Abstract: A turbine engine is described that includes an intake, an inlet duct configured to receive fluid from the intake, and an outer bypass duct configured to receive fluid from the intake. The turbine engine further includes a drive shaft, a tower shaft mechanically coupled to the drive shaft, and an electric generator mechanically coupled to the tower shaft. The electric generator is located between the inlet duct and the outer bypass duct.

Abstract: A turbine engine is described that includes an intake, an inlet duct configured to receive fluid from the intake, and an outer bypass duct configured to receive fluid from the intake. The turbine engine further includes a drive shaft, a tower shaft mechanically coupled to the drive shaft, and an electric generator mechanically coupled to the tower shaft. The electric generator is located between the inlet duct and the outer bypass duct.

Abstract: A turbine engine is described that includes a drive shaft and an electric generator comprising a first rotating element comprising a magnet array, wherein the first rotating element is configured to rotate in a first direction based on a rotation of the drive shaft. The turbine engine further includes a second rotating element comprising a coil array, wherein the second rotating element is configured to rotate in a second direction based on the rotation of the drive shaft, wherein the second direction is opposite to the first direction.

Abstract: A turbine engine is described that includes a drive shaft and an electric generator, wherein the electric generator includes a first rotating element comprising a first magnet array and mechanically coupled to the drive shaft. The electric generator further includes a second rotating element comprising a second magnet array and mechanically coupled to the drive shaft and an armature comprising a first coil array and a second coil array, wherein the first rotating element is configured to rotate at a particular velocity relative to the first coil array, and the second rotating element is configured to rotate at the particular velocity relative to the second coil array.

Abstract: A turbine engine is described that includes a drive shaft and an electric generator comprising a first rotating element comprising a magnet array, wherein the first rotating element is configured to rotate in a first direction based on a rotation of the drive shaft. The turbine engine further includes a second rotating element comprising a coil array, wherein the second rotating element is configured to rotate in a second direction based on the rotation of the drive shaft, wherein the second direction is opposite to the first direction.

Abstract: A turbine engine is described that includes a drive shaft and an electric generator, wherein the electric generator includes a first rotating element comprising a first magnet array and mechanically coupled to the drive shaft. The electric generator further includes a second rotating element comprising a second magnet array and mechanically coupled to the drive shaft and an armature comprising a first coil array and a second coil array, wherein the first rotating element is configured to rotate at a particular velocity relative to the first coil array, and the second rotating element is configured to rotate at the particular velocity relative to the second coil array.

Abstract: A turbine engine is described that includes an intake, an inlet duct configured to receive fluid from the intake, and an outer bypass duct configured to receive fluid from the intake. The turbine engine further includes a drive shaft, a tower shaft mechanically coupled to the drive shaft, and an electric generator mechanically coupled to the tower shaft. The electric generator is located between the inlet duct and the outer bypass duct.

Abstract: One embodiment of the present invention is a unique thrust augmented gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for thrust augmented gas turbine engines. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.