A nested compressor-turbine layout converts atmospheric or seawater heat into mechanical power without fuel, cutting complexity and pollution.
Generators on the main aircraft engines power ducted propulsor modules, boosting thrust without extra thermal engines, weight, or complexity.
A fuel cell handles cruise thrust while combustion engines add take-off and climb power, cutting emissions without the weight of full fuel cell propulsion.
A flexible fluid pocket adds controlled internal pressure during polymerization to improve resin impregnation and limit porosity in turbomachine composites.
Electrical torque assists turbine engine spools at idle, cutting taxi fuel burn while avoiding asymmetric thrust and poor ground handling.
An integrated fixed annular structure guides grids and deflects reverse flow to cut thrust reverser mass, volume, and assembly complexity.
Adaptive control of heat engines and electric machines uses density altitude and power demand to support autorotation and reduce fuel use.
An integrated fixed structure guides cascades and deflects reverse flow to cut thrust reverser mass, drag, and architecture complexity.
Reversible modular sections let field users reconfigure an aerial vehicle for changing payloads and missions while cutting development time and cost.