A single ram air inlet feeds both the cabin pack and heat exchanger, improving pressure recovery while cutting drag, weight, and ECS complexity.
Integrally molded depressions and crests help lightweight thermoplastic aircraft ducts absorb impacts and delay cracking during handling.
Surface depressions and ridges help lightweight thermoplastic aircraft conduits resist tool-impact cracking while delaying damage onset.
An integrated fairing stiffener forms the air inlet, improving component cooling while preserving structural strength and reducing drag.
Aircraft fairings can lose cooling access when stiffeners block inlet placement; integrating the inlet into the stiffener preserves strength and airflow.
Aerodynamic compression walls accelerate free-stream air at the turbine discharge to increase total-to-static pressure ratio.
Segmented inlets with swept edges reduce total pressure losses and spillage, allowing larger precoolers closer to the fan.
A Y-shaped airliner fuselage bifurcates into angled extensions to house a medial fan and NACA inlet.
Fixed diverter structures with S-shaped cross sections reduce excrescence drag and fuel burn by optimizing pressure recovery without mechanical actuators.
A tandem air inlet apparatus uses a forward flush heat exchanger inlet to swallow the boundary layer before it reaches the Pitot inlet.
Raised intake opening with integrated diverter flanges prevents hazardous fluid ingestion while maintaining airflow performance.
A dynamic flow control flap adjusts the air duct inlet cross-section to minimize flight drag while maximizing ground airflow mass.