialize this technology. Please contact the Technology Transfer Office at This email address is being protected from spambots. You need JavaScript enabled to view it. to initiate licensing discussions. Follow this link for more information: http://technology.nasa.gov/patent/TB2016/LEW-TOPS-53.